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b3e805d029b97b99bee43b2771e1f3006fcf6827 | f5f41d427e165a46b51c8b06f6c2010b4213033a | /Scilab/19mcmi23jan24c.sce | 621ada7c5c0c7b9e513926130a9b415a59e73ad5 | [] | no_license | rissuuuu/IT_LAB | a40f6ea5311f5d8012364cfa3d3ad37d83be3afd | 8d0f44a2b8b20ed1101c34a5cb263e6229c200cc | refs/heads/master | 2021-01-03T05:06:49.877644 | 2020-02-12T07:42:44 | 2020-02-12T07:42:44 | 239,934,733 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 101 | sce | 19mcmi23jan24c.sce | x=0:5;
y=[8 10 25 36 52 59];
x_new=0:.01:5;
y_new=interp1(x,y,x_new,'linear');
plot(x,y,'d')
disp(x)
|
f18bac9d81a9e43d17d4c9899c80ab2c211bc6a4 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1364/CH11/EX11.10.2/11_10_2.sce | 11173c5256360a715e07e2653b01c028a938ca0e | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 488 | sce | 11_10_2.sce | clc
//initialisation of variables
g= 32.2 //ft/sec^2
H= 100//ft
L= 1000 //ft
h1= 0.03
h= 0.05
h2= 0.4
d= 6//in
le= 1021 //ft
//CALCULATIONS
u1= sqrt((2*g*H)/(1+h+h2+(h1*L/0.5)))
Q= %pi*(d/12)^2*u1/4
u2= sqrt((H*2*g)/(1+h+(1/16)*(1+h+h2+(h1*L/0.5))))
Q1= %pi*(d/24)^2*u2/4
r= sqrt((d/12)/(2*h1*le))
//RESULTS
printf (' rate of discharge without a nozzle= %.2f ft^3/sec',Q)
printf (' \n rate of discharge= %.2f ft^3/sec',Q1)
printf (' \n diameter of nozzle= %.2f in',r)
|
ca6185c1dda5dbaf0c45d742e4989d6673f12896 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3673/CH5/EX5.7/Ex5_7.sce | 9d02a03fe4eb3c23a1f3973900aebc5f9990fde4 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 791 | sce | Ex5_7.sce | //Example 5_7 page no:197
clc
V=20;
f=5*10^3;//frequency in Hz
R=100;
C=0.2*10^-6//capacitance in farad
Xc=1/(2*%pi*f*C)
Ir=V/R
disp(Ir,"current in the resistance branch is (in A)")
Ic=V/Xc
disp(Ic,"current in the capacitive branch is (in A)")
It=Ir+(%i*Ic)
disp(It,"total current is (in A)")
[It_polar,Theta]=polar(It)
Theta=atand(Ic/Ir)
Z_mag=V/It_polar
Z_ang=0-Theta;
disp(It_polar,"the magnitude of current is (in A)")
disp(Theta,"the angle of current is (in degree)")
disp(Z_mag,"the magnitude of total impedance is (in ohm)")
disp(Z_ang,"the angle of total impedance is (in degree)")
disp("the values varies slightly with text book hence values are rounded off in text book")
//the values varies slightly with text book hence values are rounded off in text book
|
d181dc303120bd1820b77255fbf3932e2d1660cd | 931df7de6dffa2b03ac9771d79e06d88c24ab4ff | /Aimer VS Robots Easy.sce | 0bb7ebd9a6ddd9375853bd7a74d029dca7c86c53 | [] | no_license | MBHuman/Scenarios | be1a722825b3b960014b07cda2f12fa4f75c7fc8 | 1db6bfdec8cc42164ca9ff57dd9d3c82cfaf2137 | refs/heads/master | 2023-01-14T02:10:25.103083 | 2020-11-21T16:47:14 | 2020-11-21T16:47:14 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 118,056 | sce | Aimer VS Robots Easy.sce | Name=Aimer VS Robots Easy
PlayerCharacters=Aimer
BotCharacters=wide_strafe.bot;WIDE2.bot;wide_3.bot;wide_4.bot
IsChallenge=true
Timelimit=60.0
PlayerProfile=Aimer
AddedBots=wide_4.bot;wide_3.bot;wide_4.bot;wide_strafe.bot;wide_3.bot;wide_strafe.bot;wide_strafe.bot;wide_strafe.bot;wide_3.bot;wide_4.bot;wide_4.bot;WIDE2.bot;WIDE2.bot;WIDE2.bot;WIDE2.bot;WIDE2.bot
PlayerMaxLives=1
BotMaxLives=1;1;1;1;1;1;1;1;1;1;1;1;1;1;1;1
PlayerTeam=1
BotTeams=2;2;2;2;2;2;2;2;2;2;2;2;2;2;2;2
MapName=empty.map
MapScale=3.0
BlockProjectilePredictors=true
BlockCheats=true
InvinciblePlayer=false
InvincibleBots=false
Timescale=1.0
BlockHealthbars=false
TimeRefilledByKill=0.0
ScoreToWin=0.0
ScorePerDamage=0.0
ScorePerKill=10.0
ScorePerMidairDirect=0.0
ScorePerAnyDirect=0.0
ScorePerTime=1.0
ScoreLossPerDamageTaken=10.0
ScoreLossPerDeath=0.0
ScoreLossPerMidairDirected=0.0
ScoreLossPerAnyDirected=0.0
ScoreMultAccuracy=false
ScoreMultDamageEfficiency=false
ScoreMultKillEfficiency=false
GameTag=VALORANT,APEX,CSGO,Fortnite
WeaponHeroTag=Revolver
DifficultyTag=3
AuthorsTag=@Lac0caL
BlockHitMarkers=false
BlockHitSounds=false
BlockMissSounds=false
BlockFCT=false
Description=EZ
GameVersion=2.0.1.2
ScorePerDistance=0.0
MBSEnable=false
MBSTime1=0.25
MBSTime2=0.5
MBSTime3=0.75
MBSTime1Mult=1.0
MBSTime2Mult=2.0
MBSTime3Mult=3.0
MBSFBInstead=false
MBSRequireEnemyAlive=false
LockFOVRange=false
LockedFOVMin=60.0
LockedFOVMax=120.0
LockedFOVScale=Clamped Horizontal
[Aim Profile]
Name=Aimbot
MinReactionTime=0.1
MaxReactionTime=0.1
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=90.0
FlickSpeed=10.0
FlickError=0.0
TrackSpeed=10.0
TrackError=0.0
MaxTurnAngleFromPadCenter=90.0
MinRecenterTime=0.0
MaxRecenterTime=0.0
OptimalAimFOV=90.0
OuterAimPenalty=0.0
MaxError=0.0
ShootFOV=15.0
VerticalAimOffset=-70.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
AimingStyle=Original
ScanSpeedMultiplier=1.0
MaxSeekPitch=30.0
MaxSeekYaw=30.0
AimingSpeed=5.0
MinShootDelay=0.3
MaxShootDelay=0.6
[Aim Profile]
Name=Default
MinReactionTime=0.3
MaxReactionTime=0.4
MinSelfMovementCorrectionTime=0.001
MaxSelfMovementCorrectionTime=0.05
FlickFOV=30.0
FlickSpeed=1.5
FlickError=15.0
TrackSpeed=3.5
TrackError=3.5
MaxTurnAngleFromPadCenter=75.0
MinRecenterTime=0.3
MaxRecenterTime=0.5
OptimalAimFOV=30.0
OuterAimPenalty=1.0
MaxError=40.0
ShootFOV=15.0
VerticalAimOffset=0.0
MaxTolerableSpread=5.0
MinTolerableSpread=1.0
TolerableSpreadDist=2000.0
MaxSpreadDistFactor=2.0
AimingStyle=Original
ScanSpeedMultiplier=1.0
MaxSeekPitch=30.0
MaxSeekYaw=30.0
AimingSpeed=5.0
MinShootDelay=0.3
MaxShootDelay=0.6
[Bot Profile]
Name=wide_strafe
DodgeProfileNames=wide_strafe_dodge
DodgeProfileWeights=1.0
DodgeProfileMaxChangeTime=5.0
DodgeProfileMinChangeTime=1.0
WeaponProfileWeights=100.0;100.0;100.0;100.0;100.0;100.0;100.0;100.0
AimingProfileNames=Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot
WeaponSwitchTime=60.0
UseWeapons=true
CharacterProfile=wide_strafe_char
SeeThroughWalls=true
NoDodging=false
NoAiming=false
AbilityUseTimer=0.1
UseAbilityFrequency=1.0
UseAbilityFreqMinTime=0.3
UseAbilityFreqMaxTime=0.6
ShowLaser=false
LaserRGB=X=1.000 Y=0.300 Z=0.000
LaserAlpha=1.0
[Bot Profile]
Name=WIDE2
DodgeProfileNames=wide_2
DodgeProfileWeights=1.0
DodgeProfileMaxChangeTime=5.0
DodgeProfileMinChangeTime=1.0
WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0
AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default
WeaponSwitchTime=3.0
UseWeapons=true
CharacterProfile=wide_strafe_char2
SeeThroughWalls=true
NoDodging=true
NoAiming=false
AbilityUseTimer=0.1
UseAbilityFrequency=1.0
UseAbilityFreqMinTime=0.3
UseAbilityFreqMaxTime=0.6
ShowLaser=false
LaserRGB=X=0.810 Y=0.200 Z=0.000
LaserAlpha=1.0
[Bot Profile]
Name=wide_3
DodgeProfileNames=wide_strafe_dodge
DodgeProfileWeights=1.0
DodgeProfileMaxChangeTime=5.0
DodgeProfileMinChangeTime=1.0
WeaponProfileWeights=100.0;100.0;100.0;100.0;100.0;100.0;100.0;100.0
AimingProfileNames=Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot
WeaponSwitchTime=60.0
UseWeapons=true
CharacterProfile=wide_3
SeeThroughWalls=true
NoDodging=true
NoAiming=false
AbilityUseTimer=0.1
UseAbilityFrequency=1.0
UseAbilityFreqMinTime=0.3
UseAbilityFreqMaxTime=0.6
ShowLaser=false
LaserRGB=X=1.000 Y=0.300 Z=0.000
LaserAlpha=1.0
[Bot Profile]
Name=wide_4
DodgeProfileNames=wide_strafe_dodge
DodgeProfileWeights=1.0
DodgeProfileMaxChangeTime=5.0
DodgeProfileMinChangeTime=1.0
WeaponProfileWeights=100.0;100.0;100.0;100.0;100.0;100.0;100.0;100.0
AimingProfileNames=Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot
WeaponSwitchTime=60.0
UseWeapons=true
CharacterProfile=wide_4
SeeThroughWalls=true
NoDodging=true
NoAiming=false
AbilityUseTimer=0.1
UseAbilityFrequency=1.0
UseAbilityFreqMinTime=0.3
UseAbilityFreqMaxTime=0.6
ShowLaser=false
LaserRGB=X=1.000 Y=0.300 Z=0.000
LaserAlpha=1.0
[Character Profile]
Name=Aimer
MaxHealth=2.0
WeaponProfileNames=Revolver;;;;;;;
MinRespawnDelay=1.0
MaxRespawnDelay=5.0
StepUpHeight=75.0
CrouchHeightModifier=0.5
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=50.0
MovementType=Base
MaxSpeed=1000.0
MaxCrouchSpeed=500.0
Acceleration=16000.0
AirAcceleration=16000.0
Friction=8.0
BrakingFrictionFactor=2.0
JumpVelocity=1000.0
Gravity=3.0
AirControl=0.25
CanCrouch=true
CanPogoJump=false
CanCrouchInAir=false
CanJumpFromCrouch=false
EnemyBodyColor=X=0.000 Y=0.145 Z=0.290
EnemyHeadColor=X=0.000 Y=0.145 Z=0.290
TeamBodyColor=X=0.000 Y=0.000 Z=255.000
TeamHeadColor=X=255.000 Y=255.000 Z=255.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Cuboid
MainBBHeight=270.0
MainBBRadius=60.0
MainBBHasHead=true
MainBBHeadRadius=23.0
MainBBHeadOffset=13.0
MainBBHide=true
ProjBBType=Cylindrical
ProjBBHeight=230.0
ProjBBRadius=55.0
ProjBBHasHead=true
ProjBBHeadRadius=45.0
ProjBBHeadOffset=0.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=true
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=0.0
BlockSpawnFOV=0.0
BlockSpawnDistance=0.0
RespawnAnimationDuration=0.5
AllowBufferedJumps=false
BounceOffWalls=false
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=1.0
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.25
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=2048.0
VerticalSpawnOffset=0.0
TerminalVelocity=0.0
CharacterModel=Endo
CharacterSkin=Default
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=false
ViewBobTime=0.0
ViewBobAngleAdjustment=0.0
ViewBobCameraZOffset=0.0
ViewBobAffectsShots=false
IsFlyer=false
FlightObeysPitch=false
FlightVelocityUp=800.0
FlightVelocityDown=800.0
[Character Profile]
Name=wide_strafe_char
MaxHealth=9999.0
WeaponProfileNames=Rocket Launcher;;;;;;;
MinRespawnDelay=60.0
MaxRespawnDelay=60.0
StepUpHeight=0.0
CrouchHeightModifier=0.75
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=0.0
MovementType=Base
MaxSpeed=0.0
MaxCrouchSpeed=500.0
Acceleration=8000.0
AirAcceleration=16000.0
Friction=0.0
BrakingFrictionFactor=0.0
JumpVelocity=0.0
Gravity=3.0
AirControl=0.0
CanCrouch=false
CanPogoJump=true
CanCrouchInAir=false
CanJumpFromCrouch=false
EnemyBodyColor=X=255.000 Y=0.000 Z=0.000
EnemyHeadColor=X=255.000 Y=255.000 Z=255.000
TeamBodyColor=X=0.000 Y=0.000 Z=255.000
TeamHeadColor=X=255.000 Y=255.000 Z=255.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Cuboid
MainBBHeight=270.0
MainBBRadius=60.0
MainBBHasHead=true
MainBBHeadRadius=23.0
MainBBHeadOffset=13.0
MainBBHide=true
ProjBBType=Cylindrical
ProjBBHeight=0.02
ProjBBRadius=0.01
ProjBBHasHead=false
ProjBBHeadRadius=25.0
ProjBBHeadOffset=-10.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=false
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=555.0
BlockSpawnFOV=0.0
BlockSpawnDistance=555.0
RespawnAnimationDuration=1.0
AllowBufferedJumps=true
BounceOffWalls=true
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=0.1
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.25
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=0.0
VerticalSpawnOffset=0.0
TerminalVelocity=0.0
CharacterModel=Endo
CharacterSkin=Default
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=true
ViewBobTime=0.0
ViewBobAngleAdjustment=0.0
ViewBobCameraZOffset=0.0
ViewBobAffectsShots=false
IsFlyer=false
FlightObeysPitch=false
FlightVelocityUp=800.0
FlightVelocityDown=800.0
[Character Profile]
Name=wide_strafe_char2
MaxHealth=9999.0
WeaponProfileNames=BB 2;;;;;;;
MinRespawnDelay=60.0
MaxRespawnDelay=60.0
StepUpHeight=0.0
CrouchHeightModifier=0.75
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=0.0
MovementType=Base
MaxSpeed=0.0
MaxCrouchSpeed=500.0
Acceleration=8000.0
AirAcceleration=16000.0
Friction=0.0
BrakingFrictionFactor=0.0
JumpVelocity=0.0
Gravity=3.0
AirControl=0.0
CanCrouch=false
CanPogoJump=false
CanCrouchInAir=false
CanJumpFromCrouch=false
EnemyBodyColor=X=255.000 Y=0.000 Z=0.000
EnemyHeadColor=X=255.000 Y=255.000 Z=255.000
TeamBodyColor=X=0.000 Y=0.000 Z=255.000
TeamHeadColor=X=255.000 Y=255.000 Z=255.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Cuboid
MainBBHeight=270.0
MainBBRadius=60.0
MainBBHasHead=true
MainBBHeadRadius=23.0
MainBBHeadOffset=13.0
MainBBHide=true
ProjBBType=Cylindrical
ProjBBHeight=0.02
ProjBBRadius=0.01
ProjBBHasHead=false
ProjBBHeadRadius=25.0
ProjBBHeadOffset=-10.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=false
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=555.0
BlockSpawnFOV=0.0
BlockSpawnDistance=555.0
RespawnAnimationDuration=1.0
AllowBufferedJumps=false
BounceOffWalls=true
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=0.1
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.25
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=0.0
VerticalSpawnOffset=0.0
TerminalVelocity=0.0
CharacterModel=Endo
CharacterSkin=Default
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=true
ViewBobTime=0.0
ViewBobAngleAdjustment=0.0
ViewBobCameraZOffset=0.0
ViewBobAffectsShots=false
IsFlyer=false
FlightObeysPitch=false
FlightVelocityUp=800.0
FlightVelocityDown=800.0
[Character Profile]
Name=wide_3
MaxHealth=9999.0
WeaponProfileNames=BB 3;;;;;;;
MinRespawnDelay=60.0
MaxRespawnDelay=60.0
StepUpHeight=0.0
CrouchHeightModifier=0.75
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=0.0
MovementType=Base
MaxSpeed=0.0
MaxCrouchSpeed=500.0
Acceleration=8000.0
AirAcceleration=16000.0
Friction=0.0
BrakingFrictionFactor=0.0
JumpVelocity=0.0
Gravity=3.0
AirControl=0.0
CanCrouch=false
CanPogoJump=false
CanCrouchInAir=false
CanJumpFromCrouch=false
EnemyBodyColor=X=255.000 Y=0.000 Z=0.000
EnemyHeadColor=X=255.000 Y=255.000 Z=255.000
TeamBodyColor=X=0.000 Y=0.000 Z=255.000
TeamHeadColor=X=255.000 Y=255.000 Z=255.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Cuboid
MainBBHeight=270.0
MainBBRadius=60.0
MainBBHasHead=true
MainBBHeadRadius=23.0
MainBBHeadOffset=13.0
MainBBHide=true
ProjBBType=Cylindrical
ProjBBHeight=0.02
ProjBBRadius=0.01
ProjBBHasHead=false
ProjBBHeadRadius=25.0
ProjBBHeadOffset=-10.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=false
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=555.0
BlockSpawnFOV=0.0
BlockSpawnDistance=555.0
RespawnAnimationDuration=1.0
AllowBufferedJumps=false
BounceOffWalls=true
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=0.1
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.25
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=0.0
VerticalSpawnOffset=0.0
TerminalVelocity=0.0
CharacterModel=Endo
CharacterSkin=Default
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=true
ViewBobTime=0.0
ViewBobAngleAdjustment=0.0
ViewBobCameraZOffset=0.0
ViewBobAffectsShots=false
IsFlyer=false
FlightObeysPitch=false
FlightVelocityUp=800.0
FlightVelocityDown=800.0
[Character Profile]
Name=wide_4
MaxHealth=9999.0
WeaponProfileNames=BB 4;;;;;;;
MinRespawnDelay=60.0
MaxRespawnDelay=60.0
StepUpHeight=0.0
CrouchHeightModifier=0.75
CrouchAnimationSpeed=1.0
CameraOffset=X=0.000 Y=0.000 Z=0.000
HeadshotOnly=false
DamageKnockbackFactor=0.0
MovementType=Base
MaxSpeed=0.0
MaxCrouchSpeed=500.0
Acceleration=8000.0
AirAcceleration=16000.0
Friction=0.0
BrakingFrictionFactor=0.0
JumpVelocity=0.0
Gravity=3.0
AirControl=0.0
CanCrouch=false
CanPogoJump=false
CanCrouchInAir=false
CanJumpFromCrouch=false
EnemyBodyColor=X=255.000 Y=0.000 Z=0.000
EnemyHeadColor=X=255.000 Y=255.000 Z=255.000
TeamBodyColor=X=0.000 Y=0.000 Z=255.000
TeamHeadColor=X=255.000 Y=255.000 Z=255.000
BlockSelfDamage=false
InvinciblePlayer=false
InvincibleBots=false
BlockTeamDamage=false
AirJumpCount=0
AirJumpVelocity=800.0
MainBBType=Cuboid
MainBBHeight=270.0
MainBBRadius=60.0
MainBBHasHead=true
MainBBHeadRadius=23.0
MainBBHeadOffset=13.0
MainBBHide=true
ProjBBType=Cylindrical
ProjBBHeight=50.0
ProjBBRadius=1.0
ProjBBHasHead=false
ProjBBHeadRadius=100.0
ProjBBHeadOffset=1.0
ProjBBHide=true
HasJetpack=false
JetpackActivationDelay=0.2
JetpackFullFuelTime=4.0
JetpackFuelIncPerSec=1.0
JetpackFuelRegensInAir=false
JetpackThrust=6000.0
JetpackMaxZVelocity=400.0
JetpackAirControlWithThrust=0.25
AbilityProfileNames=;;;
HideWeapon=false
AerialFriction=0.0
StrafeSpeedMult=1.0
BackSpeedMult=1.0
RespawnInvulnTime=0.0
BlockedSpawnRadius=555.0
BlockSpawnFOV=0.0
BlockSpawnDistance=555.0
RespawnAnimationDuration=1.0
AllowBufferedJumps=false
BounceOffWalls=true
LeanAngle=0.0
LeanDisplacement=0.0
AirJumpExtraControl=0.0
ForwardSpeedBias=0.1
HealthRegainedonkill=0.0
HealthRegenPerSec=0.0
HealthRegenDelay=0.0
JumpSpeedPenaltyDuration=0.0
JumpSpeedPenaltyPercent=0.25
ThirdPersonCamera=false
TPSArmLength=300.0
TPSOffset=X=0.000 Y=150.000 Z=150.000
BrakingDeceleration=0.0
VerticalSpawnOffset=0.0
TerminalVelocity=0.0
CharacterModel=Endo
CharacterSkin=Default
SpawnXOffset=0.0
SpawnYOffset=0.0
InvertBlockedSpawn=true
ViewBobTime=0.0
ViewBobAngleAdjustment=0.0
ViewBobCameraZOffset=0.0
ViewBobAffectsShots=false
IsFlyer=false
FlightObeysPitch=false
FlightVelocityUp=800.0
FlightVelocityDown=800.0
[Dodge Profile]
Name=wide_strafe_dodge
MaxTargetDistance=0.0
MinTargetDistance=0.0
ToggleLeftRight=true
ToggleForwardBack=false
MinLRTimeChange=1.0
MaxLRTimeChange=1.0
MinFBTimeChange=0.2
MaxFBTimeChange=0.5
DamageReactionChangesDirection=true
DamageReactionChanceToIgnore=0.5
DamageReactionMinimumDelay=0.125
DamageReactionMaximumDelay=0.25
DamageReactionCooldown=1.0
DamageReactionThreshold=0.0
DamageReactionResetTimer=0.1
JumpFrequency=0.1
CrouchInAirFrequency=0.0
CrouchOnGroundFrequency=0.0
TargetStrafeOverride=Ignore
TargetStrafeMinDelay=0.125
TargetStrafeMaxDelay=0.25
MinProfileChangeTime=0.0
MaxProfileChangeTime=0.0
MinCrouchTime=0.3
MaxCrouchTime=0.6
MinJumpTime=0.0
MaxJumpTime=1.0
LeftStrafeTimeMult=1.0
RightStrafeTimeMult=1.0
StrafeSwapMinPause=0.0
StrafeSwapMaxPause=0.25
BlockedMovementPercent=0.5
BlockedMovementReactionMin=0.125
BlockedMovementReactionMax=0.2
WaypointLogic=Ignore
WaypointTurnRate=200.0
MinTimeBeforeShot=0.15
MaxTimeBeforeShot=0.25
IgnoreShotChance=0.0
ForwardTimeMult=1.0
BackTimeMult=1.0
DamageReactionChangesFB=false
[Dodge Profile]
Name=wide_2
MaxTargetDistance=0.0
MinTargetDistance=0.0
ToggleLeftRight=true
ToggleForwardBack=false
MinLRTimeChange=1.0
MaxLRTimeChange=1.0
MinFBTimeChange=0.2
MaxFBTimeChange=0.5
DamageReactionChangesDirection=true
DamageReactionChanceToIgnore=0.5
DamageReactionMinimumDelay=0.125
DamageReactionMaximumDelay=0.25
DamageReactionCooldown=1.0
DamageReactionThreshold=0.0
DamageReactionResetTimer=0.1
JumpFrequency=0.0
CrouchInAirFrequency=0.0
CrouchOnGroundFrequency=0.0
TargetStrafeOverride=Mimic
TargetStrafeMinDelay=0.125
TargetStrafeMaxDelay=0.25
MinProfileChangeTime=0.0
MaxProfileChangeTime=0.0
MinCrouchTime=0.3
MaxCrouchTime=0.6
MinJumpTime=0.0
MaxJumpTime=1.0
LeftStrafeTimeMult=1.0
RightStrafeTimeMult=1.0
StrafeSwapMinPause=0.0
StrafeSwapMaxPause=0.25
BlockedMovementPercent=0.5
BlockedMovementReactionMin=0.125
BlockedMovementReactionMax=0.2
WaypointLogic=Ignore
WaypointTurnRate=200.0
MinTimeBeforeShot=0.15
MaxTimeBeforeShot=0.25
IgnoreShotChance=0.0
ForwardTimeMult=1.0
BackTimeMult=1.0
DamageReactionChangesFB=false
[Weapon Profile]
Name=Revolver
Type=Hitscan
ShotsPerClick=1
DamagePerShot=3500.0
KnockbackFactor=30.0
TimeBetweenShots=0.2
Pierces=false
Category=SemiAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=1.0
HeadshotCapable=true
HeadshotMultiplier=3.0
MagazineMax=3
AmmoPerShot=1
ReloadTimeFromEmpty=2.0
ReloadTimeFromPartial=2.0
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
ProjectileGraphic=Ball
VisualLifetime=10.0
BounceOffWorld=false
BounceFactor=0.5
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=1.0
CanAimDownSight=true
ADSZoomDelay=0.1
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=30.0
RecoilNegatable=false
DecalType=1
DecalSize=200.0
DelayAfterShooting=0.0
BeamTracksCrosshair=true
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=1.0
FlatKnockbackVertical=1.0
HitscanRadius=0.0
HitscanVisualRadius=10.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=2.0
AimPunchResetTime=0.05
AimPunchCooldown=0.5
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=false
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=2
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=1.0
FlatKnockbackVerticalMin=1.0
ADSScope=No Scope
ADSFOVOverride=70.0
ADSFOVScale=Clamped Horizontal
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
WeaponModel=Law Bringer
WeaponAnimation=Primary
UseIncReload=false
IncReloadStartupTime=0.0
IncReloadLoopTime=0.0
IncReloadAmmoPerLoop=1
IncReloadEndTime=1.0
IncReloadCancelWithShoot=true
WeaponSkin=Default
ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000
SpreadDecayDelay=0.0
ReloadBeforeRecovery=true
3rdPersonWeaponModel=Bolt Action Sniper
3rdPersonWeaponSkin=Default
ParticleMuzzleFlash=None
ParticleWallImpact=Gunshot
ParticleBodyImpact=Spike B
ParticleProjectileTrail=None
ParticleHitscanTrace=None
ParticleMuzzleFlashScale=1.0
ParticleWallImpactScale=5.0
ParticleBodyImpactScale=0.7
ParticleProjectileTrailScale=1.0
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=100.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,5.0
SpreadSCA=1.0,1.0,-1.0,5.0
SpreadMSA=1.0,1.0,-1.0,5.0
SpreadMCA=1.0,1.0,-1.0,5.0
SpreadSSH=0.0,0.1,0.0,0.0
SpreadSCH=1.0,1.0,-1.0,5.0
SpreadMSH=0.0,0.1,0.0,0.0
SpreadMCH=1.0,1.0,-1.0,5.0
MaxRecoilUp=5.0
MinRecoilUp=3.0
MinRecoilHoriz=0.5
MaxRecoilHoriz=1.0
FirstShotRecoilMult=1.0
RecoilAutoReset=true
TimeToRecoilPeak=0.03
TimeToRecoilReset=0.3
AAMode=0
AAPreferClosestPlayer=true
AAAlpha=1.0
AAMaxSpeed=360.0
AADeadZone=0.0
AAFOV=360.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.175
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Weapon Profile]
Name=Rocket Launcher
Type=Projectile
ShotsPerClick=1
DamagePerShot=1.0
KnockbackFactor=0.0
TimeBetweenShots=1.0
Pierces=false
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=800.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=2500.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=100.000 Y=0.000 Z=0.000
MaxTravelTime=5.0
MaxHitscanRange=100000.0
GravityScale=0.0
HeadshotCapable=false
HeadshotMultiplier=1.0
MagazineMax=0
AmmoPerShot=1
ReloadTimeFromEmpty=0.5
ReloadTimeFromPartial=0.5
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=25.0
DelayBeforeShot=0.0
ProjectileGraphic=Arrow
VisualLifetime=0.1
BounceOffWorld=false
BounceFactor=0.0
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=2.8
CanAimDownSight=false
ADSZoomDelay=0.0
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=0.0
RecoilNegatable=false
DecalType=0
DecalSize=20.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=0.0
FlatKnockbackVertical=0.0
HitscanRadius=0.0
HitscanVisualRadius=6.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=true
AimPunchAmount=30.0
AimPunchResetTime=0.2
AimPunchCooldown=0.1
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=0.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=0.0
FlatKnockbackVerticalMin=0.0
ADSScope=No Scope
ADSFOVOverride=72.099998
ADSFOVScale=Clamped Horizontal
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
WeaponModel=Rocket Launcher
WeaponAnimation=Secondary
UseIncReload=false
IncReloadStartupTime=0.0
IncReloadLoopTime=0.0
IncReloadAmmoPerLoop=1
IncReloadEndTime=0.0
IncReloadCancelWithShoot=true
WeaponSkin=Default
ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000
SpreadDecayDelay=0.0
ReloadBeforeRecovery=true
3rdPersonWeaponModel=Minigun
3rdPersonWeaponSkin=Default
ParticleMuzzleFlash=None
ParticleWallImpact=Rocket
ParticleBodyImpact=None
ParticleProjectileTrail=Fission Dealer
ParticleHitscanTrace=Tracer
ParticleMuzzleFlashScale=1.0
ParticleWallImpactScale=1.0
ParticleBodyImpactScale=1.0
ParticleProjectileTrailScale=1.2
Explosive=true
Radius=300.0
DamageAtCenter=120.0
DamageAtEdge=0.1
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=true
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=true
SpreadSSA=1.0,1.0,-1.0,0.0
SpreadSCA=1.0,1.0,-1.0,0.0
SpreadMSA=1.0,1.0,-1.0,0.0
SpreadMCA=1.0,1.0,-1.0,0.0
SpreadSSH=0.0,0.1,-1.0,0.0
SpreadSCH=1.0,1.0,-1.0,0.0
SpreadMSH=1.0,1.0,-1.0,0.0
SpreadMCH=1.0,1.0,-1.0,0.0
MaxRecoilUp=0.0
MinRecoilUp=0.0
MinRecoilHoriz=0.0
MaxRecoilHoriz=0.0
FirstShotRecoilMult=1.0
RecoilAutoReset=false
TimeToRecoilPeak=0.05
TimeToRecoilReset=0.35
AAMode=2
AAPreferClosestPlayer=false
AAAlpha=0.5
AAMaxSpeed=0.5
AADeadZone=0.0
AAFOV=180.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=true
TriggerBotDelay=0.001
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.095
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Weapon Profile]
Name=BB 2
Type=Projectile
ShotsPerClick=1
DamagePerShot=1.0
KnockbackFactor=30.0
TimeBetweenShots=0.3
Pierces=true
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=700.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=980.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=10.0
MaxHitscanRange=100000.0
GravityScale=0.02
HeadshotCapable=false
HeadshotMultiplier=1.0
MagazineMax=5
AmmoPerShot=1
ReloadTimeFromEmpty=1.7
ReloadTimeFromPartial=1.7
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=50.0
DelayBeforeShot=0.0
ProjectileGraphic=Arrow
VisualLifetime=0.3
BounceOffWorld=false
BounceFactor=0.0
BounceCount=0
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=0.8
CanAimDownSight=true
ADSZoomDelay=0.1
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=30.0
RecoilNegatable=false
DecalType=0
DecalSize=0.1
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=1.0
FlatKnockbackVertical=1.0
HitscanRadius=30.0
HitscanVisualRadius=7.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=30.0
AimPunchResetTime=0.2
AimPunchCooldown=0.1
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=5.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=1.0
FlatKnockbackVerticalMin=1.0
ADSScope=No Scope
ADSFOVOverride=70.0
ADSFOVScale=Clamped Horizontal
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
WeaponModel=Stud Gun
WeaponAnimation=Primary
UseIncReload=false
IncReloadStartupTime=0.0
IncReloadLoopTime=0.0
IncReloadAmmoPerLoop=1
IncReloadEndTime=0.0
IncReloadCancelWithShoot=true
WeaponSkin=Default
ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000
SpreadDecayDelay=0.0
ReloadBeforeRecovery=true
3rdPersonWeaponModel=Minigun
3rdPersonWeaponSkin=Default
ParticleMuzzleFlash=None
ParticleWallImpact=None
ParticleBodyImpact=None
ParticleProjectileTrail=Spike B
ParticleHitscanTrace=Bullet
ParticleMuzzleFlashScale=1.0
ParticleWallImpactScale=1.0
ParticleBodyImpactScale=1.0
ParticleProjectileTrailScale=0.75
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=100.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,5.0
SpreadSCA=1.0,1.0,-1.0,5.0
SpreadMSA=1.0,1.0,-1.0,5.0
SpreadMCA=1.0,1.0,-1.0,5.0
SpreadSSH=0.0,0.1,0.0,0.0
SpreadSCH=1.0,1.0,-1.0,5.0
SpreadMSH=0.0,0.1,0.0,0.0
SpreadMCH=1.0,1.0,-1.0,5.0
MaxRecoilUp=3.0
MinRecoilUp=1.0
MinRecoilHoriz=0.5
MaxRecoilHoriz=1.0
FirstShotRecoilMult=1.0
RecoilAutoReset=true
TimeToRecoilPeak=0.03
TimeToRecoilReset=0.55
AAMode=0
AAPreferClosestPlayer=true
AAAlpha=1.0
AAMaxSpeed=360.0
AADeadZone=0.0
AAFOV=360.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.175
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Weapon Profile]
Name=BB 3
Type=Projectile
ShotsPerClick=1
DamagePerShot=1.0
KnockbackFactor=30.0
TimeBetweenShots=0.3
Pierces=true
Category=FullyAuto
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=900.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=1100.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=10.0
MaxHitscanRange=100000.0
GravityScale=0.02
HeadshotCapable=false
HeadshotMultiplier=1.0
MagazineMax=5
AmmoPerShot=1
ReloadTimeFromEmpty=2.0
ReloadTimeFromPartial=2.0
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=50.0
DelayBeforeShot=0.0
ProjectileGraphic=Shuriken
VisualLifetime=0.3
BounceOffWorld=false
BounceFactor=0.5
BounceCount=0
HomingProjectileAcceleration=1.0
ProjectileEnemyHitRadius=1.2
CanAimDownSight=true
ADSZoomDelay=0.1
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=30.0
RecoilNegatable=false
DecalType=1
DecalSize=30.0
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=1.0
FlatKnockbackVertical=1.0
HitscanRadius=30.0
HitscanVisualRadius=7.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=30.0
AimPunchResetTime=0.2
AimPunchCooldown=0.1
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=5.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=1.0
FlatKnockbackVerticalMin=1.0
ADSScope=No Scope
ADSFOVOverride=70.0
ADSFOVScale=Clamped Horizontal
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
WeaponModel=Stud Gun
WeaponAnimation=Primary
UseIncReload=false
IncReloadStartupTime=0.0
IncReloadLoopTime=0.0
IncReloadAmmoPerLoop=1
IncReloadEndTime=0.0
IncReloadCancelWithShoot=true
WeaponSkin=Default
ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000
SpreadDecayDelay=0.0
ReloadBeforeRecovery=true
3rdPersonWeaponModel=Minigun
3rdPersonWeaponSkin=Default
ParticleMuzzleFlash=None
ParticleWallImpact=None
ParticleBodyImpact=None
ParticleProjectileTrail=Circles
ParticleHitscanTrace=Bullet
ParticleMuzzleFlashScale=1.0
ParticleWallImpactScale=1.0
ParticleBodyImpactScale=1.0
ParticleProjectileTrailScale=2.8
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=100.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,5.0
SpreadSCA=1.0,1.0,-1.0,5.0
SpreadMSA=1.0,1.0,-1.0,5.0
SpreadMCA=1.0,1.0,-1.0,5.0
SpreadSSH=0.0,0.1,0.0,0.0
SpreadSCH=1.0,1.0,-1.0,5.0
SpreadMSH=0.0,0.1,0.0,0.0
SpreadMCH=1.0,1.0,-1.0,5.0
MaxRecoilUp=3.0
MinRecoilUp=1.0
MinRecoilHoriz=0.5
MaxRecoilHoriz=1.0
FirstShotRecoilMult=1.0
RecoilAutoReset=true
TimeToRecoilPeak=0.03
TimeToRecoilReset=0.55
AAMode=0
AAPreferClosestPlayer=true
AAAlpha=1.0
AAMaxSpeed=360.0
AADeadZone=0.0
AAFOV=360.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.175
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Weapon Profile]
Name=BB 4
Type=Projectile
ShotsPerClick=1
DamagePerShot=1.0
KnockbackFactor=30.0
TimeBetweenShots=1.3
Pierces=true
Category=SemiAutoNoPrehold
BurstShotCount=1
TimeBetweenBursts=0.5
ChargeStartDamage=10.0
ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000
ChargeTimeToAutoRelease=2.0
ChargeTimeToCap=1.0
ChargeMoveSpeedModifier=1.0
MuzzleVelocityMin=X=1000.000 Y=0.000 Z=0.000
MuzzleVelocityMax=X=1000.000 Y=0.000 Z=0.000
InheritOwnerVelocity=0.0
OriginOffset=X=0.000 Y=0.000 Z=0.000
MaxTravelTime=10.0
MaxHitscanRange=100000.0
GravityScale=0.2
HeadshotCapable=false
HeadshotMultiplier=1.0
MagazineMax=3
AmmoPerShot=1
ReloadTimeFromEmpty=3.0
ReloadTimeFromPartial=3.0
DamageFalloffStartDistance=100000.0
DamageFalloffStopDistance=100000.0
DamageAtMaxRange=50.0
DelayBeforeShot=0.0
ProjectileGraphic=Ball
VisualLifetime=0.3
BounceOffWorld=false
BounceFactor=1.5
BounceCount=2
HomingProjectileAcceleration=0.0
ProjectileEnemyHitRadius=1.2
CanAimDownSight=true
ADSZoomDelay=0.1
ADSZoomSensFactor=0.7
ADSMoveFactor=1.0
ADSStartDelay=0.0
ShootSoundCooldown=0.08
HitSoundCooldown=0.08
HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000
ADSBlocksShooting=false
ShootingBlocksADS=false
KnockbackFactorAir=30.0
RecoilNegatable=false
DecalType=0
DecalSize=0.1
DelayAfterShooting=0.0
BeamTracksCrosshair=false
AlsoShoot=
ADSShoot=
StunDuration=0.0
CircularSpread=true
SpreadStationaryVelocity=0.0
PassiveCharging=false
BurstFullyAuto=true
FlatKnockbackHorizontal=1.0
FlatKnockbackVertical=1.0
HitscanRadius=30.0
HitscanVisualRadius=7.0
TaggingDuration=0.0
TaggingMaxFactor=1.0
TaggingHitFactor=1.0
RecoilCrouchScale=1.0
RecoilADSScale=1.0
PSRCrouchScale=1.0
PSRADSScale=1.0
ProjectileAcceleration=0.0
AccelIncludeVertical=false
AimPunchAmount=30.0
AimPunchResetTime=0.2
AimPunchCooldown=0.1
AimPunchHeadshotOnly=false
AimPunchCosmeticOnly=true
MinimumDecelVelocity=5.0
PSRManualNegation=false
PSRAutoReset=true
AimPunchUpTime=0.05
AmmoReloadedOnKill=0
CancelReloadOnKill=false
FlatKnockbackHorizontalMin=1.0
FlatKnockbackVerticalMin=1.0
ADSScope=No Scope
ADSFOVOverride=70.0
ADSFOVScale=Clamped Horizontal
ADSAllowUserOverrideFOV=true
IsBurstWeapon=false
ForceFirstPersonInADS=true
ZoomBlockedInAir=false
ADSCameraOffsetX=0.0
ADSCameraOffsetY=0.0
ADSCameraOffsetZ=0.0
QuickSwitchTime=0.1
WeaponModel=Molecule Cannon
WeaponAnimation=Primary
UseIncReload=false
IncReloadStartupTime=0.0
IncReloadLoopTime=0.0
IncReloadAmmoPerLoop=1
IncReloadEndTime=0.0
IncReloadCancelWithShoot=true
WeaponSkin=Default
ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000
SpreadDecayDelay=0.0
ReloadBeforeRecovery=true
3rdPersonWeaponModel=Minigun
3rdPersonWeaponSkin=Default
ParticleMuzzleFlash=None
ParticleWallImpact=None
ParticleBodyImpact=None
ParticleProjectileTrail=Circles
ParticleHitscanTrace=Bullet
ParticleMuzzleFlashScale=1.0
ParticleWallImpactScale=1.0
ParticleBodyImpactScale=1.0
ParticleProjectileTrailScale=2.7
Explosive=false
Radius=500.0
DamageAtCenter=100.0
DamageAtEdge=100.0
SelfDamageMultiplier=0.5
ExplodesOnContactWithEnemy=false
DelayAfterEnemyContact=0.0
ExplodesOnContactWithWorld=false
DelayAfterWorldContact=0.0
ExplodesOnNextAttack=false
DelayAfterSpawn=0.0
BlockedByWorld=false
SpreadSSA=1.0,1.0,-1.0,5.0
SpreadSCA=1.0,1.0,-1.0,5.0
SpreadMSA=1.0,1.0,-1.0,5.0
SpreadMCA=1.0,1.0,-1.0,5.0
SpreadSSH=0.0,0.1,0.0,0.0
SpreadSCH=1.0,1.0,-1.0,5.0
SpreadMSH=0.0,0.1,0.0,0.0
SpreadMCH=1.0,1.0,-1.0,5.0
MaxRecoilUp=3.0
MinRecoilUp=1.0
MinRecoilHoriz=0.5
MaxRecoilHoriz=1.0
FirstShotRecoilMult=1.0
RecoilAutoReset=true
TimeToRecoilPeak=0.03
TimeToRecoilReset=0.55
AAMode=0
AAPreferClosestPlayer=true
AAAlpha=1.0
AAMaxSpeed=360.0
AADeadZone=0.0
AAFOV=360.0
AANeedsLOS=true
TrackHorizontal=true
TrackVertical=true
AABlocksMouse=false
AAOffTimer=0.0
AABackOnTimer=0.0
TriggerBotEnabled=false
TriggerBotDelay=0.0
TriggerBotFOV=1.0
StickyLock=false
HeadLock=false
VerticalOffset=0.0
DisableLockOnKill=false
UsePerShotRecoil=false
PSRLoopStartIndex=0
PSRViewRecoilTracking=0.45
PSRCapUp=9.0
PSRCapRight=4.0
PSRCapLeft=4.0
PSRTimeToPeak=0.175
PSRResetDegreesPerSec=40.0
UsePerBulletSpread=false
PBS0=0.0,0.0
[Map Data]
reflex map version 8
global
entity
type WorldSpawn
String32 targetGameOverCamera end
Float sky.timeOfDay 18.699097
String256 title SS
UInt8 playersMin 1
UInt8 playersMax 16
Bool8 modeCTF 1
Bool8 mode1v1 1
Bool8 mode2v2 1
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|
d7d1356a9bb04d8b2309eb9455a4a1c2fd795569 | 097689cb15f57ed753422489c1129404769b863a | /SSH/chapter03/work/work01/work1_1.tst | fd7a23fab22a7e303aa150e939b414117bd5fbe1 | [] | no_license | Beeru4/project | f247ae4a6669ba8b93965c0fa50d2cfe285e1918 | cf12bce4d6d5750f8ff2f748182249724e287a76 | refs/heads/master | 2020-05-15T13:33:40.217444 | 2019-05-17T07:50:21 | 2019-05-17T07:50:21 | 182,304,194 | 0 | 0 | null | null | null | null | GB18030 | Scilab | false | false | 806 | tst | work1_1.tst | PL/SQL Developer Test script 3.0
29
--计算所交税金
-- Created on 2019/3/20 by J.Z
declare
-- Local variables here
v_sal emp.sal%TYPE;
--税率
v_s NUMBER(7,3);
--速算扣除数
v_ss NUMBER(7,3);
begin
--查出员工工资
SELECt SAL - 1500 INTO v_sal FROM emp WHERE ENAME = 'KING';
CASE
WHEN v_sal <= 1500 THEN
v_s:=0.03;
v_ss:=0;
WHEN v_sal <= 4500 THEN
v_s:=0.1;
v_ss:=105;
WHEN v_sal <= 9000 THEN
v_s:=0.2;
v_ss:=555;
WHEN v_sal <= 3500 THEN
v_s:=0.25;
v_ss:=1005;
END CASE;
DBMS_OUTPUT.PUT_LINE('所交税务金额:' || TO_CHAR(v_sal * v_s - v_ss));
end;
0
0
|
90c4f118104f31412273c9d4cf451c47c98f3803 | 33d7960e39a3e71591538dccbe1dd4014c377e78 | /Sample Solution/CompFin_2017_SS_Exercise_01_MathQF.sce | aad3c47ef23a7c0d49b29f5e004977cd2522f72f | [] | no_license | wiiwins/Compfin | 529e2997994babb9e3795283ddbd8ec782131148 | 2629685421e970a369ec797b76dda3d2803bcbcf | refs/heads/master | 2020-05-18T01:25:39.357847 | 2019-06-27T11:21:46 | 2019-06-27T11:21:46 | 184,090,400 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 561 | sce | CompFin_2017_SS_Exercise_01_MathQF.sce | // C-Exercise 01
clear;
funcprot(0);
function Vn = capital (V0, r, n, c)
// simple rate
if (c == 0) then
Vn = V0 * (1+r)^n;
// continuous rate
elseif (c == 1) then
Vn = V0 * exp(r*n);
// wrong value for parameter s
else
error("Error: Argument for compound type must be 0 (continuous) or 1 (simple).");
end
endfunction
// test parameters as in C-Exercise 01
V0 = 1000;
r = 0.05;
n = 10;
c = 0;
// call function with test parameters
Vn = capital(V0, r, n, c)
disp(Vn)
|
32426381782cd7efeab890f1a81b737266958399 | 449d555969bfd7befe906877abab098c6e63a0e8 | /479/CH13/EX13.4/Example_13_4.sce | 5c1116c471b172eb282b68b15e56b8393e3f1391 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,011 | sce | Example_13_4.sce | //Chemical Engineering Thermodynamics
//Chapter 13
//Thermodynamics in Phase Equilibria
//Example 13.4
clear;
clc;
//Given
T = [80.6 79.0 77.3 61.4];//Various temperature in deg cel
x1 = [0.0 15.0 29.0 100.0];//mole fraction of CHCl3 in liquid phase
y1 = [0.0 20.0 40.0 100.0];//mole fraction of CHCl3 in vapour phase
P1 = [1370 1310 1230 700];//Vapour pressure of CHCl3 in mm Hg
P = 760;//Total pressure in mm Hg
//To Calculate the equilibrium data i.e y/x and compare with the experimental values
//From equation 13.27 (page no 245);K = y1/x1 = Pi/P
mprintf('Temperature Experimental Calculated');
for i = 1:4
mprintf('\n %f',T(i));
if x1(i) == 0
mprintf(' Not defined');
else
K_ex(i) = y1(i)/x1(i);
mprintf(' %f',K_ex(i));
end
K_c(i) = P1(i)/P;
mprintf(' %f',K_c(i));
end
if K_ex(i) == K_c(i)
then mprintf('\n\n The liquid solution is perfect');
else
mprintf('\n\n The liquid solution is imperfect');
end
//end |
76a195db897e888530fa47838690e1e5fb23a1ed | 449d555969bfd7befe906877abab098c6e63a0e8 | /812/CH12/EX12.08/12_08.sce | cd86a974902fe177a78e54df8ebb5a795cf78d36 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,239 | sce | 12_08.sce | //velocity and entropy//
pathname=get_absolute_file_path('12.08.sce')
filename=pathname+filesep()+'12.08-data.sci'
exec(filename)
//Density at section 1(in lbm/ft^3):
d1=p1*144/R/T1
//Velocity at section 2(in ft/sec):
V2=(p1-p2)*144/d1/V1*32.2+V1
//Density at section 2(in lbm/ft3):
d2=d1*V1/V2
//Temperature at section 2(in R):
T2=p2/d2/R*144
//Mach number at section 2:
M2=V2/sqrt(k*R*32.16*T2)
//Stagnation Temperature at section 2(in R):
T02=T2*(1+(k-1)/2*M2^2)
//Stagnation pressure at section 2 (in psia):
p02=p2*(T02/T2)^(k/(k-1))
//Mach Number at section 1:
M1=V1/sqrt(k*R*32.16*T1)
//Stagnation temperature at section 1(in R):
T01=T1*(1+(k-1)/2*M1^2)
//Energy added(in Btu/lbm):
E=Cp*(T02-T01)
//Change in entropy(in Btu/(lbm-R)):
dS=Cp*log(T2/T1)-(Cp-Cv)*log(p2/p1)
printf("\n\nRESULTS\n\n")
printf("\n\nVelocity at section 2: %.3f ft/sec\n\n",V2)
printf("\n\nDensity at section 2: %.3f lbm/ft^3\n\n",d2)
printf("\n\nTemperature at section 2: %.3f R\n\n",T2)
printf("\n\nStagnation Temperature at section 2: %.3f R\n\n",T02)
printf("\n\nStagnation pressure at section 2: %.3f psia\n\n",p02)
printf("\n\nEnergy added: %.3f Btu/lbm\n\n",E)
printf("\n\nChange in entropy: %.3f Btu/(lbm-R)\n\n",dS)
|
9bfc5a970cba6e9f2da6f75ebc75acde89ed35b2 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2123/CH5/EX5.26/Exa_5_26.sce | 9b4041366264dc322ea0f289696c700762777f96 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 506 | sce | Exa_5_26.sce | //Example No. 5.26
clc;
clear;
close;
format('v',9);
//Given Data :
V1=675;//V
alfa1=90.5;//degree
N1=350;//rpm
Ia1=30;//A
N2=500;//rpm
Rf=0.22;//ohm
Ra=0.22;//ohm
Ia2=Ia1*N2/N1;//A
disp(Ia2,"Armature current of converter in A : ");
Va1=V1*sqrt(2)/%pi*(1+cosd(alfa1));//V
Eb1=Va1-Ia1*(Ra+Rf);//V
//Eb1/Eb2=Ia1*N1/(Ia2*N2)
//Eb2=Va2-Ia2*(Ra+Rf)
Va2=Eb1*Ia2*N2/(Ia1*N1)+Ia2*(Ra+Rf);//V
alfa2=acosd(Va2/V1/sqrt(2)*%pi-1);//degree
disp(alfa2,"Fringe angle of converter in degree : ");
|
0f3c7f08c9c4e0efbb31325b4171680cdb99e23d | 449d555969bfd7befe906877abab098c6e63a0e8 | /2135/CH4/EX4.17/Exa_4_17.sce | 77047330b8295fc0e7c91bb326803afb32fbf989 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,000 | sce | Exa_4_17.sce | //Exa 4.17
clc;
clear;
close;
format('v',7);
//Given Data :
m=1;//Kg
p1=1;//bar
T1=290;//K
p2=30;//bar
T2=290;//K
n=1.3;//constant
R=300;//Nm/KgK
Cv=0.72;//KJ/KgK
disp("part (a) Isothermally")
V1=R*T1/p1/10^5;//m^3/Kg
V2=p1*V1/p2;//m^3/Kg
w=p1*10^5*V1*log(V2/V1)/1000;//KJ/Kg
disp(w,"Workdone in KJ/Kg : ");
deltaU=m*Cv*(T2-T1);//KJ(as T1=T2)
disp(deltaU,"Change in internal energy in KJ : ");
q=w+deltaU;//KJ/Kg
disp(q,"Heat transfer in KJ/Kg : ");
S2subS1=m*R/1000*log(V2/V1)+m*Cv*log(T2/T1);//KJ/KgK
disp(S2subS1,"Change in entropy in KJ/KgK : ");
disp("part (b) Polytropically")
T2=T1*(p2/p1)^((n-1)/n);//K
disp(T2,"Temperature T2 in K : ");
V1=R*T1/p1/10^5;//m^3/Kg
V2=(p1/p2)^(1/n)*V1;//m^3/Kg
w= m*R/1000*(T1-T2)/(n-1);;//KJ/Kg
disp(w,"Workdone in KJ/Kg : ");
deltaU=m*Cv*(T2-T1);//KJ(as T1=T2)
q=w+deltaU;//KJ/Kg
disp(q,"Heat transfer in KJ/Kg : ");
S2subS1=m*R/1000*log(V2/V1)+m*Cv*log(T2/T1);//KJ/KgK
disp(S2subS1,"Change in entropy in KJ/KgK : ");
|
a138d2df7238c4d5e355c1c524e7dde351641679 | 1db0a7f58e484c067efa384b541cecee64d190ab | /macros/convmtx.sci | c0aa89179ce1e8e55b33d564d6db27f0fce0dbfa | [] | no_license | sonusharma55/Signal-Toolbox | 3eff678d177633ee8aadca7fb9782b8bd7c2f1ce | 89bfeffefc89137fe3c266d3a3e746a749bbc1e9 | refs/heads/master | 2020-03-22T21:37:22.593805 | 2018-07-12T12:35:54 | 2018-07-12T12:35:54 | 140,701,211 | 2 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 939 | sci | convmtx.sci | //Convolution Matrix
//convmtx(h,n) returns the convolution matrix for vector h. If h is a
//column vector and X is a column vector of length n, then convmtx(h,n)*X
//gives the result of the convolution oof h and X.If R is a row vector and X//is a row vector of length N, then X*convmtx(R,N) gives the convolution of R and X.
//Example:
//Generate a simple convolution matrix.
//
// h = [%i 1 2 3];
// convmtx(h,7) //Convolution matrix
//
//Author
//Debdeep Dey
function t=convmtx(v,n);
n=double(n);
[mv,nv]=size(v);
v=v(:);
//put Toeplitz code inline
c = [v; zeros(n-1,1)];
r = zeros(n,1);
m = length(c);
x = [r(n:-1:2) ; c(:)];
cidx = (0:m-1)';
ridx = n:-1:1;
t = cidx(:,ones(n,1)) + ridx(ones(m,1),:); //Toeplitz subscripts
t(:) = x(t); //actual data
//t = single(t);
// end of toeplitz code
if mv < nv then
t = t.';
end
endfunction
|
1ee63ece77ed32fa1acd50fdd3c4f3b99c73e169 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2762/CH4/EX4.5.3/4_5_3.sce | 69d2367e5905c23b2c222dea46842ea7d0e216ee | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 601 | sce | 4_5_3.sce | //Transport Processes and Seperation Process Principles
//Chapter 4
//Example 4.5-3
//Principles of Steady State Heat Transfer
//given data in si units
//nomenclature of unmentioned specifications similar to previous example
D=0.05;//diameter of the tube in m
A=%pi*D*D/4;
fr=4;//mass flow rate in kg/s
G=fr/A;
mu=7.1e-4;
Re=(D*G)/mu;
Cp=120;//Specific Heat in J/kg K
k=13;
Pr=(Cp*mu)/k
hl=(k/D)*0.625*((Re*Pr)^0.4);
dT=505-500;//when liq is heated from 500 to 505 K
q=fr*Cp*dT;
dTw=30;//temp diff b/w fluid and Tw
Ad=q/(hl*dTw);
L=Ad/(%pi*D);
mprintf("the tube length= %f m",L)
|
2b57d658d4bb7c5cd04bca9bfe2a54131d2a06f6 | 449d555969bfd7befe906877abab098c6e63a0e8 | /181/CH7/EX7.45/example7_45.sce | ebe93dd8997bf51f67e42527cad608970cee3484 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,680 | sce | example7_45.sce | // Calculate input admittance
// Basic Electronics
// By Debashis De
// First Edition, 2010
// Dorling Kindersley Pvt. Ltd. India
// Example 7-45 in page 348
clear; clc; close;
// Given data
mu=20; // Amplification factor
rd=10*10^3; // Dynamic resistance in K-ohms
gm=2*10^-3; // Transconductance in mA/V
Cgs=3*10^-12; // Gate-source capacitance in pF
Cds=1*10^-12; // Drain-source capacitance in pF
Cgd=2*10^-12; // Gate-drain capacitance in pF
// Calculation
printf("(a)Rd = 50 K\n");
printf("At f=1000Hz\n");
Ygs=%i*2*%pi*10^3*Cgs;
Yds=%i*2*%pi*10^3*Cds;
Ygd=%i*2*%pi*10^3*Cgd;
Yd=2*10^-6;
gd=10^-4;
Av=(-gm+Ygd)/(gd+Yd+Yds+Ygs);
C1=Cgs+(17.7*Cgd);
printf("Av = %0.1f\nC1 = %0.1e F\n\n",Av,C1);
printf("At f=10^6Hz\n");
Ygs1=%i*1.88*10^-6;
Yds1=%i*0.628*10^-6;
Ygd1=%i*1.26*10^-6;
Av1=(-gm+Ygd1)/(gd+Yd+Yds+Ygs);
R1=10^6/2.48;
C2=37.6*10^-12;
printf("Av = %0.1f\nR1 = %0.2e ohm\nC1=%0.1e F\n\n",Av1,R1,C2);
Zl=%i*5*10^4;
Yl=%i*2*10^-6;
printf("(b)Zl = j5*10^4;Yl = j2*10^-6\n");
printf("For f=1000Hz\n");
Av2=-gm/(gd+Yl);
C3=Cgs+(20.2*Cgd);
R2=20.8*10^6;
printf("Av = %0.2f\nR1 = %0.2e ohm\nC1 = %0.1e F\n\n",Av2,R2,C3);
printf("For f=10^6Hz\n");
Av3=(-200+(%i*1.26))/(10+(%i*3.88));
C4=Cgs+(18.4*Cgd);
R3=10^6/8.64;
printf("Av = %0.2f\nR1 = %0.2e ohm\nC1 = %0.2e F",Av3,R3,C4);
// Result
// (a)Rd = 50 K
// At f=1000Hz
// Av = -19.6
// C1 = 3.8e-011 F
// At f=10^6Hz
// Av = -19.6
// R1 = 4.03e+005 ohm
// C1=3.8e-011 F
// (b)Zl = j5*10^4;Yl = j2*10^-6
// For f=1000Hz
// Av = -19.99
// R1 = 2.08e+007 ohm
// C1 = 4.3e-011 F
// For f=10^6Hz
// Av = -17.34
// R1 = 1.16e+005 ohm
// C1 = 3.98e-011 F |
739bfd737b65de2e218f1ae17d4719e8b6a40792 | 449d555969bfd7befe906877abab098c6e63a0e8 | /380/CH9/EX9.2/Ex9_2.sce | 3106beeb9fdd6ba8761f36e22887da2cf05158b2 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,092 | sce | Ex9_2.sce | //Caption:Find the efficiency
//Exa:9.2
clc;
clear;
close;
V=230;//in volts
f=60;//in Hertz
P=6;//no. of poles
N_s=120*f/P;//synchronous speed (in rpm)
V_1=V/sqrt(3);//per phase voltage (in Volts)
R_2=0.25;//in ohms
R_1=0.5;//in ohms
X_1=0.75;//in ohms
X_2=0.5;//in ohms
X_m=100;//in ohms
R_c=500;//in ohms
s=0.025;//slip
Z_1=R_1+%i*X_1;//in ohms
Z_2=(R_2/s)+%i*X_2;//in ohms
Z=(0.002-(%i*.01)+(0.10025-%i*0.0050125));
Z_e=(1/Z);//equivalent impedance (in ohms)
Z_in=Z_1+Z_e;//input impedance (in ohms)
I_1=V_1/Z_in;//in Amperes
theta=atand(imag(I_1)/real(I_1));
P_in=3*V_1*real(I_1);
P_scl=3*(abs(I_1))^2*R_1;
E_1=V_1-I_1*Z_1;
I_c=E_1/R_c;//core loss current
I_m=-%i*E_1/X_m;
I_phy=I_c+I_m;//excitation current (in Amperes)
I_2=I_1-I_phy;//rotor current (in Amperes)
P_m=3*abs(I_c)*abs(I_c)*R_c;//core loss (in Watts)
P_ag=P_in-P_scl-P_m;//air gap power (in Watts)
P_rcl=3*abs(I_2)*abs(I_2)*R_2;//rotor copper loss (in Watts)
P_d=P_ag-P_rcl;//power developed (in Watts)
P_o=P_d-150;//output power (in Watts)
Eff=P_o/P_in;
disp(Eff*100,'Efficiency (%)='); |
b8754c0b42b50531eee9093516c41a6106e8cf14 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1445/CH2/EX2.19/ch2_ex_19.sce | dbac96db806ea4f4721a2b3dd0032d0ac57df022 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,594 | sce | ch2_ex_19.sce | //CHAPTER 2- STEADY-STATE ANALYSIS OF SINGLE-PHASE A.C. CIRCUIT
//Example 19
disp("CHAPTER 2");
disp("EXAMPLE 19");
//VARIABLE INITIALIZATION
z1=4+(%i*3); //impedance in rectangular form in Ohms
z2=6-(%i*8); //impedance in rectangular form in Ohms
z3=1.6+(%i*7.2); //impedance in rectangular form in Ohms
v=100 //in volts
//SOLUTION
//solution (i)
//Admittance of each parallel branch Y1 and Y2
Y1=1/z1;
Y2=1/z2;
disp("SOLUTION (i)");
disp(sprintf("Admittance parallel branch 1 is %3f %3fj S", real(Y1), imag(Y1)));
disp(sprintf("Admittance parallel branch 2 is %3f+%3fj S", real(Y2), imag(Y2)));
disp(" ");
//solution (ii)
//Total circuit impedance Z=(Z1||Z2)+Z3
z=z3+(z2*z1)/(z1+z2)
disp("SOLUTION (ii)");
disp(sprintf("Total circuit impedance is %3f %3fj S", real(z), imag(z)));
//solution in the book is wrong as there is a total mistake in imaginery part 7.2+0.798=11.598
//
//solution (iii)
//Supply current I=V/Z
i=v/z;
function [z,angle]=rect2pol(x,y);
z0=sqrt((x^2)+(y^2)); //z is impedance & the resultant of x and y
angle=atan(y/x)*(180/%pi); //to convert the angle from radians to degrees
endfunction;
[z, angle]=rect2pol(real(i), imag(i));
//disp(sprintf("%f, %f",z,angle));
//disp(sprintf("%f, %f",real(i), imag(i)));
pf=cos(angle*%pi/180);
disp("SOLUTION (iii)");
disp(sprintf("The power factor is %f",pf));
//solution (iv)
//Power supplied by source = VI cosΦ or I^2 . R
P=v*real(i)*pf;
disp("SOLUTION (iv)");
disp(sprintf("The power supplied by source is %f watt",P));
//END
|
d15783ade31cd9c98a93e6a605ff13bf142f6745 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1016/CH5/EX5.18/es5_18.sce | 72218141405e3653c5ccd0d5301a1052fc1e3998 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 297 | sce | es5_18.sce | clc;clear;
//Example 5.18
//given values
Vs1=4.6;//Stopping Potential in V
Vs2=12.9;//Stopping Potential in V
f1=2*10^15;//frequency in Hz
f2=4*10^15;//frequency in Hz
e=1.6*10^-19;//the charge on electron in C
//calculations
h=((Vs2-Vs1)*e)/(f2-f1)
disp(h,'The Plancks const in Js') |
b8ca83f540b0bee40f9e63afb31ab2faf0f34bb1 | 08e6015408a35a317d4d0b609af8ccae9b88a3bf | /src/03/a/RAM8.tst | 38d6ae807a14650e5ac9b5c986dab681065b93d9 | [
"MIT"
] | permissive | lekhacman/nand2teris | 38c7aa44b2329ccf102333af5dc1dd542869144b | 520ca48a492b6ac8966330ddaf5174c19e5a8f7f | refs/heads/master | 2023-01-06T18:36:35.660251 | 2020-12-27T09:08:39 | 2020-12-27T09:08:39 | 209,975,266 | 1 | 0 | MIT | 2022-12-10T03:13:50 | 2019-09-21T11:41:33 | Scilab | UTF-8 | Scilab | false | false | 5,415 | tst | RAM8.tst | // This file is part of www.nand2tetris.org
// and the book "The Elements of Computing Systems"
// by Nisan and Schocken, MIT Press.
// File name: projects/03/a/RAM8.tst
load RAM8.hdl,
output-file RAM8.out,
compare-to RAM8.cmp,
output-list time%S1.4.1 in%D1.6.1 load%B2.1.2 address%D3.1.3 out%D1.6.1;
set in 0,
set load 0,
set address 0,
tick,
output;
tock,
output;
set load 1,
tick,
output;
tock,
output;
set in 11111,
set load 0,
tick,
output;
tock,
output;
set load 1,
set address 1,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set in 3333,
set address 3,
tick,
output;
tock,
output;
set load 1,
tick,
output;
tock,
output;
set load 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set in 7777,
tick,
output;
tock,
output;
set load 1,
set address 7,
tick,
output;
tock,
output;
set load 0,
tick,
output;
tock,
output;
set address 3,
eval,
output;
set address 7,
eval,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set in %B0101010101010101,
set address 0,
tick,
output;
tock,
output;
set address 1,
tick,
output,
tock,
output;
set address 2,
tick,
output,
tock,
output;
set address 3,
tick,
output,
tock,
output;
set address 4,
tick,
output,
tock,
output;
set address 5,
tick,
output,
tock,
output;
set address 6,
tick,
output,
tock,
output;
set address 7,
tick,
output,
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 0,
set in %B1010101010101010,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 0,
set in %B0101010101010101,
tick,
output,
tock,
output;
set address 1,
set in %B1010101010101010,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 1,
set in %B0101010101010101,
tick,
output,
tock,
output;
set address 2,
set in %B1010101010101010,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 2,
set in %B0101010101010101,
tick,
output,
tock,
output;
set address 3,
set in %B1010101010101010,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 3,
set in %B0101010101010101,
tick,
output,
tock,
output;
set address 4,
set in %B1010101010101010,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 4,
set in %B0101010101010101,
tick,
output,
tock,
output;
set address 5,
set in %B1010101010101010,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 5,
set in %B0101010101010101,
tick,
output,
tock,
output;
set address 6,
set in %B1010101010101010,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 6,
set in %B0101010101010101,
tick,
output,
tock,
output;
set address 7,
set in %B1010101010101010,
tick,
output;
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
set load 1,
set address 7,
set in %B0101010101010101,
tick,
output,
tock,
output;
set load 0,
set address 0,
tick,
output;
tock,
output;
set address 1,
eval,
output;
set address 2,
eval,
output;
set address 3,
eval,
output;
set address 4,
eval,
output;
set address 5,
eval,
output;
set address 6,
eval,
output;
set address 7,
eval,
output;
|
422dd39d5ec6a5c2357e2abaf9e9da19bdae1bd3 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2252/CH5/EX5.6/Ex5_6.sce | e175fff9b44ab8e239ef38a3c73c38593a14ee01 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 362 | sce | Ex5_6.sce |
N=800//no. of turns
dI=10-5//change in current
dB=1.2-.8//corresponding change in flux density
A=15D-4//cross sectional area
L=A*N*dB/dI
mprintf("Self inductance of coil,L=%f H\n",L)
di=5-10//change in current
dt=.04//time taken for change
e=-L*di/dt
mprintf("Induced emf when the current falls uniformly from 10 A to 5 A in 0.04 sec=%d V",round(e))
|
23384761b830133c910e775a6949dad6470a82fd | cb952289471732053d3db787d93f249ea37a7e55 | /5º PERÍODO/Processamento Digital de Sinais/TRABALHO/modelo.sce | b2df33e80a1f010e4837be8841f52b68d4847d66 | [] | no_license | kaikecc/UFRN | 647d09e6beeadfeabfb59f479cd77a5c2ff7bebc | 821cce2e36808e890a75714d71b7cc1a24e52c27 | refs/heads/master | 2022-08-09T19:23:52.552924 | 2022-06-23T21:27:05 | 2022-06-23T21:27:05 | 177,469,993 | 1 | 1 | null | null | null | null | UTF-8 | Scilab | false | false | 289 | sce | modelo.sce | //fss = 10000;
//[acc] = sensor(10000,620,15)
function [acc] = sensor(f_s,freq_fund,A)
t = [0:1/f_s:10];
f = freq_fund;
Amp = A;
acc = 0;
for i = 1:2:1000
distancia = (Amp/i)*sin(2*%pi*i*f.*t);
acc = acc + distancia;
end
//my_fft(acc,10000);
endfunction
|
171a8b35c5f0bb3bbecfed2cbdc4165757225461 | 449d555969bfd7befe906877abab098c6e63a0e8 | /401/CH7/EX7.1/Example7_1.sce | 508092ea233bc5aac89f39b04983b95a7e8440aa | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 964 | sce | Example7_1.sce | //Example 7.1
//Program to determine the total carrier recombination lifetime and
//the power internally generated within the device
clear;
clc ;
close ;
//Given data
Tau_r=60; //ns - RADIATIVE RECOMBINATION LIFETIME
Tau_nr=100; //ns - NON RADIATIVE RECOMBINATION LIFETIME
Lambda=0.87*10^-6; //metres - PEAK EMISSION WAVELENGTH
c= 2.998*10^8; //m/s - SPEED OF LIGHT
h= 6.626*10^(-34); //J/K - PLANK's CONSTANT
e=1.602*10^(-19); //Coulumbs - CHARGE OF AN ELECTRON
i=40*10^(-3); //A - DRIVE CURRENT
//Total carrier recombination lifetime
Tau=Tau_r*Tau_nr/(Tau_r+Tau_nr);
//Internal quantum efficiency
eeta_int=Tau/Tau_r;
//Power internally generated within the device
P_int=eeta_int*h*c*i/(Lambda*e);
//Displaying the Results in Command Window
printf("\n\n\t Total carrier recombination lifetime is %0.1f ns.",Tau);
printf("\n\n\t Power internally generated within the device is %0.1f mW .",P_int/10^(-3)); |
5cee6e3f8bf8ce5fc9813c72aa3f972004635530 | 31c6b1437c7dc52b977bf6790b1b24eff7f7b5f5 | /movingaverage.sci | c4d0e152e80c3d3c524c4de4524d3fe85e07f7e4 | [] | no_license | RobinEccleston/Scilab-Snippets | 4744c071ef891cc4905cbecc000a1f5bf667a8f7 | 7886058a25ec4821cfeba6d8e148a0a2aced330c | refs/heads/master | 2021-01-26T00:48:02.042794 | 2020-02-26T11:35:49 | 2020-02-26T11:35:49 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 762 | sci | movingaverage.sci | ModuleName="movingaverage";
Version="0.01";
DateModified="13-Feb-2015";
DateOfCreation="13-Feb-2015";
Author="Rob Eccleston";
Description="When given a waveform and the number of samples to average, returns ..
a waveform with a smoothed average for the given number of sampels";
mprintf("Loading " + ModuleName + " V" + Version + ", Last Modified: " + DateModified + "\n")
function [ SmoothedWaveform ] = movingaverage(y,NumToAverage)
x=y
midpoint=NumToAverage/2;
LowerRange=floor(midpoint);
UpperRange=ceil(midpoint)-1;
x_ave=0;
for i=1+LowerRange:max(size(x))-UpperRange
x_ave(i)=sum(x(i-LowerRange:i+UpperRange))/NumToAverage;
end
SmoothedWaveform=x_ave;
endfunction
|
772e7aac48bb6322c8329016090ce95456116d26 | 449d555969bfd7befe906877abab098c6e63a0e8 | /476/CH9/EX9.14/Example_9_14.sce | 24e0050410aa590a5321f5ad40374cb51cbb4e73 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 836 | sce | Example_9_14.sce | //A Textbook of Chemical Engineering Thermodynamics
//Chapter 9
//Chemical Reaction Equilibria
//Example 14
clear;
clc;
//Given:
//Reaction: CO(g) + H2O(g) --> CO2(g) + H2(g)
K = 1; //equilibrium constant for reaction
//Mole fraction of components:
//CO: (1-e)/2
//H2O: (1-e)/2
//CO2: e/2
//H2: e/2
//To calculate fractional dissociation of steam
//(a).
//(e/2)(e/2)/[(1-e)/2][(1-e)/2] = K
//Solving we get:
e = 1/2;
mprintf('(a) Fractional dissociation of steam is %i percent',e*100);
//(b). If reactant stream is diluted with 2 mol nitrogen
//Mole fraction of components
//CO: (1-e)/4
//H20: (1-e)/4
//CO2: e/4
//H2: e/4
//so, K = (e/4)(e/4)/[(1-e)/4][(1-e)/4]
//On solving we get
e = 1/2;
mprintf('\n\n (b) After dilution fractional distillation of steam is %i percent',e*100);
//end |
6e118628a2088e086390a58a8626ba1ab4abd5cc | 449d555969bfd7befe906877abab098c6e63a0e8 | /431/CH4/EX4.12/EX4_12.sce | 1425202d70ef1f22a5490a716a3789ab9a3948c0 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 717 | sce | EX4_12.sce | //Calculate power developed and efficiency
//Chapter 4
//Example 4.12
//page 308
clear;
clc;
disp("Example 4.12")
S=0.03; //slip
SI=50; //stator input in kilowatts
SL=2; //stator loss in kilowatts
RI=SI-SL; //rotor input in kilowatts
RIL=S*RI; //rotor I^2R loss
//rotor core loss can be neglected at 3percent slip
PDR=RI-RIL; //power developed by the rotor
printf("Power developed by the rotor=%fkW",PDR);
FWL=1; //friction and windage loss in kilowatt
OP=PDR-FWL; //output power
printf("\nOutput power=%fkW",OP);
effi=(OP*100)/SI;
printf("\nEfficiency of the motor=%f percent",effi)
|
126e86701cf8abe30528ff63d47ff571b4b3c531 | 449d555969bfd7befe906877abab098c6e63a0e8 | /926/CH3/EX3.12/Chapter3_Example12.sce | eeae855a41bdb59297a649e452899a3f53b014dd | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 3,625 | sce | Chapter3_Example12.sce | //Hougen O.A., Watson K.M., Ragatz R.A., 2004. Chemical process principles Part-1: Material and Energy Balances(II Edition). CBS Publishers & Distributors, New Delhi, pp 504
//Chapter-3, Illustration 12, Page 65
//Title: Calculation of percentage composition by volume
//=============================================================================
clear
clc
//INPUT
n = 1; //Total no moles of NH3 in lb mole
v = 100; //Volume of NH3 entering in cu ft
a = [1,2,1,1]; //Stoichiometric coefficients of NH3, O2, HNO3 and H2O in overall reaction
b = [4,5,6,4];//Stoichiometric coefficients of NH3, O2, HNO3 and H2O in reaction 1
a1 = .21; //lb moles of O2 in 1 lb mole of air
b1 = .79; //lb moles of N2 in 1 lb mole of air
a2 = .2; //Amount of excess O2
T = [20,700]; //Temperature at which gases enters the process and leave the catalyzer in degree C
P = [755,743]; //Pressure at which gases enters the process and leaves the catalyzer in mm Hg
T2 = 273; //Temperature at standard conditions in K
P2 = 760; //Pressure at standard conditions in mm Hg
V = 359; //Volume at standard conditons in cu ft
N = .85; //lb moles of NH3 oxidised in catalyzer
c = .9; //Nitric oxide entering the tower oxidised to Nitric acid
MW = 63; //Molecular weight of HNO3 in lb/lb mole
//CALCULATIONS
//part(a)
T1 = T(1)+273;
T3 = T(2)+273;
n1 = a(2)*n; //O2 required in lb moles
n2 = n1*(n+a2); //O2 supplied in lb moles
n3 = n2/a1; //Air supplied in lb moles
v1 = V*(T1/T2)*(P2/P(1)); //Volume of NH3 in cu ft
v2 = n3*v1; //Volume of air supplied
v3 = v2*v/v1; //Volume of air per 100 ft of NH3 in cu ft
//part(b)
n4 = b1*n3; //N2 present in air in lb moles
n5 = n3+n; //Total lb moles of gas entering the catalyzer
x1 = n*100/n5; //Composition of NH3 by volume %
x2 = n2*100/n5; //Composition of O2 by volume %
x3 = n4*100/n5; //Composition of N2 by volume %
//Part(c)
n6 = n - N; //lb moles of NH3 leaving catalyzer
n7 = b(2)*N/b(1); //lb moles of O2 consumed in catalyzer
n8 = n2 - n7; //lb moles of O2 leaving catalyzer
n9 = b(4)*N/b(1); //lb moles of NO formed in catalyzer
n10 = b(3)*n9/b(4); //lb moles of H2O formed in catalyzer
N1 = n4+n6+n8+n9+n10; //lb moles of total quantity of gas leaving catalyzer
y1 = n9*100/N1; //Composition of NO by volume %
y2 = n10*100/N1; //Composition of H2O by volume %
y3 = n6*100/N1; //Composition of NH3 by volume %
y4 = n8*100/N1; //Composition of O2 by volume %
y5 = n4*100/N1; //Composition of N2 by volume %
//part(d)
N2 = n*v/v1; //lb moles of NH3 per 100 cu ft
N3 = N1*N2; //lb moles of gas leaving catalyzer
v4 = N3*V; //Volume at standard conditions of gas leaving catalyzer in cu ft
v5 = v4*(P2/P(2))*(T3/T2); //Volume of gas laeving catalyzer per 100 cu ft NH3 entering in cu ft
//part(e)
N4 = N2*n9; //lb moles of NO produced in catalyzer
N5 = N4*c; //lb moles of NO oxidised in tower
W = N5*MW; //Weight of HNO3 formed in lb
//OUTPUT
mprintf('\n (a) Volume of air per %3.0f cu ft NH3 entering is %4.0f cu ft',v,v3);
mprintf('\n (b) Percentage composition by volume of gases entering catalyzer:- \n NH3 = %2.1f \n O2 = %3.1f \n N2 = %3.1f',x1,x2,x3);
mprintf('\n (c) Percentage composition by volume of gases leaving catalyzer:- \n NO = %2.1f \n H2O = %3.1f \n NH3 = %2.1f \n O2 = %3.1f \n N2 = %3.1f',y1,y2,y3,y4,y5);
mprintf('\n (d) Volume of gases leaving catalyzer per %3.0f cu ft of NH3 entering is %4.0f cu ft',v,v5);
mprintf('\n (e) Weight of HNO3 produced per %3.0f cu ft of NH3 entering is %3.1f lb',v,W);
//========================END OF PROGRAM====================================== |
e90a26db0a9c446ac815683fed8fc0b97ab7a254 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3819/CH4/EX4.12/Ex4_12.sce | 164896dc47107aa38d0490a864a3404c32128f98 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 376 | sce | Ex4_12.sce | // A Textbook of Fluid Mecahnics and Hydraulic Machines - By R K Bansal
// Chapter 4-Buoyancy and Floatation
//// Problem 4.12
//Given Data Set in the Problem
dens=1000
g=9.81
D=4
d=2.4
h=4
SG=0.6
AB=d/2
AG=h/2
BG= AG-AB
//Calculaions
I=%pi/64*D^4
Vol=%pi/4*D^2*d
GM=I/Vol-BG //Meta centric height
mprintf("The meta centric height is %f m\n",GM)
|
cb9a193a20e9907d85427738e0d40bbf38172986 | a45f93853fdb67523e71e3e7fb88c4298eae1ef7 | /Screens/Confirm File Overwrite Dialog Screen.tst | 2299847da6322d6f79ead0199991dcb10c0b86c7 | [] | no_license | voarsh/Disney-Treasure-Planet-Battle-at-Procyon | 68192cbfdf8b823bc8399e3ea1e62d4976b74aed | 99cbbc70701ef6e8f9d95eba1052635de992910f | refs/heads/master | 2020-04-16T01:44:03.761947 | 2016-06-08T10:25:05 | 2016-06-08T10:25:05 | 38,745,932 | 3 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 1,297 | tst | Confirm File Overwrite Dialog Screen.tst | ScreenName String 'Confirm File Overwrite Dialog Screen'
ImplName String 'Dialog Screen'
ElementChunkArray Int 4
ScreenElementType Int 0
ImplName String 'Front End Dialog Screen Backdrop'
TabIndex Int 1
Selectable Bool True
Enabled Bool True
ReferenceArea Rect( 61, 165, 603, 436 ) # left,top,right,bottom
ScreenElementType Int 1
ImplName String 'Open Dialog Next Button'
TabIndex Int 3
Selectable Bool True
Enabled Bool True
ReferenceArea Rect( 205, 300, 355, 344 ) # left,top,right,bottom
Font String 'BlackChancery16'
Text String 'IDGS_TPFRONTENDTEXT02_YES'
Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 )
HotKey Int -1
ScreenElementType Int 1
ImplName String 'Open Dialog Previous Button'
TabIndex Int 4
Selectable Bool True
Enabled Bool True
ReferenceArea Rect( 439, 300, 589, 344 ) # left,top,right,bottom
Font String 'BlackChancery16'
Text String 'IDGS_TPFRONTENDTEXT02_NO'
Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 )
HotKey Int -1
ScreenElementType Int 1
ImplName String 'Center Justify Label'
TabIndex Int 5
Selectable Bool False
Enabled Bool True
ReferenceArea Rect( 0, 236, 800, 269 ) # left,top,right,bottom
Font String 'UniversLightBold14'
Text String 'IDGS_TPFRONTENDTEXT02_FILECHANGE_OVERWRITE'
Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 )
HotKey Int -1
|
e6eada542e317e131f15b4db39c637659a4d1bce | 449d555969bfd7befe906877abab098c6e63a0e8 | /824/CH8/EX8.12/8_12.sce | 74bfd801092b22873fc5f2a196e3f1bda0ba51f5 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 569 | sce | 8_12.sce | //clear//
clc
clear
exec("8.12data.sci");
t=1:10:250;
for i=1:length(t)
T(i)=2*t(i)+283;
k2(i)=4.58*exp((E2/1.987)*((1/500)-(1/T(i))))
k1(i)=3.3*exp((E1/1.987)*((1/300)-(1/T(i))))
Ca(i)=Cao/(1+tau*k1(i))
kappa=UA/(vo*Cao)/Cp
G(i)=-(tau*k1(i)/(1+k1(i)*tau))*DH1-(k1(i)*tau*k2(i)*tau*DH2/((1+tau*k1(i)) *(1+tau*k2(i))));
Tc=(To+kappa*Ta)/(1+kappa);
Cb(i)=tau*k1(i)*Ca(i)/(1+k2(i)*tau);
R(i)=Cp*(1+kappa)*(T(i)-Tc);
Cc=Cao-Ca(i)-Cb(i);
F(i)=G(i)-R(i);
end
plot(T',[G R])
xtitle( 'Figure E8-12.1', 'T (K)', 'G(T),R(T)' ) ;
legend(['G(T)';'R(T)']);
|
5462b2f9b6885393a0590ca27144818000c316bc | 449d555969bfd7befe906877abab098c6e63a0e8 | /51/CH7/EX7.5/7_5.sce | c559c777de3acb2c48126e868de4ee932205b97e | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 742 | sce | 7_5.sce | clc;
clear;
D=0.1;//m
H=0.3;//m
v=50;//km/hr
Dm=20;//mm
T=20;//degree C
fm=49.9;//Hz ; frequency for the model
//f=func(D,H,V,d,vis)
//f=T^(-1); D=l; H=L; V=L*(T^(-1)); d=M*(L^(-3)); vis=M*(L^(-1))*(T^(-1))
//by applying pi theorem,
//(f*D/V)=funct((D/H),(d*V*D/vis))
//hence; Dm/Hm = D/H, dm*Vm*Dm/vism = d*V*D/vis, and (f*D/V)=(fm*Dm/Vm)
Hm=(Dm*H*1000/(D*1000));//mm
V=v*1000/3600;//m/s
vism=1/1000;//kg/(m*s)
vis=1.79/100000;//kg/(m*s)
d=1.23;//kg/(m^3)
dm=998;//kg/(m^3)
Vm=(vism*d*D*V*1000)/(vis*dm*Dm);//m/s
f=(V/Vm)*(Dm/(D*1000))*fm;//Hz
disp("mm",Hm,"The model dimension =")
disp("m/s",Vm,"The velocity at which the test should be performed=")
disp("Hz",f,"The predicted prototype vortex shredding frequency =") |
b74e09fc3153d0a6e7c999457c0b167acb0f00ec | 676ffceabdfe022b6381807def2ea401302430ac | /utilities/FieldConvert/Tests/wallNormalData.tst | 9be958160e97fa21fa4660c130559612642fda11 | [
"MIT"
] | permissive | mathLab/ITHACA-SEM | 3adf7a49567040398d758f4ee258276fee80065e | 065a269e3f18f2fc9d9f4abd9d47abba14d0933b | refs/heads/master | 2022-07-06T23:42:51.869689 | 2022-06-21T13:27:18 | 2022-06-21T13:27:18 | 136,485,665 | 10 | 5 | MIT | 2019-05-15T08:31:40 | 2018-06-07T14:01:54 | Makefile | UTF-8 | Scilab | false | false | 740 | tst | wallNormalData.tst | <?xml version="1.0" encoding="utf-8"?>
<test>
<description> Fitst part of wallNormalData module (projection a point to the boudndary) </description>
<executable>FieldConvert</executable>
<parameters> -f -e -m wallNormalData:bnd=0:xorig="0,0":projDir="1,1":nptsH=3:distH=0.002 wallNormalData.xml wallNormalData.fld wallNormalData.pts</parameters>
<files>
<file description="Session File">wallNormalData.xml</file>
<file description="Session File">wallNormalData.fld</file>
</files>
<metrics>
<metric type="Linf" id="1">
<value variable="x" tolerance="1e-6">0.354968</value>
<value variable="y" tolerance="1e-6">0.354968</value>
</metric>
</metrics>
</test>
|
889d457f1773d2d841e559d64dc8f71ff4e14ab3 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2780/CH3/EX3.3/Ex3_3.sce | 028baf7dff5bfcc81c8d28b8ad8fb1c72f13d843 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 377 | sce | Ex3_3.sce | clc
//to calculate width of slit
//direction of minima in fraunhofer diffraction due to single slit is given by %pi/lambda*e*siuntheta=+m*%pi,where m=1,2,3
//angular spread of the central maximum on either side of the incident light is sintheta=lambda/e,where m=1,position of first minima
lambda=5000*10^-8
e=lambda/sin(%pi/6)
disp("width of slit is e="+string(e)+"cm")
|
e3301725691dcbe606be994d0949ba28d83345d1 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3751/CH2/EX2.18/Ex2_18.sce | 4b9f5a90bb62f307901449389d079565d204e83c | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,358 | sce | Ex2_18.sce | //Fluid system - By - Shiv Kumar
//Chapter 2 - Impact of Jet
//Example 2.18
clc
clear
//Given Data:-
Vi=18; //velocity of Jet at Inlet of, m/s
u=6; //Velocity of Vane, m/s
ui=u;
uo=u;
AoD=120; //Angle of deflection of the Jet, degrees
//Data Used:-
g=9.81; //Acceleration due to gravity, m/s^2
//Computations:-
beta_i=(180-AoD)/2; //degrees
beta_o=beta_i;
//(i)
alpha_i=beta_i-asind(ui*sind(180-beta_i)/Vi); //degrees
//(ii)
Vrwi=Vi*cosd(alpha_i)-ui; //m/s
Vfi=Vi*sind(alpha_i); //m/s
Vri=Vfi/sind(beta_i); //m/s
Vro=Vri;
Vfo=Vro*sind(beta_o); //m/s
Vwo=Vro*cosd(beta_o)-uo; //m/s
alpha_o=atand(Vfo/Vwo); //degrees
Vo=Vfo/sind(alpha_o); //m/s
//(iii)
W=(Vi*cosd(alpha_i)+Vwo)*u/g; //N-m/N
//Results(a):-
printf("(i)Angle of Jet at Inlet, alpha_i=%.2f Degrees \n", alpha_i)
printf("(ii)Absolute velocity of Jet at Outlet, Vo=%.2f m/s with angle alpha_o=%.2f Degrees \n", Vo,alpha_o) //The answer vary due to round off error
printf("(iii)Work done per N of Water=%.2f N-m/N", W) //The answer vary due to round off error
|
d2a14ccbd58e6a40945cd0cdeabbb200375a7eb6 | a5f0fbcba032f945a9ee629716f6487647cafd5f | /Machine_Learning/demos/Ensemble_Demo.sce | 90067678ee72f90e8221a347f4b712efcf9f0cd3 | [
"BSD-2-Clause"
] | permissive | SoumitraAgarwal/Scilab-gsoc | 692c00e3fb7a5faf65082e6c23765620f4ecdf35 | 678e8f80c8a03ef0b9f4c1173bdda7f3e16d716f | refs/heads/master | 2021-04-15T17:55:48.334164 | 2018-08-07T13:43:26 | 2018-08-07T13:43:26 | 126,500,126 | 1 | 1 | null | null | null | null | UTF-8 | Scilab | false | false | 743 | sce | Ensemble_Demo.sce | // Demo for Ensemble classifier -- Scilab
getd('../macros')
// Data preparation for gaussian
M = csvRead('Datasets/standard.csv')
x = M(:, [1,2,3,4,5,6,7,8]);
y = M(:, 9);
y(or(isnan(x),'c'),:) = []
x(or(isnan(x),'c'),:) = []
probMat = naiveBayes(x, y)
testx = x;
pred1 = naiveBayesGaussian(x, y, probMat, testx)
// Data preparation for multinomial
x = x(:, 1);
probMat = naiveMultBayes(x, y)
testx = x;
pred2 = naiveMultBayesGaussian(x, y, probMat, testx)
increment = 0.01
pred = ensemble(pred1, pred2, y, increment)
disp('Error through classifier 1 = ' + string(0.5*sqrt(norm(pred1 - y))))
disp('Error through classifier 2 = ' + string(0.5*sqrt(norm(pred2 - y))))
disp('Error through ensemble = ' + string(0.5*sqrt(norm(pred - y)))) |
4a29c9cc6b7516d2d1886d181b8058b500ee7167 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2381/CH12/EX12.4/ex_4.sce | 5a4df5fbbaa934659bf4f640cc743163dfd4ceae | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 216 | sce | ex_4.sce | //Example 4//WAVELENGTH
clc;
clear;
close;
x=1/5;//
h=60;//cm
h1=((1-x)*h);//cm
h2=((1+x)*h);//cm
disp(h1,"wavelength of waves in north-direction is,(cm)=")
disp(h2,"wavelength of waves in south-direction is,(cm)=")
|
71091e59af7e8fe7f183d6f6f88d1465014a7f52 | caafd05eb866a2bd249681ceeb5734ca2df71833 | /TP7/mcnorm.sci | 0da0b882095a3e685658c89669968232dc473fe2 | [
"MIT"
] | permissive | mmewen/MT09-numerical-analysis | 5fb1f251e86f9d43d7eeb23ce7bcc91d6ca3fa8b | cde3871aa885811bc31166e778b2a4f052e74b64 | refs/heads/master | 2021-01-11T22:11:18.631204 | 2017-01-14T10:59:23 | 2017-01-14T10:59:23 | 78,934,966 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 98 | sci | mcnorm.sci | function z = mcnorm (A, y)
// résoud A'Az = A'y
z = (A'*A)\(A'*y);
endfunction
|
faa0c2985c368305634b41a13c70d66a8b4ba64d | 449d555969bfd7befe906877abab098c6e63a0e8 | /1619/CH4/EX4.1.4/Example4_1_4.sce | 7c9bf02fca69d43a96ab7704f3741bf2668c5d54 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 168 | sce | Example4_1_4.sce | //Example 4.1.4 page 4.6
clc;
clear;
R= 0.65;
P0= 10*10^-6;
Ip= R*P0;
Ip=Ip*10^6; //convertinf in uA...
printf("The generated photocurrent is %.1f uA",Ip);
|
01fb3520752d489429c9a6f3e1b2bfed7b13634c | 449d555969bfd7befe906877abab098c6e63a0e8 | /2708/CH19/EX19.5/ex_19_5.sce | 445e60ce3d54518d430b4a8bf7e860b47d5f10de | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 370 | sce | ex_19_5.sce | //Example 19.5 // energy of electron
clc;
clear;
//given data :
h=6.626D-34;// plank constant in J-s
a=.3D-9;// unit cell width in m
p=h/(2*a);// electron momentum
m=9.1D-31;// mass of electron in Kg
E=p^2/(m*2);// formula for energy
disp(p,"electron momentum in Kg m/s")
E=E/1.6D-19;// ro convert in ev
disp(E,"energy of electron at this momentum in eV")
|
6689ba5c9b9f04b093e757946bdf44820650b2d4 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1472/CH8/EX8.5/8_5.sce | 26e087c0dbd29b6f3601d232f3c17b8d13fc4e29 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 226 | sce | 8_5.sce | clc
//initialization of varaibles
Q=826 //B/lb
T=860 //R
T1=2000+460 //R
T2=1000+460 //R
//calculations
ds=Q/T
dsgas=Q*(log(T2)-log(T1))/(T1-T2)
dst=ds+dsgas
//results
printf("Total entropy change = %.3f B/R",dst)
|
191ceed9f9899ca095688fd4fa165b6c39233320 | 676ffceabdfe022b6381807def2ea401302430ac | /solvers/CompressibleFlowSolver/Tests/Perturbation_NS_M15_square_CBC_par.tst | 1ee3222c4fb233244525279cff6b6eb79fd07378 | [
"MIT"
] | permissive | mathLab/ITHACA-SEM | 3adf7a49567040398d758f4ee258276fee80065e | 065a269e3f18f2fc9d9f4abd9d47abba14d0933b | refs/heads/master | 2022-07-06T23:42:51.869689 | 2022-06-21T13:27:18 | 2022-06-21T13:27:18 | 136,485,665 | 10 | 5 | MIT | 2019-05-15T08:31:40 | 2018-06-07T14:01:54 | Makefile | UTF-8 | Scilab | false | false | 1,248 | tst | Perturbation_NS_M15_square_CBC_par.tst | <?xml version="1.0" encoding="utf-8"?>
<test>
<description>Euler, pressure perturbation to test RiemannInvariant CBC, supersonic Navier-Stokes equations parallel</description>
<executable>CompressibleFlowSolver</executable>
<parameters>--use-scotch Perturbation_NS_M15_square_CBC_par.xml</parameters>
<processes>8</processes>
<files>
<file description="Session File"> Perturbation_NS_M15_square_CBC_par.xml</file>
<file description="Restart File"> Perturbation_NS_M15_square_CBC_par.rst</file>
</files>
<metrics>
<metric type="L2" id="1">
<value variable="rho" tolerance="1e-12">6.78967e-06</value>
<value variable="rhou" tolerance="1e-12">0.0025751</value>
<value variable="rhov" tolerance="1e-12">0.00155111</value>
<value variable="E" tolerance="1e-12">17373.8</value>
</metric>
<metric type="Linf" id="2">
<value variable="rho" tolerance="1e-12">0.000231056</value>
<value variable="rhou" tolerance="1e-12">0.210912</value>
<value variable="rhov" tolerance="1e-12">0.0508178</value>
<value variable="E" tolerance="1e-12">69537.9</value>
</metric>
</metrics>
</test>
|
a32f5e50423a70b650b34653507f7e59c052547d | 449d555969bfd7befe906877abab098c6e63a0e8 | /3683/CH3/EX3.12/Ex3_12.sce | 7d4365df52348c0bf40784d83f3260cc328c1ee6 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,176 | sce | Ex3_12.sce | Bf=1450//width of flange, in mm
Df=120//thickness of flange, in mm
d=400//effective depth, in mm
m=13.33//modular ratio
Ast=1800//in sq mm
Asc=450//in sq mm
top_cover=30//in mm
M=200*10^6//in N-mm
//assume x>Df; equating moments of area on compression and tension sides about N.A.
x=(m*Ast*d+Bf*Df^2/2+(1.5*m-1)*Asc*top_cover)/(m*Ast+Bf*Df+(1.5*m-1)*Asc)//in mm
//we find that x<Df, hence our assumption that x>Df is wrong
//to find x using Bf(x^2)/2 + (1.5m-1)Asc(x-d')=mAst(d-x), which becomes of the form px^2+qx+r=0
p=Bf/2
q=m*Ast+(1.5*m-1)*Asc
r=-(m*Ast*d+(1.5*m-1)*Asc*top_cover)
//solving quadratic equation
x=(-q+sqrt(q^2-4*p*r))/(2*p)//in mm
//as x<Xc, beam is under-reinforced; let stress in concrete at level of steel be equal to 'a' times the stress in concrete at top
a=(x-top_cover)/x
//taking moments about tensile steel
sigma_cbc=M/(Bf*x*(d-x/3)/2+(1.5*m-1)*Asc*a*(d-top_cover))//in MPa
sigma_st=m*sigma_cbc*(d-x)/x//in MPa
sigma_sc=1.5*m*a*sigma_cbc//in MPa
mprintf("Stress in concrete=%f N/mm^2\nStress in tension steel=%f N/mm^2\nStress in compression steel=%f N/mm^2",sigma_cbc,sigma_st,sigma_sc)
//answer in textbook is incorrect
|
e09fe96370d7da5a03c7f22874eb09b57278a62c | 449d555969bfd7befe906877abab098c6e63a0e8 | /3788/CH4/EX4.3.4/Ex4_3_4.sce | f40655044e5437d221cc92834d4edd8e33d16854 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 560 | sce | Ex4_3_4.sce | //Example 4.3.4
// Calculate the GT ratio and also if the Noise temperature is risen
//Variables
clc
clear
D = 30
na = 0.68
lam = 0.0723
temp0 = 79
temp1 = 88
//Calculation
Gr = na*((%pi*D)/lam)^2
GrdB = 10*log10(Gr)
Ts0 = 10*log10(temp0)
Ts1 = 10*log10(temp1)
GT = GrdB - Ts0
GTnew = GrdB - Ts1
//Result
printf("The Gain of antenna is %f dB \n",GrdB)
printf("System noise temperature is %f dBK \n",Ts1)
printf("Earth station GT ratio is %f dB/K \n",GT)
printf("If the temperature rises to 88K ,then new GT ratio is %f dB/K",GTnew)
|
b74f2fc74240c03f2d37e0859677cb741b22826f | 449d555969bfd7befe906877abab098c6e63a0e8 | /620/CH5/EX5.3/example5_3.sce | 994dd2739e6ccd42bd76ec58606dd456182d2a2e | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 312 | sce | example5_3.sce | disp("Part a");
v1=9;
v2=2*1.5;
i=75*10^(-3);
v=v1-v2;
r=v/i;
disp("the resistance value (in Ω) required is"); disp(r);
disp("Part b");
p=v*i*10^3;
disp("the power rating (in mW) of the transistor is"); disp(p);
disp("Part c");
p1=v2*i*10^3;
disp("the power used (in mW) by the radio is"); disp(p1); |
0629addef99527c33d3dd6d72be7276ecf3cdd42 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1748/CH2/EX2.46/Exa2_46.sce | 273af171c278bd6a193cf1098231416394128b65 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 575 | sce | Exa2_46.sce | //Exa 2.46
clc;
clear;
close;
//Given data :
format('v',5);
R2inner=0.4;//in ohm
X2inner=2;//in ohm
R2outer=2;//in ohm
X2outer=0.4;//in ohm
//At standstill :
S=1;//unitless
Ratio=(R2outer*S/(R2outer^2+S^2*X2outer^2))/(R2inner*S/(R2inner^2+S^2*X2inner^2));//unitless
disp(Ratio,"Ratio of torque produced by two cages at standstill : ");
//At Full load :
S=5;//in %
S=5/100;//fractional
Ratio=(R2outer*S/(R2outer^2+S^2*X2outer^2))/(R2inner*S/(R2inner^2+S^2*X2inner^2));//unitless
disp(Ratio,"Ratio of torque produced by two cages at full load(slip=5%) : "); |
a5fc0f545ce08ee37cb74c30935265ca82d0badd | 449d555969bfd7befe906877abab098c6e63a0e8 | /1163/CH10/EX10.1/example_10_1.sce | 2f0d868616e7f72770e1bf673c453eeea0f91559 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 384 | sce | example_10_1.sce | clear;
clc;
disp("--------------Example 10.1---------------")
k=4;
n=5;
datawords=2^k; // number of datawords
codewords=2^n; // number of codewords
printf("The 4B/5B block coding scheme has %d datawords and %d codewords.\n 16 out of 32 codewords are used for message transfer and the rest are either used for other purposes or unused.",datawords,codewords); // display result
|
409ce426b0722d81c9aa46eac3b3e1f338824fbb | 1b3c63cb7f854378c5f1991637692ae2bf8265ac | /stabsep/teststabsep.sce | f1fa00d98da160aa9b5fa5bed293c6dcec96c038 | [] | no_license | FOSSEE-Internship/FOSSEE-Control-Systems-Toolbox | 9900107267e5f508f77858d128e01293966e9e10 | 2878a38e4e55806b1777f9da2e0395f321e1c952 | refs/heads/master | 2020-12-02T18:20:34.659219 | 2017-10-26T12:26:57 | 2017-10-26T12:26:57 | 96,516,803 | 0 | 1 | null | 2017-10-26T13:44:56 | 2017-07-07T08:24:44 | Scilab | UTF-8 | Scilab | false | false | 246 | sce | teststabsep.sce | //test case
sys=ssrand(1,1,10);t=0.1;
sys=dscr(sys,t);
[ga,gs]=stabsep(sys);
[a,b,c,d]=abcd(sys);
savematfile('checkstabsep.mat','a','b','c','d','t');
scf();
bode(ga);
title("antistabel part");
scf();
bode(gs);
title("stable part");
|
9457f5d0be1c6a5fe681aa9615abb699b6008fd8 | c6bf685755436b2a7bf289ac90bec98340fe97fe | /PRINCIPIO_DA_INDUCAO_INFINITA.sce | 647806f9f0dac9c7847dd62984f25235108dff24 | [] | no_license | ivybin/PROGRAMAS-SCE | 82296ac10f4fb02d6e283f64e910666c6103063a | e61918ceae020bd33fcf223908f7decdec1c41b4 | refs/heads/master | 2023-07-23T12:55:08.711868 | 2021-09-02T17:22:23 | 2021-09-02T17:22:23 | 400,595,765 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 115 | sce | PRINCIPIO_DA_INDUCAO_INFINITA.sce | clear;
clc;
k=7;
P=0;
for i=1:1:k
P=P+(i^2);
M=(i/6)*(1+i)*((2*i)+1);
C=[P M];
disp(C);
end
|
72634a278987bd5957265836249655497e2f7a88 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1301/CH3/EX3.15/ex3_15.sce | 56cc6d8451699da5ef9f370aa9fea34f1c71a36b | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 275 | sce | ex3_15.sce | clc;
g=32; //gravitational constant in ft/sec square
m=50; //mass in slugs
w=m*g; //calculating weight in lb
disp(w,"Weight in lb = ");
w=50; //weight in lb
m=w/g //calculating mass in slugs.
disp(m,"Mass in slugs = "); //displaying result |
70b54b0724b6b241053c592d0dd8dec1ec985981 | 449d555969bfd7befe906877abab098c6e63a0e8 | /339/CH6/EX6.1/ex6_1.sce | cf22485dae30e0f01e4c96aab0feef0bac2bd4e1 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 802 | sce | ex6_1.sce | //define physical constants
q=1.60218e-19;
k=1.38066e-23;
// define material properties
Nc_300=[1.04e19 2.8e19 4.7e17];
Nv_300=[6e18 1.04e19 7e18];
mu_n= [3900 1500 8500];
mu_p= [1900 450 400];
Wg= [0.66 1.12 1.424];
T0=273;
T=-50:250; // temperature range in centigrade
sigma=zeros(3, length(T));
for s=1:3 //loop through all semi conductor materials
Nc=Nc_300(s)*((T+T0)/300).^(3/2);
Nv=Nv_300(s)*((T+T0)/300).^(3/2);
sigma(s,:)=[q*sqrt(Nc.*Nv).*(exp(-Wg(s)./(2*k*(T+T0)/q)))*(mu_n(s)+mu_p(s))];
end;
plot(T,sigma(1,:),'r');
mtlb_hold on
plot(T,sigma(2,:),'b')
plot(T,sigma(3,:),'g')
legend('Ge','Si','GaAs',2);
title('Conductivity of semiconductor at different temperatures');
xlabel('Temperature, {\circ}C');
ylabel('Conductivity \sigma, \Omega^{-1}cm^{-1}'); |
ab338688ffdc4afed24b3024bb6cf7f76f50bf59 | fe33c0b16926678447c084c04df084926a9ca29a | /tractrix.sce | f3ab991fe24853b311c59e48f2f5d0457ff65eae | [] | no_license | askmrsinh/SEM2_AM | bbcf34ce205abe763cb5c85df5f01544cdcdfca5 | da613da5c22f20ab1a814f28315e34b0c2c59a13 | refs/heads/master | 2021-09-28T03:09:19.415553 | 2016-08-18T15:14:23 | 2016-08-18T15:14:23 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 170 | sce | tractrix.sce | //x=a*cos(t)+(a/2)log(tan^2(t/2)), y=a*sin(t)
a=2;
t=0:%pi/64:%pi;
n=(tan(t/2))^2;
x=a*cos(t)+((a/2)*log(n));
y=a*sin(t);
plot(-x,y)
plot(x,y)
title('TRACTRIX')
|
262928826c62438c86af006b17364373be32a504 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2522/CH7/EX7.10/exm7_10.sce | 0820ba668b167cf6c28918ab26b2de1ebcc5df0a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 969 | sce | exm7_10.sce | //page no 235
// example no 7.10
// RIGHT ROTATION (RRC & RAR) OF BITS.
clc;
// initially
printf('Accumulator= 81H \n');
printf('D7 D6 D5 D4 D3 D2 D1 D0 \n');
printf(' 1 0 0 0 0 0 0 1 =81H \n \n');
printf('CY= 0 \n \n');
printf('RRC \n \n');
printf('CY= 1 \n \n');
// carry flag is set because D0 bit was 1.
printf('D7 D6 D5 D4 D3 D2 D1 D0 \n');
printf(' 1 1 0 0 0 0 0 0 =C0H \n \n'); // after the executuion of RRC.
// RRC instruction places D0 bit in CY flag as well as in D7 bit.
// initially
printf('Accumulator= 81H \n');
printf('D7 D6 D5 D4 D3 D2 D1 D0 \n');
printf(' 1 0 0 0 0 0 0 1 =81H \n \n');
printf('CY= 0 \n \n');
printf('RAR \n \n');
printf('CY= 1 \n \n');
// carry flag is set because D0 bit was 1.
printf('D7 D6 D5 D4 D3 D2 D1 D0 \n');
printf(' 0 1 0 0 0 0 0 0 =40H \n \n'); // after the executuion of RAR.
// RAR instruction places D0 bit in CY flag & CY flags bit is send to D7 bit.
|
61135221366cf06f6084b8387a27e825734c0044 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2273/CH6/EX6.4/ex6_4.sce | e4539013f240e7e97343cd4ce202df33e8f3e341 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,005 | sce | ex6_4.sce | //calculate constants of equivalent circuit of line
clear;
clc;
//soltion
//FUNCTIONS
function [z]=rxr(A,B)//Function for the multiplication of rectangular
z(1)=A(1)*B(1)
z(2)=A(2)+B(2)
endfunction
function [a]=r2p(z)//Function for rectangular to polar
a=z(1)*complex(cosd(z(2)),sind(z(2)))
endfunction
//given
P=100*10^6;//VA
Vrl=220*1000;//V
Zse_=complex(1,6);
Zseo=(Zse_*(Vrl^2))/(P*100);
Zse=[abs(Zseo) atand(imag(Zseo)/real(Zseo))];
A=[1 0.8];
B=[169.52 84.6];
C=[0.00135 90];
D=A;
CZ=rxr(C,Zse);
Ao_=r2p(A)+r2p(CZ);
Ao=[abs(Ao_) atand(imag(Ao_)/real(Ao_))];
printf("Ao = %.5f∠%.2f°\n",Ao(1),Ao(2));
DZ=rxr(D,Zse);
Bo_=r2p(B)+r2p(DZ);
Bo=[abs(Bo_) atand(imag(Bo_)/real(Bo_))];
printf("Bo = %.2f∠%.2f° ohm\n",Bo(1),Bo(2));
Co=C;
Do=A;
printf("Co = %.5f∠%d° siemens\n",Co(1),Co(2));
printf("Do = %d∠%.1f°",Do(1),Do(2));
//the value of Ao is different because book has a calculation mistake and according to book it is 0.9799∠11.49°
|
1e3958e92d56982dc3bf7cef11a71bddd6909e61 | 449d555969bfd7befe906877abab098c6e63a0e8 | /61/CH18/EX18.1/ex18_1.sce | 18752a615c7c5ab40e6962c99a743a941010f042 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 277 | sce | ex18_1.sce | //Ex18.1
C=1000*10^-12; //Switche capacitor value in farads
R=1000; //resistance in ohms
T=R*C; //Time period
f=1/T; //Frequency at which switch should operate
disp(f,'Frequency at which each switch should operate(in hertz)' )
disp('Duty cycle should be 50%') |
b3d88a6523fba2ddb1471fac3e1e6705863fa49f | 449d555969bfd7befe906877abab098c6e63a0e8 | /2048/DEPENDENCIES/oe.sci | 767bd39d04582947d306ba406c7860c5e6a8b756 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 3,190 | sci | oe.sci |
// OE Model parameter estimation
///////////////////////////////////////
/////////// ARX Model /////////////////
function [thetaN_arx,covt_arx,nvar,res] = arxc(data,na,nb,nk)
az = max(na,nb+nk-1);
zer = zeros(az,1);
zd = data;
// Zeros appended
zd1(:,1) = [zer; zd(:,1)];
zd1(:,2) = [zer; zd(:,2)];
[r,c] = size(zd1);
t = az+1:r;
yt = zd1(:,1); ut = zd1(:,2);
yt1 = yt'; ut1 = ut'; // row vector
len1 = length(yt1);
yt2 = zeros(1,len1-az); ut2 = zeros(1,len1-az);
// arx(Data,[na nb nk])
for i=1:na
yt2 = [yt2; -yt1(t-i)];
end;
for i=nk:nb+nk-1
ut2 = [ut2; ut1(t-i)];
end;
[r1,c1] = size(yt2); [r2,c2] = size(ut2);
phit = [yt2(2:r1,:); ut2(2:r2,:)];
m1 = phit*phit';
[qm,rm] = qr(m1);
m2 = phit*zd(:,1);
thetaN_arx = inv(rm)*qm'*m2;
// thetaN_arx = inv(m1)*m2;
// thetaN_arx = m1\m2;
[r11,c11] = size(thetaN_arx);
a = thetaN_arx(1:na); b = thetaN_arx(na+1:r11);
// Sum of squared residuals
yhat = phit'*thetaN_arx;
res = zd(:,1) - yhat;
N = length(res);
q = rank(phit);
ssr = res'*res;
sig2 = ssr/(N-q);
nvar = sqrt(sig2);
cov_arx = inv(m1);
covt_arx = diag(cov_arx);
endfunction;
///////////////////////////////
//////////////////////////////
///////////////////////////////////////
////////// Model Display /////////////
function disp_mod(N1,covN1)
len = length(covN1);
B1 = pol2str(N1);
ind = strindex(B1,['+','-']);
ind = ind - 1;
B2 = strsplit(B1,ind);
covB = string(covN1);
if ascii(B2(1)) == 32
B2 = B2(2:len+1);
end;
B3(1) = ' ';
for i=1:len
B3(i) = strsubst(B2(i),'*x','(+-' + covB(i) + ')*x');
end;
B4 = B3(1);
for i=2:len
B4 = B4 + ' ' + B3(i);
end;
disp(B4);
endfunction;
///////////////////////////////////////
///////////////////////////////////////
function [thetaN_oe,covN_oe,nvar,resid] = oe(zd,nb,nf,nk)
[thetaN,covfN,nvar,res] = arxc(zd,nf,nb,nk);
[r1,c1] = size(thetaN);
yt = zd(:,1);
m=50;
if nf==0
thetaN_oe = thetaN;
covN_oe = covfN;
else
for k=1:m
a = thetaN(1:nf);
b = thetaN(nf+1:r1);
A = [1 a']; // Filter
y = yt(1:length(u))';
yf = deconvol(y,A);
uf = deconvol(u,A);
zf = [yf(1:length(uf))' uf'];
zdf = detrend(zf,'constant');
[thetaNf,covf_a,nvar,resid] = arxc(zdf,nf,nb,nk)
thetaN = thetaNf;
a1 = thetaN(1:nf);
b = (norm(a-a1))/norm(a1);
if b<0.005
break;
end;
end;
thetaN_oe = thetaN;
covN_oe = covf_a;
end;
[rt,ct] = size(thetaN_oe);
f_oe = [1 thetaN_oe(1:nf)']; b1 = zeros(1,nk);
b_oe = [b1 thetaN_oe(nf+1:rt)'];
cov_f = covN_oe(1:nf); cov_b = covN_oe(nf+1:rt);
x = poly(0,'x');
if nf ==0
disp('Discrete time model: y(t) = B(x)u(t) + e(t)');
else
disp('Discrete time model: y(t) = [B(x)/F(x)]u(t) + e(t)');
end;
F = poly(f_oe,'x','coeff');
cov_f1 = [0 cov_f'];
B = poly( b_oe,'x','coeff');
cov_b1 = cov_b';
if nb==0
error('All B parameters are zero');
else
disp('B(x) = ');
disp_mod(B,cov_b);
end;
if nf~=0
disp('F(x) = ');
disp_mod(F,cov_f1);
end;
endfunction;
|
8cc617afab60fd2fcde582d8a4ce7339e75d1ac3 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2510/CH17/EX17.12/Ex17_12.sce | 5ef496cff73e33f11cdf5dd6e12eb974f61cf073 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,762 | sce | Ex17_12.sce | //Variable declaration:
w = 1 //Length of tube (m)
S = 10/10**3 //Fin patch (m)
//From example 17.10:
t = 1/10**3 //Thickness of fin (m)
ro = 0.0125 //Radius of tube (m)
Af = 3.94*10**-3 //Fin surface area (m^2)
Tb = 145 //Excess temperature at the base of the fin (K)
h = 130 //Heat transfer coefficient (W/m^2.K)
Qf = 64 //Fin heat transfer rate (W)
//Calculation:
Nf = w/S //Number of fins in tube length
wb = w-Nf*t //Unfinned base length (m)
Ab = 2*%pi*ro*wb //Unfinned base area (m^2)
At =Ab+Nf*Af //Total transfer surface area (m^2)
Qt = h*(2*%pi*ro*w*Tb) //Total heat rate without fins (W)
Qb = h*Ab*Tb //Heat flow rate from the exposed tube base (W)
Qft = Nf*Qf //Heat flow rate from all the fins (W)
Qt2 = Qb+Qft //Total heat flow rate (W)
Qm = h*At*Tb //Maximum heat transfer rate (W)
no = Qt2/Qm //Overall fin efficiency
Eo = Qt2/Qt //Overall effectiveness
Rb = 1/(h*Ab) //Thermal resistance of base (K/W)
Rf = 1/(h*Nf*Af*no) //Thermal resistance of fins (K/W)
//Result:
printf("1. The total surface area for heat transfer is : %.3f m^2 .",At)
printf("2. The exposed tube base total heat transfer rate is : %.1f W .",Qb)
printf("Or, the exposed tube base total heat transfer rate is : %.0f Btu/h .",Qb*3.412)
printf("3. The overall efficiency of the surface is : %.1f %%",no*100)
printf("4. The overall surface effectiveness is : %.2f .",Eo)
|
4ffe7231780524d58732508d5122b71906f921a5 | 449d555969bfd7befe906877abab098c6e63a0e8 | /191/CH5/EX5.15/Example5_15.sce | 1d91279ed1d8920ba525cf6c4c88bc3ee3d7b198 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 899 | sce | Example5_15.sce | //Least square aproximation method with exponential functions
clc;
clear;
close();
xi = [0 0.25 0.4 0.5];
yi = [9.532 7.983 4.826 5.503];
wi = ones(1,4);
//data corresponding to linearised problem
Xi = [0 0.25 0.4 0.5];
Yi = [2.255 2.077 1.574 1.705];
wi = ones(1,4);
format('v',6);
//Representation of equation in matrix form
W = [sum(wi) sum(wi.*xi); sum(wi.*xi) sum(wi.*xi.*xi)];
Y = [sum(wi.*Yi); sum(wi.*Yi.*Xi)];
C = inv(W)*Y;
A = C(1);
B = C(2);
a = exp(2.281);
b = B;
disp(a, 'a = ');
disp(b, 'b = ');
//So the non linear system becomes
disp('9.532-a+7.983*exp(0.25*b)-a*exp(0.5*b)+4.826*exp(0.4*b)-a*exp(0.8*b)+5.503*exp(0.5*b)-a*exp(b) = 0');
disp('1.996*a*exp(0.25*b)-0.25*a*a*exp(0.5*b)+1.930*a*exp(0.4*b)-0.4*a*a*exp(0.8*b)+2.752*a*exp(0.5*b)-0.5*a*a*exp(b) = 0');
//Applying Newtons Method we get
a = 9.731;
b = -1.265;
disp(a , 'a = ');
disp(b , ' b = '); |
c67c06c0658266d102e6275b5878684e6a6a7990 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1892/CH3/EX3.1/Example3_1.sce | 911ba76a7b33685a2b05ff838637431c0f3fc677 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 351 | sce | Example3_1.sce | // Example 3.1
clear; clc; close;
format('v',8);
// Given data
Lm=30;//in mH
Iph=3;//in Ampere
Rm=15;//in Ohm
//Calculations
tau_ed=Lm/Rm;//in ms
tdash=1/2*tau_ed;//in ms
disp(tdash,"(i) Time taken by the phase current to decay to zero in ms : ");
Energy=1/4*Lm*Iph^2;//in mW
disp(Energy,"(ii) Energy returned to supply in mW : ");
|
de340ed386cbe0812124e153fb2b1a4863e4717a | 23573b967e8324d44226379d70559b8f0ea34905 | /code/Symphonymat/Assignment_Problem.sce | 419d9ee9fda8f28a53128f66bba37ca193c16d41 | [] | no_license | FOSSEE/FOT_Examples | 91c8b8e9dc58545604b2c2af41a7e22f702b78f3 | 75947a7aa5a3955fe5a72e09f55bbdc05e3b8751 | refs/heads/master | 2020-03-22T09:00:48.306061 | 2018-07-24T04:49:25 | 2018-07-24T04:49:25 | 139,807,736 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 3,226 | sce | Assignment_Problem.sce | //Reference :H.A. Eiselt and C.-L.SAndblom,"Linear Programming and its Applications",Springer-Verlag Berlin Heidelberg 2007,chapter 2.9
//The public works department of a region has issued contracts for five new projects. Each of the three contractors who have shown interest in the projects has submitted bids for those projects. The bids given by contactors are as given below
// =====================================================================
// Project1 Project2 Project3 Project4 Project5
// ---------------------------------------------------------------------
// Contractor1 20 - 10 9 15
// Contractor2 18 12 13 8 16
// Contractor3 - 11 12 7 17
// =====================================================================
//The resource requirement of the contractors for each projects and the total resources available with them are as given
// =============================================================================
// Project1 Project2 Project3 Project4 Project5 Available Resources
// -----------------------------------------------------------------------------
// Contractor1 70 - 40 30 50 120
// Contractor2 65 45 40 35 55 100
// Contractor3 - 45 35 40 50 70
// ============================================================================
//The objective of the contractors is to minimize the total cost
clc;
nProjects = 5;
nContractors = 3;
bids = [20 10000 10 9 15;18 12 13 8 16; 10000 11 12 7 17];
reqResource = [70 10000 40 30 50;65 40 40 35 55; 10000 45 35 40 50];
availResource = [120; 100; 70];
nVar = nProjects*nContractors; // Calculated the dimension of the problem
IntCon = 1:nVar; // Indicating the integer variables
lb = zeros(1,nVar);
ub = ones(1,nVar);
// Linear constraints
// Linear equality constraints
beq = ones(nProjects,1);
for i = 1:nProjects
Aeq(i,i:nProjects:nVar) = 1;
end
// Linear inequality constraints
b = availResource;
for j = 1:nContractors
index = (j-1)*nProjects+1:j*nProjects;
A(j,index) = reqResource(j,:);
end
// Objective function
for j = 1:nContractors
index = (j-1)*nProjects+1:j*nProjects;
Cost(index,1) = bids(j,:)';
end
options = list("time_limit", 2500);
[xopt,fopt,status,output] = symphonymat(Cost,IntCon,A,b,Aeq,beq,lb,ub,options);
// Result representation
select status
case 227
disp(" Optimal Solution Found")
case 228
disp("Maximum CPU Time exceeded")
case 229
disp("Maximum Number of Node Limit Exceeded")
case 230
disp("Maximum Number of Iterations Limit Exceeded.")
end
for j = 1:nContractors
index = (j-1)*nProjects+1:j*nProjects;
Contractor(j).Project = string(find(xopt(index)==1));
end
ResolurceUtilized = ((A*xopt)./b)*100;
for j = 1:nContractors
disp(strcat(["Projects assigned to contractor",string(j)," : ", Contractor(j).Project],' '));
disp(strcat(["Resource utilized by contractor ",string(j)," : ",string(ResolurceUtilized(j)),"%"]));
end
disp(strcat(["Total cost : ",string(fopt)]))
|
762412a6d36090ef8330a7b6dcc0101557aab828 | d85de2a62f5fbfb9e691d794ec0ca36c9ee5fcb4 | /scenes/spheres/spheres.sce | 4a70eef3c0a16e4f8562f3d09663cab56f24ea32 | [
"MIT"
] | permissive | Drezil/htrace | 117b7deed9f5a24cb822ce1fa042a85a8845bc0f | cdc0cb1ffa3a0f31092c0c9e4e1b123c62979793 | refs/heads/master | 2016-09-08T01:41:28.629578 | 2015-02-05T13:05:09 | 2015-02-05T13:05:09 | 25,707,425 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 687 | sce | spheres.sce | # camera: eye, center, up, fovy, width, height
camera 1 3 8 1 1 0 0 1 0 45 500 500
# recursion depth
depth 5
# background color
background 0 0 0
# global ambient light
ambience 0.2 0.2 0.2
# light: position and color
light 0 50 0 0.3 0.3 0.3
light 50 50 50 0.3 0.3 0.3
light -50 50 50 0.3 0.3 0.3
# spheres: center, radius, material
sphere 0.0 1.0 0.0 1.0 1.0 0.0 0.0 1.0 0.0 0.0 1.0 1.0 1.0 100.0 0.2
sphere -1.0 0.5 2.0 0.5 0.0 1.0 0.0 0.0 1.0 0.0 1.0 1.0 1.0 200.0 0.2
sphere 3.0 2.0 1.5 2.0 0.0 0.0 1.0 0.0 0.0 1.0 1.0 1.0 1.0 50.0 0.2
# planes: center, normal, material
plane 0 0 0 0 1 0 0.2 0.2 0.2 0.2 0.2 0.2 0.0 0.0 0.0 100.0 0.1
|
2c6a6e996f75ccfa732c80844beadbdaeb172127 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1538/CH18/EX18.5/Ex18_5.sce | 921407a589950915669dfd53f00ce53a4e15e55a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 599 | sce | Ex18_5.sce | //example-18.5
//page no-548
//given
//resistance of wire at 70 degree celcius is 57.2 ohm and at 25 degrees celcius 50 ohm
R25=50 //ohm
R70=57.2 //ohm
T1=25 //degree C
T2=70 //degree C\
//as we know that
//Rt=R0*(1+t*alpha)
//putting above values in the above given equation we get
//R25=R0*(1+25*alpha) -------(1)
//R70=R0*(1+70*alpha) --------(2)
//applying R70/R25
//we get
//R70/R25=(1+70*alpha)/(1+25*alpha)
//solving for alpha we get equation as follows
alpha=(R70-R25)/(T2*R25-T1*R70) //K^-1
printf ("the temperature coefficient of resistance is %f K^-1",alpha)
|
3c06dcafecfa18a3d465ac0ba141014833a7c860 | 7c8f8373b8f5e06d3ebe218c8485afadb95cf70f | /scilab/Fibonacci.sce | 61e5efbd8a4ccc713bad3e05bb09b903d091e3b0 | [] | no_license | invalidCorgi/polibuda | 432b41e3ebbd169812017f0fd462b59f428b9516 | 4a4cd16efee42e010140bd991fbd5cf034955507 | refs/heads/master | 2021-09-24T11:50:05.097437 | 2018-10-09T11:12:10 | 2018-10-09T11:12:10 | 119,171,250 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 129 | sce | Fibonacci.sce | F=[1 1]
i=0.5
j=3
while(modulo(i,1)<>0)
i=input("Podaj n:")
end
while(j<=i)
F(1,j)=F(1,j-1)+F(1,j-2)
j=j+1
end
|
30e5558ec99d760cfd5f9b9c5fb5d05cfce98833 | 178822612bcd418dc12ba7a649304a24ab618d60 | /Numerical Analysis/El Hadji NGOM projet Scilab(Amélioré)/Projet 2 Systhèmes non linéaires/Secante.sci | b431879af8fa221d629e8bd3fedec83e18fe2cd1 | [] | no_license | engom/Math_Problem_Solving | b56c6cbfbff6c416c519795b9ab8f0c0bbba5ea3 | 6538c476681ae4ee803ea9b3a8944c5f370e1961 | refs/heads/master | 2022-05-25T01:13:16.123161 | 2016-02-13T11:32:28 | 2016-02-13T11:32:28 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 385 | sci | Secante.sci | // fonction test du code (exepmle d'évaluation) et paramétres
function y=f(x)
y=x^2-2;
endfunction
eps=10^-8
K=1000
k=0
x0 = 0.5
x1 = 1
a=0
b=3
// Methode des Secantes
function[z,k]=Secante(f,a,b,x0,x1,eps,K)
x=x0
y=x1
while (abs(f(x))>eps & k<K)
x= x - f(x)*((x-y)/(f(x)-f(y)))
k=k+1
end
z=x
endfunction
|
7dc5ba6cf5bec3754d0e96e9d395de6898e8d0f1 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2096/CH1/EX1.72/ex_1_72.sce | a943769948786fb27ce074063d58bea3fa9d955a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 395 | sce | ex_1_72.sce |
//Example 1.72// percentage error
clc;
clear;
I=5;//current in ampere
V=230;//volts
pf=1;//power factor
n=60;//no. of revolutions
t=360;//total time in seconds
nr=520;//normal disc no. of revolutions per kWh
E=((V*I*pf*360)/(3600*1000));//energy consumed in 360 seconds in kWh
Er= n/nr;//energy recorded by the meter
Per=((Er-E)/E)*100;//percentage error
disp(Per,"percentage error is (fast)")
|
9a26bf1f6718b2766fb0e993d90f2e1760fd614b | 449d555969bfd7befe906877abab098c6e63a0e8 | /2621/CH3/EX3.4/Ex3_4.sce | ef10a78ec9eb3041687684f695f38254914360dd | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 571 | sce | Ex3_4.sce | // Example 3.4
clc;
clear;
close;
// Given data
format('v',9);
Rin= 2*10^6;// in Ω
Rout= 75;// in Ω
f0= 5;// in Hz
A= 2*10^5;//unit less
B=1;// for voltage follower
Rf= 0;
Af= 1;// voltage gain (since Rf=0)
Rin_f= A*Rin;// input resistance in Ω
Rin_f= Rin_f*10^-9;// in GΩ
Rout_f= Rout/A;//output resistance in Ω
f_f= f0*A;// bandwidth in Hz
f_f= f_f*10^-6;// in MHz
disp(Af,"The voltage gain is : ");
disp(Rin_f,"The input resistance in GΩ is : ");
disp(Rout_f,"The output resistance in Ω is : ")
disp(f_f,"The bandwidth in MHz is : ");
|
fe1b82c0250932817d95914f69f4f97404bb9f94 | 449d555969bfd7befe906877abab098c6e63a0e8 | /260/CH5/EX5.15/5_15.sce | 17458f6f2ab7218be9343cc98f05a0a4bbac01e5 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 69 | sce | 5_15.sce | //Eg-5.15
//pg-253
clear
clc
printf('Theoretical Question\n') |
5b40a660d070a5a152b07ca491822474ad9cb401 | e41b69b268c20a65548c08829feabfdd3a404a12 | /3DCosmos/Data/Scripts/Astronomy/Mars/_SUB/_SUB_general.SCI | 54e94cfeb2709953c711b20979835752a2209b50 | [
"LicenseRef-scancode-khronos",
"MIT"
] | permissive | pvaut/Z-Flux | 870e254bf340047ed2a52d888bc6f5e09357a8a0 | 096d53d45237fb22f58304b82b1a90659ae7f6af | refs/heads/master | 2023-06-28T08:24:56.526409 | 2023-03-01T12:44:08 | 2023-03-01T12:44:08 | 7,296,248 | 1 | 1 | null | 2023-06-13T13:04:58 | 2012-12-23T15:40:26 | C | WINDOWS-1252 | Scilab | false | false | 2,829 | sci | _SUB_general.SCI |
function makepartialcircle(obj,vc1,vc2)
{
vc2=vc2-0.007*vecnorm(vc2-vc1);
ang=vecangle(vc1,vc2);
resol=ang*20+2;
for i=0 to resol-1 do {
obj.addpoint(@point(vecrotate(vc1,vecnorm(vc1*vc2),ang*i/resol)));
}
obj.addpoint(@point(vc2));
}
function G_MarsRadius()
{
return(3396.2);
}
function SUB_init()
{
#create "loading data" frame
loadingframe=T_getscene.Universe.addscreenframe("Loading");
loadingframe.add("Text3D",
"UnitX":vector(0.1,0,0),"UnitY":vector(0,0.1,0),"Position":point(0.3,0.4,0),
"Content":'Loading data',"Color":color(1,0,0),"EnableLight":false,"DepthTest":DepthTestDisable);
loadingframe.visible=false;
}
Monthnames=list('Januari','Februari','March','April','May','June','July','August','September','October','November','December');
function datestring(tm)
{
rs=str(tm.day);if rs.length<2 then rs="0"+rs;
rs=rs+" "+monthnames(tm.month-1)+" "+str(tm.year);
return(rs);
}
function longit2string(longit)
{
longit=longit/Pi*180;
while (longit<-180) do longit=longit+360;
while (longit> 180) do longit=longit-360;
if longit>=0 then return(str(round(longit,1))+"° "+'East');
else return(str(round(-1*longit,1))+"° "+'West');
}
function lattit2string(lattit)
{
lattit=lattit/Pi*180;
if lattit>=0 then return(str(round(lattit,1))+"° "+'North');
else return(str(round(-1*lattit,1))+"° "+'South');
}
function SUB_showloading(status)
{
T_getscene.Universe.Loading.visible=status;
render;
}
function SUB_createleftpanel()
{
#create offset to make space for left panel
#T_getviewport.xoffsetfrac=-0.07;
PanelLeft=root.SC.Universe.addscreenframe("PanelLeft");
return(PanelLeft);
}
function SUB_G_leftpanel()
{
return(root.SC.Universe.PanelLeft);
}
function SUB_G_leftpaneloffsett()
{
return(0.01);
}
function SUB_G_sidepanelcolor()
{
return(color(0.65,0.65,0.65));
}
createvar(linespanelframe);
createvar(linespanelypos);
function PanelLines_init(ipanelframe,ipanelypos)
{
linespanelframe=ipanelframe;
linespanelypos=ipanelypos;
}
function PanelLines_add(content)
{
retobj=linespanelframe.add("Text3D","Content":content,"EnableLight":false,"UnitX":vector(0.02,0,0),"UnitY":vector(0,0.02,0),
"Position":point(SUB_G_leftpaneloffsett+0.01,linespanelypos,0),"Color":SUB_G_sidepanelcolor);
linespanelypos=linespanelypos-0.028;
return(retobj);
}
function PanelLines_skip()
{
linespanelypos=linespanelypos-0.028;
}
function SUB_testcmd()
{
kbst=UIGetKeyPressed;
if (kbst.Length==1) then {
if (kbst>="a") and (kbst<="g") then {
Store("Cmd",kbst);
render;
stop;
}
if kbst=="0" then SetMonitorStatus(false);
if kbst=="1" then SetMonitorStatus(true);
if kbst=="9" then ShutdownComputer;
}
} |
a3a231e0ede9cc35649eeb71906f5bf83452bebb | 449d555969bfd7befe906877abab098c6e63a0e8 | /1016/CH9/EX9.1/ex9_1.sce | 4f939d011f6b336e657651726acc24b2d8fa1685 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 155 | sce | ex9_1.sce | clc;clear;
//Example 9.1
//given data
V=20000;//applied voltage in V
//calculation
W=12.25/(sqrt(V));
disp(W,'de broglie wavelength in angstrom') |
bcaedb243fdca3f93d6934fa3104b9a50d97d942 | 333d6160f9a6d9e23a6bea06cd03e5e8fa8785a9 | /RobotLab1/SciLab/RunScripts.sce | 9b37131c1101109d82535e1f2cc5b8c27355f8d8 | [
"MIT"
] | permissive | DmitryIo/ROBOTS | 6f6bb12a8e08dd28024136ee1a8a84ea7254da60 | 777f0884a098c4f21d044985c25a8be276334116 | refs/heads/master | 2023-04-30T12:52:54.082977 | 2021-05-17T19:55:34 | 2021-05-17T19:55:34 | 294,091,170 | 3 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 212 | sce | RunScripts.sce | pathname = get_absolute_file_path("RunScripts.sce");
exec(pathname + 'LoadData.sce', -1);
exec(pathname + 'MakeModel.sce', -1);
//xcos(pathname + 'Simulation.zcos');
//exec(pathname + 'DrawSimulation.sce', -1);
|
b43ea5b2402e2ba4ce8d2cf33b4cc8f0ee243af3 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3554/CH3/EX3.2/Ex3_2.sce | aef9fea925512800f1a73b18b9c57a393f165f51 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,123 | sce | Ex3_2.sce | // Exa 3.2
clc;
clear all;
// Given data
//Refer fig. 3.4
Rm=100;//Ohms
Im=50; ///micro Amp
// Solution
//For 0-1mA range
// Ish*Rsh=Im*Rm;
disp("The four linear equations are as follows:");
printf(' R1+R2+R3+R4 = %.2f \n ',50*100/950); //say-equaion (3.1)
//For 0-10 mA range
printf('R1+R2+R3-(50/9950)*R4= % .3f \n ',100*50/9950); //say-equation(3.2)
//For 0-50 mA range
printf('R1+R2-(50/49950)*R3-(50/49950)*R4 = %.3f \n ',100*50/49950); //say-equation(3.3)
//For 0-100mA range
printf('R1-(50/99950)*R2-(50/99950)*R3-(50/99950)*R4 = %.3f \n ',50*100/99950);//say-equation(3.4)
//converting it into matrix form
A=[1 1 1 1;1 1 1 -(50/9950);1 1 -(50/49950) -(50/49950);1 (-50/99950) (-50/99950) (-50/99950)];
B=[-50*100/950 ; -100*50/9950 ; -100*50/49950 ; -50*100/99950];
[R,y]=linsolve(A,B);A*R+B;//linear equaion solving function
disp("The value of R1,R2 R4 and R4 are given as follows-");
printf(' R1 = %.5f Ohms \n R2= %.5f Ohms \n R3= %.5f Ohms \n R4= %.5f Ohms \n ',R(1),R(2),R(3),R(4));
// The value of R3 vary due to round off errors
|
2968957bd913a4d395e9a618c03aba70d5ffa15e | fcd4bce0080771389b4a69338ed6443153942183 | /cores/n64/mupen64plus-rsp-paraLLEl/lightning/check/ldstr-c.tst | 6ddc86e1558e1d7aca82aa45c30ef3b1c70daa85 | [
"MIT",
"LGPL-2.1-only",
"MPL-1.1",
"LicenseRef-scancode-mame",
"GPL-1.0-or-later",
"Zlib",
"GPL-2.0-only",
"LGPL-2.1-or-later",
"MPL-2.0",
"CC-PDDC",
"LicenseRef-scancode-public-domain",
"LicenseRef-scancode-proprietary-license",
"LicenseRef-scancode-brian-gladman-3-clause",
"BSD-3-Clause"... | permissive | wulfebw/retro | d4fcf9229b257b3c495f54b1aeb3ea36004ae4aa | dad4b509e99e729e39a2f27e9ee4120e3b607f58 | refs/heads/master | 2022-10-23T07:17:55.320585 | 2020-06-12T01:38:06 | 2020-06-12T01:38:06 | 260,832,205 | 8 | 1 | MIT | 2020-06-12T01:38:08 | 2020-05-03T05:06:17 | C | UTF-8 | Scilab | false | false | 3,064 | tst | ldstr-c.tst | #include "ldst.inc"
#if __WORDSIZE == 64
# define LDSTL(N, R0, R1) \
movi %R0 $(t0 + $offui) \
str_i %R0 %R1 \
movi %R0 $(t0 + $offl) \
movi %R1 L##N \
str_l %R0 %R1
# define SI(C, N, x, X, R0) \
movi %R0 $(t0 + $off##x) \
ldr_##x %R0 %R0 \
beqi L##x##C %R0 L##X##N \
calli @abort \
L##x##C:
# define LDRL(C, N, R0, R1) \
UI(C, N, i, I, R0) \
SI(C, N, l, L, R0)
#else
# define LDSTL(C, R0, R1)
# define SI(C, N, x, X, R0) \
movi %R0 $(t0 + $off##x) \
ldr_##x %R0 %R0 \
beqi L##x##C %R0 I##X##N \
calli @abort \
L##x##C:
# define LDRL(C, N, R0, R1)
#endif
#define UI(C, N, x, X, R0) \
movi %R0 $(t0 + $offu##x) \
ldr_u##x %R0 %R0 \
beqi Lu##x##C %R0 X##N \
calli @abort \
Lu##x##C:
#define LDST1(X, N, R0, R1) \
movi %R0 $(t0 + $offc) \
movi %R1 C##N \
str_c %R0 %R1 \
movi %R0 $(t0 + $offuc) \
str_c %R0 %R1 \
movi %R0 $(t0 + $offs) \
movi %R1 S##N \
str_s %R0 %R1 \
movi %R0 $(t0 + $offus) \
str_s %R0 %R1 \
movi %R0 $(t0 + $offi) \
movi %R1 I##N \
str_i %R0 %R1 \
LDSTL(N, R0, R1) \
movi %R0 $(t0 + $offf) \
SI(X, N, c, C, R0) \
UI(X, N, c, C, R0) \
SI(X, N, s, S, R0) \
UI(X, N, s, S, R0) \
SI(X, N, i, I, R0) \
LDRL(X, N, R0, R1) \
#define LDST0(R0, R1) \
LDST1(0_##R0##_##R1, 0, R0, R1) \
LDST1(1_##R0##_##R1, 1, R0, R1) \
LDST1(2_##R0##_##R1, 2, R0, R1) \
LDST1(3_##R0##_##R1, 3, R0, R1)
#define LDST(V0, V1, V2, R0, R1, R2) \
LDST0(V0, V1) \
LDST0(V0, V2) \
LDST0(V0, R0) \
LDST0(V0, R1) \
LDST0(V0, R2) \
LDST0(V1, V0) \
LDST0(V1, V2) \
LDST0(V1, R0) \
LDST0(V1, R1) \
LDST0(V1, R2) \
LDST0(V2, R0) \
LDST0(V2, R1) \
LDST0(V2, R2)
.code
prolog
/* Simple test to simplify validating encodings before
* brute force tests */
movi %r0 $(t0 + $offc)
movi %r1 0x81
str_c %r0 %r1
movi %r0 $(t0 + $offuc)
str_c %r0 %r1
movi %r0 $(t0 + $offs)
movi %r1 0x8001
str_s %r0 %r1
movi %r0 $(t0 + $offus)
str_s %r0 %r1
movi %r0 $(t0 + $offi)
movi %r1 0x80000001
str_i %r0 %r1
#if __WORDSIZE == 64
movi %r0 $(t0 + $offui)
str_i %r0 %r1
movi %r0 $(t0 + $offl)
movi %r1 0x8000000000000001
str_l %r0 %r1
#endif
movi %r0 $(t0 + $offc)
ldr_c %r0 %r0
beqi Lc %r0 XC
calli @abort
Lc:
movi %r0 $(t0 + $offuc)
ldr_uc %r0 %r0
beqi Luc %r0 0x81
calli @abort
Luc:
movi %r0 $(t0 + $offs)
ldr_s %r0 %r0
beqi Ls %r0 XS
calli @abort
Ls:
movi %r0 $(t0 + $offus)
ldr_us %r0 %r0
beqi Lus %r0 0x8001
calli @abort
Lus:
movi %r0 $(t0 + $offi)
ldr_i %r0 %r0
beqi Li %r0 XI
calli @abort
Li:
#if __WORDSIZE == 64
movi %r0 $(t0 + $offui)
ldr_ui %r0 %r0
beqi Lui %r0 0x80000001
calli @abort
Lui:
movi %r0 $(t0 + $offl)
ldr_l %r0 %r0
beqi Ll %r0 0x8000000000000001
calli @abort
Ll:
#endif
LDST(v0, v1, v2, r0, r1, r2)
// just to know did not abort
prepare
pushargi ok
ellipsis
finishi @printf
ret
epilog
|
e0e780634fc0f43642c92e10744a06470c40bc9c | 449d555969bfd7befe906877abab098c6e63a0e8 | /1826/CH8/EX8.12/ex8_12.sce | 5ebf8d3b69e8ba776694d5cfefb02292466c6396 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 74 | sce | ex8_12.sce | // Example 8.12, page no-216
clear
clc
printf("Theorotical Exam[ple")
|
a375ab607bbf0eb4ac9926e8c75d89e8fde4d4e3 | 1bb72df9a084fe4f8c0ec39f778282eb52750801 | /test/RT10.prev.tst | b63a4188a314fa10120bcb9fe0dc8b8a410138cb | [
"Apache-2.0",
"LicenseRef-scancode-unknown-license-reference"
] | permissive | gfis/ramath | 498adfc7a6d353d4775b33020fdf992628e3fbff | b09b48639ddd4709ffb1c729e33f6a4b9ef676b5 | refs/heads/master | 2023-08-17T00:10:37.092379 | 2023-08-04T07:48:00 | 2023-08-04T07:48:00 | 30,116,803 | 2 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 157 | tst | RT10.prev.tst | [2,[3,4]] * [1,[0,1],[0,0,1]] =
rsize1=2, rsize2=3, rsizer=4
[[2],[3,6],[0,3,6],[0,0,3,4]]
3*x + 6*x*y + 3*x^2*y + 6*x^2*y^2 + 3*x^3*y^2 + 4*x^3*y^3 + 2
|
8aa7bab3667fa85d43a227c71e4e2686a1b20cc3 | 0812f3bb6f3cc038b570df68ccee4275da04b11f | /models/complexity_1000/Applied_Thermodynamics_and_Engineering/CH7/EX7.17/7_17.sce | e22098dec95b80f6bd6b948412f9c96a4308cda1 | [] | no_license | apelttom/20-semester_PhD_thesis | edc0b55580bae9d364599932cd73cf32509f4b7a | ff28b115fcf5e121525e08021fa0c02b54a8e143 | refs/heads/master | 2018-12-26T22:03:38.510422 | 2018-12-14T20:04:11 | 2018-12-14T20:04:11 | 106,552,276 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 78 | sce | 7_17.sce | clc;
hR=-281102;
hP=2*-393520+3*-241830;
h=-hR+hP
disp(h,"molar enthalpY is")
|
dc226c37afef69ede533636c7b1325f46e6f73cd | 449d555969bfd7befe906877abab098c6e63a0e8 | /3204/CH17/EX17.8/Ex17_8.sce | cac6cc4fd164dc06d32d52a9f7bfdf1e4894af30 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 546 | sce | Ex17_8.sce | // Initilization of variables
m=2 // kg // mass of the particle
v_0=20 // m/s // speed of rotation of the mass attached to the string
r_0=1 // m // radius of the circle along which the particle is rotated
r_1=r_0/2 // m
// Calculations
// here, equating (H_0)_1=(H_0)_2 i.e (m*v_0)*r_0=(m*v_1)*r_1 (here, r_1=r_0/2). On solving we get v_1 as,
v_1=2*v_0 // m/s
// Tension is given by eq'n,
T=(m*v_1^2)/r_1 // N
// Results
clc
printf('The new speed of the particle is %f m/s \n',v_1)
printf('The tension in the string is %f N \n',T)
|
018399b672442e8bd2f5ab4d0047225a95c27258 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1271/CH16/EX16.10/example16_10.sce | 3713daccac96e170d8bc715ca927edbab4c0a741 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 486 | sce | example16_10.sce | clc
// Given that
l = 1e-10 //length of box in m
e = 1.6e-19 // charge on an electron in C
m = 9.1e-31 // mass of electron in kg
h = 6.62e-34 // Planck constant in J-sec
// Sample Problem 10 on page no. 16.18
printf("\n # PROBLEM 10 # \n")
printf("Standard formula used \n")
printf("E = (n^2 * h^2) / (8 * m * l^2) \n")
n = 1 // for n=1
E = (n^2 * h^2) / (8 * m * l^2)
n = 2 // for n=2
E_ = (n^2 * h^2) / (8 * m * l^2)
d = (E_ - E) * (1 / e)
printf("\n Energy difference is %f eV.",d)
|
76da682313da0360cf80279139578db813a7efa3 | bd2dd6dcbf234dcda02553cfe9990ff2cc91f09a | /boringstep.sce | 84bee0385c690e5b006e9bf81b281f53724ce101 | [] | no_license | jdelacruz26/matlabcode | 13165d9aa0c40cd120c7903e2bdd3a2e02208898 | f4264a28bb92a7c6908c84f9fc948b34312dd70f | HEAD | 2016-09-06T08:10:45.762319 | 2015-05-31T05:57:14 | 2015-05-31T05:57:14 | 20,492,021 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 880 | sce | boringstep.sce | // Response to Unit Step Input R(s)=1/s for K=50, 100
//
K1 = 100; K2 = 50;
numg = poly([1],'s','c');
deng = poly([0 12 1],'s','c');
num1 = K1*numg; num2 = K2*numg;
// Transfer function
G1 = syslin('c',numg,deng);
G2 = syslin('c',num1,numg);
G3 = syslin('c',num2,numg);
G4 = syslin('c',numg,numg)
G5 = G1*G2;
G6 = G1*G3;
G01 = G5/.G4;
G02 = G6/.G4
t = 0:0.001:2;
step_resp1 = csim('step',t,G01) //
step_resp2 = csim('step',t,G02)//
setting=step_resp1(length(t));
disp(setting)
scf(2)
subplot(2,1,1)
plot(t,step_resp1)
a=gca();
a.children.children(1).thickness=3;
xgrid();
title('Step response for K100','fontsize',4);
xlabel('time[sec]','fontsize',2);
ylabel('c(t)','fontsize',2);
subplot(2,1,2)
plot(t,step_resp2)
a=gca();
a.children.children(1).thickness=3;
xgrid();
title('Step response for K50','fontsize',4);
xlabel('time[sec]','fontsize',2);
ylabel('c(t)','fontsize',2);
|
06c3f61c865a1bf2919f1b2d13487f73c7089050 | 449d555969bfd7befe906877abab098c6e63a0e8 | /371/CH11/EX11.6/11_6.sci | 62b8d9f6328ee1aa704a8e3f1c518e5ea390fb7a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 292 | sci | 11_6.sci | //Control of DC motors//
//Example 11.6//
printf('Reactive power at rated speed and rated load=72.79KVAR');
printf('\nReactive power at rated speed and 10 percent load=0.1*72.79=7.279KVAR');
printf('\nSimilarly reactive power at 10percent speed and 10 percent load=0.1*127.08=12.71KVAR'); |
4166f89b6c37908e0c4cc87f4ff150101a9f969e | 449d555969bfd7befe906877abab098c6e63a0e8 | /608/CH22/EX22.13/22_13.sce | 0020438dc67ce294a4e1534d0e57ab1824e403d8 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 573 | sce | 22_13.sce | //Problem 22.13: For the induction motor of Problems 22.10 to 22.12, determine the resistance of the rotor winding required for maximum starting torque.
//initializing the variables:
V = 415; // in Volts
f = 50 ; // in Hz
nr = 24; // in rev/sec
p = 4/2; // no. of pole pairs
R2 = 0.35; // in Ohms
X2 = 3.5; // in Ohms
//calculation:
//At the moment of starting, slip,
s = 1
//Maximum torque occurs when rotor reactance equals rotor resistance
//for maximum torque
R2 = s*X2
printf("\n\n Result \n\n")
printf("\nresistance of the rotor is %.1f Ohm",R2) |
09739f73fb6dc27b8d3314cd5ce86ad3539b4beb | 1573c4954e822b3538692bce853eb35e55f1bb3b | /DSP Functions/allpasslp2bsc/test_7.sce | 5e97411a73f0fe0fa4961aaa224a202fadb0a9a9 | [] | no_license | shreniknambiar/FOSSEE-DSP-Toolbox | 1f498499c1bb18b626b77ff037905e51eee9b601 | aec8e1cea8d49e75686743bb5b7d814d3ca38801 | refs/heads/master | 2020-12-10T03:28:37.484363 | 2017-06-27T17:47:15 | 2017-06-27T17:47:15 | 95,582,974 | 1 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 246 | sce | test_7.sce | // Test #7 : For 1 output argument
exec('./allpasslp2bsc.sci',-1);
[n]=allpasslp2bsc(0.22,[0.45,0.93]);
disp(n);
//
//Scilab Output
//n=0.7504814 0.5620834 - 0.8270806i
//
//Matlab Output
//n=0.7505 + 0.0000i 0.5621 - 0.8271i
|
d35c89d0aecfe8db764e2d467a5988cd311490a9 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2951/CH5/EX5.3.A/additional_ex_3.sce | 88f008dff4aaa49e5cbf0aa708af89846365d756 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 710 | sce | additional_ex_3.sce | clc;
clear;
fm=5;// maximum analog frequency in kHz
Min_dyna_range=35;
Vr=3; //Voltage in the receiver in V
//a)
F_sampling=2*fm;
//b)
n=Min_dyna_range/6;
k=(Vr-(-Vr)+1);// inclusive of sign bit
//c)
Resolution=Vr/(2^(7));
//d)
Max_quant_Error=Resolution/2
disp(F_sampling,"a)Minimum Sampling Rate(in kHz) =");
disp(n,"b) Minimum dynamic Range is");
disp(" But Closest whole number is 6. Henc,6 bits must be used for amplitude" );
disp("But the amplitude range is from -3 to +3 V,hence a sign bit also ");
disp( k,"becomes necessary..Therefore,the total number of bits");
disp(Resolution,"c) Resolution(in V) =");
disp(Max_quant_Error," d)MAximum Quantization Error (in V) ");
|
33f26e0450c42c581c7d9dcc5373f65867683108 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3705/CH8/EX8.5/Ex8_5.sce | 39cad6526cba2913032a64f85530b9c6ae815f33 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 938 | sce | Ex8_5.sce |
clear//
//Variable Declaration
sigma_x=8000 //Stress in x in psi
sigma_y=4000 //Stress in y in psi
tau_xy=3000 //Stress in xy in psi
//Calculations
R=sqrt(((sigma_x-sigma_y)*0.5)**2+tau_xy**2) //Resultant Stress in psi
//Principal Stresses
sigma1=(sigma_x+sigma_y)*0.5+R //Principal Stress in psi
sigma2=(sigma_x+sigma_y)*0.5-R //Principal Stress in psi
//Principal Direction
theta1=atan(2*tau_xy*(sigma_x-sigma_y)**-1)*0.5*180*%pi**-1 //Principal direction in degrees
theta2=theta1+90 //Second pricnipal direction in degrees
//Normal Stress
sigma_xdash=0.5*(sigma_x+sigma_y)+0.5*(sigma_x-sigma_y)*cos(2*theta1*%pi*180**-1)+tau_xy*sin(2*theta1*%pi*180**-1)
//Result
printf("\n The principal stresses are as follows")
printf("\n sigma1= %0.0f psi and sigma2= %0.0f psi",sigma1,sigma2)
printf("\n The corresponding directions are")
printf("\n Theta1= %0.1f degrees and Theta2= %0.1f degrees",theta1,theta2)
|
deab72780b44deea7da3b9f4b966ce34de0ad0e2 | 1bb72df9a084fe4f8c0ec39f778282eb52750801 | /test/PF9.prev.tst | 8f4aab17df0abe476093313609987288176e3425 | [
"Apache-2.0",
"LicenseRef-scancode-unknown-license-reference"
] | permissive | gfis/ramath | 498adfc7a6d353d4775b33020fdf992628e3fbff | b09b48639ddd4709ffb1c729e33f6a4b9ef676b5 | refs/heads/master | 2023-08-17T00:10:37.092379 | 2023-08-04T07:48:00 | 2023-08-04T07:48:00 | 30,116,803 | 2 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 779 | tst | PF9.prev.tst | result postfix=[1, 1, x, -, 8, ^, /, 3, 1, x, -, 4, ^, /, 1, x, 2, ^, -, 2, ^, /, -, 2, 1, x, -, 2, ^, /, 1, x, 3, ^, -, 2, ^, /, +, 6, /]
(x^2 - 6*x^3 + 6*x^4 + 50*x^5 - 225*x^6 + 468*x^7 - 588*x^8 + 468*x^9 - 225*x^10 + 50*x^11 + 6*x^12 - 6*x^13 + x^14) / ( - 14*x + 89*x^2 - 338*x^3 + 848*x^4 - 1466*x^5 + 1765*x^6 - 1446*x^7 + 663*x^8 + 340*x^9 - 1598*x^10 + 2924*x^11 - 3536*x^12 + 2924*x^13 - 1598*x^14 + 340*x^15 + 663*x^16 - 1446*x^17 + 1765*x^18 - 1466*x^19 + 848*x^20 - 338*x^21 + 89*x^22 - 14*x^23 + x^24 + 1)
vectors: [0,0,1,-6,6,50,-225,468,-588,468,-225,50,6,-6,1],[1,-14,89,-338,848,-1466,1765,-1446,663,340,-1598,2924,-3536,2924,-1598,340,663,-1446,1765,-1466,848,-338,89,-14,1]
coefficients: [0,0,1,8,29,82,198,426,841,1556,2726,4568,7373,11522,17507,25958]
|
1b5a67d92aff033f17d9a1eadab99b32987adb39 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1826/CH2/EX2.13/ex2_13.sce | 4379df46624f0143736360bdd4e165c91b3de1d0 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 457 | sce | ex2_13.sce | // Example 2.13, page no-37
clear
clc
//(i)
h=1
k=1
l=1
a=4.12*10^-10
d=a/sqrt(h^2+k^2+l^2)
printf("\nFor (111) plane\nThe lattice spacing is %.3f*10^-10 m",d*10^10)
//(ii)
h=1
k=1
l=2
a=4.12*10^-10
d=a/sqrt(h^2+k^2+l^2)
printf("\n\nFor (112) plane\nThe lattice spacing is %.3f*10^-10 m",d*10^10)
//(iii)
h=1
k=2
l=3
a=4.12*10^-10
d=a/sqrt(h^2+k^2+l^2)
printf("\n\nFor (123) plane\nThe lattice spacing is %.3f*10^-10 m",d*10^10)
|
d6bcf25cffbc538e28e45500b612f278e14b1da1 | 0ade4f8a7ec375e54db514312b562334ab304d3e | /data/benchmark/Nguyen_10.tst | a35a3a38b2b2cbc08ffdd3eb59cf484e2696cd4e | [] | no_license | zeta1999/go-pge | 39ac86612d4a90c1e53d2c45c1177e98b3bcf4e4 | 99a4b600185145bcc047e8e42cecfd2346b6b16d | refs/heads/master | 2021-01-01T11:10:20.053388 | 2014-01-16T16:06:50 | 2014-01-16T16:06:50 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 56,012 | tst | Nguyen_10.tst | x y
f(xs)
0.750533 0.359142 1.277028
0.626756 0.572443 0.986035
0.575985 0.124983 1.080826
0.637816 0.072959 1.187716
0.789063 0.664825 1.117093
0.770345 0.112760 1.383921
0.263469 0.766723 0.375120
0.560233 0.329157 1.005713
0.767056 0.476004 1.233733
0.205027 0.663801 0.320723
0.389380 0.199585 0.744159
0.601640 0.768951 0.813494
0.296838 0.644369 0.467691
0.096926 0.642710 0.154931
0.865920 0.804129 1.056831
0.042194 0.244393 0.081856
0.225724 0.443540 0.404310
0.042429 0.380967 0.078750
0.614541 0.597276 0.953520
0.017652 0.205253 0.034561
0.730035 0.802032 0.927315
0.452880 0.910537 0.536727
0.310434 0.887540 0.385702
0.014543 0.877455 0.018589
0.768613 0.813500 0.955064
0.855638 0.448694 1.360513
0.770039 0.722707 1.044270
0.932023 0.929864 0.960091
0.336583 0.604887 0.543327
0.371845 0.441512 0.656986
0.618695 0.619399 0.944459
0.606706 0.792445 0.800633
0.726321 0.637489 1.067370
0.892292 0.444048 1.406025
0.848425 0.783095 1.063441
0.908888 0.333539 1.490697
0.062505 0.864369 0.081094
0.550118 0.708293 0.794088
0.009142 0.008715 0.018283
0.460471 0.332446 0.840078
0.991703 0.084279 1.667977
0.728813 0.976067 0.746282
0.060565 0.785778 0.085566
0.656094 0.364647 1.139834
0.274892 0.484231 0.480472
0.581878 0.659086 0.868965
0.708539 0.727845 0.971675
0.525157 0.509271 0.875455
0.704957 0.518162 1.125877
0.857993 0.663646 1.191918
0.624149 0.600126 0.964580
0.497031 0.722290 0.715507
0.993244 0.717928 1.262014
0.644764 0.904366 0.743069
0.583833 0.028550 1.102004
0.650270 0.462032 1.083848
0.189822 0.578873 0.315887
0.510843 0.908059 0.601634
0.162178 0.009145 0.322923
0.619545 0.930627 0.693699
0.450785 0.075907 0.868835
0.789918 0.033872 1.419777
0.180413 0.889638 0.225979
0.807096 0.454498 1.297914
0.577755 0.875709 0.699559
0.795443 0.645766 1.140734
0.630222 0.759597 0.854654
0.171600 0.690631 0.263258
0.996513 0.733322 1.247544
0.707787 0.054198 1.298399
0.576759 0.851769 0.718341
0.496499 0.298718 0.910511
0.220725 0.731313 0.325909
0.367627 0.913118 0.439391
0.256605 0.920545 0.307291
0.465514 0.837297 0.601029
0.137821 0.910111 0.168615
0.209201 0.781673 0.294793
0.679623 0.003560 1.256992
0.962215 0.826178 1.112037
0.938094 0.033108 1.611981
0.901802 0.113211 1.558848
0.930759 0.933232 0.954852
0.894510 0.720580 1.172074
0.730934 0.978530 0.745327
0.102013 0.088699 0.202872
0.228826 0.341636 0.427450
0.735231 0.306159 1.279135
0.980203 0.514538 1.446126
0.935506 0.450331 1.449307
0.258367 0.712594 0.386660
0.844696 0.909811 0.918104
0.160770 0.812608 0.220142
0.676521 0.595747 1.036457
0.117064 0.923115 0.140937
0.253375 0.992092 0.274206
0.612794 0.648858 0.916537
0.624182 0.105469 1.162372
0.079799 0.703508 0.121577
0.014758 0.195606 0.028952
0.598134 0.392369 1.040618
0.598399 0.014294 1.126526
0.107074 0.613017 0.174821
0.739365 0.829220 0.910263
0.059674 0.478135 0.105902
0.106623 0.473383 0.189436
0.730402 0.621555 1.084783
0.961904 0.438823 1.485125
0.107048 0.818791 0.145970
0.816280 0.424151 1.328080
0.800063 0.668487 1.125975
0.462578 0.649347 0.710869
0.154369 0.324232 0.291491
0.648420 0.348908 1.135078
0.847544 0.765814 1.080734
0.087012 0.758607 0.126147
0.393033 0.029880 0.765641
0.116495 0.375689 0.216250
0.394928 0.478296 0.683133
0.449354 0.583915 0.724823
0.489718 0.074136 0.938170
0.372922 0.577677 0.610436
0.588648 0.014781 1.110353
0.820582 0.960230 0.838833
0.612637 0.058817 1.148065
0.746772 0.309718 1.293907
0.719756 0.237976 1.281246
0.823749 0.600843 1.210395
0.225788 0.505624 0.391724
0.137830 0.098044 0.273469
0.150833 0.152895 0.297017
0.069840 0.693258 0.107350
0.859205 0.322395 1.436612
0.455502 0.189565 0.864065
0.722563 0.903935 0.818070
0.932770 0.771714 1.151438
0.285254 0.566361 0.474925
0.433323 0.912081 0.514030
0.300157 0.583259 0.493575
0.251313 0.587502 0.413959
0.814393 0.269979 1.401927
0.166807 0.812170 0.228438
0.504133 0.466911 0.862690
0.329015 0.588772 0.537413
0.620336 0.822957 0.790645
0.175764 0.246383 0.339160
0.689869 0.769350 0.914385
0.573315 0.482514 0.960985
0.855291 0.964387 0.860309
0.848801 0.762049 1.085841
0.415481 0.955864 0.465712
0.093363 0.638175 0.149758
0.996802 0.397009 1.548851
0.015188 0.304235 0.028981
0.496613 0.023390 0.952640
0.685840 0.509430 1.105812
0.102562 0.163027 0.202049
0.732986 0.039858 1.337120
0.914536 0.283293 1.521399
0.622172 0.438192 1.055477
0.694481 0.801390 0.890489
0.123725 0.008052 0.246811
0.852209 0.398360 1.387592
0.457913 0.302394 0.844038
0.129974 0.832430 0.174474
0.667970 0.684478 0.959749
0.552561 0.197098 1.029414
0.095605 0.217561 0.186419
0.249232 0.201904 0.483298
0.712059 0.439194 1.182767
0.516016 0.193121 0.968491
0.427395 0.189174 0.814213
0.839189 0.975623 0.834364
0.088572 0.201342 0.173339
0.115360 0.414400 0.210724
0.450584 0.169427 0.858511
0.287263 0.203606 0.554952
0.464235 0.499007 0.786282
0.964922 0.977144 0.919645
0.985807 0.044929 1.665753
0.611411 0.166114 1.132244
0.482574 0.833780 0.623774
0.762190 0.069934 1.377639
0.803208 0.813691 0.988454
0.181752 0.870412 0.232995
0.039826 0.391408 0.073609
0.741212 0.724011 1.011632
0.801567 0.400796 1.323021
0.956755 0.685504 1.265385
0.412997 0.284033 0.770550
0.292267 0.061887 0.575144
0.684395 0.424944 1.151954
0.651445 0.386731 1.123113
0.652408 0.796520 0.848969
0.865459 0.989643 0.835992
0.803393 0.730215 1.072421
0.315969 0.837812 0.415823
0.627632 0.242705 1.140038
0.345670 0.282216 0.650846
0.636042 0.151443 1.174434
0.729212 0.414218 1.219871
0.302376 0.780533 0.423181
0.787696 0.449789 1.276478
0.314112 0.403282 0.568371
0.279954 0.148743 0.546521
0.451811 0.516998 0.759071
0.692183 0.260659 1.233321
0.168134 0.955636 0.193143
0.167965 0.579855 0.279701
0.471682 0.333126 0.858811
0.031812 0.292920 0.060904
0.601086 0.879403 0.721188
0.265975 0.360361 0.491934
0.793035 0.455982 1.279382
0.304257 0.698725 0.458762
0.805450 0.034647 1.441419
0.522383 0.475623 0.887135
0.021450 0.882182 0.027259
0.903403 0.188367 1.543089
0.762391 0.227724 1.345644
0.284960 0.912164 0.344110
0.262227 0.941126 0.305312
0.314105 0.108072 0.614326
0.190204 0.973080 0.212788
0.233689 0.778575 0.329713
0.667857 0.611169 1.014394
0.935373 0.647714 1.283633
0.105531 0.267928 0.203155
0.047174 0.563021 0.079756
0.672618 0.881919 0.792092
0.325590 0.055235 0.638760
0.319978 0.417287 0.575111
0.006852 0.623916 0.011122
0.896429 0.739673 1.153983
0.840446 0.949255 0.867542
0.411793 0.182083 0.787272
0.070717 0.490352 0.124664
0.316041 0.786540 0.439044
0.038041 0.411050 0.069728
0.970399 0.990394 0.904917
0.474552 0.897274 0.570026
0.047131 0.918697 0.057182
0.508145 0.968092 0.551632
0.212788 0.392480 0.390256
0.734312 0.103954 1.332919
0.436179 0.145523 0.836028
0.528204 0.066483 1.005739
0.014687 0.673937 0.022952
0.424540 0.898107 0.513305
0.592128 0.113132 1.109120
0.548516 0.568718 0.878691
0.834394 0.071183 1.478026
0.952794 0.829524 1.100670
0.702405 0.052037 1.290361
0.734024 0.488548 1.182998
0.574740 0.415777 0.994605
0.014312 0.288614 0.027440
0.624817 0.291356 1.120593
0.919013 0.255141 1.538534
0.062536 0.016918 0.124972
0.431552 0.531251 0.721262
0.132968 0.166836 0.261471
0.556081 0.807683 0.729690
0.712812 0.005512 1.307907
0.939601 0.625738 1.308720
0.003871 0.891741 0.004863
0.914853 0.664413 1.247794
0.254306 0.893849 0.315180
0.458765 0.358656 0.829325
0.170839 0.179946 0.334528
0.929574 0.495503 1.409969
0.011385 0.216554 0.022238
0.685037 0.652978 1.005082
0.560026 0.501908 0.931385
0.566912 0.075654 1.070986
0.909205 0.140511 1.562478
0.759976 0.661051 1.087570
0.449843 0.279462 0.835909
0.929122 0.557398 1.359673
0.554831 0.129864 1.044727
0.701535 0.137531 1.278593
0.741556 0.266278 1.303264
0.343517 0.994207 0.367225
0.847181 0.390446 1.386032
0.802081 0.334036 1.358147
0.654195 0.355201 1.141069
0.209541 0.758051 0.302106
0.648521 0.116630 1.199809
0.482414 0.354446 0.870163
0.936647 0.025642 1.610622
0.822225 0.949497 0.852954
0.495514 0.633268 0.766573
0.868543 0.260329 1.475333
0.496704 0.723858 0.714087
0.173130 0.215419 0.336569
0.427466 0.226373 0.807979
0.257322 0.855130 0.333955
0.776666 0.267212 1.352061
0.447473 0.496232 0.760997
0.878141 0.568625 1.296915
0.106811 0.181709 0.209706
0.471680 0.862321 0.591314
0.397138 0.746804 0.567688
0.492208 0.846138 0.626518
0.576703 0.875988 0.698197
0.774348 0.288044 1.340883
0.564177 0.153831 1.056813
0.266081 0.216458 0.513632
0.853999 0.609534 1.236290
0.088383 0.352041 0.165709
0.968065 0.675594 1.285666
0.743557 0.217640 1.321884
0.645431 0.492290 1.060223
0.867407 0.853616 1.002528
0.698592 0.566562 1.085301
0.746095 0.282644 1.303687
0.689298 0.708337 0.966007
0.808824 0.348494 1.359972
0.637908 0.804384 0.826047
0.314326 0.028931 0.618093
0.257232 0.224181 0.496076
0.251380 0.654367 0.394718
0.988684 0.758864 1.212223
0.929265 0.531601 1.381229
0.202828 0.409636 0.369548
0.596041 0.723431 0.841538
0.171573 0.306810 0.325519
0.939341 0.453008 1.451508
0.238444 0.507083 0.412939
0.835425 0.422447 1.352776
0.519228 0.797482 0.693216
0.919506 0.139976 1.575048
0.335102 0.687814 0.508187
0.279323 0.246327 0.534766
0.862104 0.952376 0.880307
0.074661 0.362363 0.139496
0.788931 0.621504 1.153816
0.858265 0.150801 1.496244
0.563628 0.696584 0.819590
0.783328 0.376617 1.312372
0.267651 0.830072 0.356937
0.857035 0.460953 1.354021
0.525713 0.152654 0.991989
0.593105 0.159836 1.103628
0.039916 0.896778 0.049812
0.555922 0.532247 0.909451
0.118904 0.687906 0.183293
0.657567 0.875978 0.782628
0.363633 0.847853 0.470622
0.019447 0.501574 0.034101
0.183827 0.829415 0.246883
0.207996 0.510406 0.360361
0.552809 0.380377 0.975100
0.139269 0.645599 0.221761
0.482308 0.400434 0.854266
0.910657 0.755635 1.149846
0.945652 0.929724 0.969900
0.816530 0.846060 0.966264
0.969676 0.964375 0.940047
0.570104 0.380025 1.002427
0.551953 0.744532 0.771221
0.686634 0.830035 0.855625
0.620314 0.554918 0.988129
0.578340 0.556316 0.928411
0.343835 0.837093 0.451461
0.596893 0.853030 0.739358
0.771556 0.132686 1.382246
0.509733 0.897734 0.608353
0.292996 0.802295 0.401497
0.269681 0.526651 0.460645
0.499271 0.012047 0.957501
0.639886 0.408306 1.096038
0.915405 0.778504 1.128905
0.544549 0.892801 0.649855
0.638309 0.534541 1.025440
0.709768 0.191124 1.279584
0.721707 0.842178 0.879796
0.810392 0.303735 1.382783
0.839242 0.973659 0.836823
0.805389 0.350609 1.354463
0.302592 0.943513 0.349815
0.885627 0.115803 1.538252
0.149083 0.490419 0.262050
0.892661 0.952782 0.902437
0.707045 0.326341 1.230611
0.011318 0.522887 0.019611
0.046364 0.443026 0.083746
0.289298 0.565328 0.481788
0.049713 0.054807 0.099236
0.918224 0.931231 0.948418
0.393673 0.469255 0.684239
0.794706 0.554943 1.213119
0.930315 0.949818 0.933034
0.738945 0.883184 0.854943
0.003950 0.763709 0.005706
0.164952 0.223306 0.320256
0.829526 0.108074 1.466615
0.126998 0.250032 0.245438
0.089951 0.809457 0.123945
0.799775 0.325606 1.359031
0.654370 0.563783 1.028926
0.731207 0.083670 1.330866
0.595249 0.929611 0.670779
0.860019 0.852441 0.997561
0.286218 0.057164 0.563730
0.372950 0.277913 0.700767
0.792963 0.668939 1.117784
0.324723 0.071060 0.636482
0.694689 0.791660 0.899617
0.126361 0.290429 0.241495
0.123463 0.528816 0.212656
0.514476 0.016252 0.984028
0.959302 0.576256 1.373127
0.085201 0.249906 0.164909
0.947949 0.391700 1.501408
0.206744 0.709200 0.311559
0.454096 0.349954 0.824125
0.486439 0.589100 0.777365
0.032092 0.430529 0.058316
0.752814 0.240214 1.328128
0.420325 0.918576 0.495343
0.709724 0.049123 1.301677
0.833497 0.658895 1.170644
0.341966 0.138239 0.664282
0.190766 0.855336 0.248756
0.932123 0.525295 1.389278
0.040423 0.642807 0.064693
0.909727 0.108151 1.569448
0.692085 0.615315 1.042206
0.570047 0.216461 1.054156
0.961835 0.996879 0.890662
0.816262 0.653255 1.157162
0.731997 0.395153 1.233702
0.953174 0.927499 0.978044
0.420107 0.517312 0.708981
0.189490 0.737346 0.278867
0.891020 0.562313 1.315929
0.371274 0.194243 0.711960
0.766256 0.329908 1.312093
0.518518 0.777461 0.706415
0.412499 0.010027 0.801760
0.788069 0.074505 1.414052
0.871304 0.815490 1.049065
0.741334 0.080474 1.346174
0.486437 0.020806 0.934756
0.421705 0.592516 0.679087
0.818952 0.297080 1.396868
0.264366 0.363893 0.488374
0.040596 0.821195 0.055305
0.738673 0.557276 1.142870
0.622966 0.271907 1.124022
0.049076 0.601386 0.080899
0.247031 0.538100 0.419942
0.470386 0.224305 0.883754
0.304358 0.731272 0.446120
0.442559 0.311128 0.815385
0.425940 0.272420 0.795880
0.528416 0.747992 0.739164
0.677757 0.674524 0.979453
0.268294 0.031826 0.529904
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ce04db4b793d06fc7739764bcc686f887ecaf1e6 | a6e58ee44f93c31b00278a8bf6609103c3daa7eb | /fslib/hartley.tst | 3538d08898035adbaaed05ef4d0abd2b67c5e40f | [] | no_license | bykolodny/The-Forth-Scientific-Library | 4965c1ba0ad2ea28a14c881203f17d1d02a83cfb | d05fb4591be0a21a1066547112f788ddef67b81b | refs/heads/master | 2022-12-03T23:49:13.353261 | 2020-08-24T11:24:08 | 2020-08-24T11:24:08 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 4,549 | tst | hartley.tst | \ hartley.tst Additional Hartley Transform Utilities and test code
\ Supplement to Forth Scientific Library Algorithm #8
\ This code conforms with ANS requiring:
\ 1. The Floating-Point word set
\ F2DUP FDUP two floats
\ F2DROP FDROP two floats
\ F2* F2/ Multiply and divide float by two
\ F> Test for greater than
\ : F2DUP FOVER FOVER ;
\ : F2DROP FDROP FDROP ;
\ : F2* 2.0e0 F* ;
\ : F2/ 2.0e0 F/ ;
\ : F> FSWAP F< ;
\ by Marcel Hendrix, October 8, 1994.
\ (c) Copyright 1994 Marcel Hendrix. Permission is granted by the
\ author to use this software for any application provided this
\ copyright notice is preserved.
CR .( HARTLEY.TST V1.0 8 October 1994 MH )
: ifht ( addr #elts -- )
fht ;
\ Calculate Fourier coefficients from the FHT algorithm output
\ 1024 CONSTANT datasize ( test for accuracy )
64 CONSTANT datasize ( test for speed )
datasize FLOAT ARRAY data{
datasize 2/ 1+ FLOAT ARRAY RealPts{
datasize 2/ 1+ FLOAT ARRAY ImagPts{
\ Expects to work with an UNNORMALIZED Hartley transform result.
\ Performs the normalization on the fly.
: FHT->FFT
1e datasize S>F FSQRT F/ FRAME| a |
datasize 2/
1 ?DO
data{ I } F@
data{ datasize I - } F@ F2DUP
F+ a F* RealPts{ I } F!
F- a F* ImagPts{ I } F!
LOOP
|FRAME ;
\ Calculate the power spectrum from the FHT algorithm output.
\ Expects to work with an UNNORMALIZED Hartley transform result.
\ Performs the normalization on the fly.
datasize 2/ 1+ FLOAT ARRAY PowerF{
: FHT->POWER
datasize 2/
1 ?DO
data{ I } F@ FDUP F* data{ datasize I - } F@ FDUP F*
F+ F2* datasize S>F F/ PowerF{ I } F!
LOOP ;
\ Generate a test function.
datasize FLOAT ARRAY InputData{
: GENERATE PI datasize 2/ S>F F/ 0E FRAME| a b |
datasize
0 ?DO
a FCOS 2E F*
a 3E F* FCOS 3E F* F+
a 10E F* FCOS 5E F* F+
datasize 200 > IF a 200E F* FCOS 50E F* F+
THEN
FDUP data{ I } F! InputData{ I } F!
b a F+ &a F!
LOOP
|FRAME ;
1E-3 FCONSTANT noisefloor \ Smaller than this, a coefficient is noise
: SHOW-DATA datasize 0 ?DO
data{ I } F@ FABS noisefloor
F> IF CR ." component " I 1- 4 .R ." = "
data{ I } F@ FE.
THEN
LOOP ;
: SHOW-DIFF 0e
datasize 0 ?DO
data{ I } F@
InputData{ I } F@ F- FABS F+
LOOP
datasize S>F F/
CR ." Total weighted error = " FE. ;
: SINE-TEST GENERATE
data{ datasize fht SHOW-DATA
data{ datasize ifht SHOW-DIFF ;
: SHOW-FFT GENERATE data{ datasize fht FHT->FFT
datasize 2/
1 ?DO
ImagPts{ I } F@ RealPts{ I } F@ F2DUP
FABS FSWAP FABS F+ noisefloor
F> IF CR I 4 .R 2 SPACES
." (Real, Imag) = (" FE. ." ," FE. ." )"
ELSE F2DROP
THEN
LOOP ;
: SHOW-POWER GENERATE data{ datasize fht FHT->POWER
datasize 2/
1 ?DO
PowerF{ I } F@ FDUP noisefloor
F> IF CR I 4 .R 2 SPACES ." Power component = " FE.
ELSE FDROP
THEN
LOOP ;
: .SPEED
GENERATE
." Testing..." CR
100 0 DO
data{ datasize fht
data{ datasize ifht
LOOP
." (100 64-point FHT + IFHT pairs)"
CR ." 80386 @ 33 MHz in iForth (80 bit) : 2.80 sec."
CR ." T800 @ 20 MHzin tForth (32 bit) : 3.54 sec."
CR ." RTX-2000 @ 10 MHz in F83, FFT+IFFT : 1.7 sec." CR ;
: .SPEED-FHT
GENERATE
." Testing..." CR
100 0 DO
data{ datasize fht
LOOP
." (100 " datasize 0 .R ." -point real FHT's)" CR ;
: .ABOUT
CR ." SINE-TEST for an example,"
CR ." SHOW-FFT computes an example FFT from the FHT,"
CR ." SHOW-POWER computes an example power spectrum from the FHT,"
CR ." .SPEED demonstrates conversion speed FHT + IFHT,"
CR ." .SPEED-FHT demonstrates conversion speed FHT." ;
CR .ABOUT
|
c26d13552be785c6588e2be16bf9ff8991d28346 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3648/CH16/EX16.10/Ex16_10.sce | ebdc42c1e69813d5f18120b1776aac9bf8d7b926 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 501 | sce | Ex16_10.sce | //Example 16_10
clc();
clear;
//To find the absolute potential and how much energy is needed to pull the electrons from atom
k=9*10^9 //Units in N meter^2/C^2
q=1.6*10^-19 //Units in C
r=5.3*10^-11 //Units in meters
v=(k*q)/r //Units in V
printf("The absolute potential is V=%.1f V\n",v)
Vinfinity=0 //Units in V
deltaV=Vinfinity-v //Units in V
work=-q*deltaV //Units in J
printf("The energy that is required is W=")
disp(work)
printf("J")
|
f123e9536b0892a70fa8b78e95f65ebb20485ef8 | 8217f7986187902617ad1bf89cb789618a90dd0a | /source/2.2/macros/percent/%rrp.sci | 8f9794971670012d539203fddd83bc1c198c4e2c | [
"MIT",
"LicenseRef-scancode-warranty-disclaimer",
"LicenseRef-scancode-public-domain"
] | permissive | clg55/Scilab-Workbench | 4ebc01d2daea5026ad07fbfc53e16d4b29179502 | 9f8fd29c7f2a98100fa9aed8b58f6768d24a1875 | refs/heads/master | 2023-05-31T04:06:22.931111 | 2022-09-13T14:41:51 | 2022-09-13T14:41:51 | 258,270,193 | 0 | 1 | null | null | null | null | UTF-8 | Scilab | false | false | 271 | sci | %rrp.sci | function f=%rrp(f1,p2)
// %rrp(f,p) calcule la division a droite de la matrice de fractions
//rationnelles f et de la matrice de polynomes p. (f/p)
//!
if prod(size(p2)) <>1 then f=f1*invr(p2),return,end
[n1,d1]=f1(2:3)
[n1,p2]=simp(n1,p2*d1)
f=tlist('r',n1,p2,f1(4))
|
f39982a07fa7339d1cd3c567a2b2b0b0519ebed4 | 05b2bd67239938195f6ea021fd482c06f69c9145 | /Codebook 2doParcial.sci | 8de974601a1b60fff777348c480ead77ff910ecc | [] | no_license | ZimmSebas/Metodos | 213aa8af793726409cf0346c3315663aa59ae835 | 5fb6f28413064194ae8f625da48914b471bb50f7 | refs/heads/master | 2020-03-31T15:18:35.349807 | 2019-12-21T23:19:21 | 2019-12-21T23:19:21 | 152,331,779 | 5 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 13,712 | sci | Codebook 2doParcial.sci | //Codebook de Scilab pt 2!
//Indice
//1ra parte: Aproximacion de Autovalores y Autovectores
//gershgorin(A). Muestra las cotas de los autovalores de A dada dicha matriz.
//potencia(A, z0, max_iter). Dada una matriz A y un vector z0 (estimación de posible autovector) y una cantidad de iteraciones max_iter aproxima al autovalor cuyo módulo es el radio espectral (mayor valor absoluto).
//2da parte: Interpolación y mínimos cuadrados
//InterpolacionLagrange(X,pto). Interpolacion de Lagrange, toma un conjunto de pares de elementos (x,f(x)) y un pto a aproximar
//DDs(X). Calcula diferencias divididas de Newton dado un conjunto de pares de elemntos (x,f(x))
//InterpolacionNewton(X,pto). Interpolacion de Newton, toma un conjunto de pares de elementos X (x,f(x)) y un pto a aproximar
// FactoRQ(A) Factoriza una matriz A en Q,R (usado en mínimos cuadrados)
//minimoscuad(xi,y,gr): Toma un conjunto de puntos xi, y un conjunto de f(xi)=y, y un grado de polinomio. Aproxima un polinomio por minimos cuadrados y devuelve el error.
//Chevyshev(n). Calcula las raices de un polinomio de Chevyshev para n nodos interpolantes
//polinomioInter(fn,n). Dada una funcion fn y un nro de nodos n, calcula la Interpolacion de Newton de las raices de un polinomio de Chevyshev
//3ra parte: Metodos de Integración
//reglaTrapecio(fn,a,b). Aplica método del trapecio a una función fn de a hasta b.
//reglaSimpson(fn,a,b). Aplica método del Simpson a una función fn de a hasta b.
//metodoCompTrapecio(fn,a,b,n). Aplica método del trapecio a una función fn de a hasta b en n intervalos.
//metodoCompSimpson(fn,a,b,n). Aplica método del Simpson a una función fn de a hasta b en n intervalos.
//reglaTrapecioExt(fn,x1,x2,y1,y2). Aplica método del trapecio a una función fn de x1 a x2 y de y1 a y2.
//IntDosS(f,a,b,cx,dx,n,m). Aplica método de Simpson a una función fn de dos variables desde a hasta b, y desde cx a dx en N iteraciones de x e M iteraciones de Y.
//IntDosT(f,a,b,cx,dx,n,m). Aplica método de trapecio a una función fn de dos variables desde a hasta b, y desde cx a dx en N iteraciones de x e M iteraciones de Y.
//4ta parte: Adicionales!
//errorcalc(a,b) Calcula el error absoluto y el error relativo
//reverse(arr). Algoritmo que da vuelta los indices de un arreglo
//ploty(fn,l,in,r). Plotea con funcion, limite izq, intervalo, limite der
//comp_metodos(N) Comparador de tiempos de métodos armado.
// -------------------------------------- ------------------------------------------
// 1ra parte: Aproximacion de Autovalores y Autovectores
// -------------------------------------- ------------------------------------------
//gershgorin(A). Muestra las cotas de los autovalores de A dada dicha matriz.
function gershgorin(A)
sz = size(A, 1);
for i = 1:sz
suma = 0;
for j = 1:sz
if (i <> j)
suma = suma + abs(A(i,j));
end;
end;
mprintf("|lambda - %f| <= %f\n", A(i,i), suma);
end;
endfunction
// poly([A], "x") -> polinomio caracteristico de la matriz A
//(det(lambda*I - A) = p(lambda))
// Dado un polinomio mónico (o normalizado) p(lambda) una matriz
// A es compañera del polinomio si det(lambda*I - A) = p(lambda),
// es decir, si el polinomio característico de A es p.
function ej_3(A)
sz = size(A, 1);
for k = 0:10
mprintf("k = %d\n", k)
A(sz,sz) = 1 + 0.1*k;
p = poly([A], "x");
x = roots(p);
disp(x)
av = spec(A);
disp(av)
gershgorin(A);
end
endfunction
//potencia(A, z0, max_iter). Dada una matriz A y un vector z0 (estimación de posible autovector) y una cantidad de iteraciones max_iter
// aproxima al autovalor cuyo módulo es el radio espectral (mayor valor absoluto).
function rho = potencia(A, z0, max_iter)
sz = size(z0, 1)
for i = 1:max_iter
w = A*z0
//disp(w)
if(i <> max_iter)
z = w / norm(w, %inf)
z0 = z
end
end
//Elegimos la componente de mayor valor absoluto
k = 1
for i = 2:sz
if( abs(w(i)) > abs(w(k)))
k = i
end
end
rho = w(k) / z0(k)
endfunction
// -------------------------------------- ------------------------------------------
// 2da parte: Interpolación y mínimos cuadrados
// -------------------------------------- ------------------------------------------
//InterpolacionLagrange(X,pto). Interpolacion de Lagrange, toma un conjunto de pares de elementos (x,f(x)) y un pto a aproximar
function y = InterpolacionLagrange(X,pto)
sz = size(X,1)
for i = 1:sz
nume = 1
deno = 1
for j = 1:sz
if (i <> j)
nume = (pto - X(j,1)) * nume
end
end
for j = 1:sz
if (i <> j)
deno = (X(i,1) - X(j,1)) * deno
end
end
l(i) = nume/deno;
end
y = 0;
for i = 1:sz
y = l(i) * X(i, 2) + y
end
endfunction
//DDs(X). Calcula diferencias divididas de Newton dado un conjunto de pares de elemntos (x,f(x))
function D = DDs(X)
sz = size(X,1)
for i = 1:sz
D(i,1) = X(i,2)
end
for i = 2:sz
for j = 1:sz-(i-1)
D(j,i) = ( D(j+1,i-1) - D(j,i-1)) / ( X(j+i-1,1) - X(j,1) )
end
end
//disp(D)
endfunction
//InterpolacionNewton(X,pto). Interpolacion de Newton, toma un conjunto de pares de elementos X (x,f(x)) y un pto a aproximar
function y = InterpolacionNewton(X,pto)
sz = size(X,1)
y = X(1,2)
D = DDs(X)
for i = 2:sz
pr = 1
for j = 1:i-1
pr = (pto - X(j,1)) * pr
end
y = y + pr*D(1,i)
end
endfunction
// FactoRQ(A) Factoriza una matriz A en Q,R (usado en mínimos cuadrados)
function [Q,R] = FactoRQ(A) // A debe tener columnas LI
sz = size(A,2)
Q(:,1) = A(:,1)/norm(A(:,1))
V(1) = norm(A(:,1))
for i = 2:sz
suma = 0
for j = 1:i-1
suma = suma + (A(:,i)'*Q(:,j))*Q(:,j)
end
Q(:,i) = A(:,i) - suma
V(i) = norm(Q(:,i))
Q(:,i) = Q(:,i)/V(i)
end
R = diag(V)
for i = 1:sz
for j = i+1:sz
R(i,j) = A(:,j)'*Q(:,i)
end
end
endfunction
//minimoscuad(xi,y,gr): Toma un conjunto de puntos xi, y un conjunto de f(xi)=y, y un grado de polinomio. Aproxima un polinomio por minimos cuadrados y devuelve el error.
function [p, err] = minimoscuad(xi, y, gr)
szy = size(y,1);
n = gr+1;
A = eye(szy, n);
for j = 1:n
for i = 1:szy
A(i, j) = xi(i)**(j-1);
end
end
[Q,R] = FactoRQ(A);
b = Q'*y
sz = size(R,1)
x(sz) = b(sz)/R(sz,sz)
for i = 1:sz-1 //ResUELVE QR
suma = 0
for j = 1:i
suma = suma + x(sz-j+1)*R(sz-i,sz-j+1)
end
x(sz-i) = (b(sz-i)-suma)/R(sz-i,sz-i)
end
p = poly(x, 'x', "coeff")
E = A*x-y;
err = E'*E;
endfunction
//Chevyshev(n). Calcula las raices de un polinomio de Chevyshev para n nodos interpolantes
function rot = Chevyshev(n)
for i = 1:n
rot(i) = cos( ((2*i)-1) *%pi/ (2*n) )
end
endfunction
//polinomioInter(fn,n). Dada una funcion fn y un nro de nodos n, calcula la Interpolacion de Newton de las raices de un polinomio de Chevyshev
function pf = polinomioInter(fn,n)
rot = Chevyshev(n)
sz = size(rot,1)
for i = 1:sz
X(i,1) = rot(i)
X(i,2) = fn(rot(i))
end
D = DDs(X)
sz = size(D,1)
p(1) = 1
pf = p(1) * D(1,1)
for j = 2:sz
p(j) = p(j-1) * poly([-X(j-1,1),1],'x','coeff')
pf = pf + p(j) * D(1,j)
end
endfunction
//ej11
function y = ej11(x)
y = cos(x)
endfunction
//Chevyshev(n,a,b). Calcula las raices de un polinomio de Chevyshev para n nodos interpolantes en un intervalo general a,b.
function rot = ChevyshevGen(n,a,b)
rot = Chevyshev(n)
for i = 1:n
rot(i) = (a+b+rot(i)*(b-a) )/ 2
end
endfunction
//polinomioInterGen(fn,n,a,b). Dada una funcion fn y un nro de nodos n, y par de puntos a,b de rango; calcula la Interpolacion de Newton de las raices de un polinomio de Chevyshev para un intervalo general[a,b]
function pf = polinomioInterGen(fn,n,a,b)
rot = ChevyshevGen(n,a,b)
sz = size(rot,1)
for i = 1:sz
X(i,1) = rot(i)
X(i,2) = fn(rot(i))
end
D = DDs(X)
sz = size(D,1)
p(1) = 1
pf = p(1) * D(1,1)
for j = 2:sz
p(j) = p(j-1) * poly([-X(j-1,1),1],'x','coeff')
pf = pf + p(j) * D(1,j)
end
endfunction
//polyChevyshev(n) Crea el polinomio de Chevyshev de n nodos y calcula sus raices
function rot = polyChevyshev(n)
T1(1) = 1
T2(1) = 0
T2(2) = 1
for i = 1:n-1
sz2 = size(T2,1)
for j = 1:sz2+1
if (j == 1)
T3(j) = 0
else
T3(j) = T2(j-1)*2
end
end
sz1 = size(T1,1)
for j = 1:sz1
T3(j) = T3(j) - T1(j)
end
T1 = T2
T2 = T3
end
pc = poly(T3','x','coeff')
rot = roots(pc)
endfunction
// -------------------------------------- -----------------------------------------------------
// 3ra parte: Metodos de Integración
// -------------------------------------- -----------------------------------------------------
//reglaTrapecio(fn,a,b). Aplica método del trapecio a una función fn de a hasta b.
function y = reglaTrapecio(fn, a, b)
h = b-a;
y = h/2 * (fn(a) + fn(b));
endfunction
//reglaSimpson(fn,a,b). Aplica método del Simpson a una función fn de a hasta b.
function y = reglaSimpson(fn, a, b)
h = (b-a)/2;
med = (b+a)/2;
y = h/3 * (fn(a) + 4*fn(med) + fn(b));
endfunction
//metodoCompTrapecio(fn,a,b,n). Aplica método del trapecio a una función fn de a hasta b en n intervalos.
function y = metodoCompTrapecio(fn, a, b, n)
h = (b-a)/n;
suma = 0;
for i = 0:n
asd = a + i*h;
if(i == 0 | i == n)
suma = suma + fn(asd);
else
suma = suma + 2*fn(asd);
end
end
y = suma * h/2;
endfunction
//metodoCompSimpson(fn,a,b,n). Aplica método del Simpson a una función fn de a hasta b en n intervalos.
function y = metodoCompSimpson(fn, a, b, n)
h = (b-a)/n;
suma = 0;
for i = 0:n
if(i == 0 | i == n)
suma = suma + fn(a + i*h);
else
if (pmodulo(i,2) == 1)
suma = suma + 4*fn(a + i*h);
else
suma = suma + 2*fn(a + i*h);
end
end
end
y = suma * h/3;
endfunction
//reglaTrapecioExt(fn,x1,x2,y1,y2). Aplica método del trapecio a una función fn de x1 a x2 y de y1 a y2.
function y = reglaTrapecioExt(fn,x1,x2,y1,y2)
h = (y2-y1)*(x2-x1)/4;
y = h * (fn(x1,y1)+fn(x2,y1)+fn(x1,y2)+fn(x2,y2));
endfunction
//IntDosS(f,a,b,cx,dx,n,m). Aplica método de Simpson a una función fn de dos variables desde a hasta b, y desde cx a dx en N iteraciones de x e M iteraciones de Y.
function y = IntDosS(f,a,b,cx,dx,n,m)
deff('z=aux1(y)','z=f(a,y)')
deff('z=aux2(y)','z=f(b,y)')
temp = metodoCompSimpson(aux1,cx(a),dx(a),m) + metodoCompSimpson(aux2,cx(b),dx(b),m)
h = (b-a)/n
for i=1:n-1
xi = a+i*h
deff('z=aux(y)','z=f(xi,y)')
if pmodulo(i,2) == 0 then
temp = temp + 2*(metodoCompSimpson(aux,cx(xi),dx(xi),m))
else
temp = temp + 4*(metodoCompSimpson(aux,cx(xi),dx(xi),m))
end
end
y = (h/3) * temp
endfunction
//IntDosT(f,a,b,cx,dx,n,m). Aplica método de trapecio a una función fn de dos variables desde a hasta b, y desde cx a dx en N iteraciones de x e M iteraciones de Y.
function y = IntDosT(f,a,b,cx,dx,n,m)
deff('z=aux1(y)','z=f(a,y)')
deff('z=aux2(y)','z=f(b,y)')
temp= (metodoCompTrapecio(aux1,cx(a),dx(a),m)/2) + (metodoCompTrapecio(aux2,cx(b),dx(b),m)/2)
h = (b-a)/n
for i=1:n-1
xi = a+i*h
deff('z=aux(y)','z=f(xi,y)')
temp = temp + (metodoCompTrapecio(aux,cx(xi),dx(xi),m))
end
y = h * temp
endfunction
// -------------------------------------- -----------------------------------------------------
// 4ta parte: Adicionales!
// -------------------------------------- -----------------------------------------------------
// Comparador de tiempos de métodos armado.
function [x,t] = comp_metodos(N)
A = 8*eye(N,N) + 2*diag(ones(N-1, 1), 1) + 2*diag(ones(N-1, 1), -1) + diag(ones(N-3,1), 3) + diag(ones(N-3,1), -3)
b = ones(N,1)
tic();
lusolver(A,b);
t(1)=toc();
eps = 10^-6;
x0 = zeros(N,1);
tic();
gausssolver(A,b,x0,eps);
t(2) = toc();
eps = 10^-12;
tic();
gausssolver(A,b,x0,eps);
t(3) = toc();
endfunction
// Calcula el error absoluto y el error relativo
function y = errorcalc(a,b)
y(1) = abs(a - b)
y(2) = abs(a - b)/abs(a)
mprintf("error absoluto %0.15f \n", y(1))
mprintf("error relativo %0.15f \n", y(2))
endfunction
// Algoritmo que da vuelta los indices de un arreglo
function y = reverse(arr)
n = length(arr)
y = (1:n)
for i = 1:n
y(n+1-i) = arr(i)
end
endfunction
//ploty(fn,l,in,r). Plotea con funcion, limite izq, intervalo, limite der
function ploty(fn,l,in,r)
// xdel(winsid());
x = [l:in:r];
// n = size(x);
// yy = zeros(1,n(2));
// plot(x,yy)
plot(x,fn)
a = gca();
a.auto_scale = "off";
endfunction
|
16a43a4be3b8c7bb52f0e77e3e8458893d8335da | 449d555969bfd7befe906877abab098c6e63a0e8 | /3821/CH10/EX10.23/Example10_23.sce | d0335c351dc5ba233999f410fca02f5f085f3b72 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,314 | sce | Example10_23.sce | /////////Chapter 10 Properties Of Steam
///Example 10.23 Page No:203
///Find Constant pressure process
//Input data
clc;
clear;
ms=1000; //Steam in Kg/h
P=16; //Absolute pressure in bar
x2=0.9; //Steam is dry
t1=30+273; //temperature in degree celsius
tsup=380; //tmperature rised in degree celsius
//from steam table(pressure basis at 16 bar)
h1=125.7; //in KJ/Kg
ts=201.4; //In degree celsius
hf=858.5; //in kJ/Kg
hfg=1933.2; //in kJ/Kg
hg=2791.7; //in kJ/Kg
Cps=2.3;
//Calculation
h2=hf+x2*hfg; //Final enthalpy of wet steam in KJ/Kg
Q1=(ms*(h2-h1))*(10^(-3)); //Constant pressure process in KJ/h
h3=hg+Cps*(tsup-ts); //Final enthalpy of superheated steam in KJ/g
Q2=(ms*(h3-h2))*(10^(-3)); //Suprheated steam in KJ/h
//Output
printf('Final enthalpy of wet steam= %f KJ/Kg \n ',h2);
printf('Constant pressure process= %f KJ/h \n',Q1);
printf('Final enthalpy of superheated steam= %f KJ/g \n',h3);
printf('Suprheated steam= %f KJ/h \n',Q2);
|
06a4d37b89b5434ecee40bd875e8d839a02559b5 | b2d3db891e489d6c9c22b9c1b7d78745a13f2ebc | /FIR_Filter_Windowing.sce | 91227cf0d6ce56825f60a7d46e5461b3d8f98452 | [] | no_license | rajas1612/Digital-Signal-Processing | 28f1eee626141f34b71f36fe4f338c2380065a0c | 7b040622bab80a30910a3cde431c7a253c76439d | refs/heads/main | 2023-04-02T22:46:16.605197 | 2021-04-01T12:05:32 | 2021-04-01T12:05:32 | 335,709,667 | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 2,673 | sce | FIR_Filter_Windowing.sce | clear;
clc;
close;
pi=%pi;
M=5; // 2*Tau + 1 = M
Tau=2;
n=0:1:Tau;
hd=zeros(1,Tau+1);
Wh=zeros(1,Tau+1);
//CALCULATING hd
for i = 1 : length(n)
if n(i)==Tau
hd(i)=0.25;
else
hd(i)=sin(pi/4*(n(i)-Tau))/(pi*(n(i)-Tau));
end
end
scf(1);
complete_hd = [hd,flipdim(hd(1:Tau),2)];
title("Plot of hd(n)");
plot2d3(complete_hd);
xlabel("n");
ylabel("hd(n)");
e = gce(); // get current entity to change the thickness of the graph plots
e.children.thickness = 4;
a = gca(); // get current axes to change axis properties
a.x_location = "origin";
a.y_location = "origin";
a.title.font_size = 5;
// CALCULATING coefficients
for i=0:length(hd)-1
if i-(M-1)/2 > 0
k= i - (M-1)/2;
else
k= (M-1)/2 - i;
end
Wh(i+1)=1-2*k/(M-1);
end
scf(2);
complete_Wh = [Wh,flipdim(Wh(1:Tau),2)];
plot2d3(complete_Wh);
title("Plot of Bartlett Window");
xlabel("n");
ylabel("Wh(n)");
e = gce(); // get current entity to change the thickness of the graph plots
e.children.thickness = 4;
a = gca(); // get current axes to change axis properties
a.x_location = "origin";
a.y_location = "origin";
a.title.font_size = 5;
H=hd.*Wh //element wise multiplication
scf(3);
complete_H=[H,flipdim(H(1:Tau),2)];
plot2d3(complete_H);
title("Plot of H(n)");
xlabel("n");
ylabel("H(n)");
e = gce(); // get current entity to change the thickness of the graph plots
e.children.thickness = 4;
a = gca(); // get current axes to change axis properties
a.x_location = "origin";
a.y_location = "origin";
a.title.font_size = 5;
w = -%pi:0.01:%pi;
Hw= zeros(1,length(w));
phase_Hw= zeros(1,length(w));
for i=1:length(w)
for j=1:length(H)
if j==Tau+1
Hw(i) = Hw(i) + H(j);
else
Hw(i) = Hw(i)+H(j)*cos(w(i)*(Tau- j+1))*2;
end
end
if Hw(i)>0
phase_Hw(i) = -Tau*w(i);
else
phase_Hw(i) = %pi - Tau*w(i);
end
end
scf(4);
plot2d3(w,Hw);
title("Magnitude response"); xlabel("w");
ylabel("H(w)");
e = gce(); // get current entity to change the thickness of the graph plots
e.children.thickness = 4;
a = gca(); // get current axes to change axis properties
a.x_location = "origin";
a.y_location = "origin";
a.title.font_size = 5;
scf(5);
plot2d3(w,phase_Hw);
title("Phase response");
xlabel("w");
ylabel("Phase angle");
e = gce(); // get current entity to change the thickness of the graph plots
e.children.thickness = 4;
a = gca(); // get current axes to change axis properties
a.x_location = "origin";
a.y_location = "origin";
a.title.font_size = 5;
|
283beb1dc6af4de78b0ad9b787ab966b8f40a0ac | 449d555969bfd7befe906877abab098c6e63a0e8 | /3871/CH8/EX8.2/Ex8_2.sce | 46b4b909159c1bfdc1a66e17e579eba402b52767 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 946 | sce | Ex8_2.sce | //===========================================================================
//chapter 8 example 2
clc;clear all;
//variable declaration
V = 220; //voltage in V
I = 5; //current in A
Rp = 8800; //resistance of pressure in Ω
V1 = 6; //voltage excited in V
//calculations
P1 = V*I; //power consumed in current coil circuit in W
P2 = (V^2)/(Rp); //power consumed in pressure coil circuit in W
P = P1+P2; //total power consumed in W
P11 = V1*I; //power consumed in current coil circuit in W
P21 = (V^2)/(Rp); //power consumed in pressure coil circuit in W
PP = P11+P21; //total power consumed in W
//result
mprintf("total power consumed for direct load arrangement = %3.2f W",P);
mprintf("\ntotal power consumed for phanton loading with current circuit = %3.1f W",PP);
|
1e6ab9d9f88ccb95e41dd8ccd2fd50c88405e2c8 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1943/CH11/EX11.3/Ex11_3.sce | 92f75f60c473628906a3077629ea9a00204dd4c0 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,445 | sce | Ex11_3.sce |
clc
clear
//Input data
a=215//Current in A
v=210//Voltage in V
e=85//Efficiency in percent
q=11.8//Quantity of fuel supplied in kg/h
cv=43//Calorific value in MJ/kg
af=18//Air fuel ratio
w=560//Water in litres/h
tw=38//Temeparature in degree C
te=97//Temeparature in degree C
cp=1.04//Specific heat in kJ/kg.K
ta=30//Temeparature in degree C
l=32//Percentage lost
sw=4.187//Specific heat in kJ/kg.K
//Calculations
P=(a*v)/1000//Power in kW
BP=(P/(e/100))//Brake power in kW
E=(q/3600)*cv*1000//Energy supplied in kW
mg=(q/3600)*(1+af)//Rate of gases in kg/s
he=(mg*cp*(te-ta))+((w/3600)*sw*tw)//Heat carried away by exhaust gases in kW
hj=(l/100)*E//Heat lost to jacket cooling water in kW
pBP=(BP/E)*100//Percentage
pE=(E/E)*100//Percentage
phe=(he/E)*100//Percenatge
phj=(hj/E)*100//Percenatge
//Output
printf(' ENERGY BALANCE SHEET \n (in kW) (in percent)\n 1. Brake power %3.2f %3.2f \n 2. Heat carried away by exhaust gases %3.2f %3.2f \n 3. Heat lost to jacket cooling water %3.2f %3.2f \n 4. Heat loss unaccounted %3.2f %3.2f \n Total %3.2f %3.2f',BP,pBP,he,phe,hj,phj,(E-(BP+he+hj)),(((E-(BP+he+hj))/E)*100),E,(pBP+phe+phj+(((E-(BP+he+hj))/E)*100)))
|
1eefba8f8c7a2e745a4dc6e3c96f415b443769aa | 449d555969bfd7befe906877abab098c6e63a0e8 | /770/CH2/EX2.15/2_15.sce | 7e351006adefbff0ce441e76089f74ab8d55c9a3 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,682 | sce | 2_15.sce | clear;
clc;
// Example - 2.15
// Page number - 67
printf("Example - 2.15 and Page number - 67\n\n");
//Given
T = 250+273.15;//[K]
R = 8.314;//[J/mol*K]
P = 39.76;//[bar] Vapour pressure of water at T
P = P*10^(5);//[N/m^(2)]
Tc = 647.1;//[K] - Cricitical temperature
Pc = 220.55*10^(5);//[N/m^(2)] - Cricitical pressure
w = 0.345;//Acentric factor
M = 18.015;// Molecular weight of water
// Using peng-Robinson equation of stste
m = 0.37464 + 1.54226*w - 0.26992*w^(2);
Tr = T/Tc;
alpha = (1 + m*(1 - Tr^(1/2)))^(2);
a = ((0.45724*(R*Tc)^(2))/Pc)*alpha;//[Pa*m^(6)/mol^(2)]
b = (0.07780*R*Tc)/Pc;//[m^(3)/mol]
// Cubuc form of Peng-Robinson equation of stste is given by
// V^(3) + (b-(R*T)/P)*V^(2) - ((3*b^(2)) + ((2*R*T*b)/P) - (a/P))*V+b^(3) + ((R*T*(b^(2))/P) - ((a*b)/P) = 0;
// Solving the cubic equation
deff('[y]=f(V)','y=V^(3)+(b-(R*T)/P)*V^(2)-((3*b^(2))+((2*R*T*b)/P)-(a/P))*V+b^(3)+((R*T*(b^(2)))/P)-((a*b)/P)');
V_1 = fsolve(-1,f);
V_2 = fsolve(0,f);
V_3 = fsolve(1,f);
//The largest root is for vapour phase,
V_vap = V_3;//[m^(3)/mol] - Molar volume (saturated vapour)
V_vap = V_vap*10^(6)/M;//[cm^(3)/g]
printf(" The moar volume of saturated water in the vapour phase (V_vap) is %f cm^(3)/g\n",V_vap);
//The smallest root is for liquid phase,
V_liq = V_1;//[m^(3)/mol] - molar volume (saturated liquid)
V_liq = V_liq*10^(6)/M;//[cm^(3)/g]
printf(" The moar volume of saturated water in the liquid phase (V_liq) is %f cm^(3)/g\n",V_liq);
//From steam table at 250 C, V_vap = 50.13 [cm^(3)/g] and V_liq = 1.251 [cm^(3)/g].
printf(" From steam table at 250 C, V_vap = 50.13 [cm^(3)/g] and V_liq = 1.251 [cm^(3)/g]");
|
520d20e3f1eaf3812c4e6f26efc5be882b4a850d | d7087cf730b37f76170323e080c090f8094979ac | /test/eval_expr/a4.tst | 0df4e015093b0c5511ae51cb7fe9ce5cbf3f0b20 | [] | no_license | VladimirMeshcheriakov/42sh | 025dffe358b86f48eaf7751a5cb08d4d5d5366c4 | 52d782255592526d0838bc40269f6e71f6a51017 | refs/heads/master | 2023-03-15T17:26:20.575439 | 2015-06-26T12:44:05 | 2015-06-26T12:44:05 | null | 0 | 0 | null | null | null | null | UTF-8 | Scilab | false | false | 130 | tst | a4.tst | <cmd>
../build/42sh</cmd>
<ref>
bash</ref>
<stdin>
echo $((((1 + ((((1 - 42))))) / (435 * ((23 + 34) - 12) * 1) + 2)))
</stdin>
|
da1e48fd1008ee6a8f940acb156e6f85fecdd055 | 449d555969bfd7befe906877abab098c6e63a0e8 | /3836/CH15/EX15.2/Ex15_2.sce | 1bec40dcf45e21cefb9edff2a308943635e89fcf | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 259 | sce | Ex15_2.sce | clear
//
//Initialisation
f=50 //frequency
C=2*10**-6 //Capacitance
//Calculation
w=2*%pi*f //Angular Frequency
Xc=1/(w*C) //Reactance
//Result
printf("\n Reactance, Xl = %.2f KOhm",Xc/1000)
|
591fbefda1ee0c98d355174f5854f7a6b4fabefb | 449d555969bfd7befe906877abab098c6e63a0e8 | /75/CH4/EX4.9/ex_8.sce | 7c502a29939374e5887519946c674b6cadc5343a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 460 | sce | ex_8.sce | // PG (223)
deff('[y]=f(x)','y=exp(x)')
x=[-1.0 -0.6919 0.0310 0.7229 1.0]; // defining x
r3 = 0.996294 + 0.997955*x + 0.536722*x^2 + 0.176139*x^3;
norm(exp(x)-r3,'inf'); // cubic least squares approximation
deff('[y]=g(x)','y=0.994571+0.997308*x+0.542991*x^2+0.177347*x^3')
// c3=g(x);
x1=x(1,1);
(exp(x1)-g(x1))
x2=x(1,2);
(exp(x2)-g(x2))
x3=x(1,3);
(exp(x3)-g(x3))
x4=x(1,4);
(exp(x4)-g(x4))
x5=x(1,5);
(exp(x5)-g(x5))
|
2c0b888ffe3af926d2d31f43ac05ed97042ead33 | 449d555969bfd7befe906877abab098c6e63a0e8 | /2858/CH12/EX12.6/Ex12_6.sce | 18fb2ad9212f82c9451887b95f2d6d731b42271c | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 360 | sce | Ex12_6.sce | //example 12.6
clc; funcprot(0);
Qws=1005-250;
Qwp=250;
epsilon=0.65;
L=11;
Ds=1.5;
Es=14000;
Ap=%pi/4*1.5^2;
Ep=21e6;
Cp=0.04;
Db=1.5;
mus=0.3;
p=%pi*1.5;
Nc=9;
qp=105*Nc;
se1=(Qwp+epsilon*Qws)*L/(Ap*Ep);
se2=Qwp*Cp/(Db*qp);
Iws=2+0.35*sqrt(L/Ds);
se3=Qws/p/L*Ds/Es*(1-mus^2)*Iws;
se=se1+se2+se3;
disp(se*1000,"net settlement in mm");
|
7e5b77e846e5c748c7d2bb6dd9dedd7ce2bf50c2 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1991/CH8/EX8.16/16.sce | baa86909ff50ef7a047692f285df6bcd06d09b31 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 263 | sce | 16.sce | clc
clear
//input
c=65*10^-6 //capcacitor
v=12 //voltage
f=90 //frequency
//calculation
vmax=v*sqrt(2)//peak pd
qmax=c*vmax//from eqn Q=CV
irms=v*2*%pi*f*c//maximum charge from capacitor reactance
//output
printf("the maximum charge is %3.3f A",irms)
|
c9ad9fa3f68825362aae54f35acbe6cafa40be7c | 449d555969bfd7befe906877abab098c6e63a0e8 | /2048/CH11/EX11.4/mv_mac1.sce | ea499c83c2ab80bec7c016b70e0b54bfbd9e7e4a | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 1,315 | sce | mv_mac1.sce | // MacGregor's first control problem, discussed in Example 11.4 on page 213.
// 11.4
exec('mv.sci',-1);
exec('cl.sci',-1);
exec('cosfil_ip.sci',-1);
exec('zpowk.sci',-1);
exec('xdync.sci',-1);
exec('rowjoin.sci',-1);
exec('polsize.sci',-1);
exec('left_prm.sci',-1);
exec('t1calc.sci',-1);
exec('indep.sci',-1);
exec('seshft.sci',-1);
exec('makezero.sci',-1);
exec('move_sci.sci',-1);
exec('colsplit.sci',-1);
exec('clcoef.sci',-1);
exec('cindep.sci',-1);
exec('polmul.sci',-1);
exec('poladd.sci',-1);
exec('tfvar.sci',-1);
exec('l2r.sci',-1);
exec('transp.sci',-1);
exec('tf.sci',-1);
exec('covar_m.sci',-1);
exec('polyno.sci',-1);
// MacGregor's first control problem
A = [1 -1.4 0.45]; dA = 2; C = [1 -0.5]; dC = 1;
B = 0.5*[1 -0.9]; dB = 1; k = 1; int1 = 0;
[Sc,dSc,Rc,dRc] = mv(A,dA,B,dB,C,dC,k,int1);
[Nu,dNu,Du,dDu,Ny,dNy,Dy,dDy,yvar,uvar] = ...
cl(A,dA,B,dB,C,dC,k,Sc,dSc,Rc,dRc,int1);
// Simulation parameters for stb_disc.xcos
Tc = Sc; gamm = 1; [zk,dzk] = zpowk(k);
D = 1; N_var = 1; Ts = 1; st = 0;
t_init = 0; t_final = 1000;
[Tcp1,Tcp2] = cosfil_ip(Tc,1); // Tc/1
[Rcp1,Rcp2] = cosfil_ip(1,Rc); // 1/Rc
[Scp1,Scp2] = cosfil_ip(Sc,1); // Sc/1
[Bp,Ap] = cosfil_ip(B,A); // B/A
[zkp1,zkp2] = cosfil_ip(zk,1); // zk/1
[Cp,Dp] = cosfil_ip(C,D); // C/D
|
d370f2103b60d0a9b787af1dbc8aea1bf98197f3 | 449d555969bfd7befe906877abab098c6e63a0e8 | /14/CH9/EX9.3/example_9_3.sce | 583bc4af1095c90b09ca13dff7c6a2e5264c3a23 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 584 | sce | example_9_3.sce | //Chapter 9
//Page 236
//Example 9.3
//losscoeff
clear;clc;
I1 = 1;I2 = 0.8;
V3 = 1;pf1 =1;pf2 = pf1;pf3 = pf1;
Za = 0.04 + %i * 0.16;Ra = real(Za);
Zb = 0.03 + %i * 0.12;Rb = real(Zb);
Zc = 0.02 + %i * 0.08;Rc = real(Zc);
V1 = V3 + I1 * Za;disp(V1,'Voltage at bus 1,V1 in per unit')
V2 = V3 + I2 * Zb;disp(V2,'Voltage at bus 2,V2 in per unit')
disp('Transmission Loss Co-efficients')
B11 = (Ra + Rc) / (abs(V1) * pf1)^2;disp(B11,'B11 in per unit')
B12 = Rc / (abs(V1) * abs(V2) * pf1 * pf2);disp(B12,'B12 in per unit')
B22 = (Rb + Rc) / (abs(V2) * pf2)^2;disp(B22,'B22 in per unit')
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f4741f29c56616d87c4b0be29d74da16f38706a0 | 449d555969bfd7befe906877abab098c6e63a0e8 | /569/CH9/EX9.1/9_1.sci | c09ae6edd640da8a1d6c6bfb7d6af6ebcb034d90 | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 622 | sci | 9_1.sci | // calculating the length of mean free path
clc;
T=273+20;
P=101.3*10^3;
mfp=22.7*10^-6*T/P;
disp(mfp,'length of mean free path when pressure is one atmospheric pressure(m)')
P=133;
mfp=22.7*10^-6*T/P;
disp(mfp,'length of mean free path when pressure is one torr(m)')
P=133*10^-3;
mfp=22.7*10^-6*T/P;
disp(mfp,'length of mean free path when pressure is one micrometer of Hg(m)')
P=249.1;
mfp=22.7*10^-6*T/P;
disp(mfp,'length of mean free path when pressure is one inch of water(m)')
P=133*10^-6;
mfp=22.7*10^-6*T/P;
disp(mfp,'length of mean free path when pressure is 10^-3 micrometer of Hg(m)')
|
a4cd7ac2b71dfd6a2b6a7d80302dd736a01e5d33 | 449d555969bfd7befe906877abab098c6e63a0e8 | /1460/CH11/EX11.7/11_7.sce | c6c6aa050bd7b1cdf157e231115d4986cd2e864c | [] | no_license | FOSSEE/Scilab-TBC-Uploads | 948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1 | 7bc77cb1ed33745c720952c92b3b2747c5cbf2df | refs/heads/master | 2020-04-09T02:43:26.499817 | 2018-02-03T05:31:52 | 2018-02-03T05:31:52 | 37,975,407 | 3 | 12 | null | null | null | null | UTF-8 | Scilab | false | false | 315 | sce | 11_7.sce | clc
//initialization of variables
P=30 //lb/in^2
T=1000+460 //R
Pd=14.7 //lb/in^2
w=60 //lbm/sec
eta=0.95 //percent
R=53.3
gamma=1.35
cp=0.264
//calculations
V2s=sqrt(2*gamma*32.2*53.3*T*(1-(Pd/P)^(0.259))/(gamma-1))
V2=eta*V2s
Fn=w*(V2)/32.2
//results
printf("Thrust of the engine = %d ft/sec",Fn)
|
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