pierreqi/scilab_code · Datasets at Hugging Face

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Example2_5_3.sce

//Example 2.5.3 page 2.26 clc; clear; lamda = 850; sigma= 20; D_mat = 0.055/(3*10^5*lamda); sigma_m= sigma*1*D_mat; D_mat=D_mat*10^12; // in Ps... sigma_m=sigma_m*10^9; //in ns//// printf("The material Dispersion is %.2f Ps/nm-Km",D_mat); printf("\n\nThe Pulse spreading is %.4f ns/Km",sigma_m);

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clear; //clc(); // Example 8.14 // Page: 198 printf("Example-8.14 Page no.-198\n\n"); //***Data***// P = 100;//[psia] // Composition in liquid phase is x_a = 0.05;// Mole fraction of methane x_b = 0.40;// Mole fraction of butane x_c = 0.55;// mole fraction of pentane // We have to take the help of the following equations // ( x_a + x_b + x_c ) = 1 and ( y_a + y_b + y_c ) = 1 // ( y_a/x_a ) = K_a; ( y_b/x_b ) = K_b; and ( y_c/x_c ) = K_c; // We draw a straight line across figure 8.20 from 100psia to different temperatures like 0,5,10,15,20,25,30 degF and read the three K factors T = [15.8 0.087 0.024;16 0.105 0.026;16.2 0.115 0.03;16.8 0.13 0.035;17.2 0.15 0.04;17.8 0.17 0.045;18.2 0.175 0.0472727]; printf(" Calculations for the various assumed temperatures are given in the table below\n\n"); printf(" Temperature \t\t y_a \t\t y_b \t\t\t y_c \t\t\t y \n\n"); T_b = 0;//[F] Bubble point j=1; for i = 1:7 y_a = x_a*T(i,j); y_b = x_b*T(i,j+1); y_c = x_c*T(i,j+2); y = y_a + y_b + y_c; T_b = T_b + 5; printf(" %f \t\t %f \t\t %f \t\t %f \t\t %f\n ",T_b,y_a,y_b,y_c,y); end printf(" \n For the temperature 30 deg F the summation of the mole fractions in the vapor phase is close enough to unity, so, bubble point is 30 degF\n"); printf(" And compositions in the vapor phase are the values given in the above table corresonding to the temperature 30 deg F, i.e.\n\n"); printf(" y_methane = %f \n y_butane = %f \n y_pentane = %f",y_a,y_b,y_c);

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//clear// clear; clc; //Example 15.4 //Given N = 28; xF = 0.5/12; // [ft] yF = 0.035/12; //[ft] km = 26; // [Btu/ft-h-F] AT = 2.830; //[ft^2/ft] Ab = 0.416; //[ft^2/ft] hi = 1500; //[Btu/ft^2-h-F] G = 5000; //[lb/h-ft^2] Tavg = 130; //[F] Tw = 250; //[F] mu = 0.046; //[lb/ft-h], from Appendix 8 Cp = 0.25; //[Btu/lb-F], from Appendix 15 k = 0.0162; //[Btu/ft-h-F], from Appendix 12 ID_shell = 3.068/12; //[ft], from Appendix 5 OD_pipe = 1.9/12; //[ft], from Appendix 5 //cross sectional area of shell space Ac = %pi/4*(ID_shell^2-OD_pipe^2)-N*xF*yF //[ft^2] //The perimeter of air space Ap = %pi*ID_shell+AT; //[ft] //hydraulic radius rh = Ac/Ap; //[ft] //equivalent diameter De = 4*rh; //[ft] //Reynolds Number Nre = De*h/mu //In computing mu_w the resistance of the wall and the steam film //are considered negligible, so mu_w = 0.0528; //[lb/ft-h] Npr = mu*Cp/k //Using Fig. 15.17, the heat transfer factor is jh = 0.0031; ho = jh*Cp*G*(mu/mu_w)^0.14/Npr^(2/3); //[Btu/ft^2-h-F] //For rectangular fins, disreagrding the contribution of the ends of the fins to //the perimeter, Lp = 2L and S = Lyf, where yf is the fin thickness and L is the //length of the fin. Then, from Eq.(15.11) aFxF = xF*sqrt(2*ho/(km*yF)); //From Fig. 15.16 netaF = 0.93; Dt = 1.610/12; //[ft], from Appendix 5 DLbar = (OD_pipe-Dt)/log(OD_pipe/Dt); //[ft] Ai = %pi*Dt*1.0; //[ft^2] AF = AT-Ab; //[ft^2/ft] xw = (OD_pipe-Dt)/2; //[ft] //Using Eq.(15.10), the overall coefficient Ut = 1/(Ai/(ho*(netaF*AF+Ab))+(xw*Dt/(km*DLbar))+1/hi);//[Btu/ft^2-h-F] disp('Btu/ft^2-h-F',Ut,'The overall heat transfer coefficent is')

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# Depropanizer test (from old Hysim manual) units SI thermo = VirtualMaterials.Peng-Robinson thermo + propane isobutane n-butane isopentane n-pentane thermo + n-hexane n-heptane n-octane thermo + n-nonane n-decane thermo + water stab = Tower.Tower() stab.Stage_0 + 10 # twelve stages stab.LiquidPhases = 2 cd stab.Stage_0 l = Tower.LiquidDraw() l.Port.P = 1000 cond = Tower.EnergyFeed(0) wd = Tower.WaterDraw() estT = Tower.Estimate('T') estT.Value = 25 reflux = Tower.StageSpecification('Reflux') reflux.Value = 2 cd ../Stage_5 f = Tower.Feed() f.Port.T = 50 f.Port.P = 2000 f.Port.MoleFlow = 1000 f.Port.Fraction = .1702 .1473 .1132 .1166 .1066 .0963 .0829 .0694 .0558 .0417 .005 f.Port cd ../Stage_11 l = Tower.LiquidDraw() l.Port.P = 1100 l.Port.Fraction.n-BUTANE = .02 reb = Tower.EnergyFeed(1) estT = Tower.Estimate('T') estT.Value = 100 cd .. /overhead = Stream.Stream_Material() /overhead.In -> Stage_0.l.Port /bottoms = Stream.Stream_Material() /bottoms.In -> Stage_11.l.Port /stab.MaxOuterLoops = 40 TryToSolve = 1 # start calculation /overhead.Out /bottoms.Out copy /stab /overhead /bottoms paste / /overheadClone.Out /bottomsClone.Out

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//variable initialization u=1.68*10^-27; //mass of hydrogen atom (kg) m1=16; //mass of oxygen atom in terms u m2=1; //mass of hydrogen atom in terms of u I=1.48*10^-47; //moment of inertia of OH-radical (kg m^2) h_bar=1.054*10^-34; //Planck's constant (joule second) j=5; //energy level of OH-radical c=3*10^8; //speed of light (meter/second) h=6.626*10^-34; //Plank's constant (joule second) //(a) internuclear distance mu=((m1*m2)/(m1+m2))*u; //reduced mass of the molecule (kg) r=(sqrt(I/mu))*10^10; //internuclear distance of molecule (Å) //(b) angular momentum P=h_bar*sqrt(j*(j+1)); //angular momentum of molecule (joule second) //(c) angular velocity omega=P/I; //angular velocity of molecule (radian/second) //(d) wave number B=h/(8*%pi^2*I*c); //rotational constant (m-1) no=2*B*(j+1); //wave no. of line corresponding to transition j=5 to j=6 (m-1) //(e) energy absorbed E=c*h*no; //energy absorbed in the transition j=6 to j=5 (joule) printf("\n(a) r = %.3f Å\n(b) J = %.2e joule second\n(c) ω = %.2e radian/second\n(d) wave number = %.2e m-1\n(e) E = %.1e joule",r,P,omega,no,E);

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clc // Given that F = 680 // Net brake load in N N = 360 // d = 10// Bore in cm L = 15 // Stroke in cm T = 58 // Torque in Nm v = 300 // Speed in m/min n_m = 0.8 // Mechanical efficiency n_th = 0.4 // Indicated thermal efficiency c_v = 44 // Calorific value of gasoline in MJ/kg printf("\n Example 20.3\n") N = v/(2*L*(10^(-2))) BP = (2*%pi*T*N)/60000 IP = BP/n_m p_m = (IP*60)/(L*(%pi/4)*(d^2)*N*10^(-6)) m_f = (IP*3600)/(n_th*c_v*1000) bsfc = m_f/BP printf("\n Indicated power = %f kW\n Indicate mean effective pressure = %f kN/m^2\n Fuel consumption per kWh on brake power output = %f Kg/kWh",IP,p_m,bsfc)

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//Example 1.16 // order of dark band clc; clear; //given data : u=4/3;//referactive index of soap flim t=1.5D-6;//thickness of soap flim i=60;//incident angle in degree i=i*%pi/180;// incident angle in radian w=5D-7;// wavelength in m r=sin(i)/u;//sin of refracted angle R=asin(r);//refracted angle in radian n=2*u*t*cos(R)/w n=floor(n) disp(n,"order of dark band")

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// Example 9.4.4 page 9.14 clc; clear; output=-10; //laser output sensitivity=-25; //APD sensitivity L=2; //length in km sl=0.7; //loss correspond to one splice in dB fl=3.5; //fiber loss in dB/km connector_loss=1.6; saftey_margin=4; allowed_loss=output-sensitivity; splices_loss=L*sl; fiber_loss=L*fl; margin=allowed_loss-(splices_loss+fiber_loss+connector_loss+saftey_margin); printf("\nFinal margin is %.1f dB.",margin); printf("\n\nIf laser launches a optical power of 0 dBm then,\n"); output=0; //laser output sensitivity=-25; //APD sensitivity saftey_margin=7; allowed_loss=output-sensitivity; length_fiber= (allowed_loss-(splices_loss+connector_loss+saftey_margin))/fl; increase=length_fiber-L; printf("\nIncrease in the fiber length is %.2f km.",increase); //answer in the book is 2.28, deviation of 0.01

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function [sp]=%spasp(sp1,sp2) ij1=sp1(3);ij2=sp2(3);w1=sp1(2);w2=sp2(2); ij=[ij1;ij2];w=[w1,w2]; sp=sparse(w,ij);

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clc(); clear; //Given : m = 9.109*10^-31;// eletcron mass in kg e = 1.6*10^-19; // electron charge in C //T = (2*pi*m)/(B*e) , here B is not given T = (2*%pi*m)/e;// time in s printf("T = %.2f x 10^-11 / B ",T*10^11);

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SIEMENLUKU 123456 PELAAJIA 4 IHMINEN Spartacus TIETOKONE Batiatus TIETOKONE Glaber TIETOKONE Crassus

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errcatch(-1,"stop");mode(2);//caption:Find magnitude and phase angle of Z4 arm //Ex4.6 Z1=200//impedance of first arm(in ohm) Za=30//phase angle of first arm(in degree) Z2=250//impedance of second arm(in ohm) Zb=-40//phase angle of second arm(in degree) Z3=150//impedane of third arm(in ohm) Zc=0//phase angle of third arm(in degree) Z4=(Z2*Z3)/Z1 disp(Z4,'magnitude of Z4 arm(in ohm)=') Zd=Zb+Zc-Za disp(Zd,'phase angle of Z4 arm(in degree)=') exit();

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clear; clc; close; disp('x(-t) <--> X(-w)=X*(w)'); t=-10:0.1:10; u=[ones(1,find(t==0)) zeros(1,length(t)-find(t==0))]; a=gca(); plot(t,u); poly1=a.children.children; poly1.thickness=3; poly1.foreground=2; xtitle('u(-t)','t') w=-10:0.1:10; for i=1:length(w) if w(i)==0 then delta(i)=1; else delta(i)=0; end end Xw=%pi*delta'-ones(1,length(w))./(%i*w); disp( 'U[-w]=%pi*delta(w)-1/(%i*w)');

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//generate a random permutation of the integers from 1 to n function idx = randperm(n) number = rand(1, n); [tmp, idx] = gsort(number); endfunction

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spLItTEr uWe {} FiLTer S { } fiLTer jiY {Bgw oR nOT yiqopr or nOT PWVD } mCNM -> f gRoUpER p {aGgrEGate hPQ.uA } unGRoUPer hi { } groUPfiLtER TN {} merGEr O { moDULE Gle { BRanCheS qI } MOdULe S { brANcHes v F <= ::a6:F28:2:F:CFAA:1.251.149.2/67 Not tOZjd ( 234.194.33.54/0 ) } EXporT k }

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//Optical Fiber communication by A selvarajan //example 5.2 //OS=Windows XP sp3 //Scilab version 5.5.1 clc; clear all; //given eta=0.6//quantum efficiency Po=10*10^-6//optical power in W q=1.6*10^-19//charge of an elctron in columb lambda=0.85*10^-6//wavelength in m h=6.6*10^-34//planck's constant c=3*10^8//velocity of light in m/s Rl=50//load Resistance in ohm R=(q*eta*lambda)/(h*c)//responsivity in A/W I=R*Po//current in A V=Rl*I//Voltage in V mprintf("Responsivity=%f",R) mprintf("\nCurrent=%fuA",I*10^6)//multiplication by 1e6 to convert unit from A to uA mprintf("\nVoltage=%fmV",V*10^3)//multiplication by 1e6 to convert unit from V to mV

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43_10.sce

//Problem 43.10: For the circuit shown in Figure 43.9, determine the value of the secondary current I2 if E1 = 2/_0° volts and the frequency is 1000/pi Hz. //initializing the variables: E1 = 2; // in Volts thetae1 = 0; // in degrees f = 1000/%pi; // in Hz R1 = 4; // in ohm R2 = 16; // in ohm R3 = 16; // in ohm R4 = 50; // in ohm L = 10E-3; // in Henry M = 2E-3; // in Henry //calculation: w = 2*%pi*f //voltage E1 = E1*cos(thetae1*%pi/180) + %i*E1*sin(thetae1*%pi/180) //R1e is the real part of Z1e R1e = R1 + R2 + ((R3 + R4)*(M^2)*(w^2))/((R3 + R4)^2 + (w*L)^2) //X1e is the imaginary part of Z1e X1e = w*L - (L*(M^2)*(w^3))/((R3 + R4)^2 + (w*L)^2) Z1e = R1e + %i*X1e Z2e = R3 + R4 + %i*w*L //primary current, I1 I1 = E1/Z1e //E2 E2 = %i*w*M*I1 //secondary current I2 I2 = E2/Z2e printf("\n\n Result \n\n") printf("\n secondary current I2 is %.2E +(%.2E)i A",real(I2), imag(I2))

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2_1.sce

clear clc disp('Exa-2.1'); v1=60; v2=40 //Velocities of cars wrt to observer in km/hr vr=v1-v2; //relative velocity printf('The value of relative velocity is %4.f km/h.',vr);

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Ex5_13.sce

//Initilization of variables Wa=400 //lb Wb=200 //lb theta=30 //degrees //Calculations Ta=Wa*sind(theta) //lb Tb=Wb*sind(theta) //lb //Taking moment about point O P=(Tb*12+Ta*6)/24 //lb //Result clc printf('The value of Ta is %f lb and that of Tb is %f lb,also P is %f lb',Ta,Tb,P)

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EX3_30_B.sce

//Example 3.30.B clc; syms s t; x=laplace(exp(-5*t)); y=laplace(1); z=x*y; f=ilaplace(z); disp(f);

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Ex12_12.sce

//Fluid Systems - By - Shiv Kumar //Chapter 12- Reciprocating Pumps //Example 12.12 //To Find the Maximum Speed at which the Pump may run without seperation. clc clear //Given Data:- D=10; //Plunger Diameter, cm L=20; //Stroke Length, cm H_s=4; //Suction Head, m H_d=14; //Delivery Head, m d_s=4; //Diameter of Suction Pipe, cm l_s=6; //Length of Suction Pipe, m d_d=3; //Diameter of Delivery Pipe, cm l_d=18; //Length of Delivery Pipe, m p=7.85; //Pressure (below atm.) for seperation, N/cm^2 H_a=10.3; //Atmospheric Pressure Head, m of water //Data Used:- g=9.81; //Acceleration due to gravity, m/s^2 rho=1000; //Density of water, kg/m^3 //Computations:- d_s=d_s/100; //m d_d=d_d/100; //m D=D/100; //m L=L/100; //m a_s=(%pi/4)*d_s^2; //m^2 a_d=(%pi/4)*d_d^2; //m^2 A=(%pi/4)*D^2; //m^2 r=L/2; //m H_sp=p*100^2/(rho*g); //Pressure Head of water for seperation, m (below atmosphere) (Value given in textbook is wrong due to incorrect value of p is used) H_abs=H_a-H_sp; //Absolute Pressure Head of water for seperation, m H_as_by_omega2=(l_s/g)*(A/a_s)*r; //H_as/omega^2 omega=sqrt((H_sp-H_s)/H_as_by_omega2); //rad/s N_s=omega*60/(2*%pi); //rpm H_ad_by_omega2=(l_d/g)*(A/a_d)*r; //H_as/omega^2 omega=sqrt((H_sp+H_d)/H_ad_by_omega2); //rad/s N_d=omega*60/(2*%pi); //rpm //Selecting maximum speed, if N_s>N_d then N=N_s; else N=N_d; //Result:- printf("Hence, The Maximum Speed at which Pump should be Run is %.2f rpm\n",N) //The answer vary due to round off error

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// 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/02/Invert16.tst // File created by Matthew Walsh. load Invert16.hdl, output-file Invert16.out, compare-to Invert16.cmp, output-list in%B1.16.1 invert%B1.1.1 out%B1.16.1; // Set 01. set in %B0000000000000000, set invert 0, eval, output; // Set 02. set in %B0000000000000000, set invert 1, eval, output; // Set 03. set in %B1111111111111111, set invert 0, eval, output; // Set 04. set in %B1111111111111111, set invert 1, eval, output; // Set 05. set in %B0000000011111111, set invert 0; eval, output; // Set 06. set in %B0000000011111111, set invert 1; eval, output; // Set 07. set in %B1111111100000000, set invert 0; eval, output; // Set 08. set in %B1111111100000000, set invert 1; eval, output; // Set 09. set in %B0000111100001111, set invert 0; eval, output; // Set 10. set in %B0000111100001111, set invert 1; eval, output; // Set 11. set in %B1111000011110000, set invert 0; eval, output; // Set 12. set in %B1111000011110000, set invert 1; eval, output; // Set 13. set in %B0011001100110011, set invert 0; eval, output; // Set 14. set in %B0011001100110011, set invert 1; eval, output; // Set 15. set in %B1100110011001100, set invert 0; eval, output; // Set 16. set in %B1100110011001100, set invert 1; eval, output; // Set 17. set in %B0101010101010101, set invert 0; eval, output; // Set 18. set in %B0101010101010101, set invert 1; eval, output; // Set 19. set in %B1010101010101010, set invert 0; eval, output; // Set 20. set in %B1010101010101010, set invert 1; eval, output;

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prob_8.sce

//Problem 8 //calculate the wavelength of X-rays used clear clc d=2.81//interplanar spacing in A n=1//order of beam x=10//angle of first order beam with the incident beam y=x/2//angle of incident w=2*d*sind(y)// wavelength of X-rays used in A printf('wavelength of X-rays used = %.2f A',w)

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urazy.sce

clear clf clc y = [17 2; 25 3; 5 2; 8 7; 13 5; 4 35; 15 5] x = [1 2 3 4 5 6 7]; bar(x, y ); xgrid title([' Procentowy udział urazów wybranych części ciała podczas czyszczenia konia i jazdy konnej'], 'fontsize', 3) xlabel("strefa urazów gdzie: 1-głowa, 2-plecy, 3-brzuch, 4-dłoń, 5-ręka powyrzej dłoni, 6-stopa, 7-noga powyżej stopy") ylabel("%") legend('jazda konna','czyszczenie', 2)

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Example12_5.sce

//computation of molality from mass percent clear; clc; printf("\t Example 12.5\n"); //considering 100g of solution percent=35.4;//mass percent of H3PO4 H3PO4=97.99;//mol mass of H3PO4 n=percent/H3PO4;//moles of H3PO4 mH2O=(100-percent)/1000;//mass of solvent m=n/mH2O;//molality of H3PO4, molal printf("\t the molality of H3PO4 solution is : %4.2f m\n",m); //End

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// Test # 8 : For 1 output argument exec('./allpasslp2hp.sci',-1); [n]=allpasslp2hp(0.3,0.2); disp(n); //Scilab Output //n= 0.7159210 -1 //Matlab Output //n= 0.7159 -1.0000

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13_7.sce

clc c=30 b=15 a=10 Ka=0.3872 // from table 13.8 H=4 G=15 Pa=G*H^2*Ka/2 printf('The active force per unit length Pa = %f kN/m\n',Pa) printf(' The resultant will act at a vertical distance equal to H/3 = 4/3 = 1.33 m above \n the bottom of the wall and will be inclined at an angle of 15to the back face of the wall.')

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Chapter10_example5.sce

clc clear //Input data v=6.5;//The volume of fuel in the barrel in cc d=0.3;//The dimeter of fuel pipe line in cm l=65;//The length of the fuel pipe line in cm vi=2.5;//The volume of fuel in the injection valve in cc K=78.5*10^-6;//The coefficient of compressibility of the oil per bar p1=1;//The atmospheric pressure in bar p2=180;//The pressure due to pump in bar v3=0.1;//The pump displacement necessary for the fuel in cc e=0.75;//The effective stroke of the plunger in cm pi=3.141;//Mathematical constant of pi //Calculations V1=v+((pi*d^2)/4)*l+vi;//The total initial volume in cc V=K*V1*(p2-p1);//Change in volume due to compression in cc T=(V)+v3;//Total displacement of the plunger in cc L=T*(4/pi)*(1/(e^2));//Effective stroke of the plunger in cm //Output printf('(a) The total displacement of the plunger = %3.3f cc \n (b) The effective stroke of the plunger = %3.3f cm',T,L)

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funcprot(0); // Initialization of Variable function[dms]=degtodms(deg) d = int(deg) md = abs(deg - d) * 60 m = int(md) sd = (md - m) * 60 sd=round(sd*100)/100 dms=[d m sd] endfunction Long=75.0;//longitude in degrees GST=5+25.0/60+15.0/3600;//GST in hr LMT=5.0+40.0/60;//LMT in hr //calculation LST=GST-Long/15.0*9.8565/3600+LMT+9.8565/3600*(LMT); LST=degtodms(LST); disp(LST,"LST of next day in deg min sec"); clear()

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//Fiber-optics communication technology, by Djafer K. Mynbaev and Lowell L. Scheiner //Example 3.3.3 //windows 7 //Scilab version-6.0.0 clc; clear; //given L=5;//fiber length in km NA=0.275;//numerical aperture c=3E5;//speed of light in km n1=1.48;//refractive index p=2*c*n1; e=NA*NA; d=L*e; deltatsi=(d/p)*1E9;//pulse spreading in ns //answer vary due round-off deltatsi_by_L=(deltatsi/L)//pulse spreading per unit length in ns/Km//answer vary due round-off Maximum_bit_rate=1e3/deltatsi_by_L//maximum bit rate in Mbits/s//multiplication by 1e3 to conver unit from Gbits/s to Mbits per sec mprintf("\n maximum bit rate = %.1f Mbits/s",Maximum_bit_rate);//answer vary due to rounding

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fc=900*10^6 c=3*10^8 fdm=70 Yc=c/fc V=fdm*Yc//max. speed of the vehicle Vm=V*18/5//to convert max speed in kmph disp(Vm,'maximum speed of the vehicle in kmph')

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//(Welded and Riveted Joints) Example 8.7 //Refer Fig.8.17 on page 284 //ISA angle dimensions l1 x l2 x h (mm) l1 = 200 l2 = 100 h = 10 //Static force acting on the angle P (kN) P = 150 //Permissible shear stress for the weld tau (N/mm2) tau = 70 // //Distance of C.G. of weld2 from the C.G. of the angle y2 (mm) y2 = 71.8

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disp('In a college,120 mathematics students can opt for either French(F),German(G) or Russian(R)') n=120; //total number of students F=65; //number of students studying French G=45; //number of students studying German R=42; //number of students studying Russian FandG=20; //number of students studying French and German FandR=25; //number of students studying French and Russian GandR=15; //number of students studying German and Russian FandGandR=8; //number of students studying French,German and Russian disp('using inclusion-exclusion principle:') ForGorR=F+G+R-FandG-FandR-GandR+FandGandR; disp(ForGorR,'number of students studying French or German or Russian') FGnR=FandG-FandGandR; disp(FGnR,'number of students studying French and German but not Russian') FRnG=FandR-FandGandR ; disp(FRnG,'number of students studying French and Russian but not German') GRnF=GandR-FandGandR ; disp(GRnF,'number of students studying German and Russian but not French') OF=F-FGnR-FandGandR-FRnG ; disp(OF,'number of students studying Only French') OG=G-FGnR-FandGandR-GRnF; disp(OG,'number of students studying Only German') OR=R-FRnG-FandGandR-GRnF; disp(OR,'number of students studying Only Russian') k=n-ForGorR; disp(k,'number of students not studying any of the languages')

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<<<<<<< HEAD // Copyright (C) 2018 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author:Sonu Sharma, RGIT Mumbai // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in function [num, den] = zp2tf (z, p, k) //Converts zeros / poles to a transfer function. //Calling Sequence //[num, den] = zp2tf (z, p, k) //num = zp2tf (z, p, k) //Parameters //z: Zeros //p: Poles //k: Leading coefficient (Gain) //Num: Numerator coefficients of the transfer function //den: Denomenator coefficients of the transfer function //Description //It converts zeros / poles representation to transfer function representation. //Examples //z = [1 2 3] //p = [4 5 6] //k = 5 //[num, den] = zp2tf (z, p, k) //Output : // den = // // 1. - 15. 74. - 120. // num = // // 5. - 30. 55. - 30. funcprot(0); lhs = argn(1) rhs = argn(2) if (rhs < 3 | rhs > 3) error("zp2tf : Wrong number of input arguments.") end n = k*real(poly(z,"x")); d = real(poly(p, "x")); num = coeff(n); num = flipdim(num,2); den = coeff(d); den = flipdim(den,2); ======= function [num, den] = zp2tf (z, p, k) //Converts zeros / poles to a transfer function. //Calling Sequence //[num, den] = zp2tf (z, p, k) //num = zp2tf (z, p, k) //Parameters //z: Zeros //p: Poles //k: Leading coefficient //Num: Numerator of the transfer function //den: Denomenator of the transfer function //Description //This is an Octave function. //It converts zeros / poles to a transfer function. //Examples //z = [1 2 3] // p = [4 5 6] //k = 5 //[num, den] = zp2tf (z, p, k) //num = // // 5 -30 55 -30 // //den = // // 1 -15 74 -120 funcprot(0); lhs = argn(1) rhs = argn(2) if (rhs < 3 | rhs > 3) error("Wrong number of input arguments.") end select(rhs) case 3 then if(lhs==1) num = callOctave("zp2tf", z, p, k) elseif(lhs==2) [num, den] = callOctave("zp2tf", z, p, k) else error("Wrong number of output argments.") end end >>>>>>> 6bbb00d0f0128381ee95194cf7d008fb6504de7d endfunction

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// Exa 2.6 clc; clear; // Given data // Referring circuit shown in Fig. 2.11(a) B=200; // Current gain Icq = 100*10^-6; // Amperes ADM = 500; // Voltage gain for differential mode signal CMRR_db = 80; // in dB(Common mode rejection ratio) // Solution // Since gm = Icq/Vt therefore, gm = Icq/(25*10^-3); // for Vt = 25 mV printf('Using Eq. 2.50, we have ADM = -gm*Rc so from this we get Rc as '); Rc =abs(- ADM/gm); printf(' %d kΩ. \n ',Rc/1000); printf('Since CMRR = 80 dB converting it into non dB value so CMRR = '); CMRR = 10^(CMRR_db/20); printf(' %d. \n ',CMRR); printf('Using Eq. 2.55, we get value of Re as '); // CMRR = 1+ 2*gm*Re; therefore Re = (CMRR-1)/(2*gm); printf(' %.2f MΩ. \n ',Re/10^6);

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function ydot = f(t, y) ydot = 6 * t^4 + 5 * t^3 + 4 * exp(t); endfunction h = 0.01; y(1) = 0; t(1) = 0; for i=1:50 k1 = f(t(i), y(i)); k2 = f(t(i) + h/2, y(i) + h * k1 / 2); k3 = f(t(i) + 3*h/4, y(i) + 3*h*k2/4); k4 = f(t(i) + h, y(i) + 2*h*k1/9 + h*k2/3 + 4*h*k3/9); y(i+1) = y(i) + (7/24) * h * k1 + (1/4) * h * k2 + (1/3) * h * k3 + (1/8) * h * k4; t(i+1) = t(i) + h; end euler = y(51); // find exact value exact = 6 * t.^5/5 + 5 * t.^4/4 + 4 * exp(t) - 4; error = abs(exact - y);

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function x=cosm(a) // cosm - computes the matrix cosine //%CALLING SEQUENCE // x=cosm(a) //%PARAMETERS // a : square hermitian or diagonalizable matrix // x : square hermitian matrix //! // Copyright INRIA if type(a)<>1 then error(53),end if a==[] then x=[],return,end if norm(imag(a),1)==0 then x=real(expm(%i*a)) else x=0.5*(expm(%i*a)+expm(-%i*a)); end

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// Pole placement controller for magnetically suspended ball problem, discussed in Example 9.3 on page 331. // 9.1 exec('myc2d.sci',-1); exec('desired.sci',-1); exec('zpowk.sci',-1); exec('polsplit2.sci',-1); exec('polsize.sci',-1); exec('t1calc.sci',-1); exec('indep.sci',-1); exec('move_sci.sci',-1); exec('colsplit.sci',-1); exec('clcoef.sci',-1); exec('cindep.sci',-1); exec('polmul.sci',-1); exec('seshft.sci',-1); exec('makezero.sci',-1); exec('xdync.sci',-1); exec('left_prm.sci',-1); exec('rowjoin.sci',-1); exec('pp_basic.sci',-1); exec('polyno.sci',-1); exec('cosfil_ip.sci',-1); // Magnetically suspended ball problem // Operating conditions M = 0.05; L = 0.01; R = 1; K = 0.0001; g = 9.81; //Equilibrium conditions hs = 0.01; is = sqrt(M*g*hs/K); // State space matrices a21 = K*is^2/M/hs^2; a23 = - 2*K*is/M/hs; a33 = - R/L; b3 = 1/L; a1 = [0 1 0; a21 0 a23; 0 0 a33]; b1 = [0; 0; b3]; c1 = [1 0 0]; d1 = 0; // Transfer functions G = syslin('c',a1,b1,c1,d1); Ts = 0.01; [B,A,k] = myc2d(G,Ts); //polynomials are returned [Ds,num,den] = ss2tf(G); num = clean(num); den = clean(den); // Transient specifications rise = 0.15; epsilon = 0.05; phi = desired(Ts,rise,epsilon); // Controller design [Rc,Sc,Tc,gamm] = pp_basic(B,A,k,phi); // Setting up simulation parameters for basic.xcos st = 0.0001; // desired change in h, in m. t_init = 0; // simulation start time t_final = 0.5; // simulation end time // Setting up simulation parameters for c_ss_cl.xcos N_var = 0; xInitial = [0 0 0]; N = 1; C = 0; D = 1; [Tc1,Rc1] = cosfil_ip(Tc,Rc); // Tc/Rc [Sc2,Rc2] = cosfil_ip(Sc,Rc); // Sc/Rc [Tcp1,Tcp2] = cosfil_ip(Tc,1); // Tc/1 [Np,Rcp] = cosfil_ip(N,Rc); // 1/Rc [Scp1,Scp2] = cosfil_ip(Sc,1); // Sc/1 [Cp,Dp] = cosfil_ip(C,D); // C/D

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clc; clear; n0=10^16 //donor atoms in cm^-3 q=1.6*10^-19 //electron charge in J ni=1.5*10^10 //in cm^-3 Nd=10^16 //Donors added to silicon to make it n-type) in cm^-3 GT=2.25*10^10 //Thermal generation rate of carriers under equilibrium cm^-3/s gop=10^21 //in cm^-3/s tau_n=10^-6 //in s tau_t=2.5*10^-3 //transit time in s V=1 //in V //Calculation //a) alpha_r=GT/ni^2 tau_p=(alpha_r*n0)^-1 //b) delp=gop*tau_n //c) delI=(q*V*gop*tau_n)/tau_t mprintf("a)\n") mprintf("lifetime of both type of carriers= %g s\n",tau_p) mprintf("b)\n") mprintf("excess carrier concentration= %g cm^-3\n",delp) mprintf("c)\n") mprintf("Induced change in current= %.3f A",delI)

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//Rodríguez Montiel Moisés Ulises //2NM51 function y = interpolSplin(funcTab, x) [n, m] = size(funcTab) if(n <> 2) error("No es una función tabular") end if ~(isreal(funcTab)) error('Elementos no numericos o complejos en el arreglo.'); end if(~isreal(x)) error('El numero de x ingresado no es valido'); end valx = [] valy = [] for i=1:1:m valx(i) = funcTab(1, i) valy(i) = funcTab(2, i) end d = splin(valx, valy) y = interp(x, valx, valy, d) endfunction

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// sero.bas : demo de icse // calcul coefficients optimaux du modele simplifie 5ht-plaquette // ************************************************************** // // les doubles slash introduisent des commentaires // // contexte : tue les variables de nom reserve // Copyright INRIA exec('icse.contexte'); t0=0.d0; // instant initial tf=18.d1; // instant final dti=1; // premier pas de temps dtf=2; // second pas de temps ermx=1.d-9; // test d'arret absolu sur la valeur du second membre dans // la resolution de l'etat iu=[0,0,1]; // iu :indications sur la structure du controle // iu(1)=1 si l'etat initial depend du controle constant,0 sinon // iu(2)=1 si l'etat initial depend du controle variable,0 sinon // iu(3)=1 si le second membre depend du controle constant,0 sinon nuc=7; // nombre de parametres independants du temps nuv=0; // nombre de parametres dependants du temps ilin=2; // indicateur de linearite : // 0 pour un systeme non affine // 1 pour un systeme affine dont la partie lineaire n'est pas autonome // ilin=2 pour un systeme affine dont la partie lineaire est autonome nti=80; //nombre de pas de temps correspondant a dti (premier pas de temps) ntf=50; // nombre de pas de temps correspondant a dtf (second pas de temps) // si l'on utilise un seul pas de temps,on doit prendre ntf=0 ny=4; // dimension de l'etat a un instant donne nea=0; // nombre d'equations algebriques (eventuellement nul) itmx=10; // nombre maximal d'iterations dans la resolution de // l'equation d'etat discrete a un pas de temps donne nex=8; // nombre d'experiences effectuees nob=2; // dimension du vecteur des mesures pour une experience donnee // en un instant donne ntob=9; // nombre d'instants de mesure pour une experience donnee ntobi=6; // nombre d'instants de mesure correspondant a dti (premier // pas de temps) // ne pas modifier l'instruction suivante nu=nuc+nuv*(nti+ntf+1); // dimension du vecteur des parametres de controle // // uc(1,nuc) :controle constant ucref=[2.d-4,1.d-3,1.d-2,5.d-3,2.d-2,1.5d-1,3.d-2]; uc=.1*ucref; // uv(1,nuv*(nti+ntf)):controle variable //if nuv>0, uv(1,nuv*(nti+ntf))=0; end; // itu(1,nitu) :tableau de travail entier reserve a // l'utilisateur itu=[0]; // dtu(1,ndtu) :tableau de travail double precision reserve // a l'utilisateur dtu=[0.d0]; // // y0(ny) :etat initial // (inutile si iu(1) ou iu(2) est non nul) y0=[4.d1,0.d0,0.d0,0.d0]; // tob(1,ntob) :instants de mesure (compatibilite avec ntob // et ntobi) tob=[1.d1,2.d1,3.d1,4.d1,6.d1,8.d1,1.1d2,1.6d2,1.8d2]; binf=1.d-17*ones(1,nu);// borne inf des parametres bsup=1.d1*ones(1,nu);// borne sup des parametres // // termes utiles pour une dynamique lineaire ou une observation quadratique // b(1,ny)=0; // terme constant d'une dynamique lineaire // fy(ny,ny)=0; // derivee de la dynamique par rapport a l'etat // fu(ny,nuc+nuv)=0; // derivee de la dynamique par rapport au controle obs=[0,1,1,1;0,1,0,1]; // matrice d'observation obs(nob,ny) // // don(nex*ntob*nob) :mesures prealablement entrees dans le fichier // sero.mes.Il s'agit de donnees simulees avec // uc=[2.d-4,1.d-3,1.d-2,1.d-7,1.d-6,1.d-9,1.d-7] don=read('sero.mes',1,nex*ntob*nob,'(5d15.7)'); // nap=20; // nombre d'appels du simulateur imp=2; // niveau de debug pour optim large=100; // taille de nu au dela de laquelle on choisit un optimiseur // pour les problemes de grande taille (alg='gc' dans l'appel de optim) // exec('icseinit.sce'); [co,u,g,itv,dtv]=icse(u,'icsest',nap,imp);

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clc SG=0.9; h=1.2; //m g=9.81; //m/s^2 rho_w=1000; //kg/m^3 rho=SG*rho_w; //kg/m^3 P=rho*g*h/10^3; disp("Gauge pressure P=") disp(P) disp("kN/m^2")

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clc clear all; close; x1=[1,3,7,-2,5]; x2=[3,0,-1,2]; y=conv(x1,x2) x3=[2,-1,0,3]; z=xcorr(x1,x3) c=conv(x1,x3)

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//Example No. 3_05 //Decimal to binary //Pg No. 48 clear ; close ; clc ; d = 0.65 j = 1 ; while d ~= 0 fracp(j) = floor(d*2) //integral part of d*2 d = d*2 - floor(d*2) //Fractional part of d*2 j = j+1 ; decp(j-1) = d p = 1 for i = 1:j-2 if abs(d - decp(i))< 0.001 then //Condition for terminating the recurring binary equivalent by p = 0 //finding out if the new fractional part is equal to any of the previous fractonal parts break end end if p == 0 then break end end rec_p = fracp(i+1:j-1) //Recurring part rec_p = strcat(string(rec_p)) fracp = strcat(string(fracp)) disp(strcat( [fracp,rec_p] ),'Binary equivalent = ')

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//ex10.6 B_ac=100; r_e=12; R1=62*10^3; R2=22*10^3; R_S=1*10^3; R_E=1*10^3; C2=100*10^-6; //Base circuit impedance= parallel combination of R1, R2, R_S R_th=(R1*R2*R_S)/(R1*R2+R2*R_S+R_S*R1); //Resistance looking at emitter R_in_emitter=r_e+(R_th/B_ac); //resistance of equivalent bypass RC is parallel combination of R_E,R_in_emitter R=(R_in_emitter*R_E)/(R_E+R_in_emitter); f_c=1/(2*%pi*R*C2); disp(f_c,'critical frequency of bypass RC circuit in hertz')

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SplittEr Px {} fiLTEr ca { BiTAnD ( ) or nOT z NoT IN 130 } fIlTER kt {Not M nOt JA nOT THP Or noT w } m -> S gROUpeR zW {agGRegAte BItAnd(dP) AS GZWrb ,Q.R } ungRouPeR V { } gRoUpFILTeR ueWu {bd:fd:ec:Ec:ca:EE not IN AL Y ( W, 3.214.253.218, ) oR NOt biTor (181.220.0.213, bItoR (), ) 1B:da:D8:0A:fA:d6 >> u oR noT BItOr () Or r ( 27, f1, 0.254.250.8, R, +18231., ) or bItoR () } MErgEr B { EXPort wx }

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// Example 6.10 //power coupled clc; clear; close; tha=15;//in degree po=1;//in micro watt nc=(sind(tha))^2;// pf=nc*po*10^-6;//in watts disp(pf*10^9,"power coupled in nW is")

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//Example 17_10 clc(); clear; //To find the current in battery r1=3 //Units in Ohms r2=6 //Units in Ohms ra=(r1*r2)/(r1+r2) //Units in Ohms r3=2 //Units in Ohms r4=4 //Units in Ohms rb=r3+r4 //Units in Ohms r5=6 //Units in Ohms rc=(r5*rb)/(r5+rb) //Units in Ohms r6=9 //Units in Ohms r=r6+rc //Units in Ohms v=6 //Units in V i=v/r //Units in Ohms printf("The current in battery is I=%.2f A",i)

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clc t90=75*24*60*60 // time in sec T90=0.848 Hd=1.5*100 //in cm Cv=T90*Hd^2/t90 printf('Cv = %f cm^2/sec',Cv)

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//Example 3.8 //determine(a) maximum allowable current //(b) the corresponding remp. at the centre of wire and //at the outer surface of insulation //Given ri=1.3*10^-3 //m, radius of 10 gauge wire t=1.3*10^-3 //m, thickness of rubber insulation Ti=90 //C, temp. 0f insulation To=30 //C, ambient temp. h=15 //W/m^2 C, air film coefficient km=380 //W/m C, thermal cond. of copper kc=0.14 //W/m C, thermal cond. of rubber(insulation) Rc=0.422/100 //ohm/m, eletrical resistance of copper wire //NUMERIC CALCULATIONS Tcmax=90 //X, the maximum temp. in insulation ro=ri+t //m, outside radius of 10 gauge wire Sv=((Tcmax-To)*(2*kc/ri^2))/(log(ro/ri)+kc/(h*ro)) //from eq.(xii), Sv=I^2*rho/(%pi*ri^2) I=(%pi*ri^2*Sv/Rc)^0.5 //A, Current strength printf("maximum allowable current is %f A\n",I) //(b) at r=0 Tm=To+(ri^2*Sv/2)*(1/km+(log(ro/ri))/kc+1/(h*ro)) printf("remp. at the centre of wire is %f C\n",Tm) //at r=ro Tc=30+(ri^2*Sv/(2*kc))*(kc/(h*ro)) printf("The temprature at the outer surface of insulation is %f C",Tc)

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clc //Variable declaration lamda=0.842 n1=1 q=(8+(35/60))*(%pi/180) n2=3 d=1 //Calculations //n*lamda=2*d*sin(theta) //n1*0.842=2*d*sin(q) //n3*0.842=2*d*sin(theta3) //Dividing both the eauations, we get //(n2*lamda)/(n1*lamda)=2*d*sin(theta3)/2*d*sin(q) theta3=asin((((n2*lamda)/(n1*lamda))*(2*d*sin(q)))/(2*d)) d=theta3*180/%pi; a_d=int(d); a_m=(d-int(d))*60 //Result printf('sin(theta3) =%0.3f %0.3f',a_d,a_m)

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// Calculating the heat conducted across the former from winding to core clc; disp('Example 4.11, Page No. = 4.17') // Given Data t = 2.5;// Thickness of former (in mm) t_air = 1;// Thickness of air space (in mm) lw = 150*250;// The inner dimentions of the former of field coil (in mm square) h = 200;// Winding height (in mm) s_former = 0.166;// Thermal conductivity of former (in W per meter per degree celsius) s_air = 0.05;// Thermal conductivity of air (in W per meter per degree celsius) T = 40;// Temperature rise (in degree celsius) // Calculation of the heat conducted across the former from winding to core S = 2*(150+250)*h*10^(-6);// Area of path of heat flow (in meter square) R_former = t*10^(-3)/(S*s_former);// Thermal resistance of former (in ohm) R_air = t_air*10^(-3)/(S*s_air);// Thermal resistance of former (in ohm) R0 = R_former+R_air;// Since R_former and R_air are in series. Total thermal resistance to heat flow (in ohm) Q_con = T/R0;// Heat conducted (in Watts) disp(Q_con,'Heat conducted across the former from winding to core (in Watts)='); //in book answers is 182.6 Watts. The answers vary due to round off error

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frame_left_estr.enable ="off" Apoios =[] // Escolha dos nós da estrutura nos = SelectNodesInMat(coord) // Apaga a restrição nos nós selecionados que eventualmente já tivessem apoiados if ~isempty(Restricoes) then JahApoiados = [] for i=1:size(nos,"*") JahApoiado = vectorfind(Restricoes.data,coord(nos(i),:),"r") JahApoiados = [JahApoiados JahApoiado] end Restricoes = DeleteItemInArrayStructure(JahApoiados,Restricoes) end // Escolha das restrições if ~isempty(nos) then Labels = ["Translação em X"; "Translação em Y"; "Rotação em Z"]; Apoios = evstr(x_mdialog("Restrições de apoio",Labels,["%F";"%F";"%F"])) end if ~isempty(Apoios) & or(Apoios) then // Símbolo das restrições Symbol = ["<" "^" "p" "d" "v" "s" "o"] for i=1:size(nos,"*") // Seleciona o símbolo: e caso seja o 3, vira o 7 SymIndex = sum(find(Apoios')) if SymIndex==3 then; SymIndex=SymIndex+(length(find(Apoios'))-1)*4; end // Plota a restrição plot(coord(nos(i),1),coord(nos(i),2),Symbol(SymIndex),'MarkSize',15) gce().children.mark_background = [1 0 0] // Armazena a restrição na estrutura de manipuladores de polylines Restricoes = [Restricoes; gce().children] Restricoes($).user_data = Apoios' end BotoesAnalise(2:3).enable = "off"; nao_calculado = 1; BotoesMatrizes.enable = "off" for i=1:3; frequencias(i).string = ""; end; end if ~isempty(Restricoes) then BotoesGeomet(4).enable='on' end frame_left_estr.enable ="on"

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//x^2-13*x+36 clear; clc; close; x=poly(0,'x'); p=x^2-13*x+36; factors(p)

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// // Scilab ( http://www.scilab.org/ ) - This file is part of Scilab // Copyright (C) 2012-2012 - Scilab Enterprises - Bruno JOFRET // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // // function subdemolist = demo_gateway() demopath = get_absolute_file_path("arduino.dem.gateway.sce"); subdemolist = ["Potentiometer", "analog_read.dem.sce" ; "Led Push Button", "digital_read_write.dem.sce" ; "LED dimmer", "analog_write.dem.sce" ; "Openloop DC Motor", "motor.dem.sce"; "Encoder", "encodeur.dem.sce"; "Interrupt", "interrupt_compteur.dem.sce"; "Servo position control with PID", "asserv.dem.sce"; "ServoMotor", "servomotor.dem.sce"; "Examples in documentation", "exemples_livret.dem.gateway.sce"; ]; subdemolist(:,2) = demopath + subdemolist(:,2); endfunction subdemolist = demo_gateway(); clear demo_gateway; // remove demo_gateway on stack

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// Scilab code Ex6.1: Pg:247 (2008) clc;clear; i_p = 60; // Angle of polarization, degree mu = tand(i_p); // Refractive index of the material r = 90-i_p; // Angle of refraction, degree printf("\nThe refractive index of the material = %5.3f ", mu); printf("\nThe angle of refraction = %2d degree", r); // Result // The refractive index of the material = 1.732 // The angle of refraction = 30 degree

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ZA=15+%i*15.708; ZB=20+%i*0; V=200+%i*0; IA=V/ZA; disp('i) CURRENT (IA) is = '+string (IA) +' A '); IB=V/ZB; disp('ii) CURRENT (IB) is = '+string (IB) +' A '); I=IA+IB; disp('vi) TOTAL CURRENT (I) is = '+string (I) +' A ');

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//Given that the temperature has the same value on both the centrigrade and fahrenheit scales //(C/100)=((F-32)/180) //Putting C=F C=(-32/180)/((1/100)-(1/180));//Centrigade temperature in degree C F=C;//Fahrenheit temperature in degree Fahrenheit printf('The temperature which has the same value on both the centrigrade and fahrenheit scales is %i degree C = %i degree F',C,F)

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//example1.32 clc disp("Use the loop analysis") disp("From the current source branch,") disp("I3=1 A") disp("Applying KVL to the loops without current source we get,") disp("-6(I1)-4-5(I1)+5(I2)=0 i.e. -11(I1)+5(I2)=4 ..(1)") disp("-5(I2)+5(I1)-6-4(I2)-4(I3)=0 i.e. 5(I1)-9(I2)=10 (2)") disp("Solving, we get:") disp("-11(I1)+5((5I1-10)/9)=4") disp("Therefore, -99(I1)+25(I1)-50=36") i=86/(-74) format(7) disp(i,"Therefore, I1(in A)=") i=((5*(-1.1621))-10)/9 disp(i,"and, I2(in A)=") disp("Current through 5ohm in specified direction is,") i=(-1.7567+1.1621) disp(i,"I(5ohm)[in A]=I2-I1= -1.7567-(-1.1621)=") disp("As negative, current through 5ohm flows in opposite direction to that specified in the circuit.")

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// Example 9_2 clc;funcprot(0); // Given data // From Example 9_1 D=8;// The diameter of the steel pipe in inch z_in=100;// Elevation in m z_out=22;// Elevation in m L=2.2;// The distance in km g=9.807;// The acceleration due to gravity in m/s^2 nu=1.0*10^-6;// The kinematic viscosity in m/s^2 rho=1*10^3;// The density of water in kg/m^3 dp=0;// The static pressure in Pa // Calculation D=D*2.54*10^-2;// m deltah_f=(dp/(rho*g))+(z_in-z_out);// m // From equation 9.9 sqrtoffintoRe_D=((2*g*deltah_f*D^3)/(((nu)^2)*L*10^3))^(1/2); epsilon=5*10^-5;// physical height in m Re_D=-2*sqrtoffintoRe_D*log10(((epsilon/D)/3.7)+(2.51/(sqrtoffintoRe_D)));// Reynolds number Q=(%pi*D*nu*Re_D)/4;// The volume flow rate in m^3/s Q=(Q*60)/(3.782*10^-3)// The volume flow rate in gal/min printf("The volume flow rate,Q=%4.0f gal/min",Q);

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function s2=%sir(i,j,s1,s2) // %sir(i,j,M,r) <=> r(i,j)=M //! //s2(i,j)=s1 // if type(i)==10 then // s2('num'),s2('den'),sl('dt') [lhs,rhs]=argn(0) if rhs<>3 then error(21),end nams=['num','den','dt'] kf=find(i==nams) if kf==[] then error(21),end s2=s1;kf=kf+1 if size(s2(kf))<>size(j) then if kf<>4|prod(size(j))>1 then warning('inserted element '+i+' has inconsistent dimension') end end s2(kf)=j return end if type(i)==4 then i=find(i),end if type(j)==4 then j=find(j),end [m,n]=size(s2(2)) if type(i)<>1 then i=horner(i,l),end if type(j)<>1 then j=horner(j,c),end if s1==[] then // insertion d'une matrice vide if i==[]|j==[] then s=s2,return,end row=%f col=%f [m,n]=size(s2(2)) if and(size(i)==[-1 -1]) then row=%t else if and(i(:)==(1:m)') then row=%t,end end if and(size(j)==[-1 -1]) then col=%t else if and(j(:)==(1:n)') then col=%t,end end if ~row&~col then error('inserting [] in submatrix --> forbidden!'),end if row&col then s2=[],return,end if row then j1=[] for jj=1:n if ~or(jj==j) then j1=[j1 jj] ,end end s2=s2(:,j1) else i1=[] for ii=1:m if ~or(ii==i) then i1=[i1 ii] ,end end s2=s2(i1,:) end else [n,d]=s2(2:3),[ld,cd]=size(d),l=maxi(i),c=maxi(j) if l>ld then d(ld+1:l,:)=ones(l-ld,cd),ld=l,end if c>cd then d(:,cd+1:c)=ones(ld,c-cd),end n(i,j)=s1,[l,c]=size(s1),d(i,j)=ones(l,c) s2=tlist(['r','num','den','dt'],n,d,s2(4)) end

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//Finding of Loss of Head //Given q1=200; d1=150; d2=300; g=9.81; //To Find v1=200*(4/%pi)*(100/150)^2; disp(v1); v2=200*(4/%pi)*(100/300)^2; disp(v2); h=((v1-v2)^2)/20*g; h1=h/1000; disp(" Loss of Head ="+string(h1)+" meter of water");

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refs/heads/master

2020-12-24T13:18:20.656259

2014-09-29T16:14:00

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sci

aantalrollen.sci

function r = aantalrollen(t) r = ceil(t / 10) end plot(0:100, aantalrollen)

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/1364/CH14/EX14.3.3/14_3_3.sce

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FOSSEE/Scilab-TBC-Uploads

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refs/heads/master

2020-04-09T02:43:26.499817

2018-02-03T05:31:52

37,975,407

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null

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Scilab

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213

sce

14_3_3.sce

clc //initialisation of variables g= 32.2 //ft/sec^2 Z= 36 //ft r= 4 //in r1= 12 //in //CALCULATIONS w= (sqrt(2*g*Z/((r1/12)^2-(r/12)^2)))*(60/(2*%pi)) //RESULTS printf (' minimum speed= %.f rev/min',w)

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/NLP_Project/test/blog/bow/bow.12_4.tst

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no_license

mandar15/NLP_Project

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2020-05-20T13:36:05.842840

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bow.12_4.tst

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andreucm/essential_maths_roboticists

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refs/heads/master

2022-07-16T05:18:15.976563

2022-07-01T08:36:47

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erfc.sce

std_dev = 2; //in [cm]. x = [-10:0.1:10]; f = erfc(abs(x/(std_dev*sqrt(2)))); figure('BackgroundColor',[1 1 1]); plot(x,f); ph = gca(); // handle ph.x_label.text = 'O^t_L-O^e_L'; ph.y_label.text = 'L(O^t_L)'; ph.axes_visible = ["on","on","off"] ph.grid = [1,1]; ph.auto_scale="on";

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/NZFunctions/StatisticalFunctions/FLProdNZ-UM-01.tst

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kamleshm/intern_fuzzy

c2dd079bf08bede6bca79af898036d7a538ab4e2

aaef3c9dc9edf3759ef0b981597746d411d05d34

refs/heads/master

2021-01-23T06:25:46.162332

2017-07-12T07:12:25

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FLProdNZ-UM-01.tst

-- The intellectual and technical concepts contained herein are proprietary to Fuzzy Logix, LLC. -- and may be covered by U.S. and Foreign Patents, patents in process, and are protected by trade -- secret or copyright law. Dissemination of this information or reproduction of this material is -- strictly forbidden unless prior written permission is obtained from Fuzzy Logix, LLC. -- Functional Test Specifications: -- -- Test Category: Statistical Functions -- -- Last Updated: 05-30-2017 -- -- Author: <kamlesh.meena@fuzzyl.com> -- -- BEGIN: TEST SCRIPT -- BEGIN: TEST(s) -----******************************************************************************************************************************* ---FLProd -----**************************************************************** SELECT a.TickerSymbol, EXTRACT(YEAR FROM b.TxnDate) AS CalendarYear, COUNT(b.TxnDate) AS NumTxnDates, FLProd(1.0 + LN(b.ClosePrice/a.ClosePrice)) - 1.0 AS AnnualReturn FROM finStockPrice a, finStockPrice b WHERE a.TickerSymbol IN ('AAPL','HPQ','IBM','MSFT','ORCL') AND b.TickerID = a.TickerID AND b.DateIdx = a.DateIdx + 1 GROUP BY a.TickerSymbol, EXTRACT(YEAR FROM b.TxnDate) ORDER BY 1,2 LIMIT 20; --------------------------------------------------------------------- -----****************************************************************

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/2414/CH16/EX16.9/Ex16_9.sce

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no_license

FOSSEE/Scilab-TBC-Uploads

948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1

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Ex16_9.sce

clc; close(); clear(); //page no 530 //prob no. 16.9 c=3*10^8; //speed of light in m/s Td=400*10^-6 //s d=c*Td/2 //in m mprintf(' d=%.0f Km ',d*10^-3);

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/3129/CH16/EX16.6/Ex16_6.sce

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FOSSEE/Scilab-TBC-Uploads

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2020-04-09T02:43:26.499817

2018-02-03T05:31:52

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Ex16_6.sce

//Finding the Performance Parameters of a Three-Phase Induction Motor with frequency and voltage Control //Example 16.6(Page No- 714) clc clear //given data p = 4; Vl = 460; Va = Vl/sqrt(3); Vs = Va; f = 60;//Hz w = 2*%pi*f; w_b = 2*w/p; d = Va/w_b; R_r = 0.38; Rs = 0.66 Xs = 1.14; X_r = 1.71; //part(a) w_s = w_b; bet = 1; Va = d*w_s; s_m = R_r/(sqrt(Rs^2+bet^2*(Xs+X_r)^2)); w_m = w_s*(1-s_m); Tm = (3*Vs^2)/(2*w_s*(Rs+sqrt(Rs^2+(Xs+X_r)^2))); printf('(a)\t Maximum torque for 60Hz is %.2f N.m',Tm); //At f = 30Hz w_s = 2*2*%pi*30/4; bet = 30/60; Va = d*w_s; s_m = R_r/sqrt(Rs^2+bet^2*(Xs+X_r)^2); w_m = w_s*(1-s_m); Tm = (3*Va^2)/(2*w_s*(Rs+sqrt(Rs^2+bet^2*(Xs+X_r)^2))); printf(' \n \t Maximum torque for 30Hz is %.2f N.m',Tm); //part(b) //At 60Hz bet = 1; w_b = 2*(w/p); w_s = w_b; Va = d*w_s; s_m = R_r/((Xs+X_r)); w_m = w_s*(1-s_m); Tm = (Va/bet)^2*(3/(2*w_b*(Xs+X_r))); printf('\n (b)\t The maximum Torque for 60Hz is %.2f N.m',Tm); //At 30Hz bet = 0.5; w_b = 2*(w/p); w_s = 94.25; Va = 132.79; s_m = R_r/(bet*(Xs+X_r)); w_m = w_s*(1-s_m); Tm = (Va/bet)^2*(3/(2*w_b*(Xs+X_r))); printf('\n \t The maximum Torque for 30Hz is %.2f N.m',Tm);

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/NLP_Project/test/tweet/bow/bow.1_3.tst

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mandar15/NLP_Project

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2020-05-20T13:36:05.842840

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2021-04-16T08:52:19

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% Examples for the conversion of reaction equations to ordinary % differential equations. % Example taken from Feinberg (Chemical Engineering): species := {A1,A2,A3,A4,A5}; reac2ode { A1 + A4 <> 2A1, rho, beta, A1 + A2 <> A3, gamma, epsilon, A3 <> A2 + A5, theta, mue}; inputmat; outputmat; % Computation of the classical reaction matrix as difference % of output and input matrix: reactmat := outputmat-inputmat; % Example with automatic generation of rate constants and automatic % extraction of species. species := {}; reac2ode { A1 + A4 <> 2A1, A1 + A2 <> A3, A3 <> A2 + A5}; on rounded; species := {}; reac2ode { A1 + A4 <> 2A1, 17.3* 22.4**1.5, 0.04* 22.4**1.5 }; end;

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function [M]= impli(t,T,h,x) for i=1:x/h-1, u(i,1)=i*h*(1-i*h), end M=[0;u;0] A=2*eye(x/h-1,x/h-1) for j=1:x/h-2, A(j,j+1)=-1, A(j+1,j)=-1, end for k=1:T/t, plot([0;u;0]) halt() v=inv(eye(x/h-1,x/h-1)+t/h^2*A)*u M=[M [0;v;0]] u=v end endfunction

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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 3.3w //calculation of average velocity and average acceleration //given data A=1//given value of constant A B=4//given value of constant B C=-2//given value of constant C D=5//given value of constant D t=4//time(in s) t1=0//initial time(in s) for calculation of average velocity and average acceleration t2=4//final time(in s) for calculation of average velocity and average acceleration function x=f(t) x=(A*(t^3))+(B*(t^2))+(C*t)+D endfunction function a=f1(t) a=(6*A*t)+(2*B) endfunction //calculation v=derivative(f,t)//formula of velocity na=f1(t)//formula of acceleration x1=f(t1);//formula of position of the particle at t1 time x2=f(t2);//formula of position of the particle at t2 time vavg=(x2-x1)/(t2-t1);//formula of average velocity v1=derivative(f,t1);//formula of velocity of the particle at t1 time v2=derivative(f,t2);//formula of velocity of the particle at t2 time aavg=(v2-v1)/(t2-t1);//formula of average acceleration printf('\nthe velocity of particle at t=4 s is %3.2f m/s',v); printf('\nthe acceleration of particle at t=4 s is %3.2f m/s^2',na) printf('\nthe average velocity of the particle between t=0 s and t=4 s is %3.2f m/s',vavg); printf('\nthe average acceleration of the particle between t=0 s and t=4 s is %3.2f m/s^2',aavg);

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//To determine the best location of the substation for a given set of loads //Page 123 clc; clear; //Various loads and how they are positioned on the corners of a square of length 25km L1=5000; //(0,25) L2=8000; //(25,25) L3=3000; //(25,0) L4=6000; //(0,0) L=25;//Length of the square TL=L1+L2+L3+L4; // Total load X=((L1*0)+(L2*L)+(L3*L)+(L4*0))/TL // X coordinate Y=((L1*25)+(L2*L)+(L3*0)+(L4*0))/TL// Y coordinate printf('The Susbstation must be located at (%g km,%g km)\n',X,Y)

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clc // given data i=10/100.0 // rate Acost=90000 // cost of A in Rs Bcost=75000 // cost of B in Rs Acashfl=26000 // annual cash flow of A in Rs Bcashfl=26000 // annual cash flow of B in Rs nA=5 // useful life of A in years nB=4 // useful life of B in years NPVA=Acashfl*(((1+i)**nA) - 1)/(i*(1+i)**nA) - Acost // NPV for A NPVB=Bcashfl*(((1+i)**nB) - 1)/(i*(1+i)**nB)- Bcost // NPV for B printf( "\nThe NPV for A is Rs %.0f",NPVA) printf( "\nThe NPV for B is Rs %.0f",NPVB) AEA=i*NPVA/(1-(1+i)**(-nA)) AEB=i*NPVB/(1-(1+i)**(-nB)) printf( "\nThe AE for A is Rs %.0f",AEA) printf( "\nThe AE for B is Rs %.0f",AEB) printf( "\nThe machine B will have higher profitability")

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//Calculate the maximum voltage gain and bandwidth of multistage amplifier clear; clc; //soltion //FUNCTIONS function [z]=prll(r1,r2)//Function for the parallel combination of resistor z=r1*r2/(r1+r2); endfunction //given rin=10*10^6;//ohm //input resistance of JFET Rd=10*10^3;//ohm Rs=500;//ohm Rg=470*10^3;//ohm Rl=470*10^3;//ohm Cc=0.01*10^-6;//Farad Csh=100*10^-12;//Farad Cs=50*10^-6;//Farad rd=100*10^3;//ohm gm=2*10^-3;//S Rac2=prll(Rd,Rl); Rac1=prll(Rd,Rg); Req=prll(rd,prll(Rd,Rl)); Am=ceil(gm*Req); Am2=Am*Am; //Voltage gain of two stage amplifier printf("Voltage gain of two stage amplifier= %.0f\n",Am2); R_=prll(rd,Rd)+prll(Rg,rin); f1=1/(2*%pi*Cc*R_); //lower cutoff frequency f1_=f1/(sqrt(sqrt(2)-1)); f2=1/(2*%pi*Csh*Req); //upper cutoff frequency f2_=f2*(sqrt(sqrt(2)-1)); BW=f2_-f1_; printf("Bandwidth= %.1f kHz",BW/1000); //There is a slight error in f1 due to use of R'(here R_)=479 kΩ and in f2 due to approaximation of Req there is a slight variation

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clear; clc; printf("\t\t\tExample Number 2.2\n\n\n"); // multilayer cylindrical system // illustration2.2 // solution ID = 0.02;// [m] inner diameter of steel OD = 0.04;//[m] outer diameter of steel t = 0.03;//[m] thickness of asbestos insulation // system is like three concentric cylinders T1 = 600;// [degree celsius] inside wall temperature T2 = 100;// [degree celsius] outside insulation temperature Ks = 19;//[W/m degree celsius] heat transfer coefficient of steel Ka = 0.2;// [W/m degree celsius] heat transfer coefficient of asbestos // heat flow is given by per unit length Q_l = ((2*22*(T1-T2)/7)/((log(OD/ID)/Ks)+(log(0.1/OD)/Ka)));// [W/m] // above calculated heat flow is used to calculate the interface temperature // between the outside wall and the insulation Ta = Q_l*(log(0.1/OD)/(2*3.14*Ka))+T2;// [degree celsius] Ta is interface temperature printf("heat flow is given by %f W/m",Q_l); printf("\n the interface temperature is %f degree celsius ",Ta);

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exp_4_1.sce

A= input("Enter Amplitude: "); theta = input("Enter theta in radian "); F= input("Enter Frequency "); Fs= input("Enter sampling frequency "); n= 0:1:((2*Fs)/F); // here time period T is 1/f and f is F/Fs and we want signal for 2 cycle so 2*Fs/F. Xn= A*cos(2*%pi *(F/Fs)*n + theta); figure(1); plot2d(n,Xn); xlabel("n"); ylabel("X(n)"); title("Discrete time sine wave") E_Xn = sum(Xn.*Xn); // here we have to use '.*' not only '*' . disp("Energy is :"); disp(E_Xn); save('Energy.dat','Xn'); clear Xn;

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Example_4_3.sce

//Example 4.3 The following observations constitute a random sample from an unknown population clear; clc; x=[14 19 17 20 25]; n=5; M=sum(x)/n; s_d=sqrt(sum((x-M)^2)/4); SE=s_d/sqrt(n); disp(SE,"Standard Error =",s_d,"Standard Mean",M,"Mean");

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Expanding for base=2, level=4, reasons+features=same Refined variables=a,b ReasonFactory: same, code="same" SameReason.consider( "2a²-2b+2", "4a²-4b+4") = same form as 4a²-4b+4

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clc; e=-1.6*10^-19; //charge on electron in Coulomb q=20*10^-6; //charge in Coulomb r1=0.1; //r1 in m r2=0.05; //r2 in m Va=9*10^9*(q/r1); //calculating voltage at A Vb=9*10^9*(q/r2); //calculating voltage at B V=Va-Vb; //potential difference W=V*e; //calculating work done in joule disp(W,"Work done to take the electron from A to B in Joule = "); //displaying result

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Example24_3.sce

exec('electrostatics.sci', -1) //Given that q1 = +3.1*10^-9 //in C q4 = q1 q2 = -5.9*10^-9 //in C q5 = q2 q3 = -3.1*10^-9 //in C //Sample Problem 24-3 printf("**Sample Problem 24-3**\n") //Using gauss law flux = (q1+q2+q3)/Eo printf("The flux through the surface is equal to %fN.m^2/C", flux)

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// **** Purpose **** // This code performs dampped Fourier transform from t <--> omega. // **** Variables **** // [A]: real, Nx2 // <= input data as function of time. [time, value]. Time must be in // unit of hbar/eV (0.658fs) // [E_max]: real, 1x1 // <= max value of FT frequency, in unit of eV // [dE]: real, 1x1 // <= dE of FT frequency, in unit of eV // [func]: string, 'sin', 'cos', exp' // <= def of FT, sin(wt), cos(wt), or exp(iwt) // [FT_A]: real, Nx2 // => data in frequency domanin. [frequency, value]. omega in unit of eV // **** Version **** // 08/10/2015 // **** Comment **** // This code will output signed FT coefficients. Usually in singal process // we will only consider its spectrum density, i.e. (abs(FT_A)).^2. function FT_A=PIL_FT_damp(A,E_max,dE,func) [lhs,rhs]=argn(); if rhs==3 then func='sin' end A=A-repmat(A(1,:),length(A(:,1)),1); t=A(:,1); dt=t(2)-t(1) tot_w=fix(E_max/dE); FT_A=zeros(tot_w,2); FT_A(:,1)=linspace(0,E_max,tot_w)'; F_damp=(1-3*(t/t($)).^2+2*(t/t($)).^3) for n=1:tot_w select func case 'sin' FT_A(n,2)=sqrt(1/2*%pi)*sum((sin(FT_A(n,1)*t)).*F_damp.*A(:,2))*dt; case 'cos' FT_A(n,2)=sqrt(1/2*%pi)*sum((cos(FT_A(n,1)*t)).*F_damp.*A(:,2))*dt; case 'exp' FT_A(n,2)=sqrt(1/2*%pi)*sum((exp(%i*FT_A(n,1)*t)).*F_damp.*A(:,2))*dt; else disp('Error: PIL_FT_damp, wrong FT function!') abort; end end endfunction

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clear //Given h=6.625*10**-34 c=3*10**8 l=5600*10**-10 a=5 //Calculation E=(h*c)/l n=a/E //Result printf("\n Number of visible photons emitted per second is %0.2f *10**19 ",n*10**-19)

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//Chapter 15: Antennas for Special Applications //Example 15-26.1 clc; //Variable Initialization t1 = 0.3e-9 //Echo time off the top of pavement (s) t2 = 2.4e-9 //Echo time off bottom of pavement (s) t3 = 14.4e-9 //Echo time off bottom of water pocket (s) er_1 = 4 //Relative permittivity of pavement (unitless) er_2 = 81 //Relative permittivity of water pocket (unitless) c = 3e8 //Speed of light (m/s) //Calculations d1 = (t2-t1)*c/(2*sqrt(er_1)) d2 = (t3-t2)*c/(2*sqrt(er_2)) //Result mprintf("The thickness of pavement is %.2f m",d1) mprintf("\nThe thickness of water pocket is %.1f m",d2)

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function out=a(n) if (n==0) out=2*lambda/%pi; else out=-2/(n*%pi)*sin(n*(%pi-lambda)); end endfunction N=1000; t=linspace(0.01,5,4); lambda=%pi/2; theta=linspace(0,2*%pi,1000); p=100; for i=1:N somme=a(0)/2; for n=1:p somme=somme+a(n)*cos(n*theta)*exp(-n^2*t(i)); end drawlater; subplot(2,2,i); plot(theta,somme,'b'); set(gca(),'data_bounds',[0 2*%pi -0.2 1.2]); drawnow; end

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sce

fuglaaOWDodgeTrack.sce

Name=fuglaaOWDodgeTrack PlayerCharacters=ow-heavysurgerifle BotCharacters=ow-rotation.rot IsChallenge=true Timelimit=60.0 PlayerProfile=ow-heavysurgerifle AddedBots=ow-rotation.rot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=2 BotTeams=1 MapName=boxernobounds.map MapScale=2.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=3.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Overwatch, OW WeaponHeroTag=Soldier DifficultyTag=3 AuthorsTag=fuglaa BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Dodge and track GameVersion=1.0.8.0 ScorePerDistance=0.0 MBSEnable=true MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false [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 [Bot Profile] Name=ow-fast DodgeProfileNames=Short Strafes 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=ow-lawbringer SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Profile] Name=Bot Profile DodgeProfileNames=MidStrafes 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=ow-lawbringer SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Profile] Name=Bot Profile2 DodgeProfileNames=Long Strafes 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=ow-lawbringer SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Rotation Profile] Name=ow-rotation ProfileNames=ow-fast;Bot Profile;Bot Profile2 ProfileWeights=1.0;1.0;1.0 Randomized=true [Character Profile] Name=ow-heavysurgerifle MaxHealth=120.0 WeaponProfileNames=Heavy Surge Rifle;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=58.333332 CrouchHeightModifier=0.7 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=641.666687 MaxCrouchSpeed=350.0 Acceleration=16041.666992 AirAcceleration=0.0 Friction=0.0 BrakingFrictionFactor=0.0 JumpVelocity=700.0 Gravity=2.625 AirControl=0.12 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=true EnemyBodyColor=X=1.000 Y=1.000 Z=1.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=1.000 Z=1.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=170.334137 MainBBRadius=32.238731 MainBBHasHead=true MainBBHeadRadius=15.748805 MainBBHeadOffset=-5.249601 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=170.334137 ProjBBRadius=40.298412 ProjBBHasHead=true ProjBBHeadRadius=19.686007 ProjBBHeadOffset=-5.249601 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.0 JetpackFullFuelTime=0.0 JetpackFuelIncPerSec=0.1 JetpackFuelRegensInAir=false JetpackThrust=0.1 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.0 AbilityProfileNames=Run.abilsprint;;;Punch.abilmelee HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=0.9 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=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=0.000 Z=150.000 BrakingDeceleration=10500.0 VerticalSpawnOffset=0.0 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Character Profile] Name=ow-lawbringer MaxHealth=200.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=1.0 StepUpHeight=58.333332 CrouchHeightModifier=0.7 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=641.666687 MaxCrouchSpeed=350.0 Acceleration=16041.666992 AirAcceleration=0.0 Friction=0.0 BrakingFrictionFactor=0.0 JumpVelocity=700.0 Gravity=2.625 AirControl=0.12 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=true EnemyBodyColor=X=1.000 Y=1.000 Z=1.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=1.000 Z=1.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=153.140213 MainBBRadius=36.388447 MainBBHasHead=true MainBBHeadRadius=18.789669 MainBBHeadOffset=-6.263223 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=153.140213 ProjBBRadius=45.485558 ProjBBHasHead=true ProjBBHeadRadius=23.487087 ProjBBHeadOffset=-6.263223 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.0 JetpackFullFuelTime=0.0 JetpackFuelIncPerSec=0.1 JetpackFuelRegensInAir=false JetpackThrust=0.1 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.0 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=0.9 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 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=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=0.000 Z=150.000 BrakingDeceleration=10500.0 VerticalSpawnOffset=0.0 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Dodge Profile] Name=Short Strafes MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.2 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=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=MidStrafes MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.32 MaxLRTimeChange=0.35 MinFBTimeChange=0.25 MaxFBTimeChange=0.6 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.2 DamageReactionMinimumDelay=0.13 DamageReactionMaximumDelay=0.16 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.2 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Oppose TargetStrafeMinDelay=0.13 TargetStrafeMaxDelay=0.18 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.1 MaxCrouchTime=0.1 MinJumpTime=0.0 MaxJumpTime=0.0 LeftStrafeTimeMult=0.9 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Long Strafes MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.5 MaxLRTimeChange=1.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.2 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=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Heavy Surge Rifle Type=Hitscan ShotsPerClick=1 DamagePerShot=20.0 KnockbackFactor=0.1 TimeBetweenShots=0.11265 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.1 ChargeStartDamage=0.0 ChargeStartVelocity=X=0.100 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=0.1 ChargeTimeToCap=0.1 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=0.100 Y=0.000 Z=0.000 MuzzleVelocityMax=X=0.100 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=10.0 MaxHitscanRange=999999.0 GravityScale=0.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=25 AmmoPerShot=1 ReloadTimeFromEmpty=1.660547 ReloadTimeFromPartial=1.660547 DamageFalloffStartDistance=3500.0 DamageFalloffStopDistance=5833.333496 DamageAtMaxRange=10.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.379403 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=true ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=true DecalType=1 DecalSize=7.875 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=false SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=3.15 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=25 CancelReloadOnKill=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=51.0 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=false IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=true ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=0.1 DamageAtCenter=0.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.0 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,0.0,0.0 SpreadSCA=0.0,0.1,0.0,0.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=0.0,0.1,0.0,0.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=0.0,0.1,0.0,0.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=0.0,0.1,0.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.1 TimeToRecoilReset=0.1 AAMode=2 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=1.5 AADeadZone=0.0 AAFOV=75.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=true AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.01 TriggerBotFOV=0.1 StickyLock=false HeadLock=true 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 [Melee Ability Profile] Name=Punch MaxCharges=1.0 ChargeTimer=0.25 ChargesRefundedOnKill=0.0 DelayAfterUse=1.0 FullyAuto=false AbilityDuration=0.1 HurtboxRadius=229.485748 HurtboxDamage=30.0 HurtboxGroundKnockbackFactor=4.0 HurtboxAirKnockbackFactor=4.0 BlockAttackTimer=0.5 AbilityBlockedWhenAttacking=false AmmoPerShot=0 FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 AIUseInCombat=false AIUseOutOfCombat=false AIUseOnGround=false AIUseInAir=false AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=false AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Sprint Ability Profile] Name=Run MaxCharges=1.0 ChargeTimer=0.1 ChargesRefundedOnKill=0.0 DelayAfterUse=0.1 FullyAuto=false AbilityDuration=0.0 BlockAttackWhileSprinting=true AbilityBlockedWhenAttacking=false SpeedModifier=1.3 45DegreeSprint=true 90DegreeSprint=false 135DegreeSprint=false 180DegreeSprint=false TapToSprint=true Block45DegreesWhenSprinting=false AIUseInCombat=false AIUseOutOfCombat=false AIUseOnGround=false AIUseInAir=false AIReuseTimer=1.0 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=2000.0 AIMaxTargFOV=15.0 AIDamageReaction=false AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Map 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clc; p1=0.1; // pressure at state 1 in MPa p2=6; // Pressure at state 2 in MPa // (a).Pump work for water vf1=0.001043; // specific volume in m^3/kg wp=-vf1*(p2-p1)*10^3; // Pump work for water disp ("kJ",wp,"(a).Pump work for water ="); // (b).For steam h1=2675.5;// specific enthalpy in kJ/kg s1=7.3595;// specific entropy in kJ/kg K // From superheated steam table t2=675; // Temperature at state 2 in degree celcius h2=3835.3;// specific enthalpy in kJ/kg wc=-(h2-h1); // Compressor work for steam disp ("kJ/kg",wc,"(b).Compressor work for steam =");

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; get-value after sat (set-option :produce-models true) (set-logic QF_UF) (declare-fun x () Bool) (assert (= x false)) (check-sat) (get-value (x))

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//pathname=get_absolute_file_path('3.10.sce') //filename=pathname+filesep()+'3.10-data.sci' //exec(filename) //Seating capacity: c=500 //Heat requirement per person(in kcal/hr): q=50 //Enthalpy of water entering the pipe(in kcal/kg): h1=80 //Enthalpy of water leaving the pipe(in kcal/kg): h2=45 //Difference in elevation of inlet and exit pipe(in m): z=10 //Acceleration due to gravity(in m/s^2): g=9.81 //Heat to be supplied(in kcal/hr): Q=c*q //Heat lost by water(in kcal/kg): Ql=-Q //By SFEE: //Quantity of water circulated(in kg/hr): m=(Ql*10^3*4.18)/(g*z+(h2-h1)*10^3*4.18) printf("\nRESULT\n") printf("\nWater circulation rate = %f kg/min",m/60)

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// Exa 5.6 clc; clear; close; // Given data N=8;// Number of bits f=1*10^6;// in Hz T=1/f; Tc= N*T;// in second disp(Tc*10^6,"Time of conversion in micro second")

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//Caption:time_response_and_peak_overshoot //example 12.8 //page 521 s=%s; syms t; num=sym('8*(s+1)'); den=sym('(s^2+2*s+2)'); CL=num/den; disp(CL,"C(s)/R(s)="); //for unit step response R(s)=1/s; d=CL*(1/s); disp(d,"C(s)="); c=ilaplace(d,s,t); disp(c,"c(t)="); //for peak time we get tp=%pi/2 t=%pi/2 a=s*d; a=simple(a) Cmax=4*(1+1.414*exp(-t)*sin(t-(%pi/4))) Css=limit(a,s,0); disp(Css,"Css="); Mp=((Cmax-Css)/Css)*100 Mp=float(Mp) disp(Mp,"peak_overshoot=")

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clc,clear printf('Example 1.29\n\n') P=8 //Poles A=2 //Wave wound armature Z=480 //number of armature conductors I_a=200 I=I_a/A //Part(i) theta_m=0 //Geometric nuetral axis amp_turns_PP_d=Z*I*theta_m/360 //De-magnetising ampere-turns per pole amp_turns_PP_c=Z*I*(1/(2*P)-theta_m/360) //Cross-magnetising ampere-turns per pole printf('Part(i)\nDe-magnetising ampere-turns per pole is %.0f',amp_turns_PP_d) printf('\nCross-magnetising ampere-turns per pole is %.0f\n\n',amp_turns_PP_c) //Part(ii) theta_e2=6 //angle shift of brushes in degrees electrical theta_m2=theta_e2/(P/2) //angle shift of brushes in degrees mechanical amp_turns_PP_d2=Z*I*theta_m2/360 //De-magnetising ampere-turns per pole amp_turns_PP_c2=Z*I*(1/(2*P)-theta_m2/360) //Cross-magnetising ampere-turns per pole printf('Part(ii)\nDe-magnetising ampere-turns per pole is %.0f',amp_turns_PP_d2) printf('\nCross-magnetising ampere-turns per pole is %.0f',amp_turns_PP_c2)

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W=2*10^-6; Dp=1.25*10^-3; Tp=10^-6; Lp=sqrt(Dp*Tp); a=(W^2)/(2*(Lp^2)); //to prove a<<1 printf('\n The value of (W^2)/(2*(Lp^2)) is %f which is <<1',a); W=2*10^-6; We=1*10^-6; c=1/0.0010; d=1/0.000010; disp("γ=1/(1+((σn*W)/(σp*We)))"); b=1/(1+((c*W)/(d*We))); //say γ=b printf('\n The value of γ is %f',b);

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PL/SQL Developer Test script 3.0 17 -- Created on 15.08.2014 by ZHURAVOV_VB declare -- Local variables here cursor l_obj_cur is select distinct o.name from xxdoo_db_schemes_t s, xxdoo_db_objects_t o where 1=1 and o.type in ('TYPE') and o.scheme_id = s.id and s.name = 'Books'; begin -- Test statements here for o in l_obj_cur loop dbms_output.put_line('grant execute,debug on '||lower(o.name)||' to apps with grant option;'); end loop; end; 0 0

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clc clear disp("Example 8.8") printf("\n") disp("convert the following binary numbers to decimal") disp("a)11.101 b)0.0111 c)110.1101") //Given binary number i=1;w=1 bin=11.101 //separating integer part IP=floor(bin) IP1=IP //separating decimal part DP=modulo(bin,1) //converting decimal value to interger p=4 DP=DP*10^p //should change power of 10 as according to number of digits in decimal digit //storing each integer digit in I(i) while(IP>0) I(i)=modulo(IP,10); IP=floor(IP/10); i=i+1; end //storing each decimal digit in D(w) while(DP>0) D(w)=modulo(DP,2) DP=(DP/10) DP=floor(DP) w=w+1; end //to do zero padding of remaining erm of D(w) if(length(D)<p) q=length(D) for f=q+1 :p D(f)=0 end end if(IP1>0) for i=1:length(I)//checking whether it is a binary number or not if(I(i)>1) then disp('not a binary number') abort end end end if(IP1>0) IP=0 for i=1:length(I) //multipliying bits of integer part with their position values and adding IP=IP+(I(i)*2^(i-1)) end end DP=0 for z=1:length(D) //multipliying bits of decimal part with their position values and adding DP=DP+(D(z)*2^(-1*(length(D)+1-z))) end decimal=IP+DP //displaying the output printf("Decimal format is") disp(decimal)

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// Exa 3.7 clc; clear; close; // Given data I_Z1 = 20;// in mA I_Z1= I_Z1*10^-3;// in A I_Z2 = 30;// in mA I_Z2= I_Z2*10^-3;// in A V_Z1 = 5.6;// in V V_Z2 = 5.75;// in V del_IZ = I_Z2-I_Z1;// in A del_VZ = V_Z2-V_Z1;// in V r_Z = del_VZ/del_IZ;// in ohm disp(r_Z,"Resistance of zener diode in ohm is");

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//Theory Example