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//chapter 2 //Rrad=36.5ohm //Irms=Im/sqrt(2) printf("\n"); Im=1.22;//on applying Kvl Pavg=36.5*(1.122/sqrt(2))^2; printf("the average power is %gW",Pavg);
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//(Welded and Riveted Joints) Example 8.3 //Refer Fig.8.10 on page 279 //Width of the steel plates w (mm) w = 120 //Thickness of the steel plates t (mm) t = 12.5 //Maximum tensile stress sigmat (N/mm2) sigmat = 110 //Total length of the weld to be added at start and stop lExt (mm) lExt = 15
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clc,clear printf('Example 1.2\n\n') Pole=4 phi=21*10^-3 //flux produced by each pole in webers N=1120 //Speed of armature in r.p.m Coils=42 turns_per_coil=8 Turns=Coils * turns_per_coil Z=2*Turns //Number of armature conductors //Part(i) A1=Pole //no of parallel paths for lap winding E1=phi*N*Z*Pole/(60*A1) printf('(i) e.m.f generated is %.3f V',E1) //Part(ii) A2=2 //wave winding E2=E1 //as mentioned in the question N2=E2/(phi*Z*Pole/(60*A2)) //E=phi*N*Z*Pole/(60*A) printf('\n(ii) For wave-wound armature,above calculated e.m.f is generated at %.0f r.p.m',N2)
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clc; T1=1*10**-6; f=100*10**3; R1=10*10**3; R2=10*10**3; T=1/f; C1=T1/(0.69*R1); disp('pF',C1*10**12,"C1="); T2=T-T1; C2=T2/(0.69*R1); disp('pF',C2*10**12,"C2=");
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a='Siddhant'; k=input("Enter the key") encrypt=""; decrypt=""; for i=1:length(a) b=part(a,i) //disp(b) c=ascii(b); //disp(c) if c>=97 & c<=122 then c = c+modulo(k,26); if(c>122) c=c-26; end end if c>=65 & c<=90 then c = c+modulo(k,26); if(c>90) c=c-26; end end encrypt = encrypt+ascii(c); end disp(encrypt) for i=1:length(encrypt) b=part(encrypt,i) //disp(b) c=ascii(b); //disp(c) if c>=97 & c<=122 then c = c-modulo(k,26); if(c<97) c=c+26; end end if c>=65 & c<=90 then c = c-modulo(k,26); if(c<65) c=c+26; end end decrypt = decrypt+ascii(c); end disp(decrypt)
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// Filtrage Spatial: Filtre Gaussien function image_out=filtreGaussien(image) SizeX = size(image, 1); SizeY = size(image, 2); image_out = zeros(SizeX, SizeY); //calqueMedian = zeros(3, 3); for X = 3 : SizeX-2, for Y = 3 : SizeY-2, image_out(X, Y) = round((image(X-2, Y-2)+2*image(X-1, Y-2)+3*image(X, Y-2)+2*image(X+1, Y-2)+image(X+2, Y-2)+2*image(X-2, Y-1)+6*image(X-1, Y-1)+8*image(X, Y-1)+6*image(X+1, Y-1)+2*image(X+2, Y-1)+3*image(X-2, Y)+8*image(X-1, Y)+10*image(X, Y)+8*image(X+1, Y)+3*image(X+2, Y)+2*image(X-2, Y+1)+6*image(X-1, Y+1)+8*image(X, Y+1)+6*image(X+1, Y+1)+2*image(X+2, Y+1)+image(X-2, Y+2)+2*image(X-1, Y+2)+3*image(X, Y+2)+2*image(X+1, Y+2)+image(X+2, Y+2))/98); end end endfunction
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//Chapter-8, Example 8.9, Page 350 //============================================================================= clc clear //INPUT DATA D=0.1;//Outer diamter of the pipe in m Ta=30;//Ambient temperature of air degree C Ts=170;//Surface temperature in degree C e=0.9;//Emissivity //CALCULATIONS Tb=(Ts+Ta)/2;//Film temperature in degree C k=0.0321;//Thermal conductivity in W/m.K v1=(23.13*10^-6);//Kinematic viscosity in m^2/s b=0.00268;//Coefficient of thermal expansion in 1/K Pr=0.688;//Prantl number Ra=((9.81*b*D^3*(Ts-Ta)*Pr)/(v1^2));//Rayleigh number Nu=(0.6+((0.387*Ra^(1/6))/(1+(0.559/Pr)^(9/16))^(8/27)))^2;//Nussults number h=(Nu*k)/D;//Heat transfer coefficient in W/m^2.K Q=(h*3.1415*D*(Ts-Ta))+(e*3.1415*D*5.67*10^-8*((Ts+273)^4-(Ta+273)^4));//Total heat loss per meter length of pipe in m //OUTPUT mprintf('Total heat loss per meter length of pipe is %3.2f W/m',Q) //=================================END OF PROGRAM==============================
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function [x,y,typ]=vmm_4(job,arg1,arg2) // Copyright INRIA x=[];y=[];typ=[]; select job case 'plot' then standard_draw(arg1) case 'getinputs' then //** GET INPUTS [x,y,typ]=standard_inputs(arg1) case 'getoutputs' then [x,y,typ]=standard_outputs(arg1) case 'getorigin' then [x,y]=standard_origin(arg1) case 'set' then x=arg1; graphics=arg1.graphics model=arg1.model exprs=graphics.exprs while %t do [ok,Wts,exprs]=scicos_getvalue('Set VMM Block',['Weight Matrix'],list('vec',-1),exprs) if ~ok then break,end if ok then model.sim=list('vmm_c',5) model.opar=list(Wts) // model.in=ipsize(1) // model.in2=ipsize(2) // model.out=ipsize(1) // model.out2=size(Wts,2) graphics.exprs=exprs; x.graphics=graphics; x.model=model break; end end case 'define' then Wts=[1 0 0 0; 0 1 0 0; 0 0 1 0; 0 0 0 1] model=scicos_model() model.sim=list('vmm_c',5) model.in=-[1:4]' model.intyp=-ones(4,1) model.out=-[1:4]' model.outtyp=-ones(4,1) model.opar=list() model.blocktype='d' model.dep_ut=[%t %f] exprs=[sci2exp(Wts)] gr_i=['txt='' VMM 4x4 '';';'xstringb(orig(1),orig(2),txt,sz(1),sz(2),''fill'')'] x=standard_define([10 9],model, exprs,gr_i) end endfunction
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function [] = kiks_gui_robotvis(id) // Display mode mode(0); // Display warning for floating point exception ieee(1); // ----------------------------------------------------- // (c) 2000-2004 Theodor Storm <theodor@tstorm.se> // http://www.tstorm.se // ----------------------------------------------------- global("KIKS_FIRE_HDL","KIKS_GRIPPER_L_HDL","KIKS_GRIPPER_R_HDL","KIKS_GRIPPER_HDL","KIKS_NR_HDL","KIKS_LINVIS_GR_HDL","KIKS_LINVIS_HDL","KIKS_RBT_HDL","KIKS_RBTSENS_HDL","KIKS_RBTWHL_HDL","KIKS_RBTLMP_HDL","KIKS_RBTDIOD_HDL"); for j = 1:8 // !! L.9: Unknown function kiks_robotsenspatch not converted, original calling sequence used KIKS_RBTSENS_HDL(id,j) = kiks_robotsenspatch(id,j); end; // !! L.11: Unknown function kiks_robotdiodpatch not converted, original calling sequence used KIKS_RBTDIOD_HDL(id,1) = kiks_robotdiodpatch(id,[0.8,0.9,0.8]); // !! L.12: Unknown function kiks_robotdiodpatch not converted, original calling sequence used KIKS_RBTDIOD_HDL(id,2) = kiks_robotdiodpatch(id,[0.8,0.9,0.8]); // !! L.13: Unknown function kiks_robotwheelpatch not converted, original calling sequence used KIKS_RBTWHL_HDL = mtlb_i(KIKS_RBTWHL_HDL,id,kiks_robotwheelpatch(id)); // !! L.14: Matlab function sprintf not yet converted, original calling sequence used // !! L.14: Matlab function patch not yet converted, original calling sequence used KIKS_GRIPPER_HDL = mtlb_i(KIKS_GRIPPER_HDL,id,patch("Facecolor",[0.3,0.3,0.3],"EdgeColor","none","Erase","xor","tag",sprintf("@kheppatch %d",id))); // !! L.15: Matlab function sprintf not yet converted, original calling sequence used // !! L.15: Matlab function patch not yet converted, original calling sequence used KIKS_GRIPPER_L_HDL = mtlb_i(KIKS_GRIPPER_L_HDL,id,patch("Facecolor",[0.3,0.3,0.3],"EdgeColor","none","Erase","xor","tag",sprintf("@kheppatch %d",id))); // !! L.16: Matlab function sprintf not yet converted, original calling sequence used // !! L.16: Matlab function patch not yet converted, original calling sequence used KIKS_GRIPPER_R_HDL = mtlb_i(KIKS_GRIPPER_R_HDL,id,patch("Facecolor",[0.3,0.3,0.3],"EdgeColor","none","Erase","xor","tag",sprintf("@kheppatch %d",id))); // !! L.17: Unknown function kiks_robotpatch not converted, original calling sequence used KIKS_RBT_HDL = mtlb_i(KIKS_RBT_HDL,id,kiks_robotpatch(id)); // !! L.18: Unknown function kiks_robotlmppatch not converted, original calling sequence used KIKS_RBTLMP_HDL = mtlb_i(KIKS_RBTLMP_HDL,id,kiks_robotlmppatch(id)); // !! L.19: Matlab function sprintf not yet converted, original calling sequence used // !! L.19: Matlab function patch not yet converted, original calling sequence used KIKS_LINVIS_HDL = mtlb_i(KIKS_LINVIS_HDL,id,patch("Facecolor",[0.25,0.3,0.35],"EdgeColor","none","Erase","xor","tag",sprintf("@kheppatch %d",id))); // !! L.20: Matlab function sprintf not yet converted, original calling sequence used // !! L.20: Matlab function patch not yet converted, original calling sequence used KIKS_LINVIS_GR_HDL = mtlb_i(KIKS_LINVIS_GR_HDL,id,patch("Facecolor",[0.5,0.65,0.6],"EdgeColor","none","Erase","xor","tag",sprintf("@kheppatch %d",id))); // !! L.21: Matlab function sprintf not yet converted, original calling sequence used // !! L.21: Matlab function patch not yet converted, original calling sequence used KIKS_FIRE_HDL = mtlb_i(KIKS_FIRE_HDL,id,patch("Visible","off","Facecolor",[1,0.4,0.4],"EdgeColor","none","Erase","xor","tag",sprintf("@kheppatch %d",id))); endfunction
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// Test #6 : Input Argument #2 range test exec('./allpassbpc2bpc.sci',-1); [n,d]=allpassbpc2bpc([0.3,0.1],[-1.4,0.9]); //!--error 10000 //Wt must lie between -1 and 1 //at line 46 of function allpassbpc2bpc called by : //[n,d]=allpassbpc2bpc([0.3,0.1],[-1.4,0.9]);
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1_4.sce
clc //initialisation of variables clear spo= 0.9 h= 3 //ft d= 2 //ft w= 62.4 //lb/ft^3 H= 0.71 //ft //CALCULATIONS do= spo*w de= w*d bc= do*h Pt= (bc*(h/2)+bc*d+de*(d/2))*(h+d) y= (bc*(h/2)+bc*d+de*(d/2)*(d/3))*(h+d)/Pt+H //RESULTS printf("Total pressure = %d lb",Pt) printf ('\n position of centre of ressure above the base = %.2f ft position of centre of pressure above the axis ',y)
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//clc() m = 1;//kg percent1 = 20;//% mwaterin = m * percent1 / 100; mdrysolid = m - mwaterin; percent2 = 2.44;//% mout = mdrysolid / (1 - percent2/100); mwaterout = mout - mdrysolid; mremoved = mwaterin - mwaterout; percentremoved = mremoved * 100 / mwaterin ; disp("kg",mremoved,"weight of water removed = ") disp("%",percentremoved,"percentage of water removed = ")
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// Additional solved numerical questions , Example(set 1) 2 , pg 348 l=0.7*10^-3//length(in m) E=8.8*10^10//youngs modulus(in N/m^2) d=2800//density(in kg/m^3) p=1//fundamental mode n= p*sqrt(E/d)/(2*l) //natural frequency printf("Fundamental frequency of quartz crystal)\n") printf("n=%.2f Hz",n)
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// Test # 1 : No Input Arguments exec('./allpasslp2lp.sci',-1); [n,d]=allpasslp2lp(); //!--error 10000 //Number of input arguments should be 2 //at line 28 of function allpasslp2lp called by : //[n,d]=allpasslp2lp();
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// 08.05.21 function Drwline(varargin) global Wfile FID MilliIn PenThick PenThickInit; Nall=length(varargin); Thick=0; Tmp=varargin(Nall); if type(Tmp)==1 & length(Tmp)==1 Thick=round(varargin(Nall)*PenThickInit); Str='\special{pn '+string(Thick)+'}%'; if Wfile=='default' mprintf('%s\n',Str); else mfprintf(FID,'%s\n',Str); end Nall=Nall-1; end for N=1:Nall Tmp=varargin(N); Pdata=Flattenlist(Tmp); for II=1:length(Pdata) Clist=MakeCurves(Op(II,Pdata)); DinM=Dataindex(Clist); for n=1:size(DinM,1) Tmp=DinM(n,:); Data=Clist(Tmp(1):Tmp(2),:); Mojisu=0; for I=1:size(Data,1) Tmp=Data(I,:); X=round(MilliIn*Tmp(1)); X=string(X); Y=-round(MilliIn*Tmp(2)); Y=string(Y); Str='\special{pa '+X+" "+Y+'}'; if Wfile=='default' mprintf('%s',Str); else mfprintf(FID,'%s',Str); end Mojisu=Mojisu+length(Str); if Mojisu>80 if Wfile=='default' mprintf('%c\n','%'); else mfprintf(FID,'%c\n','%'); end Mojisu=0; end end if Mojisu~=0 if Wfile=='default' mprintf('%s\n','%'); else mfprintf(FID,'%s\n','%'); end end; if Wfile=='default' mprintf('%s\n','\special{fp}%'); else mfprintf(FID,'%s\n','\special{fp}%'); end end end end; Str='%'; if Thick>0 Tmp=PenThick/PenThickInit; // modified Setpen(Tmp); end endfunction
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clc; clear all; disp("Boundary layer thickness") //uU=X //y/delta=Y //X=2*Y-Y^2; L=1.5;//m length of plate w=1;// m width of plate v=0.12;// m/s velocity of water mu=10^(-3);// N-s/m^2 U=0.12;//m/s free stream velocity rho=1000;//kg/m^3 density of water ReL=rho*U*L/mu; delta=5.48*L*1000/(ReL)^0.5;//mm disp("mm",delta,"thickness of boundary layer =") Cf=1.46/((ReL)^0.5);// coefficent of drag disp(Cf,"Coefficient of drag =")
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function K=lqg(P,r) // returns the (strictly proper) lqg (H2) controller // for the augmented plant P [A,B1,B2,C1,C2,D11,D12,D21,D22]=smga(P,r); if norm(D11,1) <> 0 then warning('lqg: D11 is not zero! (set to zero)');end //if norm(D22,1) <> 0 then warning('lqg: D22 is not zero!');end dom=P(7); if dom=[] then warning('lqg: time domain unspecified, assumed continuous'); dom='c';end P12=syslin(dom,A,B2,C1,D12); Kc=lqr(P12); P21=syslin(dom,A,B1,C2,D21); Kf=lqe(P21); P22=syslin(dom,A,B2,C2,D22); K=obscont(P22,Kc,Kf);
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//2.22 clc; Vm=230*2^0.5; Vdc=2*Vm/%pi*cosd(30); R=Vdc/4; printf("dc value of voltage = %.1f V", Vdc) IL=4; I=2*2^0.5/%pi*IL; P_input_active=230*I*cosd(30); printf("\n Active input power= %.2f W", P_input_active) P_input_reactive=230*I*sind(30); printf("\n reactive input power= %.2f Vars", P_input_reactive) P_input_appearent=230*I; printf("\n Active input power= %.2f VA", P_input_appearent) disp('When freewheeling diode is present') Vm=230*2^0.5; Vdc=Vm/%pi*(1+cosd(30)); printf("dc value of voltage = %.1f V", Vdc) IL=Vdc/R; I=2*2^0.5/%pi*IL*cosd(15); P_input_active=230*I*cosd(15); printf("\n Active input power= %.2f W", P_input_active) P_input_reactive=230*I*sind(15); printf("\n reactive input power= %.2f Vars", P_input_reactive) P_input_appearent=230*I; printf("\n Active input power= %.2f VA", P_input_appearent) disp('When Th3 get open circuit') Vdc=230/(2^0.5*%pi)*(1+cosd(30)); printf("dc value of voltage = %.3f V", Vdc) Idc=Vdc/R; printf("\nAverage dc output current = %.2f A", Idc)
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funcprot(0) xdel(winsid()); //------------------------------------------------------------------------- //------------------------------------------------------------------------- //-------------------- DM maths - probabilité ------------------------- //----------------- Lienardy Morgan - Tika Jihade --------------------- //------------------------------------------------------------------------- //------------------------------------------------------------------------- //------------------------------------------------------------------------- //-------------------------- Fonctions -------------------------------- //------------------------------------------------------------------------- //Genere N nombres de loi uniforme entre 0 et 1 function nombres=genLoiUniform(N) //Matrice colonne contenant nos N nombres de la loi uniforme nombres=grand(1,N,"unf",0,1) endfunction //------------------------------------------------------------------------- //Genere N nombres de loi de Poisson avec comme parametre lambda function nombres=genLoiPoisson(N,lambda) nombres=grand(1,N,"poi",lambda) endfunction //------------------------------------------------------------------------- //Genere N nombres de loi Normale avec comme parametres l'esperance 'm' et l'ecart type 'sigma' function nombres=genLoiNormale(N,m,sigma) nombres=grand(1,N,"nor",m,sigma) endfunction //------------------------------------------------------------------------- //Genere N nombres suivant la fonction scilab 'rand' function nombres=genRandLoiUniform(N) nombres=rand(1,N) endfunction //------------------------------------------------------------------------- //Realise le test du Chi2 pour la loi de Poisson avec N nombres (param lambda)) //nbClasses represente le nombre de classes que l'on souhaite avoir pour le test //l'intervalle est [ plus petite valeur obtenue ; plus grande valeur obtenue+1 ] function b=testChi2LoiPoisson(N, lambda, nbClasses) nombres=genLoiPoisson(N,lambda); mini=int(min(nombres)); maxi=int(max(nombres))+1; b=testChi2(nombres,'poi',mini,maxi,nbClasses) endfunction //------------------------------------------------------------------------- //Realise le test du Chi2 pour la loi Normale avec N nombres (param m, sigma) //function b=testChi2LoiNormale(N, m, sigma) // nombres=genLoiNormale(N,m, sigma); // mini=int(min(nombres)); // maxi=int(max(nombres))+1; // b=testChi2(nombres,'nor',mini,maxi,nbClasses) //endfunction //------------------------------------------------------------------------- //Realise le test du Chi2 //nombres : la matrice contenant des nombres que l'on souhaite tester // loi : La loi que ces nombres suivent //borneInf et borneSup : les bornes pour le decoupage des classes //nbClasses : Le nombres de classes que l'on souhaite avoir function boolean=testChi2(nombres, loi, borneInf, borneSup, nbClasses) //p doit avoir 'nbClasses' colonnes //borneInf et borneSup representent l'intervalle des nombres aléatoire //nbClasses est le nombre de classes que l'on souhaite avoir. Le decoupage se fait de maniere automatique //contient les valeurs du chi2 pour un seuil a 5% (de 1 a 14) resultChi2_5=[3.841 5.991 7.815 9.488 11.07 12.592 14.067 15.507 16.919 18.307 19.675 21.026 22.362 23.685] classes=zeros(1,nbClasses) pas=(borneSup-borneInf)/nbClasses; //ces boucles permettent de decouper les nombres en classes for i=1:size(nombres,2) for b=0:nbClasses-1 if b~=nbClasses-1 then if nombres(1,i)>=borneInf+b*pas & nombres(1,i)<borneInf+(b+1)*pas then classes(1,b+1)=classes(1,b+1)+1; break end else if nombres(1,i)>=borneInf+b*pas & nombres(1,i)<=borneInf+(b+1)*pas then classes(1,b+1)=classes(1,b+1)+1; break end end end end disp(classes) //calcul de la distance D² D2 = 0; //Ici on determine 'p' en fonction de la loi if loi=='uni' then p=ones(1,nbClasses)*(1/nbClasses); end if loi=='poi' then p=zeros(1,nbClasses); moy=0; for i=1:nbClasses moy=moy+classes(1,i)*i end moy=moy/size(nombres,2); disp(moy) for k=1:nbClasses p(1,k)=exp(-moy)*(moy.^k)/factorial(k); end end if loi=='nor' then end disp(p) // On somme les distances de chaque classe for i=1:nbClasses D2=D2+((classes(1,i)-size(nombres,2)*p(1,i))^2) / (size(nombres,2)*p(1,i)) end disp('D2 : ',D2) disp('Valeur du seuil : ',resultChi2_5(nbClasses-1)) //on compare D² et la valeur du seuil (rappel : 5%) if D2<resultChi2_5(nbClasses-1) then boolean="L hypothese initiale est valide, donc on l a garde"; else boolean='On observe un evenement qui ne peut se produire que rarement, on rejette donc l hypothese initiale'; end endfunction //------------------------------------------------------------------------- //Exercice2 - fonction qui prend en parametre une distance 's', une periode (en sec)'T' et le nombre de mouvement 'n' // Simule une marche aleatoire dans 2 sens : gauche ou droite d'une distance 's' qui se repete toutes les T secondes 'n' fois function X=marcheAlea1D(s,T,n) //Avec s la longueur du deplacement pour un lancé //Avec T la periode en seconde du lancé de piece //Avec n le nombre de lancé //--> pile = 0 = a gauche //--> face = 1 = a droite //clf; X=[0] for i=1:n val=lancePiece(); if val==0 then X=[X X(i)+s]; else X=[X X(i)-s]; end //disp(X(i)); //sleep(T*1000); end temps=[0:T:n*T]; afficheMarche1D(temps,X); endfunction //------------------------------------------------------------------------- //Fonction qui prend en parametre une distance 's', une periode (en sec)'T' et le nombre de mouvement 'n' // Simule une marche aleatoire dans 4 sens : gauche ou droite, et haut ou bas d'une // distance 's' qui se repete toutes les T secondes 'n' fois function [X,Z]=marcheAlea2D(s,T,n) //Avec s la longueur du deplacement pour un lancé //Avec T la periode en seconde du lancé de piece //Avec n le nombre de lancé //--> pileX = 0 = a gauche //--> faceX = 1 = a droite //--> pileZ = 0 = en haut //--> faceZ = 1 = en bas X=[0]; Z=[0]; for i=1:n valX=lancePiece(); valZ=lancePiece(); if valX==0 then X=[X X(i)+s]; else X=[X X(i)-s]; end if valZ==0 then Z=[Z Z(i)+s]; else Z=[Z Z(i)-s]; end //disp(X(i)); //sleep(T*1000); end temps=[0:T:n*T]; afficheMarche2D(temps,X,Z); //param3d(temps,X,Z); //plot3d(temps,temps,[Z' X']) //xtitle("X(nT,omega)","Temps (s)","Distance parcourue (gauche/droite)","Distance parcourue (haut/bas)"); endfunction //------------------------------------------------------------------------- //Affiche 3 graphes : le 1er en 3d, les 2 derniers en 2d function afficheMarche1D(axeX,axeY) plot(axeX,axeY); xtitle("X(nT,omega)","Temps (s)","Distance parcourue"); endfunction //------------------------------------------------------------------------- //Affiche 3 graphes : le 1er en 3d, les 2 derniers en 2d function afficheMarche2D(axeX,axeY,axeZ) subplot(131) param3d(axeX,axeY,axeZ); xtitle("Z(nT,omega)","Temps (s)","Distance parcourue (gauche/droite)","Distance parcourue (haut/bas)"); subplot(132) plot(axeX,axeY); xtitle("Z(nT,omega)","Temps (s)","Distance parcourue (gauche/droite)"); subplot(133) plot(axeX,axeZ); xtitle("Z(nT,omega)","Temps (s)","Distance parcourue (haut/bas)"); endfunction //------------------------------------------------------------------------- //Affiche 9 graphes avec comme param 'n' qui qui represente le nombre de mouvements //On prend T de plus en plus petit en commencant a 1, et en divisant a chaque fois par 10 function marcheAleaRapide(n) T=1;temps=[0:T:n*T]; subplot(331) plot(temps,marcheAlea1D(sqrt(T),T,n)) T=0.1;temps=[0:T:n*T]; subplot(332) xtitle("9 graphes pour la marche aleatoire rapide"); plot(temps,marcheAlea1D(sqrt(T),T,n)) T=0.01;temps=[0:T:n*T]; subplot(333) plot(temps,marcheAlea1D(sqrt(T),T,n)) T=0.001;temps=[0:T:n*T]; subplot(334) plot(temps,marcheAlea1D(sqrt(T),T,n)) T=0.0001;temps=[0:T:n*T]; subplot(335) plot(temps,marcheAlea1D(sqrt(T),T,n)) T=0.00001;temps=[0:T:n*T]; subplot(336) plot(temps,marcheAlea1D(sqrt(T),T,n)) T=0.000001;temps=[0:T:n*T]; subplot(337) plot(temps,marcheAlea1D(sqrt(T),T,n)) T=0.0000001;temps=[0:T:n*T]; subplot(338) plot(temps,marcheAlea1D(sqrt(T),T,n)) T=0.00000001;temps=[0:T:n*T]; subplot(339) plot(temps,marcheAlea1D(sqrt(T),T,n)) endfunction //------------------------------------------------------------------------- //Simule un lancer de piece en suivant le loi de bernoulli (loi binomiale pour n=1 et p=0.5) function val=lancePiece() val=grand(1,1,"bin",1,0.5) endfunction //------------------------------------------------------------------------- //Affiche 4 graphes pour la loi uniforme pour 10,100,1000 et 10000 nombres function plotLoiUniform() subplot(221) xtitle("4 graphes pour la loi uniforme pour n=10,100,1000 ,10000"); plot(genLoiUniform(10)) subplot(222) plot(genLoiUniform(100)) subplot(223) plot(genLoiUniform(1000)) subplot(224) plot(genLoiUniform(10000)) endfunction //------------------------------------------------------------------------- //Affiche 12 graphes pour la loi de Poisson pour 10,100,1000 et 10000 nombres // et pour lambda 1, 10 et 100 function plotLoiPoisson() subplot(431) plot(genLoiPoisson(10,1)) subplot(432) xtitle("12 graphes pour la loi de Poisson pour n=10,100,1000,10000 et lambda=1,10,100"); plot(genLoiPoisson(10,10)) subplot(433) plot(genLoiPoisson(10,100)) subplot(434) plot(genLoiPoisson(100,1)) subplot(435) plot(genLoiPoisson(100,10)) subplot(436) plot(genLoiPoisson(100,100)) subplot(437) plot(genLoiPoisson(1000,1)) subplot(438) plot(genLoiPoisson(1000,10)) subplot(439) plot(genLoiPoisson(1000,100)) subplot(4,3,10) plot(genLoiPoisson(10000,1)) subplot(4,3,11) plot(genLoiPoisson(10000,10)) subplot(4,3,12) plot(genLoiPoisson(10000,100)) endfunction //------------------------------------------------------------------------- //Affiche 16 graphes pour la loi de Normale pour 10,100,1000 et 10000 nombres, // pour une esperance a 10 et 100 et pour un ecart-type a 1 et 10 function plotLoiNormale() subplot(441) plot(genLoiNormale(10,10,1)) subplot(442) xtitle("16 graphes pour la loi de Normale pour n=10,100,1000,10000 m=10,100 sigma=1,10"); plot(genLoiNormale(10,10,10)) subplot(443) plot(genLoiNormale(10,100,1)) subplot(444) plot(genLoiNormale(10,100,10)) subplot(445) plot(genLoiNormale(100,10,1)) subplot(446) plot(genLoiNormale(100,10,10)) subplot(447) plot(genLoiNormale(100,100,1)) subplot(448) plot(genLoiNormale(100,100,10)) subplot(449) plot(genLoiNormale(1000,10,1)) subplot(4,4,10) plot(genLoiNormale(1000,10,10)) subplot(4,4,11) plot(genLoiNormale(1000,100,1)) subplot(4,4,12) plot(genLoiNormale(1000,100,10)) subplot(4,4,13) plot(genLoiNormale(10000,10,1)) subplot(4,4,14) plot(genLoiNormale(10000,10,10)) subplot(4,4,15) plot(genLoiNormale(10000,100,1)) subplot(4,4,16) plot(genLoiNormale(10000,100,10)) endfunction //------------------------------------------------------------------------- //Affiche 4 histogrammes pour la loi uniforme pour 10,100,1000 et 10000 nombres function histplotLoiUniform() X1=genLoiUniform(10) X2=genLoiUniform(100) X3=genLoiUniform(1000) X4=genLoiUniform(10000) xtitle("4 histogrammes pour la loi uniforme n=10,100,1000,10000"); subplot(221) histplot([0:0.1:1],X1); subplot(222) histplot([0:0.1:1],X2); subplot(223) histplot([0:0.1:1],X3); subplot(224) histplot([0:0.1:1],X4); endfunction //------------------------------------------------------------------------- //Ce fichier scilab contient l'ensemble du code pour le DM disp("- Exercice 1)"); disp("-- Partie 1"); disp("--- 1)"); disp("Test pour N=10"); disp(genLoiUniform(10)); xset("window",0); plotLoiUniform(); disp("--- 2)"); xset("window",1); histplotLoiUniform(); disp("--- 3)"); N=genLoiUniform(1000) b=testChi2(N, 'uni', 0, 1, 10) disp("Test chi2 pour 1000 nombres de loi uniforme avec 10 classes") disp(b); disp("--- 4)"); N=genRandLoiUniform(1000) b=testChi2(N, 'uni', 0, 1, 10) disp("Test chi2 pour 1000 nombres de la fonction rand avec 10 classes") disp(b); disp("--- 5)"); // disp("-- Partie 2"); disp("--- 6)"); xset("window",2); plotLoiPoisson(); xset("window",3); plotLoiNormale() disp("--- 7)"); b=testChi2LoiPoisson(1000, 10, 10) disp("Test chi2 pour 1000 nombres de loi Poisson avec 10 classes") disp(b); disp("-- Partie 3"); disp("--- 8)"); disp("- Exercice 2)"); disp("-- Partie 1"); disp("--- 1)"); //Loi Xi disp("--- 2)"); //Loi X disp("--- 3)"); xset("window",4); [X,Z]=marcheAlea2D(1,1,20); xset("window",5); [X,Z]=marcheAlea2D(1,1,100); xset("window",6); [X,Z]=marcheAlea2D(1,1,1000); disp("--- 4)"); //Esperance et variance : disp("-- Partie 2"); disp("--- 5)"); //pourquoi s²=a.T disp("--- 6)"); xset("window",7); marcheAleaRapide(1000); disp("--- 7"); //mouvement brownien disp("-- Partie 3"); disp("--- 8)"); xset("window",8); [X,Z]=marcheAlea2D(s,T,n);
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// Example 3// Ch 3 clc; clear; close; // given data R=8314; // gas constant in J/kg.mol.K T=300; // temperature 27 deg C, 27+293=300K me=0.10; //mean free path in meters rm=1.7*10^-10 //molecular radius in angstrom M=28 //im mole^-1 m0=4.8*10^-26 //mass of nitrogen molecule N = 1/[4*%pi*((rm)^2)*me]; // no. of molecules in gas printf("no. of molecules %e",N) p = [(N*m0)/M]*R*T; // max pressure in chamber in N/m2 printf("max pressure in chamber %f N/m2",p) // Note: Calculation in the book is wrong So answer in the book is wrong
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clc //initialisation of variables t1=90//F q=14.7//pasi t2=74//F P=0.4156//Psia h=2800//lbf t=1.3//F r=460//F v=144//lbf p=85.8//lbf Psat=0.6982//ft h1=0.622//ft //CALCULATIONS Pv=P-((q-P)*(t1-t2))/(h-t*(t2))//psia W=(v*Pv*1)/(p*(t1+r))//lb per cu ft R=Pv/Psat*100//percent S=h1*(Pv/(q-Pv))//lb vapor per lb dry air //RESULTS printf('The absolute humidity=% f lb per cu ft',W) printf('The relative humidity=% f percent',R) printf('specific humidity=% f lb vapor per lb dry air',S)
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clc //initialisation of variables l1=30//in n=375//rpm l2=20//in va=10//ft/sec H=50//ft g=32.2//ft/sec^2 //CALCULATIONS v=n*%pi*l1/(12*60) v1=v*l2/l1 vf=va*l2/l1 thw=H-(va*va/(2*g)) the=thw*100/H aw=100*550/(21*62.4) ae=aw*100/50 Vw=thw*g/v alp=atan(vf/Vw) k=atan(vf/(v-Vw)) //RESULTS printf ('\n most suitable angle= %.1f ',180-k*180/%pi)
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// Exa 9.3 // To calculate final phase for the pi/4-DQPSK modulation method. clc; clear all; B=['00','10','01','11','01','00','11','10','10','01','01','00'];//Given Bit stream //solution disp("Phase transition table for pi/4-DQPSK Modulation is given as ") disp(" By Referring Table 9.1 on page No 266 i.e"); disp("Symbol Phase transition") disp("00 => 45°"); disp("01 => 135°"); disp("10 => -45°"); disp("11 => -135°"); disp(""); disp("sym Dell phi(k) Phi(k)") //BitStream='001001110100111010010100'; phase=0; //Taking initial phase as zero for i=1:12 if(B(i)=='00') phase=phase+45; printf(' %s 45 %d \n',B(i),phase); end if(B(i)=='01') phase=phase+135; printf(' %s 135 %d \n',B(i),phase); end if(B(i)=='10') phase=phase-45; printf(' %s -45 %d \n',B(i),phase); end if(B(i)=='11') phase=phase-135; printf(' %s -135 %d \n',B(i),phase); end end disp(""); printf('final phase for the pi/4-DQPSK modulation method for given bitstream is %d degree\n',phase);
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sce
pad_in.sce
//*************************** IO PAD IN ******************************** if(blk_name.entries(bl)=='pad_in') then fd_io= mopen (fname+'.pads','a+'); // DEDICATED PADS code for ss=1:scs_m.objs(bl).model.ipar(1) tmp_pad = strsplit(iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries," ") //disp(iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries) if tmp_pad(3) == '3' | tmp_pad(3)== '5' then tmp_pad(3) = '1'; elseif tmp_pad(3) == '2' then tmp_pad(3) = '0'; end netout = 'net'; if tmp_pad(4)=='#int[5]'|tmp_pad(4)=='#int[4]'|tmp_pad(4)=='#int[3]'|tmp_pad(4)=='#int[2]'|tmp_pad(4)=='#int[1]'|tmp_pad(4)=='#int[0]' then if(board_num==2) if((iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries=="13 0 1 #int[1]")&(ramp_chk==1)&(sft_chk==1)) //mputl(netout+ string(blk(blk_objs(bl),2+numofip)) + "_" + string(ss) + ' ' +"13 0 4 #int[4]",fd_io) mputl("",fd_io) else mputl(netout+ string(blk(blk_objs(bl),2+numofip)) + "_" + string(ss) + ' ' + iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries,fd_io); end elseif(board_num==3) if((iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries=="0 12 5 #int[5]")&(ramp_chk==1)&(sft_chk==1)) //mputl(netout+ string(blk(blk_objs(bl),2+numofip)) + "_" + string(ss) + ' ' +"13 0 4 #int[4]",fd_io) mputl("",fd_io) else mputl(netout+ string(blk(blk_objs(bl),2+numofip)) + "_" + string(ss) + ' ' + iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries,fd_io); end end else mputl(netout+ string(blk(blk_objs(bl),2+numofip)) + "_" + string(ss) + ' ' + iopad_loc(loc_num,scs_m.objs(blk_objs(bl)).model.rpar(ss)).entries + 'tgate[' + tmp_pad(3)+ ']',fd_io); end end mclose(fd_io); end
53f7f12d709054973337997891c22a9f38f8d8a7
449d555969bfd7befe906877abab098c6e63a0e8
/887/CH12/EX12.1/12_1.sce
62b51100ca7bbd2822e828bc694ad471e3a6f585
[]
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
320
sce
12_1.sce
clc //initialisation of variables K= 2 VGS1= 5 //V VGS2= 4 //V VGS3= 3 //V VGS4= 2 //V //CALCULATIONS id1= K*(VGS1-2)^2 id2= K*(VGS2-2)^2 id3= K*(VGS3-2)^2 id4= K*(VGS4-2)^2 //RESULTS printf ('iD = %.f V ',id1) printf ('\n iD = %.f V ',id2) printf ('\n iD = %.f V ',id3) printf ('\n iD = %.f V ',id4)
4e3eb93ad13e2409f66d01b21a6d765f43996aa6
449d555969bfd7befe906877abab098c6e63a0e8
/1061/CH8/EX8.9/Ex8_9.sce
0bd6e39286c002eaec8776789212ce945a57fa7c
[]
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
444
sce
Ex8_9.sce
//Ex:8.9 clc; clear; close; n=3.6;// refractive index c=3*10^8;// speed of light in m/s y=0.85*10^-6;// wavelength in m df=275*10^9;// frequency separation of the modes in Hz L=c/(2*n*df);// crystal length in m L1=L*10^6;// crystal length in um q=2*n*L/y;// the number of longitudinal modes printf("The crystal length =%f um", L1); printf("\n The the number of longitudinal modes =%d", q); printf("\n answer is wrong in textbook");
a9f5d27da6d13c2bb54e8b5e67fc0a8ef9cbc678
449d555969bfd7befe906877abab098c6e63a0e8
/25/CH11/EX11.4/11_4.sce
317263d14e3e7df3b33037f4a214195de9fda3af
[]
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
373
sce
11_4.sce
//example:-11.4,page no.-596. //program to calculate the impedence of the diode. Cp=0.1*10^-12;Lp=2*10^-9;Cj=0.15*10^-12;Rs=10;Is=0.1*10^(-6); Io1=0;Io2=60*10^(-6);alpha=(1/25)*(10^3); R1j=1/(alpha*(Io1+Is)); // for Io=0. R2j=1/(alpha*(Io2+Is)); // for Io=60 mA. disp(R1j,'junction resistance for Io=0, in ohm = ') disp(R2j,'junction resistance for Io=0, in ohm = ')
e3c7ea493486ef4d5d9743f3c892fb3b400c61ca
75e8de13b449936c15072e897be26dfe860bf5f4
/data/samples-61.sci
7e910a4bca2b2a22d15d756dae9feb106a508701
[ "LicenseRef-scancode-public-domain" ]
permissive
MyFreertosLab/my_motors_test
98888702fd22774611b5c01f65d5c3938feb2838
2e059c196ec7be0ebd7ac9bd4f8c96585d1da169
refs/heads/master
2023-05-13T08:33:44.999855
2021-06-03T19:04:42
2021-06-03T19:04:42
373,610,906
0
0
null
null
null
null
UTF-8
Scilab
false
false
122,616
sci
samples-61.sci
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61.96678, 11648, 7576, 11632, 7200, 11632, 7552; 61.96678, 11648, 7472, 11632, 7008, 11624, 7480; 61.96678, 11656, 7712, 11632, 7008, 11624, 7480; 61.96678, 11656, 7712, 11632, 7248, 11632, 7608; 61.96678, 11648, 7856, 11632, 7072, 11632, 7392; 61.96678, 11648, 7704, 11632, 7072, 11632, 7392; 61.96678, 11648, 7704, 11640, 7536, 11632, 7552; 61.96678, 11656, 7384, 11632, 7088, 11632, 7304; 61.96678, 11648, 7800, 11632, 7088, 11632, 7304; 61.96678, 11648, 7800, 11632, 7304, 11632, 7592; 61.96678, 11648, 7704, 11632, 7088, 11632, 7320; 61.96678, 11648, 7304, 11632, 7112, 11632, 7320; 61.96678, 11648, 7304, 11632, 7112, 11632, 7712; 61.96678, 11656, 7712, 11632, 7088, 11632, 7320; 61.96678, 11648, 7768, 11632, 7184, 11632, 7320; 61.96678, 11648, 7768, 11640, 7184, 11624, 7576; 61.96678, 11648, 7624, 11632, 7608, 11632, 7352; 61.96678, 11648, 7728, 11632, 7392, 11632, 7352; 61.96678, 11648, 7728, 11632, 7392, 11624, 7456; 61.96678, 11656, 7616, 11632, 7296, 11632, 7496; 61.96678, 11648, 8016, 11632, 6816, 11632, 7496; 61.96678, 11648, 8016, 11632, 6816, 11632, 7528; 61.96678, 11656, 7824, 11632, 7328, 11632, 7560; 61.96678, 11656, 7560, 11632, 7720, 11632, 7560; 61.96678, 11656, 7560, 11632, 7720, 11624, 7544; 61.96678, 11656, 7840, 11640, 7784, 11632, 7416; 61.96678, 11648, 7608, 11640, 7408, 11632, 7416; 61.96678, 11648, 7608, 11632, 7408, 11632, 7320; 61.96678, 11648, 7480, 11640, 7344, 11632, 7584; 61.96678, 11648, 7704, 11640, 6968, 11632, 7584; 61.96678, 11648, 7840, 11640, 6968, 11632, 7272; 61.96678, 11648, 7840, 11640, 7304, 11632, 7592; 61.96678, 11648, 7984, 11640, 7152, 11632, 7592; 61.96678, 11648, 7880, 11632, 7152, 11632, 7408; 61.96678, 11656, 7880, 11632, 7224, 11632, 7608; 61.96678, 11656, 7744, 11632, 7128, 11632, 7608; 61.96678, 11656, 7824, 11632, 7128, 11632, 7368; 61.96678, 11648, 7824, 11632, 7232, 11632, 7640; 61.96678, 11648, 7832, 11632, 7496, 11632, 7640; 61.96678, 11648, 7312, 11640, 7496, 11632, 7272; 61.96678, 11656, 7312, 11640, 7824, 11624, 7616; 61.96678, 11648, 7368, 11640, 7592, 11624, 7616; 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61.96678, 11648, 7448, 11632, 7008, 11624, 7552; 61.96678, 11656, 7448, 11632, 7272, 11632, 7336; 61.96678, 11648, 7720, 11632, 7128, 11632, 7336; 61.96678, 11648, 7720, 11640, 7128, 11624, 7616; 61.96678, 11656, 7720, 11640, 7440, 11632, 7392; 61.96678, 11648, 7448, 11640, 7280, 11632, 7392; 61.96678, 11648, 7328, 11632, 7280, 11624, 7696; 61.96678, 11648, 7328, 11632, 7192, 11632, 7480; 61.96678, 11648, 7824, 11632, 7120, 11632, 7480; 61.96678, 11648, 7576, 11632, 7120, 11632, 7512; 61.96678, 11648, 7576, 11632, 7224, 11632, 7560; 61.96678, 11648, 7720, 11632, 7416, 11632, 7560; 61.96678, 11648, 7816, 11640, 7416, 11624, 7504; 61.96678, 11656, 7816, 11640, 7872, 11632, 7392; 61.96678, 11648, 7752, 11632, 7712, 11632, 7424; 61.96678, 11648, 7688, 11632, 7712, 11632, 7424; 61.96678, 11648, 7688, 11632, 7352, 11632, 7664; 61.96678, 11648, 7640, 11632, 6984, 11632, 7296; 61.96678, 11648, 7936, 11632, 6984, 11632, 7296; 61.96678, 11648, 7936, 11640, 7216, 11632, 7480; 61.96678, 11648, 8152, 11632, 7592, 11632, 7312; 61.96678, 11656, 7240, 11632, 7592, 11624, 7312; 61.96678, 11656, 7240, 11632, 7888, 11632, 7392; 61.96678, 11648, 7448, 11640, 7656, 11632, 7296; 61.96678, 11656, 7368, 11640, 7656, 11624, 7296; 61.96678, 11656, 7368, 11632, 7528, 11632, 7656; 61.96678, 11656, 7472, 11640, 7216, 11632, 7176; 61.96678, 11648, 7960, 11640, 7216, 11632, 7176; 61.96678, 11648, 7960, 11632, 7360, 11632, 7400; 61.96678, 11648, 7544, 11640, 7376, 11632, 7488; 61.96678, 11648, 7384, 11640, 7376, 11632, 7488; 61.96678, 11648, 7384, 11632, 7136, 11632, 7552; 61.96678, 11656, 8056, 11632, 7240, 11632, 7480; 61.96678, 11656, 7728, 11632, 7240, 11632, 7480; 61.96678, 11656, 7728, 11632, 7264, 11632, 7504; 61.96678, 11656, 7640, 11632, 7184, 11632, 7480; 61.96678, 11656, 7392, 11632, 7184, 11632, 7480; 61.96678, 11656, 7392, 11640, 7512, 11632, 7224; 61.96678, 11648, 7144, 11632, 7688, 11632, 7632; 61.96678, 11656, 7576, 11632, 7688, 11632, 7632; 61.96678, 11656, 7576, 11632, 7448, 11624, 7296; 61.96678, 11656, 7632, 11640, 7160, 11624, 7624; 61.96678, 11648, 7664, 11640, 7160, 11632, 7624; 61.96678, 11648, 7664, 11632, 7192, 11632, 7360; 61.96678, 11648, 7712, 11632, 7568, 11632, 7528; 61.96678, 11656, 7568, 11632, 7568, 11632, 7528; 61.96678, 11656, 7568, 11640, 7488, 11632, 7304; 61.96678, 11656, 8008, 11632, 7280, 11632, 7440; 61.96678, 11656, 7872, 11632, 7280, 11632, 7440; 61.96678, 11656, 7872, 11632, 7216, 11632, 7352; 61.96678, 11656, 7440, 11632, 6896, 11632, 7496; 61.96678, 11648, 7584, 11632, 6896, 11632, 7496; 61.96678, 11648, 7584, 11640, 7328, 11624, 7384; 61.96678, 11648, 7120, 11632, 7128, 11624, 7520; 61.96678, 11656, 7472, 11632, 7128, 11624, 7520; 61.96678, 11656, 7472, 11632, 7840, 11632, 7400; 61.96678, 11656, 7720, 11632, 7600, 11632, 7440; 61.96678, 11656, 7512, 11632, 7600, 11624, 7440; 61.96678, 11656, 7512, 11632, 7120, 11632, 7600; 61.96678, 11648, 7400, 11632, 6976, 11624, 7496; 61.96678, 11648, 7520, 11632, 6976, 11624, 7496; 61.96678, 11648, 7520, 11640, 7352, 11632, 7520; 61.96678, 11648, 7640, 11632, 7248, 11632, 7408; 61.96678, 11648, 7760, 11632, 7248, 11632, 7408; 61.96678, 11648, 7760, 11632, 7528, 11632, 7544; 61.96678, 11648, 7776, 11632, 6800, 11632, 7232; 61.96678, 11656, 7736, 11632, 6800, 11632, 7232; 61.96678, 11656, 7736, 11640, 7480, 11632, 7560; 61.96678, 11648, 8032, 11640, 7432, 11632, 7424; 61.96678, 11656, 7656, 11640, 7432, 11632, 7424; 61.96678, 11656, 7656, 11632, 7672, 11624, 7632; 61.96678, 11656, 7656, 11632, 7528, 11632, 7456; 61.96678, 11656, 8016, 11632, 7528, 11632, 7456; 61.96678, 11656, 8016, 11632, 7232, 11632, 7544; 61.96678, 11656, 7664, 11632, 6896, 11632, 7312; 61.96678, 11648, 7384, 11632, 6896, 11632, 7312; 61.96678, 11648, 7384, 11640, 7488, 11624, 7544; 61.96678, 11656, 7432, 11632, 7632, 11632, 7272; 61.96678, 11656, 7472, 11632, 7632, 11632, 7272; 61.96678, 11656, 7472, 11640, 7856, 11624, 7456; 61.96678, 11656, 8024, 11632, 7200, 11632, 7344; 61.96678, 11656, 7704, 11632, 7200, 11632, 7344; 61.96678, 11656, 7704, 11632, 7184, 11624, 7584; 61.96678, 11656, 7552, 11632, 7368, 11632, 7640; 61.96678, 11648, 7768, 11632, 7368, 11632, 7640; 61.96678, 11648, 7768, 11640, 7536, 11624, 7424; 61.96678, 11656, 7120, 11632, 7448, 11632, 7616; 61.96678, 11656, 7144, 11632, 7432, 11632, 7616; 61.96678, 11656, 7448, 11640, 7432, 11632, 7296; 61.96678, 11656, 7448, 11632, 7424, 11632, 7520; 61.96678, 11656, 7360, 11632, 7456, 11632, 7520; 61.96678, 11656, 7672, 11640, 7456, 11632, 7288; 61.96678, 11656, 7672, 11632, 7328, 11632, 7536; 61.96678, 11656, 7840, 11632, 6992, 11632, 7536; 61.96678, 11656, 7360, 11632, 6992, 11632, 7344; 61.96678, 11656, 7360, 11632, 7064, 11632, 7640; 61.96678, 11648, 7304, 11632, 7008, 11632, 7640; 61.96678, 11648, 7320, 11632, 7008, 11632, 7392; 61.96678, 11656, 7320, 11632, 7696, 11624, 7416; 61.96678, 11656, 7520, 11632, 7696, 11624, 7416; 61.96678, 11656, 7568, 11640, 7696, 11632, 7464; 61.96678, 11656, 7568, 11632, 7448, 11632, 7648; 61.96678, 11656, 7816, 11632, 7096, 11632, 7648; 61.96678, 11656, 7472, 11640, 7096, 11632, 7200; 61.96678, 11656, 7472, 11632, 7280, 11632, 7544; 61.96678, 11648, 7336, 11632, 7136, 11632, 7544; 61.96678, 11648, 7368, 11640, 7136, 11632, 7376; 61.96678, 11656, 7368, 11632, 7648, 11624, 7512; 61.96678, 11656, 7248, 11632, 7272, 11624, 7512; 61.96678, 11656, 7464, 11632, 7272, 11632, 7376; 61.96678, 11656, 7464, 11632, 7200, 11632, 7592; 61.96678, 11648, 7872, 11632, 7024, 11632, 7592; 61.96678, 11648, 7288, 11632, 7024, 11632, 7408; 61.96678, 11648, 7288, 11632, 7304, 11624, 7520; 61.96678, 11648, 7672, 11640, 7760, 11624, 7520; 61.96678, 11648, 8008, 11640, 7760, 11632, 7448; 61.96678, 11648, 8008, 11632, 7320, 11632, 7232; 61.96678, 11656, 7744, 11632, 7152, 11632, 7232; 61.96678, 11656, 7984, 11632, 7152, 11632, 7688; 61.96678, 11656, 7984, 11640, 7424, 11624, 7360; 61.96678, 11656, 8072, 11640, 7616, 11624, 7360; 61.96678, 11656, 7520, 11640, 7616, 11632, 7584; 61.96678, 11648, 7520, 11632, 7416, 11624, 7376; 61.96678, 11648, 7472, 11632, 7152, 11624, 7376; 61.96678, 11648, 7648, 11632, 7152, 11632, 7536; 61.96678, 11656, 7648, 11632, 7328, 11624, 7248; 61.96678, 11656, 7552, 11640, 7496, 11624, 7248; 61.96678, 11656, 7664, 11640, 7496, 11624, 7768; 61.96678, 11656, 7664, 11640, 7600, 11632, 7256; 61.96678, 11656, 7352, 11632, 7440, 11632, 7256; ];
e8a77057fc23bd29067bbb2fea1b7fa962c17f3c
449d555969bfd7befe906877abab098c6e63a0e8
/479/CH14/EX14.11/Example_14_11.sce
f1638614666191f1995e82aefaa8aa838f9e2ac0
[]
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
871
sce
Example_14_11.sce
//Chemical Engineering Thermodynamics //Chapter 14 //Thermodynamics of Chemical Reactions //Example 14.11 clear; clc; //Given //Basis: 1 Kgmole of benzene //C6H6 (A) + HNO3 (B) - C6H5NO2 (C) + H2O (D) T = 298;//Temperature in K R = 1.98;//gas constant in Kcal/Kgmole K //Standard enthalpy in Kcal/Kgmole at 25 deg celsius of the above components are given as H_A = 11718; H_B = -41404; H_C = -68371; H_D = 3800; //Standard entropy in Kcal/Kgmole K at 25 deg celsius of the above components are given as S_A = 41.30; S_B = 37.19; S_C = 16.72; S_D = 53.60; //To Calculate the conversion of benzene at 25 degree celsius and 1 atm del_F = (H_C+H_D-(T*(S_C+S_D)))-(H_A+H_B-(T*(S_A+S_B))); Ka = %e^(-del_F/(R*T));//Equilibrium constant x = (Ka^(1/2)/(1+(Ka^(1/2)))); mprintf('The conversion is almost %f percent for this reaction.',x*100); //end
7f6bc081fe2e252c9fbe0169ab62aa54bdd296c8
717ddeb7e700373742c617a95e25a2376565112c
/22/CH4/EX4.27/ch4ex27.sce
0389caa79920b15f8ed961fc6c1ff04b15cf641c
[]
no_license
appucrossroads/Scilab-TBC-Uploads
b7ce9a8665d6253926fa8cc0989cda3c0db8e63d
1d1c6f68fe7afb15ea12fd38492ec171491f8ce7
refs/heads/master
2021-01-22T04:15:15.512674
2017-09-19T11:51:56
2017-09-19T11:51:56
92,444,732
0
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null
2017-05-25T21:09:20
2017-05-25T21:09:19
null
UTF-8
Scilab
false
false
433
sce
ch4ex27.sce
omega_0=2*%pi*60; theta = [60 80 87]*(%pi/180); omega = (0:0.5:1000)'; mag = zeros(3,length(omega)); s=poly(0,'s') for m =1:length(theta) H=syslin('c',((s^2+omega_0^2)/(s^2+2*omega_0*cos(theta(m))*s +omega_0^2))); bode(H,10,100); end f=omega/((2*%pi))plot(f,mag(1,:),'k-',f mag(2,:),'k--',f,mag(3,:),'k-.'); xlabel('f[hz]'); ylabel('|H(j2/pi f)|'); legend('\theta=60^\circ','\theta = 80^\circ','\theta = 87^\circ',0)
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449d555969bfd7befe906877abab098c6e63a0e8
/1217/CH6/EX6.7/Exa6_7.sce
efb09ac14ddef966e7995cb194c5c488ae8a9921
[]
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
419
sce
Exa6_7.sce
// Exa 6.7 clc; clear; close; // given data C2=0.1;//in uF C3=0.0333;//in uF alfa=2*sqrt(C3/C2);//unitless disp(alfa,"According to the value of alfa i.e. : "); disp("This filter is situated between Butterworth and the Chebyshev, hence approximating Klp=1.1"); Klp=1.1;//unitless R=2.25;//in Kohm f3dB=Klp/(2*%pi*R*sqrt(C2*C3));//in KHz disp(f3dB,"f3dB in KHz is : "); //Note : Answer in the book is wrong
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449d555969bfd7befe906877abab098c6e63a0e8
/1670/CH5/EX5.44/5_44.sce
0924efdc431e58ae23f235c34427fb924e66cc85
[]
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
659
sce
5_44.sce
//Example 5.44 //Inverse Interpolation using Everett Formula //Page no. 191 clc;close;clear; printf(' \tx\td(log(x!)/dx)\t\td2\t d4\n') printf('\t----------------------------------------------------') x=[0.46,-0.0015805620,-0.0000888096,-0.000000396;0.47,0.0080664890,-0.0000872716,-0.0000000383]; h=0.001 for i=1:2 printf('\n') for j=1:4 printf('\t%g',x(i,j)) end end p(1)=-(x(1,2))/(x(2,2)-x(1,2)) for i=1:2 p(i+1)=(-x(1,2)-(p(i)^3-p(i))*x(1,3)/6-(-p(i)^3+3*p(i)^2-2*p(i))*x(1,3)/6)/(x(2,2)-x(1,2)) end for i=1:3 printf('\n\n p(%i) = %g',i,p(i)) end x=x(1,1)+p(3)*h printf('\n\n x = x0 + ph = %.8g',x);
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449d555969bfd7befe906877abab098c6e63a0e8
/1646/CH13/EX13.6/Ch13Ex6.sce
b7d4f95c4db349c603351c1e708d8328f6544a35
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
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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
509
sce
Ch13Ex6.sce
// Scilab Code Ex13.6: Page-650 (2011) clc;clear; K = 1.000074;....// Dielectric constant of the He n = 2.69e+025;....// Atomic density of He, atoms/meter-cube eps_0 = 8.85e-012;....// Electric permability of the free space, C-square/N-meter-square E = 1;....// Electric field strength, V/m p = (eps_0*(K-1)*E)/n; // Dipole moment induced in He, C-m printf("\nThe dipole moment induced in each He atom = %4.2e C-m ", p); // Result // The dipole moment induced in each He atom = 2.43e-041 C-m
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99b4e2e61348ee847a78faf6eee6d345fde36028
/Toolbox Test/latcfilt/latcfilt15.sce
94248dd67200e9030022d13760ea0ba309418e87
[]
no_license
deecube/fosseetesting
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2021-01-20T11:34:43.535019
2016-09-27T05:12:48
2016-09-27T05:12:48
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sce
latcfilt15.sce
//i/p arg k is zero k=[0 0 0 0 0 0]; x=[1 2 3 4 5 6 7]; [f,g] = latcfilt(k,x); disp(f); disp(g); //output // !--error 10000 //dimension mis-match between k and v //at line 46 of function latcfilt called by : //[f,g] = latcfilt(k,x); //matlab // 1 2 3 4 5 6 7 // // 0 0 0 0 0 0 1
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/1928/CH2/EX2.23.7/ex2_23_7.sce
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no_license
FOSSEE/Scilab-TBC-Uploads
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refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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ex2_23_7.sce
//Chapter-2,Example2_23_7,pg 2-55 B=0.2 //magnetic field e=1.6*10^-19 //charge on electron ue=0.39 //mobility of electron l=0.01 //length A=0.001*0.001 //cross section area of bar V=1*10^-3 //Applied voltage d=0.001 //sample of width r=1/(ue*e) //resistivity R=r*l/A //resistance of Ge bar //using ohm's law I=V/R Rh=r*ue //hall coefficient //using formulae for hall effect J=I/A //current density Vh=Rh*B*J*d printf("Hall voltage =") disp(Vh)
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/2753/CH5/EX5.2/Ex5_2.sce
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no_license
FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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Ex5_2.sce
//Example 5.2: clc; clear; close; //given data : Pac=2;//in W Vcc=12;//in V Ic=(Pac*sqrt(2)*sqrt(2))/Vcc;//in A format('v',5) disp(Ic,"maximum collector current is ,(A)=")
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/3775/CH2/EX2.2/Ex2_2.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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Ex2_2.sce
//Ex 2.2 page 67 clc; clear; close; diBYdt=1000;//A/s (rate of rise of current) il=10;//mA (latching current = diBYdt * tp) tp=il*10**-3/diBYdt;//s printf('Minimum duration of gating pulse = %.f micro s',tp*10**6)
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/2657/CH18/EX18.10/Ex18_10.sce
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FOSSEE/Scilab-TBC-Uploads
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Ex18_10.sce
//Calculations on gas engine clc,clear //Given: d=27,l=45 //Bore and stroke in cm D_b=1.62 //Effective diameter of the brake wheel in m t=38.5 //Duration of test in min N=8080,N1=3230 //Number of revolutions and explosions P=903 //Net load on brake in N imep=5.64 //Indicated mean effective pressure in bar Vg1=7.7 //Gas used in m^3 T1=27+273 //Temperature of the gas in K deltaP1=135 //Pressure difference of gas above atmospheric pressure in mm of water Patm=750 //Atmospheric pressure in mm of Hg CV=18420 //Calorific value of the gas in kJ/m^3 at N.T.P. m_w=183 //Mass of cooling water used in kg deltaT_w=47 //Cooling water temperature rise in degreeC //Solution: P1=Patm+deltaP1/13.6 //Gas pressure in mm of Hg P1=P1/750 //Gas pressure in bar T2=0+273,P2=1.013 //Normal temperature and pressure (N.T.P.) in K and bar Vg2=(P1/P2)*(T2/T1)*Vg1 //Gas consumption at N.T.P. in m^3 Q1=Vg2/t*CV //Heat supplied in kJ/min T=P*D_b/2 //Brake torque delivered in Nm bp=2*%pi*(N/t*1/60)*(T)*10^-3 //Brake power in kW bp=round(10*bp)/10 Q_bp=bp*60 //Heat equivalent to brake power in kJ/min A=%pi/4*d^2*10^-4 //Area of cylinder in m^2 ip=imep*10^2*l/100*A*(N1/t*1/60) //Indicated power in kW ip=round(10*ip)/10 Q_ip=ip*60 //Heat equivalent to indicated power in kJ/min fp=ip-bp //Frictional power in kW Q_fp=fp*60 //Heat equivalent to frictional power in kJ/min cp=4.1868 //Specfic heat of water in kJ/kgK Q_w=m_w/t*cp*(deltaT_w) //Heat in cooling water in kJ/min Q_e=Q1-Q_bp-Q_w //Heat to exhaust, radiation in kJ/min eta_it=Q_ip/Q1 //Indicated thermal efficiency eta_bt=Q_bp/Q1 //Brake thermal efficiency //Results: printf("\n The indicated thermal efficiency, eta_it = %.1f percent",eta_it*100) printf("\n The brake thermal efficiency, eta_bt = %.1f percent",eta_bt*100) printf("\n\n Heat balance sheet\n\t Heat supplied by the gas = %d kJ/min, %d percent",Q1,Q1/Q1*100) printf("\n\t Heat equivalent to b.p. = %d kJ/min, %.1f percent",Q_bp,Q_bp/Q1*100) printf("\n\t Heat in cooling water = %d kJ/min, %.1f percent",Q_w,Q_w/Q1*100) printf("\n\t Heat to exhaust, radiation = %d kJ/min, %.1f percent",Q_e,Q_e/Q1*100)
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/2438/CH6/EX6.3/Ex6_3.sce
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Ex6_3.sce
//========================================================================== // chapter 6 example 3 clc; clear; //input data t1 = 20; // temperature in °C alpha = 5*10^-3; //average temperature coefficient at 20°C R1 = 8; //resistance in ohm R2 = 140; //resistaance in ohm //calculation t2 = t1+((R2-R1)/(R1*alpha)); //temperature in C //result mprintf('Hence temperature under normal condition is %3.2f°C\n',t2); //============================================================================
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/1529/CH7/EX7.7/7_07.sce
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7_07.sce
//Chapter 7, Problem 7 clc; d=10*10^-2; //Diameter N=2000; //No of turns I=0.25; //Current in the coil B=0.4; //Magnetic flux density u0=4*%pi*10^-7; //permeability of free space l=%pi*d; //Calculating length of coil H=(N*I)/l; //Calculating magnetic field strength ur=B/(u0*H); //Calculating relative permeability disp("(a)"); printf("Magnetic field strength = %f A/m\n\n\n",H); disp("(b)"); printf("Relative permeability = %d",ur);
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/Adjust to Track Speed.sce
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Ahmad6543/Scenarios
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refs/heads/master
2023-03-18T23:30:49.653812
2020-09-23T06:26:05
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Adjust to Track Speed.sce
Name=Adjust to Track Speed PlayerCharacters=Alcove_Player BotCharacters=FloatingOrbr.rot IsChallenge=true Timelimit=60.0 PlayerProfile=Alcove_Player AddedBots=FloatingOrbr.rot;FloatingOrbr.rot PlayerMaxLives=0 BotMaxLives=0;0 PlayerTeam=2 BotTeams=1;1 MapName=smallspawngrid.map MapScale=6.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=true TimeRefilledByKill=0.3 ScoreToWin=6000.0 ScorePerDamage=1.0 ScorePerKill=150.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=true ScoreMultKillEfficiency=false GameTag=Tracking, Fun WeaponHeroTag=Tracking DifficultyTag=1 AuthorsTag=Stral, Disaria BlockHitMarkers=true BlockHitSounds=true BlockMissSounds=true BlockFCT=true Description=Fragile orbs spawn in front of you and float left or right. Practice making small adjustments into tracking aim. Shots on center of the hitbox deal higher DPS and projectiles or sparks are visual only. GameVersion=1.0.8.0 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 [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=FloatingOrbLeft DodgeProfileNames=HoldLeft DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=3.0 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=false CharacterProfile=FloatingOrb SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Profile] Name=FloatingOrbRight DodgeProfileNames=HoldRight DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=3.0 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=false CharacterProfile=FloatingOrb SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Profile] Name=FloatingOrbLeft+ DodgeProfileNames=HoldLeft DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=3.0 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=false CharacterProfile=FloatingOrb+ SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Profile] Name=FloatingOrbRight+ DodgeProfileNames=HoldRight DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=3.0 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=false CharacterProfile=FloatingOrb+ SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Profile] Name=FloatingOrbLeft++ DodgeProfileNames=HoldLeft DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=3.0 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=false CharacterProfile=FloatingOrb++ SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Profile] Name=FloatingOrbRight++ DodgeProfileNames=HoldRight DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=3.0 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=false CharacterProfile=FloatingOrb++ SeeThroughWalls=false NoDodging=false NoAiming=false [Bot Rotation Profile] Name=FloatingOrbr ProfileNames=FloatingOrbLeft;FloatingOrbRight;FloatingOrbLeft+;FloatingOrbRight+;FloatingOrbLeft++;FloatingOrbRight++ ProfileWeights=1.0;1.0;0.8;0.8;0.65;0.65 Randomized=true [Character Profile] Name=Alcove_Player MaxHealth=300.0 WeaponProfileNames=Alcove_Tracking_Weapon;;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=0.1 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=30.0 AirControl=0.25 CanCrouch=false CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 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=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false 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=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=5.0 BlockSpawnDistance=222222.0 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=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Character Profile] Name=FloatingOrb MaxHealth=300.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.14 MaxRespawnDelay=0.14 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=3000.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=0.0 AirControl=1.0 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=Spheroid MainBBHeight=300.0 MainBBRadius=150.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Spheroid ProjBBHeight=64.0 ProjBBRadius=32.0 ProjBBHasHead=false 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=0.02 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true 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 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Character Profile] Name=FloatingOrb+ MaxHealth=280.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.14 MaxRespawnDelay=0.14 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=3200.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=0.0 AirControl=1.0 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=Spheroid MainBBHeight=300.0 MainBBRadius=150.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Spheroid ProjBBHeight=64.0 ProjBBRadius=32.0 ProjBBHasHead=false 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=0.02 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true 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 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Character Profile] Name=FloatingOrb++ MaxHealth=270.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.14 MaxRespawnDelay=0.14 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=3400.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=0.0 AirControl=1.0 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=Spheroid MainBBHeight=300.0 MainBBRadius=150.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Spheroid ProjBBHeight=64.0 ProjBBRadius=32.0 ProjBBHasHead=false 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=0.02 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true 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 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Dodge Profile] Name=HoldLeft MaxTargetDistance=100000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.3 MaxLRTimeChange=0.3 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false 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=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=100.0 RightStrafeTimeMult=0.000001 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=HoldRight MaxTargetDistance=100000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.3 MaxLRTimeChange=0.3 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false 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=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=0.000001 RightStrafeTimeMult=100.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Alcove_Tracking_Weapon Type=Hitscan ShotsPerClick=10 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.02 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=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=60000.0 GravityScale=1.0 HeadshotCapable=false HeadshotMultiplier=0.1 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=1.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Ball VisualLifetime=0.0001 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.05 HitSoundCooldown=0.05 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=4.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot=Alcove Tracking Effect Helper ADSShoot= StunDuration=0.0 CircularSpread=false SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.01 HitscanVisualRadius=0.001 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=false AimPunchAmount=0.0 AimPunchResetTime=0.2 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=1 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=103.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=false IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 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=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 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=true PBS0=0.0,0.0 PBS1=0.0,0.0 PBS2=0.3,45.0 PBS3=0.3,90.0 PBS4=0.3,135.0 PBS5=0.3,180.0 PBS6=0.3,225.0 PBS7=0.3,270.0 PBS8=0.3,315.0 PBS9=0.3,0.0 [Weapon Profile] Name=Alcove Tracking Effect Helper Type=Projectile ShotsPerClick=1 DamagePerShot=0.0 KnockbackFactor=0.0 TimeBetweenShots=0.12 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=100000.000 Y=-1000.000 Z=-1000.000 MuzzleVelocityMax=X=100000.000 Y=1000.000 Z=1000.000 InheritOwnerVelocity=1.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=0.025 MaxHitscanRange=100000.0 GravityScale=0.0 HeadshotCapable=false HeadshotMultiplier=0.1 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=0.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=Gunshot HitParticleEffect=Blood BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=0.1 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=999.0 HitSoundCooldown=999.0 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=15.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=2.0 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=false AimPunchAmount=0.0 AimPunchResetTime=0.2 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=1 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=103.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=false IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 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=4.0,0.5,2.0,8.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=4.0,0.5,2.0,8.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 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 brush vertices 656.000000 -16.000000 2064.000000 656.000000 -16.000000 -1872.000000 656.000000 16.000000 -1872.000000 656.000000 16.000000 2064.000000 -64.000000 16.000000 -1872.000000 -64.000000 -16.000000 -1872.000000 -64.000000 -16.000000 2064.000000 -64.000000 16.000000 2064.000000 faces 0.000000 0.000000 2.000000 2.000000 -0.000000 0 1 2 3 0x00000000 __TB_empty 0.000000 0.000000 2.000000 2.000000 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/2223/CH18/EX18.47/Ex18_47.sce
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2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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// scilab Code Exa 18.47 Crossflow Radial Hydro turbine N=50; // Speed in RPM H=25; // net head in m Q=150; // discharge in m3/s P=20; // Power Output in MW d1=3.5; // runner diameter in m dr=1.3; // diameter ratio of the runner rho=1000; // density in kg/m3 g=9.81; // gravitational acceleration in m/s2 u1=%pi*d1*N/60; u2=u1/dr; c_theta1=2*u1; c_theta2=u2; w_st1=(u1*c_theta1)-(u2*c_theta2); u3=u2; c_theta3=u2; c_theta4=0; w_st2=(u3*c_theta3)-(u1*c_theta4); w_st=w_st1+w_st2; // part(a) n_h=w_st/(g*H); disp("%",n_h*1e2,"(a)the hydraulic efficiency is") Ph=rho*Q*w_st; disp("MW",Ph*1e-6,"and the hydraulic power is") n_o=P*1e6/(rho*Q*g*H); disp("%",n_o*1e2,"and the overall efficiency is") // part(b) omega=%pi*2*N/60; NS=omega*sqrt(P*1e6)*(H^(-5/4))/549.016; disp(NS,"(b)the specific speed of turbine is") // part(c) disp("(c)Adopting the flow model of the crossflow wind turbine") P_h=rho*Q*((2*(u1^2))+(u2^2)); disp("MW",P_h*1e-6,"the hydraulic power is") nh=((2*(u1^2))+(u2^2))/(g*H); disp("%",nh*1e2,"and hydraulic efficiency is")
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//Electric machines and power systems by Syed A Nasar //Publisher:TataMcgraw Hill //Year: 2002 ; Edition - 7 //Example 2.2 //Scilab Version : 6.0.0 ; OS : Windows clc; clear; bg=1; //flux density of air gap in T u0=4*3.14*10^-7; //permiability of free space lg=0.1*10^-3; //length of air gap in m sf=0.9; //stacking factor of M19 steel lm=100*10^-3; //length of the steel in m h=130; //flux density in At/m hg=bg/u0; //magnetic field intensity in A/m fg=hg*lg; //reluctance drop or magnetic potential across gap in A bm=bg/sf; //flux density in magnetic material in T Fm=h*0.1; //magnetic potenial of other member in At AT=Fm+fg; //the required ampere turn in At printf('the required ampere turn in the exciting coil is %2f in At',AT)
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//example 5.8 //page 211 clc; funcprot(0); //initialisation of variable pi=3.14; mdot=0.0022;//mas flow rate V1=220*5280/3600;//velocity V=12000/pi/6^2*4;//velocity V4=2*V-V1;//velocity //part1 F=mdot*(V4-V1)*12000; disp(F,"thurst force (lbs)"); //part2 neta=V1/V*100; disp(neta,"efficiency (%)"); Hp=F*V1/500/neta*100; disp(Hp,"theoritical horse power (hp)="); delP=mdot/2*(V4^2-V1^2); disp(delP,"change in pressure (lbs/ft^2)="); clear
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Linear Convolution.sce
clc; clear all; close; x=[1,2,3,4,5];//1 seq h=[1,0,1,0];// 2nd seq l=length(x);//4 m=length(h);//4 N=l+m-1; //length of y=8 y=[zeros(1,N)];//intializing y=0 for i=1:l //i-row for j=1:m //j-col a(i,j)=x(i)*h(j) // matrix y(i+j-1)=y(i+j-1)+a(i,j) //diagonal addition end end disp(a) disp(y,"OUTPUT") subplot(2,2,1) plot2d3(x) xlabel('n'),ylabel('x(n)') title('x(n)') subplot(2,2,2) plot2d3(h) xlabel('n'),ylabel('h(n)') title('h(n)') subplot(2,1,2) plot2d3(y) xlabel('n'),ylabel('y(n)') title('y(n)')
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//Variable declaration E=2*1000*1.6*10**-19 //in joules m=9.1*10**-31 h=6.6*10*10**-34 //Calculations p=sqrt(2*m*E) lamda= h/p //Result printf('Momentum%0.3f \n ',(p*10**23)) printf('de Brolie wavelength =%0.3f *10**-11 m \n ',(lamda*10**10))
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//Example 5.10.1: resolution clc; clear; close; format('v',8) //given data : n=4 R=1/10^n; disp(R,"resolution,R = ")
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V=250 Ia=200 Ra=0.22 Ea=V-Ia*Ra Pm=Ea*Ia Prl=600 Pmout=Pm-Prl n=1250 wm=2*%pi*n/60 Tl=Pmout/wm disp(Tl) Rf=125 Psh=V*V/Rf Pein=V*Ia+Psh effi=Pmout/Pein disp(effi)
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chapter3_ex16.sce
clc clear //input v=240;//voltage of a d.c. series motor in volts rm=0.2;//resistance of the motor in ohms w=80;// velocity of motor in rad/s i1=20;//current in amperes i2=30;//changed current in the armature in amperes //calculations //it is assumed that flux/pole is proportional to the field current e1=v-(i1*rm);//e.m.f. induced in volts when the current is 20 A e2=v-(i2*rm);//e.m.f. induced in volts when the current is 30 A W=(e2/e1)*(i1/i2)*w;//final velocity in rad/s //output mprintf('with the increased current the motor will run with a velocity of %3.2f rad/s',W)
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deff('[Xn]=f(Xn_1,c)','Xn=c*Xn_1*(1-Xn_1)'); x0=0.0001; c=[3.5:.001:4] ; orbits=[]; for i=c, orbit=orb(20000,i,x0,f); orbits=[orbits;orbit(1,$-999:$)]; end Kest=[]; C=[]; save('Test_Logidt_Chaos01_orbits_c.dat',orbits,c); for i=1:size(orbits,1), [Kesti,Ci]=Chaos01(orbits(i,:)'); C=[C,Ci]; disp(i) disp(string(round(i/size(orbits,1)*100))+'%') Kest=[Kest, median(Kesti)]; save('Test_Logidt_Chaos01_Kest_C.dat',Kest,c,C) end; plot2d(c,Kest);
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x=poly([-4 2 1],'t','c') a=horner(x,0) b=horner(x,-2) disp(a) disp(b)
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clc; //page no:2-26 //Example-2.13 //Goven carrier frequency is 1000kHz fc=1000000; fm1=300; fm2=800; fm3=1000; fusb1=(fc+fm1)/1000; disp(+'kHz',fusb1,'fusb1 is '); flsb1=(fc-fm1)/1000; disp(+'kHz',flsb1,'flsb1 is '); fusb2=(fc+fm2)/1000; disp(+'kHz',fusb2,'fusb2 is '); flsb2=(fc-fm2)/1000; disp(+'kHz',flsb2,'flsb2 is '); fusb3=(fc+fm3)/1000; disp(+'kHz',fusb3,'fusb3 is '); flsb3=(fc-fm3)/1000; disp(+'kHz',flsb3,'flsb3 is ');
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// This file is part of the materials accompanying the book // "The Elements of Computing Systems" by Nisan and Schocken, // MIT Press. Book site: www.idc.ac.il/tecs // File name: projects/01/Not16.tst load Not16.hdl, output-file Not16.out, compare-to Not16.cmp, output-list in%B1.16.1 out%B1.16.1; set in %B0000000000000000, eval, output; set in %B1111111111111111, eval, output; set in %B1010101010101010, eval, output; set in %B0011110011000011, eval, output; set in %B0001001000110100, eval, output;
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clear; clc; close; disp("Example 11.11") p=7 //in MPa, n=0.5 //and a=5 //cm/s Tdg=15 //in degree C Td=15+273 //in K br=0.002 //per degree C pk=0.004 //per degree C t=60//s, DT=30 // temp difference in degree C pc=p*(1+pk*DT) disp(pc,"(a)The new chamber pressure when the initial grain temp. is 45 degree C in MPa") r=a*(pc/p)^n r=r*(1+br*DT) //correcting for the effect of the grain temperature on burning rate. disp(r,"Burning rate when grain temp. is 45 degree C") L=a*t/100 tb=L*100/r //time to burn 3m of end burning grain at 5.61cm/s tbn=t*(p/pc) //burn time for a constant total impulse dt=t-tb disp(dt,"(b)The corresponding reduction in burn time in seconds:")
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clc; disp('Enter the message sequence: '); for i = 1:7 msg(i)=input(''); end C1 = [msg(1), msg(2), msg(3), msg(4), msg(5), msg(6), msg(7)]; C1 disp('Enter the errored message sequence: '); for i = 1:7 err(i)=input(''); end C2 = [err(1), err(2), err(3), err(4), err(5), err(6), err(7)]; C2 D = poly(0, 'D'); p = input("Enter a generator polynomial in variable D: ", "string"); G = evstr(p); disp(G, 'G(D) = '); C1 = poly([C1], 'D', 'c') C2 = poly([C2], 'D', 'c') [r1 , q1] = pdiv(C1, G); S1 = coeff(r1) ; S1 = modulo(S1, 2); disp(r1 , 'Remainder in polynomial form : ' ); disp(S1 , 'Syndrome bits for error-free codeword are : '); [r2, q2] = pdiv(C2, G); S2 = coeff(r2); S2 = modulo(S2, 2); disp(r2 , 'Remainder in polynomial form for errored codeword: ' ); disp(S2 , 'Syndrome bits for errored codeword are: ');
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<?xml version="1.0" encoding="utf-8"?> <test> <description>2D cylinder flow simulation using adaptive polynomial order</description> <executable>IncNavierStokesSolver</executable> <parameters>CylFlow_adaptiveP.xml</parameters> <files> <file description="Session File">CylFlow_adaptiveP.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="u" tolerance="1e-12">21.4162</value> <value variable="v" tolerance="1e-12">0.911291</value> <value variable="p" tolerance="1e-12">0.875288</value> </metric> <metric type="Linf" id="2"> <value variable="u" tolerance="1e-12">1.76892</value> <value variable="v" tolerance="1e-12">0.837794</value> <value variable="p" tolerance="1e-12">1.29043</value> </metric> </metrics> </test>
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pcl_file = "Hot Reaction Paradigma.pcl"; response_matching = simple_matching; active_buttons = 4; default_background_color = 60, 60, 60; default_text_color = 255, 255, 255; default_font_size = 30; default_font = "Arial"; begin; array { bitmap { filename = "stimulus_neutral_1.jpg"; } bitmap_neutral_1; bitmap { filename = "stimulus_neutral_2.jpg"; } bitmap_neutral_2; bitmap { filename = "stimulus_neutral_3.jpg"; } bitmap_neutral_3; bitmap { filename = "stimulus_neutral_4.jpg"; } bitmap_neutral_4; bitmap { filename = "stimulus_neutral_5.jpg"; } bitmap_neutral_5; } array_neutral_bitmaps; array { bitmap { filename = "stimulus_sns_1.jpg"; } bitmap_non_neutral_1; bitmap { filename = "stimulus_sns_2.jpg"; } bitmap_non_neutral_2; bitmap { filename = "stimulus_sns_3.jpg"; } bitmap_non_neutral_3; bitmap { filename = "stimulus_sns_4.jpg"; } bitmap_non_neutral_4; bitmap { filename = "stimulus_sns_5.jpg"; } bitmap_non_neutral_5; } array_non_neutral_bitmaps; array { bitmap bitmap_neutral_1; bitmap bitmap_neutral_2; bitmap bitmap_neutral_3; bitmap bitmap_neutral_4; bitmap bitmap_neutral_5; bitmap bitmap_non_neutral_1; bitmap bitmap_non_neutral_2; bitmap bitmap_non_neutral_3; bitmap bitmap_non_neutral_4; bitmap bitmap_non_neutral_5; }array_bitmaps; trial { trial_type = first_response; trial_duration = forever; stimulus_event { picture { bitmap { filename = "stimulus_neutral_1.jpg"; } bitmap_trial_test; x = 0; y = 0; text { caption = "Handelt es sich um ein Icon mit Bezug zu Instagram? \n Bitte drücke die Taste \"A\" für \"Ja\" und die Taste \"L\" für \"Nein\""; }; x = 0; y = -300; } picture_trial_test; } stimulus_event_trial_test; } trial_test; trial { trial_type = fixed; trial_duration = 1500; picture { text { caption = " "; } text_feedback; x = 0; y = 0; }; } trial_feedback; trial { trial_type = fixed; trial_duration = EXPARAM("Pause at start of each block"); picture { text { caption = " "; }; x = 0; y = 0; }; } trial_pause_start_of_block; trial { trial_type = specific_response; trial_duration = forever; terminator_button = 2; picture { bitmap { filename = "stimulus_feedback_overview.jpg"; }; x = 0; y = 0; }; } trial_feedback_overview; trial { trial_type = fixed; trial_duration = EXPARAM("Response Active Duration Stimuli"); stimulus_event { picture { bitmap { filename = "stimulus_neutral_1.jpg"; } bitmap_trial_stimuli; x=0;y=0; } picture_trial_stimuli; duration = EXPARAM("Visibility Duration Stimuli"); } stimulus_event_trial_stimuli; } trial_stimuli; trial { trial_type = fixed; picture { text { caption = "+"; font_size = 40; }; x=0;y=0; }; } trial_cross; trial { picture { text{ caption ="Pause\n\nSie haben 3 Minuten Pause. An dem Countdown erkennen Sie wann es weiter geht."; font_size = 30; }text_pause_top; x=0;y=300; text{ caption =" "; font_size = 30; }text_pause; x=0;y=100; text{ caption ="Bitte denken Sie daran:\n - So schnell und richtig wie möglich zu reagieren - Sie bekommen kein Feedback - Richten Sie Ihren Blick während der Aufgabe auf das Kreuz in der Mitte"; font_size = 30; }text_pause_bottom; x=0;y=-200; }; } trial_pause; trial { trial_type = specific_response; trial_duration = forever; terminator_button = 2; picture { text{ caption = "Gleich geht es weiter"; font_size = 40; }text_pause_button; x=0;y=0; }; } trial_pause_button; trial { trial_type = specific_response; trial_duration = forever; terminator_button = 2; picture { bitmap { filename="instruction_start.jpg"; }; x=0;y=0; }; } trial_instruction; trial { trial_type = specific_response; trial_duration = forever; terminator_button = 2; picture { bitmap { filename="instruction_test_run.jpg"; }; x=0;y=0; }; } trial_instruction_test_run; trial { trial_type = specific_response; trial_duration = forever; terminator_button = 2; picture { bitmap { filename="instruction_neutral_is_target.jpg"; }picture_instruction_block; x=0;y=0; }; } trial_instruction_block; trial { trial_type = specific_response; trial_duration = forever; terminator_button = 2; picture { bitmap { filename="instruction_end.jpg"; }; x=0;y=0; }; } trial_instruction_end;
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clc // Given that lambda = 1e-10 // wavelength of light in meter theta = 90 // angle in degree h = 6.62e-34 // Planck constant in J-sec c = 3e8 // speed of light in m/sec e = 1.6e-19 // charge on an electron in C m = 9.1e-31 // mass of an electron in kg // Sample Problem 26 on page no. 14.31 printf("\n # PROBLEM 26 # \n") printf("Standard formula used \n ") printf(" delta_lambda = (h / (m * c) * (1 - cos(theta))) \n E = h*c*(1/lambda1 - 1/lambda2)\n") delta_lambda = (h * (1 - cosd(theta))) / (m * c) E = (h * c) * ((1 / lambda) - (1 / (lambda + delta_lambda))) printf("\n Compton shift is %e m.\n Kinetic energy is %f eV.",delta_lambda,E / 1.6e-19)
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clc clear //Initialization of variables gam=62.4 pa=0 za=15 //ft va=0 pg=0 zg=0 g=32.2 //ft/s^2 d=4 //in dg=2 //in zd=25 //ft //calculations vg= sqrt(2*g*(pa/gam +za+va^2 /(2*g) -pg/gam - zg)) Ag=%pi/4 *(dg/12)^2 Q=Ag*vg A=%pi/4 *(d/12)^2 v4=Q/A pc=-v4^2 *gam/(2*g*144) pgd= za-zd - v4^2 /(2*g) pd=pgd*gam/144 pe=-v4^2 *gam/(2*g*144) pfg= za- v4^2 /(2*g) pf=pfg*gam/144 //results printf("Pressure at C = %.2f psig",pc) printf("\n Pressure at D = %.2f psig",pd) printf("\n Pressure at E = %.2f psig",pe) printf("\n Pressure at F = %.2f psig",pf)
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//find clc //solution //given W=5000//N dx=40//mm t1=850//N/mm^2 t2=850//N/mm^2 C=6 G=80000//N/mm^2 //ref fig 23.22 //D1-D2=2*d1 //D1=C*d1 //D2=C*d2 //d1/d2=1.5 //W1/W2=2.25....eq1 //W1+W2=W....eq2 //from 1 and 2,we get W1=3492//N W2=1538//N K1=(4*C-1)/(4*C-4)+(0.615/C) K2=K1 //d1=(K1*8*W1*C/(%pi*t1))^(0.5) d1=10 printf("dia of spring wires is,%f mm\n",(K1*8*W1*C/(%pi*t1))^(0.5)) printf("dia is ,say 10mm\n") printf("mean outer dia is,%f mm\n",6*d1) D1=6*d1 printf("dia of spring wires is,%f mm\n",(K2*8*W2*C/(%pi*t2))^(0.5)) printf("dia is ,say 6 mm\n") d2=6 printf("mean outer dia is,%f mm\n",6*d2) D2=6*d2 //n1=(8*W1*C^3)/(dx*G*d1) printf("number of turns are in outer coil,%f \n",1/[(8*W1*C^3)/(dx*G*d1)]) printf("numbr of turns are say 6\n") n1=6 n1b=n1+2 Ls1=n1b*d1 n2b=n1b*d1/d2 n2=n2b-2 printf("numbr of tuns in inner coil is,%f \n",n2) fL=Ls1+dx+0.15*dx printf("free length is,%f mm\n",fL) printf("outr dia of outr spring is,%f mm\n",D1+d1) printf("innr dia of outr spring is,%f mm\n",D1-d1) printf("outer dia of innr spring is,%f mm\n",D2+d2) printf("innr dia of innr spring is,%f mm\n",D2-d2)
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clc disp("the soln of eg 4.9-->Simultaneous O.D.E.") function dy_dx=fw(x,y,z); //let us have dy/dx=z, therefore d2y/dx2=dz/dx dy_dx=z, endfunction function dz_dx=fq(x,y,z); dz_dx=-y*x, endfunction y=2,z=1 for x=0:.1:3, h=.1 //step increment of 0.1 k1=h*fw(x,y,z) l1=h*fq(x,y,z) k2=h*fw(x+h/2,y+k1/2,z+l1/2) l2=h*fq(x+h/2,y+k1/2,z+l1/2) k3=h*fw(x+h/2,y+k2/2,z+l2/2) l3=h*fq(x+h/2,y+k2/2,z+l2/2) k4=h*fw(x+h,y+k3,z+l3) l4=h*fq(x+h,y+k3,z+l3) y=y+(k1+2*k2+2*k3+k4)/6 z=z+(l1+2*l2+2*l3+l4)/6 end y=y-(k1+2*k2+2*k3+k4)/6 z=z-(l1+2*l2+2*l3+l4)/6 disp(z,y,"the values of y and z repectively are");
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(unwatch all) (clear) (load "msgdisp.clp") (dribble-on "msgdisp.out") (testit) (dribble-off) (clear) (open "msgdisp.rsl" msgdisp "w") (load "compline.clp") (printout msgdisp "msgdisp.clp differences are as follows:" crlf) (compare-files msgdisp.exp msgdisp.out msgdisp) (close msgdisp)
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//Example 11.7 P=18;//Blood pressure (mm Hg) P=18*133/1.00;//Blood pressure (Pa) rho=1.00;//Density of fluid (g/ml) rho=rho*10^3;//Density of fluid (kg/m^3) g=9.80;//Acceleration due to gravity (m/s^2) h=P/(rho*g);//Height (m) printf('Height at which IV bag must be placed = %0.2f m',h) //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest
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clc //initialisation h=6.6*10^-34//j sec r=5.86*10^28 m=9.1*10^-31//kg gs=2 //CALCULATIONS a=(h*h/(2*m))*((3*r/(4*3.14*gs))^(2/3)) //resullts printf(' \n fermi energy= % 1e',a)
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//To find path and arc of contact clc //Given: t=20, T=40 m=10 //mm phi=20 //degrees //Solution: //Addendum height for each gear wheel: //Calculating the pitch circle radius of the smaller gear wheel r=m*t/2 //mm //Calculating the pitch circle radius of the larger wheel R=m*T/2 //mm //Calculating the radius of addendum circle for the larger gear wheel RA=sqrt((r*sind(phi)/2+R*sind(phi))^2+R^2*(cosd(phi))^2) //mm //Calculating the addendum height for larger gear wheel addendumg=RA-R //mm //Calculating the radius of addendum circle for the smaller gear wheel rA=sqrt((R*sind(phi)/2+r*sind(phi))^2+r^2*(cosd(phi))^2) //mm //Calculating the addendum height for smaller gear wheel addendump=rA-r //mm //Calculating the length of the path of contact Lpc=(r+R)*sind(phi)/2 //Length of the path of contact, mm //Calculating the length of the arc of contact Lac=Lpc/cosd(phi) //Length of the arc of contact, mm //Contact ratio: //Calculating the circular pitch pc=%pi*m //mm //Calculating the contact ratio CR=Lpc/pc //Contact ratio //Results: printf("\n\n Addendum height for larger gear wheel = %.1f mm.\n\n",addendumg) printf(" Addendum height for smaller gear wheel = %.1f mm.\n\n",addendump) printf(" Length of the path of contact = %.1f mm.\n\n",Lpc) printf(" Length of the arc of contact = %.1f mm.\n\n",Lac) printf(" Contact ratio = %d.\n\n",CR+1)
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//Chemical Engineering Thermodynamics //Chapter 4 //Second Law of Thermodynamics //Example 4.5 clear; clc; //Given //Air at 20 deg celsius //P1 = 250;initial pressure in atm //P2 = 10;final pressure after throttling in atm //To calculate the entropy change //According to the given conditions from figure4.5(page no 103) S1 = -0.38;//initial entropy in Kcal/Kg K S2 = -0.15;//final entroy in Kcal/Kg K del_S = S2-S1; mprintf('Change in entropy for the throttling process is %f Kcal/Kg K',del_S); //From figure 4.6(page no 104), the final temperature is -10 deg celsius //end
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//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% //% For model hidden parameters //% 2004. 8. Mengzhen KANG,Wulin //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% //clear all; close all; //exec('bin/gl_begin.sci'); xdel(winsid()); //close all graphics window disp('Using lsqr to estimate GreenLab model parameters.'); //exec(INTER_SYS_DIR+'/bin/glob_declare.sci'); exec(GL_SYS_DIR+'bin'+SEPARATOR+'glob_declare.sci'); // Read parameter file //if exists('Flag_TCL')//under interface mode //if 0 if exists('Flag_TCL') FileName=ParaFileName; else //command line mode FileName = xgetfile('*.sci', GL_SYS_DIR+'parafiles',title='open parameter file'); end realFile = FileName; [Filepath,FileID,Fileextension]=fileparts(FileName);//get file ID [fid, %v] = mopen(FileName, 'r'); if %v then disp('Parameter file read error.'); abort; end exec(GL_SYS_DIR+'bin'+SEPARATOR+'gl_read.sci'); mclose(fid); // Read target file if exists('Flag_TCL')//under interface mode FileName=DataFileName; else //command line mode FileName = xgetfile('*.dat', GL_SYS_DIR+'targetfiles',title='open target file'); end realFile = FileName; [fid, %v] = mopen(FileName, 'r'); if %v then disp('Target file read error.'); abort; end exec(GL_SYS_DIR+'bin'+SEPARATOR+'gl_read_target.sci'); //Load climate data fun = GL_SYS_DIR+'bin'+SEPARATOR+'env_fun.sci'; [water_sequence, theta_sequence, light_sequence, GC_index] = gl_env(Flag_environment, Flag_sumt, Omega, aux_paras,THETA_BASE, KSUMT, N); // organ ID: 1 blade, 2 petiel, 3 internode, 4 female flower, 5 male flower, 6 layer, 7 root //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% //% T O P O L O G Y O F P L A N T ---- C O M P U T I N G A U T O M A T O N //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% printf('Determinist Topological computation ...');timer(); if ~exists('Flag_TCL') then Flag_C_code = 1; Flag_Sci_code = 0; end if Flag_C_code == 1 then // c StateO = Gl_StateOccupy(Tu_O); [S,Nb_BI,DL,Nb_O] = topo(N,maxp,nr,RingOption,Nu_Ma,st_j,b_o,br_a,re_a,Flag_pruning,Pruning_delay,T_Pr,Nu_I,rs_A,rs_B,rt_a,Nu_O,Tu_O,StateO); end; if Flag_Sci_code == 1 then //scilab [S,Nb_O,Nb_BI,DL]= gl_topo_phy(N,maxp,Nu_Ma,Nu_I,Nu_O,st_j,b_o,br_a,re_a,rs_A,rs_B,rt_a,T_Pr,Tu_O,Flag_pruning,Pruning_delay,RingOption); end; printf(string(timer())+' seconds.\n'); //exec(GL_SYS_DIR+'bin'+SEPARATOR+'gl_disp_topo.sci'); x0 = x_Para; disp('Beginning of fitting process...'); //stop=[1.d-6,1.d-6,1.d-3,20,0,100]; [xval, fvec, info] = lsqrsolve(x0, sim_fit_HiddenPara_Vec, size(target_set,2)); disp('Done...'); select info case 0 then disp('improper input parameters.') case 1 then disp('algorithm estimates that the relative error between x and the solution is at most tol.') case 2 then disp('number of calls to the function reached.') case 3 then disp('tol is too small. No further improvement in the approximate solution x is possible.') case 4 then disp('iteration is not making good progress.') end printf("\n"); if Flag_C_code == 1 then printf('executing using C code\n'); end; if Flag_Sci_code == 1 then printf('executing using Scilab code\n'); end; //write the fit parameters into a file named optim\result\FileID_fit.m,which can be used for initial value of next fitting procedure exec(GL_SYS_DIR+'bin'+SEPARATOR+'gl_write_FitPara.sci'); //display figures exec(GL_SYS_DIR+'bin'+SEPARATOR+'gl_output_FitResult.sci'); if exists('Flag_TCL') then if Flag_TCL == 0 x_message('fitting finished.'); mdelete(GL_SYS_DIR+'targetfiles'+SEPARATOR+'targettempfile.sci'); end TCL_EvalFile(GL_SYS_DIR+'inttcl'+SEPARATOR+'fit_result_inscilab.tcl'); end clear Flag_TCL
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f=2//N/m^2( Shear stress) du=0.25//m/s(Velocity of plate) dy=0.5//mm(Distance between the two plates)
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function hasil=gausnaif(A,b) [m n]=size(A); M=[A b]; for j=1:n-1 for i = j+1:n M(i,:)=-M(i,j)/M(j,j)*M(j,:)+M(i,:); end end hasil=M; // nA=M(1:n,1:n); //nB=M(:,n+1); // hasil=sbalik(nA,nB); endfunction function hasil = sbalik(A,b) [m n]=size(A); x(n)=b(n)/A(n,n); for k=n-1:-1:1 jum =0; for j=k+1:n jum=jum+A(k,j)*x(j); end, x(k)=(b(k)-jum)/A(k,k); end hasil=x; endfunction
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//**********************************************// //**************Projet*Math*Fi******************// //**********************************************// funcprot(0) // Pour simuler W a l'instant T on ecrit une fonction function [W_T] = brownien(N,T,Sigma) n=size(Sigma);n=n(2); W_T = sqrt(T) * Sigma * rand(n,N,"gauss"); endfunction function [S_T] = black_scholes(N,T,S_0, r,sigma, Sigma) n=size(Sigma);n=n(2); d=prod(size(S_0)); S_T = diag(S_0) * (exp(T * diag(r - sigma.^2/2) * ones(d,N) + brownien(N,T,Sigma))); endfunction function [Y] = payoff_call_basket(a,S_T,K) // S_T est une matrice d*N // I_T et Y sont des vecteurs 1*N I_T= a' * S_T; Y=max(I_T-K,0); endfunction function [Y] = payoff_put_basket(a,S_T,K) // S_T est une matrice d*N // I_T et Y sont des vecteurs 1*N I_T= a' * S_T; Y=max(K-I_T,0); endfunction function []=test_simple(N,K,fonction_payoff) S_T=black_scholes(N,T,S_0, r,sigma, Sigma); payoff=exp(-r*T) * fonction_payoff(a,S_T,K); estimation=mean(payoff); ecart_type=stdev(payoff); // estimation de l'ecart type erreur=1.96*ecart_type/sqrt(N); // demi-largeur de l'intervalle de confiance printf("Direct N=%d, %f +- %f\n",N, estimation, erreur); endfunction function []=test_avec_vc(N,K,fonction_payoff) S_T=black_scholes(N,T,S_0, r,sigma, Sigma); I_T=a' * S_T; payoff= exp(-r*T) * (fonction_payoff(a,S_T,K)-I_T); // A COMPLETER -- comment utiliser la variable de controle ? estimation=mean(payoff) + I_0;// l'esperance de la variable de controle vaut I_0 ecart_type=stdev(payoff); // estimation de l'ecart type erreur=1.96*ecart_type/sqrt(N); // demi-largeur de l'intervalle de confiance printf("Direct VC N=%d, %f +- %f\n",N, estimation, erreur); endfunction function []=test_importance_sampling(N,K,fonction_payoff,optimal_m) W_T = sqrt(T) * rand(d,N,"gauss"); m = optimal_m(K,fonction_payoff); S_T = diag(S_0) * (exp(T * diag(r - sigma.^2/2) * ones(d,N) + (Sigma * (W_T + m) ) ) ); payoff = exp(-r*T) * fonction_payoff(a,S_T,K); importance = exp(-sum(W_T.*m,1)-sum(m.*m,1)*T/2); payoff = importance .* payoff; estimation=mean(payoff); // estimation de la moyenne ecart_type=stdev(payoff); // estimation de l'ecart type erreur=1.96*ecart_type/sqrt(N); // demi-largeur de l'intervalle de confiance printf("Importance N=%d, %f +- %f, mean(drift)=%f\n", N, estimation, erreur, mean(m)); endfunction //// Find_optimal_drift from Paul GLASSERMAN function [m]=Find_optimal_drift_GLAS(K,fonction_payoff) m_old=zeros(d,1); for i=1:100 //disp(i) W_T = sqrt(T) * Sigma * m_old; S_T = diag(S_0) * (exp(T * (r - sigma.^2/2) + W_T ) ); //disp(fonction_payoff(a,S_T,K)>0) for j=1:d m(j)=(fonction_payoff(a,S_T,K)>0)*sqrt(T)*(a'*(S_T.*Sigma(:,j)))/(a'*S_T); end if norm(m-m_old)<0.0005 break; end m_old=m; end m=repmat(m,1,N); endfunction //// Find_optimal_drift from Bouhari AROUNA function[gamma_n]=gamma_coeff(alpha,Beta,n) gamma_n = alpha/(Beta+n); endfunction function[U]=U_coeff(n) U = (n==0)*100+(n~=0)*(sqrt(log(n)/6)+100); endfunction function[sigma_n]=sigma_function(sigma_n_old,norme) sigma_n = sigma_n_old; U=U_coeff(sigma_n_old); sigma_n(length(sigma_n)+1)=sigma_n_old endfunction function [m]=Find_optimal_drift_Aroun(K,fonction_payoff) m_old=zeros(d,1); alpha=1; Beta=1; for n=1:10000 //disp(n) Z_n=rand(d,1,"gauss"); W_T = sqrt(T) * Sigma * Z_n; S_T = diag(S_0) * (exp(T * (r - sigma.^2/2) + W_T ) ); payoff = exp(-r*T) * fonction_payoff(a,S_T,K); Y_n = (m_old-Z_n)*(payoff**2)*exp(-m_old'*Z_n+0.5*m_old'*m_old); m = m_old - gamma_coeff(alpha,Beta,n)*Y_n; //disp(m) end //m=repmat(mean(m),d,N); m=repmat(m,1,N); endfunction //// Find_optimal_drift from direct minimization with scilab optim function function [m]=Find_optimal_drift_sci(K,fonction_payoff) m=zeros(d,N); for i=1:N //G_T = rand(d,1,"gauss"); G_T = 1/sqrt(T)*W_T(:,i); function [f, g, ind]=cost(x, ind) f = exp(-x'*G_T+0.5*x'*x); g = f*(x-G_T); endfunction m0=zeros(d,1); [fopt, mopt] = optim(cost, m0); m(:,i)=mopt; end m = mean(m,2); m = repmat(m,1,N); endfunction //////////// Main Function ////////// //// Initialisation/Calcul des coefficients // dimension du vecteur d'actifs risqués d=10; // Matrice de covariance des mouvements browniens rho=0.5; Rho = (1 - rho) *eye(d,d) + rho * ones(d,d); // Matrice de corrélationd es browniens // Les volatilites de chaque actif sigma=0.3*ones(d,1); S_0=100*ones(d,1); Gamma = diag(sigma) * Rho * diag(sigma); // fabrique la matrice sigma_i * Rho_ij * sigma_j (et oui!) Sigma=sqroot(Gamma); // Calculons une racine carree de Gamma //disp(norm(Sigma*Sigma' - Gamma)) T=1; //1 an r=0.05; //Taux instantanné annuel // Pondération du panier/de l'indice a=(1/d)*ones(d,1); S_0=100*ones(d,1); I_0= a'*S_0; //// Appel des fonctions stacksize(268435454); N=10000; //Nombre de termes pour la méthode de Monte Carlo K= 1.5 * a'*S_0; // option out of the money test_simple(N,K,payoff_call_basket); test_avec_vc(N,K,payoff_call_basket); // la variable de controle augmente la variance ! test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_GLAS); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_Aroun); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_sci); K= 1.0 * a'*S_0; // option at the money test_simple(N,K,payoff_call_basket); test_avec_vc(N,K,payoff_call_basket); // la variable de controle marche mais pas terrible test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_GLAS); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_Aroun); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_sci); K= 0.8 * a'*S_0; // option in the money test_simple(N,K,payoff_call_basket); test_avec_vc(N,K,payoff_call_basket); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_GLAS); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_Aroun); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_sci); // ce coup ci la variable de controle sert a qq chose ! // Plus K est petit et mieux ca marche K= 0.5 * a'*S_0; test_simple(N,K,payoff_call_basket); test_avec_vc(N,K,payoff_call_basket); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_GLAS); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_Aroun); test_importance_sampling(N,K,payoff_call_basket,Find_optimal_drift_sci);
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//A Textbook of Chemical Engineering Thermodynamics //Chapter 9 //Chemical Reaction Equilibria //Example 20 clear; clc; //Given: //Reaction: C2H4(g) + H2O(l) --> C2H5OH(aq) P = 85; //pressure in bar n_e = 0.015; //mol percent of ethanol n_w = 0.95; //mole percent of water n_a = 0.48; //mol percent of ethylene in vapour phase M = 18; //molecular mass of water fc = 0.9; //fugacity coeffecient for ethylene //To evaluate the equilibrium constant //K = a_c/(a_a*a_b) m_e = n_e/(n_w*M*10^-3); //mol/kg water a_c = m_e; fa = fc*n_a*P; //bar a_a = fa; //Since mol fraction of water is close to unity, so fugacity coeffecient of water is assumed to be 1 a_b = n_w; K = a_c/(a_a*a_b); mprintf('The equilibrium constant is %5.4e (mol C2H4)/(kg water bar)',K); //end
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//pagenumber 376 example 8 clear vdd=10;//volt beta1=10^-4;//ampere per square volt ids=0.5*10^-3;//ampere voltag=1;//volt vgs=(sqrt(ids/beta1)+(1)); rd=(vdd-vgs)/ids; disp("vgs = "+string((vgs))+"volt"); disp("rd = "+string((rd))+"ohm");
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clear //Given I=10 //A A=4*10**-6 //m**2 e=1.6*10**-19 //C n=8*10**28 //m**-3 l=4 //Calculation Vd=I/(n*A*e) t=l/Vd //Result printf("\n Time required by an electron is %0.3f *10**4 S", t*10**-4)
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//example 4.3 //calculate precipitation at x clc;funcprot(0); //given pA=6.6; //precipitation at A pB=4.8; //precpitation at B pC=3.7; //precipitation at C nA=72.6; //normal precipitation at A nB=51.8; //normal precipitation at B nC=38.2; //normal precipitation at C nX=65.6; //normal precipitation at X pX=(nX*pA/nA+nX*pB/nB+nX*pC/nC)/3; pX=round(pX*100)/100; mprintf("precipitation at x=%f cm.",pX);
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CrvonsfHiddenData.sci
// 08.09.19 function Out=CrvonsfHiddenData() global CRVONSFHIDDENDATA Out=CRVONSFHIDDENDATA; endfunction;
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clc // initialization of variables clear tR=0.02 // t/R ration E_A=69 //G Pa v_A=0.33 // Poisson's ratio alpha_A=21.6*10^-6 // /degree Celcius (Coefficient of expansion) E_S=207 // G Pa v_S=0.280 alpha_S=10.8*10^-6 // /degree Celcius (Coefficient of expansion) // calculations // Sig_LA=a*p+b*delT+c*sig_thS // Sig_LS=v_S*Sig_thS+d*delT E_S=E_S*10^9 E_A=E_A*10^9 a=1/tR*E_A/E_S b=-2/3*alpha_S*E_S c=-E_A/E_S d=-alpha_S*E_S // SigthS=e*p+f*delT // SigthA=g*p+h*delT e=37.16 f=0.8639*10^6 g=1/tR-e h=-f // results p=689.4 // kPa delT=100 // degree Celcius p=p*10^3 // Pa SigthA=g*p+h*delT SigthS=e*p+f*delT Sig_LA=a*p+b*delT+c*SigthS Sig_LS=v_S*SigthS+d*delT printf('Thus, for p = %.1f k Pa and delT = %.d degree celcius \n',p/10^3,delT) printf(' SigthA = %.1f M Pa, Sig_LA = %.d M Pa \n',SigthA/10^6,Sig_LA/10^6) printf(' SigthS = %.1f M Pa, Sig_LS = %.d M Pa',SigthS/10^6,Sig_LS/10^6)
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Example9_3.sce
// Electric Machinery and Transformers // Irving L kosow // Prentice Hall of India // 2nd editiom // Chapter 9: POLYPHASE INDUCTION (ASYNCHRONOUS) DYNAMOS // Example 9-3 clear; clc; close; // Clear the work space and console. // Given data P = 4 ; // Number of poles in Induction motor f = 60 ; // Frequency in Hz s_f = 5*(1/100) ; // Full-load rotor slip // Calculations // case a // slip, s = (S -S_r)/S ; // where S = Speed in rpm of the rotating magnetic field and // S_r = Speed in rpm of the rotor s = 1 ; // Slip = 1, at the instant of starting, since S_r is zero f_r_a = s * f ; // Rotor frequency in Hz at the instant of starting // case b f_r_b = s_f * f ;// Full-load rotor frequency in Hz // Display the results disp("Example 9-3 Solution : "); printf(" \n a: At the instant of starting, slip s = (S -S_r)/S ; "); printf(" \n where S_r is the rotor speed. Since the rotor speed at the "); printf(" \n instant of starting is zero, s = (S - 0)/S = 1 , or unity slip."); printf(" \n\n The rotor frequency is \n f_r = %d Hz \n\n ", f_r_a); printf(" \n b: At full-load,the slip is 5 percent(as given), and therefore"); printf(" \n s = %.2f \n f_r = %d Hz " , s_f , f_r_b);
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// SAMPLE PROBLEM 3/15 clc;clear;funcprot(0); // Given data h_1=500;// km v_1=30000;// km/h h_2=1200;// km R=6371;// km g=9.81;// The acceleration due to gravity in m/sec^2 // Calculation v_2=sqrt((v_1/3.6)^2+((2*g*(R*10^3)^2)*((10^-3/(R+h_2))-(10^-3/(R+h_1))))); printf("\nThe velocity of the satellite as it reaches point B,v_2=%4.0f m/s (or) v_2=%5.0f km/h",v_2,v_2*3.6);
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function ckSumHex=hrtFrameCalcCkSum(strFrame,comCkSum) //Recebe -> Frame com o ultimo byte de ckSum inserido e sem preambulo. //Retorna -> O ckSum do strFrame correto. vetData = hex2dec(tokens(part(strFrame,hrtFrameIni(strFrame):$),' ')); ckSumDec = vetData(1); for i=2:length(vetData)-comCkSum ckSumDec=bitxor(ckSumDec,vetData(i)); end ckSumHex = msprintf("%02s",dec2hex(ckSumDec)); endfunction
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x=[0 0.0112910099304681; 0.0375437844553138; -0.0502505723940154; 0.0237536810920502; 0.00286337692936232; -0.0268585407773543; -0.00670100836859748; 0.00681025234400021; 0.0743232780915911]; fs=4e6; R=risetime(x,fs); disp(R); //output // // 0.0000002
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clc n=3.6 R=[(n-1)/(n+1)]^2 disp(R,"R is= ")
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//CHAPTER 2- STEADY-STATE ANALYSIS OF SINGLE-PHASE A.C. CIRCUIT //Example 1 disp("CHAPTER 2"); disp("EXAMPLE 1"); //Find the Form Factor of the half-wave rectified sine wave as shown in Fig 2.20 //Peak value of voltage is Vm //Period is 2pi //v=Vm sinwt for 0<wt<pi //v=0 for pi<wt<2pi //SOLUTION //average value Vav by integrating v over 0 to pi and pi to 2pi and dividing by 2pi //assume Vm=1, as value not given //The second term of integration not computed as v=0 on the range pi to 2pi v_av=(integrate('sin(x)','x',0,%pi))/(2*%pi); //rms value //assume Vm=1, as value not given v_rms=(integrate('sin(x)^2','x',0,%pi))/(2*%pi); v_rms=sqrt(v_rms); ff=v_rms/v_av; //truncate the answer to 3 digits while displaying: disp(sprintf("The form factor is %4.3f",ff));//The answer in the textbook is wrongly shown as 1.572 //END
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Ch01Ex7.sci
// Scilab Code Ex1.7 Relativistic variation of mass with speed: Pg: 22 (2008) m0 = 1e-024; // Mass of a particle, kg v = 1.8e+08; // Speed of the particle, m/s c = 3e+08; // Speed of light, m/s m = m0/sqrt(1-(v/c)^2); // Mass of the moving particle, kg printf("\nThe mass of moving particle = %4.2e kg", m); // Result // The mass of moving particle = 1.25e-024 kg
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gainat.sci
// Gain at a point on a root locus function [K,p] = gainat(G) z = locate(1,1); x = z(1);y = z(2); p = x + %i*y; disp( p , 'p = '); K = 1 / abs(horner(G,p)) disp( K , 'K = '); plot(x,y,'.'); xstring(x,y,'K = ' + string(K)); endfunction
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PL/SQL Developer Test script 3.0 20 -- Created on 23.09.2014 by ZHURAVOV_VB declare -- Local variables here m xxdoo.xxdoo_db_merge; begin -- Test statements here m := xxdoo.xxdoo_db_merge(); -- m.m('table','t'); m.us.s('field1'); m.us.s('field2'); m.us.f('table(t) o'); m.i('field1'); m.i('field2'); m.u('field2'); m.o('field1'); -- dbms_output.put_line(m.get_text); -- end; 0 0
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Chapter14_Example9.sce
//Chapter-14, Example 14.9, Page 591 //============================================================================= clc clear //INPUT DATA T=50;//Temperature of air stream in degree C Tb=22;//Bulb temperature in degree C //CALCULATIONS Tf=(T+Tb)/2;//Film temperature in degree C p=1.14;//Density in kg/m^3 Cp=1.006;//Specific heat in J/kg.K Pr=0.7;//Prantl number u=(2*10^-5);//Dynamic viscosity in Ns/m^2 DAB=(0.26*10^-4);//DAB value in m^2/s Sc=(u/(p*DAB));//Schmidt nuber Le=(Sc/Pr);//Lewis number p1=0.01920;//Density in kg/m^3 hfg=2449;//Enthalpy in kJ/kg pA=0.0064;//Density in kg/m^3 psat=(1/12.23);//Saturation density in kg/m^3 RH=(pA/0.0817)*100;//Relative humidity //OUTPUT mprintf('Relative humidity of the airstream is %3.2f percent',RH) //=================================END OF PROGRAM==============================
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//finding output voltage// //example 4// clc //clears the command window// clear //clears// V1=10;//voltage source amplitude// Rf=50;//forward rsistance// r1=50;//internal resistance// i=V1*Rf/(Rf+r1) //current through diode during positive half cycle// C=10^-6 T=(Rf+r1)*C;//time constant during conduction// f=10*10^3 T1=1/(2*f);//time duration during which input voltage is positive// t=50*10^-6;//given time// v=V1*(1-exp(-(t/T)));//voltage across capacitor after 50micro sec// Vo=((V1-v)*Rf)/(Rf+r1);//output voltage across diode// R=20*10^3;//resistance in series// T2=(r1+R)*C;//time constant of discharging circuit// V2=v*exp(-(t/T2));//voltage at the end of 50 micro sec// printf('output voltage=%f volt',V2) //result is displayed//
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Chapter2_Example18.sce
//Chapter-2, Illustration 18, Page 76 //Title: Gas Power Cycles //============================================================================= clc clear //INPUT DATA Tmin=300;//Minimum temperature in K Tmax=1073;//Maximum temperature in K Cp=1.005;//Specific heat at constant pressure in kJ/kg-K //CALCULATIONS Wmax=Cp*((sqrt(Tmax)-sqrt(Tmin))^2);//Maximum work output in kJ/kg nB=(1-sqrt(Tmin/Tmax))*100;//Brayton cycle efficiency nC=(1-(Tmin/Tmax))*100;//Carnot efficiency r=nB/nC;//Ratio of brayton cycle efficiency to carnot efficieny //OUTPUT mprintf('Maximum work per kg of air is %3.2f kJ/kg \n Cycle efficiency is %3.0f percent \n Ratio of brayton cycle efficiency to carnot efficieny is %3.3f',Wmax,nB,r) //==============================END OF PROGRAM=================================
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clear// //Variable Declaration D=250 //Wideness in mm b=20 //Thickness of the plate in mm r=50 //Radius of the hole in mm e=50 //Eccentricity in mm sigma_max=150 //Maximum normal stress at the hole in MPa kb=2 //Stress Concentraion factor //Calculations A=b*(D-2*r)*10**-6 //Area in m^2 I=10**-12*(b*D**3*12**-1-(b*2**3*r**3*12**-1)) //Moment of inertia in m^4 //Simplfying computation a=2*r*D**-1 kt=3-3.13*a+3.66*a**2-1.53*a**3 //Stress Concentration factor //Simplfying computation b=kt*A**-1 c=kb*r*r*10**-6*I**-1 P=10**3*sigma_max*(b+c)**-1 //Maximum Load in N //Result printf("\n The maximum value of P is %0.1f kN",P)
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//Example 1_33 clc; clear;close; //Given data: RL=10;//ohm V=100;//V t_off=50*10^-6;//s C=t_off/RL/log(2);//F disp(C,"Value of C(F)");
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clc clear //Initialization of variables D=36 //in rho=0.00226 //slug/ft^3 mu=3.88e-7 //lb-sec/ft^2 umax=62.2 //ft/s V=54.5 //ft/s Nr=9.5e5 r0=18 //in r=12 //in n=8.8 k=0.4 //calculations f=0.0032 + 0.221/(Nr^0.237) Vs=sqrt(f/8) *V y=r0-r delta1=D*5*sqrt(8) /(Nr*sqrt(f)) vss=70 thick=13*delta1 //results printf("Outer edge of buffer zone is at %d",vss) printf("\n Thickness of buffer zone = %.4f in",thick)
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Ex2_21.sce
clear // // //Initilization of Variables P=20*10**3 //N //Load d=6 //mm //diameter of wire E=2*10**5 //N/mm**2 L_BO=4000 //mm //Length of BO //Calculations //Let theta be the angle between OA and OB and also between OC and OB theta=30 //Let P_OA,P_OB,P_OC be the Forces introduced in wires OA,OB,OC respectively //Due to symmetry P_OA=P_OC (same angles) //Sum of all Vertical Forces=0 //P_OA*cos(theta)+P_OB+P_OC*cos(theta)=P //After further simplifyinf we get //2*P_OA*cos(theta)+P_OB=20 ...............(1) //Let oo1 be the extension of BO //oo1=L_A1o1*(cos(theta))**-1 //From relation we get //P_OB*L_BO=P_OA*L_AO*(cos(theta))**-1 //But L_AO=L_BO*(cos(theta))**-1 //After substituting value of L_AO in above equation we get //P_OB=0.75*P_OA .......................(2) //substituting in Equation 1 we get //2*P_OA*cos(theta)+0.75*P_OA=20 P_OA=20*(2*cos(theta*%pi*180**-1)+0.75)**-1 P_OB=0.75*P_OA A=%pi*4**-1*d**2 //Vertical displacement of Load dell_l_BO=P_OB*10**3*L_BO*(A*E)**-1 //Result printf("\n Forces in each wire is:P_OA %0.2f KN",P_OA) printf("\n :P_OB %0.2f KN",P_OB) printf("\n Vertical displacement of Loadis %0.2f mm",dell_l_BO)
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clc //Intitalisation of variables clear a= 6.4*10^-6 //g ion per lit a1= 0.05 n= 2 //CALCULATIONS Ksp= a^2*a1 s= (Ksp/n^2)^(1/3) //RESULTS printf ('Ks = %.2e ',Ksp) printf ('\n solubility of Ag2CrO4 = %.2e mole per litre',s)
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function r=%sp_q_sp(a,b) //r=a.\b // Copyright INRIA r=full(a).\full(b)
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//Horizontal force P //refer fig.8.14 //Applying virtual work principle //-1500*(delta(s)*sind(30))+P*delta(s)*cosd(30)+0=0 P=1500*tand(30) //N printf("Magnitude of P=%.2f N",P)
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clc; clear; //case1: disp('To find no. of primary & secondary turns:') Bm1=1.5;//Max flux density of primary in tesla Vt1=10.7;//Terminal voltage of primary in volts Bm2=1.46;//Max flux density of secondary in tesla Vt2=10.46;//Terminal voltage of secondary in volts V1=11000;//Primary RMS voltage in volts V2=415;//Secondary RMS voltage in volts P=300e3;//Input power in volt-amphere N2=(V2)/(Vt2);//No.of turns in secondary N1=(V1)/(Vt1);//No.of turns in primary disp(N1,'No of turns in primary is') disp(N2,'No of turns in secondary is') //case2: disp('To find rated current:') I1=P/(V1); I2=P/(V2); disp(I1,'The primary rated current in amps is') disp(I2,'The secondary rated current in amps is') //case3: disp('To find primary &secondary load impedance:') Z1=(V1)/(I1); Z2=(V2)/(I2); disp(Z1,'The primary load impedance in ohms is') disp(Z2,'The secondary load impedance in ohms is')