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//Example 2.32 clc disp("C = 20 pF, L2 = 1000 uH, L1 = 100 uH, M = 20 uH") leq=100+1000+40 format(5) disp(leq,"Therefore, L_eq(in uH) = L1 + L2 + 2M =") f=(1/(2*%pi*sqrt(1140*20*10^-18)))*10^-6 format(6) disp(f,"Therefore, f(in MHz) = 1 / 2*pi*sqrt(L_eq*C) =") disp("The feedback fraction beta is given by,") b=100/1100 format(7) disp(b,"beta = V_f/V0 = X_L1 / X_L1+X_L2 = L1 / L1+L2 =") disp("It is a Hartley oscillator")
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clc RE=5*14000/3600; //Total refrigeration produced in kg/s h2=183.19; //kJ/kg h3=209.41; //kJ/kg h4=74.59; //kJ/kg h1=h4; disp("(i) The refrigerant flow rate") RE_net=h2-h1; //Net refrigerating effect produced per kg m=RE/RE_net; disp("Refrigerant flow rate =") disp(m) disp("kg/s") disp("(ii) The C.O.P. =") COP=(h2-h1)/(h3-h2); disp(COP) disp("(iii) The power required to drive the compressor =") P=m*(h3-h2); disp(P) disp("kW") disp("(iv) The rate of heat rejection to the condenser =") rate=m*(h3-h4); disp(rate) disp("kW")
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// A Textbook of Fluid Mecahnics and Hydraulic Machines - By R K Bansal // Chapter 2 - Pressure and its measurements // Problem 2.19 //Given Data Set in the Problem dens=1000 g=9.81 sg_oil=0.8 h1=20/100 h2=30/100 h3=30/100 //calculations dens_oil=sg_oil*dens dl=h1+h2-h3 //Pressure in left limb below X-X=pA-dens*g*h2 //Pressure in left limb below X-X=pB-dens*g*h3-sg_oil*dens*h1 pB_pA=dens*g*h3+sg_oil*dens*g*h1-dens*g*h2 mprintf("The difference in the pressures is equal to %f N/m^2\n",pB_pA)
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//Find the loop inductance and reactance clear; clc; //soltion //given r=(1.213*10^-2)/2;//m//radius of the conductor d=1.25;//m//spacing f=50;//Hz//freq re=r*exp(-1/4); L=4*10^-7*log(d/re); Lkm=L*1000; printf("Inductance per km(L)=%.2f*10^-4 H/Km\n",Lkm*10^4); X=2*%pi*f*Lkm; printf("Reactance(X)= %.1f ohm/km",X);
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clear; clc; printf('FUNDAMENTALS OF HEAT AND MASS TRANSFER \n Incropera / Dewitt / Bergman / Lavine \n EXAMPLE 5.4 Page 278 \n'); //Example 5.4 // Radial System with Convection //Operating Conditions h = 500; //[W/m^2.K] Heat Convection coefficientat inner surface k = 63.9; //[W/m.K] Thermal Conductivity rho = 7832; //[kg/m^3] Density c = 434; //[J/kg.K] Specific Heat alpha = 18.8*10^-6; //[m^2/s] L = 40*10^-3; //[m] Metre Ti = -20+273; //[K] Initial Temp Tsurr = 60+273; //[K] Temp of oil t = 8*60 ; //[sec] time D = 1 ; //[m] Diameter of pipe //Using eqn 5.10 and 5.12 Bi = h*L/k; Fo = alpha*t/L^2; //From Table 5.1 at this Bi C1 = 1.047; eta = 0.531; theta0=C1*exp(-eta^2*Fo); T = Tsurr+theta0*(Ti-Tsurr); //Using eqn 5.40b x=1; theta = theta0*cos(eta); Tl = Tsurr + (Ti-Tsurr)*theta; q = h*[Tl - Tsurr]; //Using Eqn 5.44, 5.46 and Vol per unit length V = pi*D*L Q = [1-(sin(eta)/eta)*theta0]*rho*c*%pi*D*L*(Ti-Tsurr); printf("\n (a) After 8 min Biot number = %.2f and Fourier Numer = %.2f \n\n (b) Temperature of exterior pipe surface after 8 min = %i degC \n\n (c) Heat Flux to the wall at 8 min = %i W/m^2 \n\n (d) Energy transferred to pipe per unit length after 8 min = %.2e J/m",Bi,Fo, T-273,q,Q); //END
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// Prob 1.5 clc; clear; close; format('v',6); // Given data ph=3;//no. of phase P=16;//no. of poles s=144;//no. of slots con=10;//no. of conductors per slot fi=0.035;//in Wb N=375;//in rpm f=P*N/120;//in Hz disp(f,"Frequency in Hz : "); s1=s/P;//no. of slots per pole m=s1/ph;//no. of slots per pole per phase alfa=180/s1;//slot angle in degree Kd=sind(m*alfa/2)/(m*sind(alfa/2));//distribution factor TotCon=s*con;//Total no. of conductors TotCon1=s*con/ph;//Total no. of conductors n=TotCon1/2;//no. of turns per phase EMF=4.44*Kd*fi*f*n;//EMF per phase in volt disp(EMF,"EMF per phase in volt : "); VL=sqrt(3)*EMF;//line voltage in volt disp(VL,"Line EMF in volt : ");
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clear;lines(0); // create a script file write(TMPDIR+'/myscript','a=1;b=2') // execute it exec(TMPDIR+'/myscript') who //create a function deff('y=foo(x)','a=x+1;y=a^2') clear a b //execute the function foo(1) // a is a variable created in the environment of the function foo // it is destroyed when foo returns who x=1 //create x to make it known by the script foo exec(foo) // a and y are created in the current environment who
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clear clc //function y = funcao(x) // y=(x(1) - 2).^4 + (x(1)-2*x(2)).^2; //endfunction function grad_x = gradiente(x) n = length (x); h = 1e-5; gg = []; for i = 1 : n x_adv = x x_adv(i) = x(i) + h; dev = (f(x_adv)- f(x))/h; gg = [gg; dev]; end grad_x = gg; endfunction function linha = derivada1(x,yj,dj) h = 1e-5; linha = (func_teta(x + h,yj,dj)- func_teta(x - h,yj,dj))/ (2*h); endfunction function duas_linha = derivada2 (x,yj,dj) h = 1e-5; duas_linha = (func_teta(x + h,yj,dj) - (2*func_teta(x,yj,dj)) + func_teta(x - h,yj,dj))/h.^2; endfunction function valor_teta=func_teta(x,yj,dj) valor_teta=f(yj+x*dj); endfunction function lambda = newton (lambda,yj,dj) //lambda = 10; tolerance = 10^-3; erro = 10; while (erro > tolerance) lambda_novo = lambda - (derivada1(lambda,yj,dj)/derivada2(lambda,yj,dj)); erro = abs (lambda_novo - lambda); lambda = lambda_novo; end lambda = lambda_novo; endfunction function otimo = steepest_descent(xk) erro = 1; tol = 1e-4; while erro > tol dk = -gradiente (xk); lambdak = newton (0.1,xk,dk); xk_new = xk + lambdak*dk erro = norm (gradiente(xk_new) - gradiente(xk)); xk = xk_new; end otimo = xk endfunction
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//o/p when char type is given as i/p a = 'hash'; efinal = 0.2; // Step prediction error r = poly2ac(a,efinal); // Autocorrelation sequence disp(r); //Output // !--error 4 //Undefined variable: rlevinson //at line 41 of function poly2ac called by : //r = poly2ac(a,efinal); // Autocorrelation seque //at line 5 of exec file called by : //ly2ac\poly2ac6.sce', -1
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//Chapter 2 : Diffraction clear; //Variable declaration lamda2=4992 //wavelenght //Calculations lamda=(4*lamda2)/3 //Result mprintf("Lamda= %d Armstrong",lamda)
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// This file is part of www.nand2tetris.org // and the book "The Elements of Computing Systems" // by Nisan and Schocken, MIT Press. // File name: projects/04/mult/Mult.tst load Divide.asm; set RAM[13] 16383, set RAM[14] 128; repeat 5000 { ticktock; }
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clc clear x1 = [1 4 3] x2 = [1 2 3 2 5] m = length(x1) n = length(x2) if m>n then //padding given two arrays for making same length x2 = [x2 zeros(1,(m-n))] elseif m<n then x1 = [zeros(1,(n-m)) x1] else disp("no padding") end s = x1 + x2 //sample-1 m = x1.*x2 //sample-1 y = 2*x1 + 3*x2 //mod-1 subplot(311) plot2d3(s) title("x1 + x2") xlabel("time") ylabel("amplitude") subplot(312) plot2d3(m) title("x1 * x2") xlabel("time") ylabel("amplitude") subplot(313) plot2d3(y) title("2*x1 + 3*x2") xlabel("time") ylabel("amplitude")
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//chapter 2 //Rrad=80*pi^2*(dl/lambda)^2 printf("\n"); dl=0.1; printf("the elemental length is given by %g",dl); Rrad=80*(%pi)^2*(0.1)^2; printf("\nthe radiation resistance is %gohm",Rrad);
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// Scilab Code Ex11.2: Page-560 (2011) clc;clear; E_o = 1e+3;....// Amplitude field vector in free space,N/C c = 3e+8;....// Speed of light,in m/s // From the relation between the amplitude of the field vector E and vector H of an EM wave in free space E_o = H_o*(sqrt(mu_o/eps))and B_o = mu_o*H_o, we have B_o = E_o/c; printf("\nThe maximum value of magnetic induction vector = %4.2e weber/A-m",B_o); // Result // The maximum value of magnetic induction vector = 3.33e-006 weber/A-m
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//Example No.9.10. //Page No 272. clc;clear; d = 10^(-6);//Electrical conductivity -[ohm^-1 m^-1]. e = 1.6*10^(-19);//Electron charge. ue = 0.85;//Electron mobility -[m^2 V^-1 s^-1]. uh = 0.04;//hole mobility -[m^2 V^-1 s^-1]. Ni = (d/(e*(ue+uh)));//intrinsic carrier concentration printf("\nThe intrinsic carrier concentration of GaAs is %3.3e m^-3",Ni);
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s=%s R1=100*10^3 R2=10^6 C1=10*10^-6 C2=10^-6 T1=(1/R1)*(1/(s*C1))*(1/R2)*(1/(s*C2)) L1=-1/(s*C1*R1); L2=-1/(s*R2*C1); L3=-1/(s*C2*R2); delta=1-(L1+L2+L3)+(L1*L3) del1=1; TF=(T1*del1)/delta ; disp(TF,"C/R = ")
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// 最適化手法入門 //以下のような x ( R^6)を探す: //C1*x = b1 (3 個の等式拘束 すなわち me=3) C1= [1,-1,1,0,3,1; -1,0,-3,-4,5,6; 2,5,3,0,1,0]; b1=[1;2;3]; //C2*x <= b2 (2 個の不等式拘束) C2=[0,1,0,1,2,-1; -1,0,2,1,1,0]; b2=[-1;2.5]; // xはciおよびcsの間: ci=[-1000;-10000;0;-1000;-1000;-1000]; cs=[10000;100;1.5;100;100;1000]; // 以下の条件のもとで 0.5*x'*Q*x + p'*x を最小化 p=[1;2;3;4;5;6]; Q=eye(6,6); //初期値を指定しない; C=[C1;C2]; b=[b1;b2]; me=3; [x,iact,iter,f]=qpsolve(Q,p,C,b,ci,cs,me) // 線形拘束 (1 から 4) のみアクティブ disp(x)
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clc; t=1200; //time in second P=100; //power in Watts V=230; //voltage in Volts R=(V^2)/P; //calculating resistance V1=115; //supply voltage in Volts E=((V1^2)*t)/R; //calculating energy disp(E,"Energy dissipated by bulb in Joule = "); //displaying result
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clc clear //INPUT DATA c=3*10^8;//Speed of light in m/s //CALCULATIONS v=((sqrt(3)*c)/2)/10^8//Speed in m/s //OUTPUT mprintf('The mass of the object is double its mass at rest, when its speed is %3.3f*10^8 m/s',v)
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If=0.99;Vt=100;Ia=120;Ra=0.1; Rpm1=932;Rpm2=1000; Ifeff=0.86;Nf=1200; rpm1=1000; Ifeff1=1.32;Rpm3=800; EA=65; Ea=Vt-(Ia*Ra) Ea1=Rpm2/Rpm1*Ea Ifar=If-Ifeff At=Nf*Ifar Ea2=Rpm2/Rpm3*Ea Nsr=(Ifeff1-If+Ifar)*(Nf)/(Ia+If) Ifeff2=If-(Nsr*(Ia+If))/Nf-Ifar N=(Ea/EA)*Rpm2
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clc; F=96500/3600; //calculating 1F disp(F,"1 Faraday in ampere.hr = "); //displaying result
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Engineering Thermodynamics by Onkar Singh,Chapter 1,Example 27") T1=(27+273);//initial temperature of air in k T2=500;//final temperature of air in k disp("let inlet state be 1 and exit state be 2") disp("by charles law volume and temperature can be related as") disp("(V1/T1)=(V2/T2)") disp("(V2/V1)=(T2/T1)") disp("or (((%pi*D2^2)/4)*V2)/(((%pi*D1^2)/4)*V1)=T2/T1") disp("since Δ K.E=0") disp("so (D2^2/D1^2)=T2/T1") disp("D2/D1=sqrt(T2/T1)") disp("say(D2/D1)=k") disp("so exit to inlet diameter ratio(k)") k=sqrt(T2/T1)
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// Scilab ( http://www.scilab.org/ ) - This file is part of Scilab // Copyright (C) 2013 - A. Khorshidi // // Copyright (C) 2012 - 2016 - Scilab Enterprises // // This file is hereby licensed under the terms of the GNU GPL v2.0, // pursuant to article 5.3.4 of the CeCILL v.2.1. // This file was originally licensed under the terms of the CeCILL v2.1, // and continues to be available under such terms. // For more information, see the COPYING file which you should have received // along with this program. function [cf, ind] = histc(n, data, normalization) // Example: // n = 10; // data = rand(1, 1000, "normal"); // [class_freq, ind] = histc(n, data) rhs = argn(2); if rhs < 2 error(msprintf(_("%s: Wrong number of input argument(s): At least %d expected.\n"), "histc", 2)); end if rhs == 3 & exists("normalization", "local") then if type(normalization) ~= 4 | size(normalization, "*") ~= 1 then error(msprintf(_("%s: Wrong type of input argument #%d: A single boolean expected.\n"), "histc", 3)); end else // By default, normalize the result normalization = %t end if type(n) ~= 1 & type(n) ~= 8 error(msprintf(_("%s: Wrong type for input argument #%d: A real matrix expected.\n"),"histc",1)); end if type(n) == 8 then n = iconvert(n, 0); // To pass to dsearch end if type(data) ~= 1 & type(data) ~= 8 error(msprintf(_("%s: Wrong type for input argument #%d: A real matrix expected.\n"),"histc",2)) end if type(data) == 8 then data = iconvert(data, 0); // To pass to dsearch end if length(n) == 1 then // The number of classes is provided if n < 1 error(msprintf(_("%s: Wrong value for input argument #%d: Must be in the interval %s.\n"),"histc",1,"[1, oo)")); elseif n ~= floor(n) error(msprintf(_("%s: Wrong type for input argument #%d: Integer expected.\n"),"histc",1)) end mind = min(data); maxd = max(data); if (mind == maxd) then mind = mind - floor(n/2); maxd = maxd + ceil(n/2); end cb = linspace(mind, maxd, n+1); // Class boundary else // The classes are provided cb = matrix(n, 1, -1); // Force row form if min(diff(cb)) <= 0 then error(msprintf(_("%s: Wrong values for input argument #%d: Elements must be in increasing order.\n"),"histc",1)) end end [ind, cf, info] = dsearch(data, cb); // cf: class frequency, ind: class number of each count // Normalization if normalization == %t then nd = size(data, "*"); // Number of data values cw = cb(2:$)-cb(1:$-1); // Bin width cf = cf./(nd*cw); // Normalization in bin heights //cf = cf./nd; // Heights normalization end endfunction
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clc;clear; //Example 4.3 //electron projected at an angle into a uniform electric field //given values v1=4.5*10^5;//initial speed in m/s alpha=37*%pi/180;//angle of projection in degrees E=200;//electric field intensity in N/C e=1.6*10^-19;//in C m=9.1*10^-31;//in kg a=e*E/m;//acceleration in m/s^2 t=2*v1*sin(alpha)/a;//time in s disp(t,'time taken by electron to return to its initial level is:') H=(v1^2*sin(alpha)*sin(alpha))/(2*a);//height in m disp(H,'maximum height reached by electron is:') s=(v1^2)*(2*sin(alpha)*cos(alpha))/(2*a);//displacement in m disp(s,'horizontal displacement(in m)when it reaches maximum height is:')
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clear; clc; printf("\t\t\tExample Number 4.10\n\n\n"); // heat loss for finite-length cylinder // illustration4.10 // solution d = 0.05;// [m] diameter of aluminium cylinder l = 0.1;// [m] length of aluminium cylinder Ti = 200;// [degree celsius] initial temperature of of cylinder Te = 70;// [degree celsius] environment temperature k = 215;// [W/m degree celsius] heat transfer coefficient of plate h = 525;// [W/square meter degree celsius] convection heat transfer coefficient alpha = 8.4*10^(-5);// [square meter/s] constant x1 = 0.00625;// [m] distance at which temperature is calculated from end t = 60;// [s] time after which temperature is measured r = 0.0125;// [m] radius at which temperature is calculated // we first calculate the dimensionless heat-loss ratio for the infinite plate and infinite cylinder which make up the multidimensional body // for the plate we have L = 0.05;// [m] A = h*L/k; B = h^(2)*alpha*t/k^(2); // from figure (4-14), for the plate, we read Q_by_Q_o_plate = 0.22; // for the cylinder r_o = 0.025;// [m] // so we calculate C = h*r_o/k; // and from figure(4-15) we have Q_by_Q_o_cyl = 0.55; // the two heat ratios may be inserted in equation(4-22) to give Q_by_Q_o_tot = Q_by_Q_o_plate+Q_by_Q_o_cyl*(1-Q_by_Q_o_plate); c = 896;// [J/kg degree celsius] specific heat of aluminium rho = 2707;// [kg/cubic meter] density of aluminium V = %pi*r_o^(2)*l;// [cubic meter] Qo = rho*c*V*(Ti-Te);// [J] Q = Qo*Q_by_Q_o_tot;// [J] the actual heat loss in the 1-minute printf(" the actual heat loss in the 1-minute is %f kJ",Q/1000);
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function Y=Ymin() global YMIN Y=YMIN; endfunction
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clear; clc; // RCFP-1d.sce // A + B <=> C // Adiabático // Estado estacionario // 2 reactores con enfriamiento intermedio // SISTEMA DE ECUACIONES DIFERENCIALES function dxdtau = f(tau,x) // Variables diferenciales CA = x(1) CB = x(2) CC = x(3) T = x(4) // Ecuación de Arrhenius kd = kd0*exp(-E/(R*T)) // Ecuación de Van't Hoff Keq = Keq0*exp(-H/(R*T)) // Velocidad de reacción // r = rd - ri = kd*CA*CB - ki*CC = kd*CA*CB - kd*CC/Keq r = kd*(CA*CB - CC/Keq) // Balance de materia para A // RDMP: d(V*CA)dt = -r*V dCAdtau = -r // Balance de materia para B // RDMP: d(V*Cb)dt = -r*V dCBdtau = -r // Balance de materia para C // RDMP: d(V*Cc)dt = r*V dCCdtau = r // Balance de energía // RDMP: d(V*RHO*CP*T)dt = -H*r*V dTdtau = -H*r/(RHO*CP) // Derivadas dxdtau(1) = dCAdtau dxdtau(2) = dCBdtau dxdtau(3) = dCCdtau dxdtau(4) = dTdtau endfunction // CONSTANTES kd0 = 1.75E8; // L/(mol*h) E = 62350; // J/mol Keq0 = 8.25E-22; // L/mol H = -136400; // J/mol R = 8.314; // J/(mol*K) RHO = 1150; // g/L CP = 3.8; // J/(g*K) F = 50; // L/h D = 3; // dm L = 800; // dm // ********* // REACTOR 1 // ********* // CONSTANTES L1 = 400; // dm V1 = %pi/4*D^2*L1 // L TAU1 = V1/F // h // ENTRADA CA0 = 1.5; CB0 = 2; CC0 = 0.1; // mol/L T0 = 310; // K x01 = [CA0;CB0;CC0;T0]; // TIEMPO DE RESIDENCIA tau1 = 0:TAU1/100:TAU1; // h l1 = 0:L1/100:L1; // dm // RESOLVER x1 = ode(x01,0,tau1,f); CA1 = x1(1,:); CA1s = CA1($) CB1 = x1(2,:); CB1s = CB1($) CC1 = x1(3,:); CC1s = CC1($) T1 = x1(4,:); T1s = T1($) XA1 = 1 - CA1/CA0; XA1s = XA1($) // ********* // REACTOR 2 // ********* // CONSTANTES L2 = L - L1; // dm V2 = %pi/4*D^2*L2 // L TAU2 = V2/F // h // ENTRADA x02 = [CA1s;CB1s;CC1s;T0]; // Enfriamiento: T1s => T0 // TIEMPO DE RESIDENCIA tau2 = 0:TAU2/100:TAU2; // h l2 = 0:L2/100:L2; // dm // RESOLVER x2 = ode(x02,0,tau2,f); CA2 = x2(1,:); CA2s = CA2($) CB2 = x2(2,:); CB2s = CB2($) CC2 = x2(3,:); CC2s = CC2($) T2 = x2(4,:); T2s = T2($) XA2 = 1 - CA2/CA0; XA2s = XA2($) // GRÁFICAS scf(1); clf(1); plot(l1,XA1,'m',l2,XA2,'m--'); xgrid; xlabel('l'); legend('XA1','XA2',-2,%f); scf(2); clf(2); plot(l1,T1,'r',l2,T2,'r--'); xgrid; xlabel('l'); legend('T1','T2',-2,%f); scf(3); clf(3); plot(T1,XA1,'mo-',T2,XA2,'m.-'); xgrid; xlabel('T'); legend('XA1','XA2',-2,%f); scf(4); plot(L1, XA2s,'mo'); xgrid; xlabel('L1'); ylabel('XA2s');
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// Exa 2.8 clc; clear; close; // Given data N_A = 6.025*10^23;// in /gm mole d = 10.5;// in gm/cc At = 108;// atomic weight of n = (N_A/At)*d;// in /cm^3 n = n * 10^6;// in /m^3 r = 10^-3;// in m A = %pi * ((r)^2);// in m^2 q = 1.6*10^-19; I = 2;// in A V = I/(n*q*A);// in m/s disp(V,"The drift velocity of an electron in m/s is"); // Note: There is calculation error to find the value of V (i.e. drift velocity), So the answer in the book is wrong
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clc //to calculate mass, momentum,total energy,kinetic energy c=3*10^8 //light speed (m/s) v=c/sqrt (2) //velocity (m/s) //let mo be the rest mass of the particle //relativistic mass m of the particle is m=mo/sqrt(1-(v/c)^2) m=1/sqrt (1-v^2/c^2) //in kg disp("mass m="+string(m)+" mo") //momentum p of the particle is p=mv p=m*v //in kg-m/s disp("momentum p="+string(p)+" mo") //total energy E of the particle E=m*c^2 //in J disp("energy E="+string(E)+" mo") //kinetic energy K=E-mo c^2 K=E-c^2 //in J disp("kinetic energy K="+string(K)+" mo") //answer is given in terms of m0 and c in the book
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Example29_9.sce
// A Texbook on POWER SYSTEM ENGINEERING // A.Chakrabarti, M.L.Soni, P.V.Gupta, U.S.Bhatnagar // DHANPAT RAI & Co. // SECOND EDITION // PART III : SWITCHGEAR AND PROTECTION // CHAPTER 3: SYMMETRICAL COMPONENTS' ANALYSIS // EXAMPLE : 3.9 : // Page number 493-494 clear ; clc ; close ; // Clear the work space and console // Given data I_A = 1000.0 // Current through line A(A) I_C = 0 // Current through line C(A) // Calculations I_B = 1000.0*exp(%i*180.0*%pi/180) // Current through line B(A) a = exp(%i*120.0*%pi/180) // Operator I_a0 = 1.0/3*(I_A+I_B+I_C) // Zero sequence component of current(A) I_b0 = I_a0 // Zero sequence component of current(A) I_c0 = I_a0 // Zero sequence component of current(A) I_a1 = 1.0/3*(I_A+a*I_B+a**2*I_C) // Positive sequence component of current(A) I_b1 = a**2*I_a1 // Positive sequence component of current(A) I_c1 = a*I_a1 // Positive sequence component of current(A) I_a2 = 1.0/3*(I_A+a**2*I_B+a*I_C) // Negative sequence component of current(A) I_b2 = a*I_a2 // Negative sequence component of current(A) I_c2 = a**2*I_a2 // Negative sequence component of current(A) // Results disp("PART III - EXAMPLE : 3.9 : SOLUTION :-") printf("\nCurrent in line A, I_A = %.f∠%.f° A", abs(I_A),phasemag(I_A)) printf("\nCurrent in line B, I_B = %.f∠%.f° A", abs(I_B),phasemag(I_B)) printf("\nCurrent in line C, I_C = %.f A", I_C) printf("\nSymmetrical current components of line A are:") printf("\n I_a0 = %.f A", abs(I_a0)) printf("\n I_a1 = %.1f∠%.f° A", abs(I_a1),phasemag(I_a1)) printf("\n I_a2 = %.1f∠%.f° A", abs(I_a2),phasemag(I_a2)) printf("\nSymmetrical current components of line B are:") printf("\n I_b0 = %.f A", abs(I_b0)) printf("\n I_b1 = %.1f∠%.f° A", abs(I_b1),phasemag(I_b1)) printf("\n I_b2 = %.1f∠%.f° A", abs(I_b2),phasemag(I_b2)) printf("\nSymmetrical current components of line C are:") printf("\n I_c0 = %.f A", abs(I_c0)) printf("\n I_c1 = %.1f∠%.f° A", abs(I_c1),phasemag(I_c1)) printf("\n I_c2 = %.1f∠%.f° A", abs(I_c2),phasemag(I_c2))
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Ex9_8.sce
// Calculating the maximum permissible output from a machine clc; disp('Example 9.8, Page No. = 9.33') // Given Data D = 2;// Diameter (in meter) ac = 50000;// Specific electric loading ez = 7.5;// emf generated in a conductor at no load (in Volts) // Calculation of the maximum permissible output from a machine P = %pi*D*ac*ez*10^(-3);// Maximum permissible output (in kW) disp(P,'Maximum permissible output (kW)='); //in book answer is 2350 (kW). The answers vary due to round off error
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clc; //Example 27.2 //page no 413 printf("Example 27.2 page no 413\n\n"); //plate and frame filter press is to be employed to filter a slurry m_dot_slurry=600*60//mass flow rate ,lb/h m=0.1//sluury contain 10% by mass solid m_dot_solids = m*m_dot_slurry//the solid flow rate in the slurry a=(1/5)//filter colth area required for 1 lb/h of solid A=m_dot_solids*(a)//filter colth area for 3600 lb/h of solids printf("\n filter colth area A=%f ft^2",A);
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4.sce
//Variable declaration mew_e=0.13; //mobility of electron(m**2/Vs) mew_h=0.05; //mobility of holes(m**2/Vs) e=1.6*10**-19; ni=1.5*10**16; //number of electron hole pairs N=5*10**28; //Calculation sigma1=ni*e*(mew_e+mew_h); //intrinsic conductivity(ohm-1 m-1) ND=N/10**8; n=ni**2/ND; sigma2=ND*e*mew_e; //conductivity(ohm-1 m-1) sigma3=ND*e*mew_h; //conductivity(ohm-1 m-1) //Result printf('intrinsic conductivity is %0.3f *10**-3 ohm-1 m-1 %0.3f \n',(sigma1*10**3),sigma2) printf('conductivity during donor impurity is %0.3f ohm-1 m-1 \n',sigma2) printf('conductivity during acceptor impurity is %0.3f ohm-1 m-1',int(sigma3))
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5 7 1 1 1 1 1 1 1 3 1 9 1 1 6 1 1 1 1 3 1 1 1 1 1 1 1 ~~~~~~~~~~~~~~~~~~~~~~~~~~ 21
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6_3_data.sci
// Aim:Refer Example 6-3 for Problem Description // Given: // Weight of Body: W=6000; //lb // Inclination of Weight: theta=30; //deg
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Example3_6.sce
//clear// //Example3.6: Time Shift Property of CTFS clear; close; clc; T =4; T1 = T/2; t = 0:T1/100:T1; Wo = 2*%pi/T; gt =(1/2)*ones(1,length(t)); a(1)=0; //k=0, ak =0 d(1)=0; for k =1:5 a(k+1) = (sin(%pi*k/2)/(k*%pi)); if(abs(a(k+1))<=0.01) a(k+1)=0; end d(k+1) = a(k+1)*exp(-sqrt(-1)*k*%pi/2); end k = 0:5 disp('Fourier Series Coefficients of Square Wave') a disp('Fourier Series Coefficients of g(t)=x(t-1)-0.5') d // figure a = gca(); a.y_location = "origin"; a.x_location = "origin"; a.data_bounds=[-1,-2;1,4]; plot2d([-t($:-1:1),t(1:$)],[-gt,gt],5) poly1 = a.children(1).children(1); poly1.thickness = 3; title('g(t)') xlabel(' t')
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example6_15.sce
//Chapter 6 //Example 6_15 //Page 119 clear;clc; md=50; lf=0.5; pf=0.75; fc=100; rc=0.05; lfc=600; id=0.1; x=fc; y=id*lfc; z=y/x; ec_pf=sqrt(1-z^2); kwd=md/lf; m1=kwd/pf; m2=kwd/ec_pf; as=fc*(m1-m2); printf("Max demand charge = Rs. %.0f/kVA/annum \n", x); printf("Expendiutre on capacitors = Rs. %.0f/kVA/annum \n", y); printf("Most economical pf = %.2f \n", ec_pf); printf("Max kW demand = %.0f kW \n", kwd); printf("Max kVA demand at %.2f pf = %.2f kVA \n", pf, m1); printf("Max kVA demand at %.2f pf = %.2f kVA \n", ec_pf, m2); printf("Annual saving = Rs. %.0f \n", as);
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5_2.sce
clc //initialisation of variables clear w= 62.4 //lbf/ft^3 g= 32.2 //ft/sec^2 v= 86.5 //ft/sec d2= 3 //in d1= 6 //in dp= 50 //lbf/in^2 //CALCULATIONS Fb= -((%pi*(w/g)*v^2*(1/d1)^2*(1-(d2/d1)^2)*0.25)-dp*144*(%pi/4)*(1/d2)^2) //RESULTS printf ('Load on the bolts = %.f lbf',Fb)
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Ex3_22.sce
// SAMPLE PROBLEM 3/22 clc;funcprot(0); // Given data m=150;// kg v_1=4;// m/s t_0=0;// s t_1=4;// s P=600;// N t_2=8;// s theta=30;// degree g=9.81;// The acceleration due to gravity in m/sec^2 // Calculation deltat=(m*0)+((m*v_1)-((v_1*2*P)/2)+(m*g*sind(theta)))/((2*P)+(m*g*sind(theta)));// s t_a=v_1+deltat;// s v_2x=((m*-v_1)+((v_1*2*P)/2)+(v_1*2*P)-(m*g*sind(theta)*t_2))/m;// m/s printf("\n(a)The time at which the skip reverses its direction,t_a=%1.2f s \n(b)The velocity of the skip,v_2x=%1.2f m/s",t_a,v_2x);
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Ex3_9.sce
clear // //Given //Variable declaration sigma1=100 //Major principal stress in N/sq.mm sigma2=-40 //Minor principal stress in N/sq.mm theta=90-60 //Angle of inclination in degrees //Calculation sigman=((sigma1+sigma2)/2)+(((sigma1-sigma2)/2)*cos((%pi/180)*(2*theta))) sigmat=((sigma1-sigma2)/2*(sin((%pi/180)*(2*theta)))) sigmaR=(sqrt(sigman**2+sigmat**2)) sigmat_max=int((sigma1-sigma2)/2) phi=int((180/%pi)*(atan(sigmat/sigman))) //Result printf("\n Resultant stress in magnitude = %0.3f N/mm^2",sigmaR) printf("\n Direction of resultant stress = %0.3f degrees",phi) printf("\n Maximum shear stress = %0.3f N/mm^2",sigmat_max)
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clc cl1=1.5 //Assigning values to parameters cl2=0.5*0.5*cl1 tec=cl1*3+cl2*4 tei=36 eo=500 n=eo*100/(eo+tei+tec) disp(n,"The efficiency is")
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Ex4_9.sce
// Initilization of variables // The given section is Z-section which is un-symmetrycal about both the axis b1=20 //cm // width of bottom flange t1=5 //cm // thickness of the bottom flange b2=2.5 //cm // thickness of the web of the flange t2=15 //cm // depth of the web b3=10 //cm // width of the top flange t3=2.5 //cm // thickness of the top flange // Calculations // Respective areas A1=b1*t1 // cm^2 // area of the bottom flange A2=b2*t2 // cm^2 // area of the web A3=b3*t3 // cm^2 // area of the top-flange // first we calculate the x co-ordinate of the centroid x1=b3-b2+(b1/2) //cm // for the bottom flange x2=b3-(b2/2) //cm // for the web x3=b3/2 //cm // for the top flange x_c=((A1*x1)+(A2*x2)+(A3*x3))/(A1+A2+A3) //cm // secondly we calculate the y co-ordinate of the centroid y1=t1/2 //cm // for the bottom flange y2=t1+(t2/2) //cm // for the web y3=t1+t2+(t3/2) //cm // for the top flange y_c=((A1*y1)+(A2*y2)+(A3*y3))/(A1+A2+A3) // cm // Results clc printf('The centroid of the cross-sectional area of a Z-section about x-axis is %f cm \n',x_c) printf('The centroid of the cross-sectional area of a Z-section about y-axis is %f cm \n',y_c)
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//Example 4.18 //Generate same floating point output in two different forms x = 5000.0; y = 0.0025; printf("%f %f %f %f\n\n", x, y, x*y, x/y); printf("%e %e %e %e", x, y, x*y, x/y);
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load Dis7.hdl, output-file Dis7.out, compare-to Dis7.cmp, output-list x%B3.1.3 y%B3.1.3 z%B3.1.3 w%B3.1.3 a%B3.1.3; set x 0, set y 0, set z 0, set w 0, eval, output; set x 0, set y 0, set z 0, set w 1, eval, output; set x 0, set y 0, set z 1, set w 0, eval, output; set x 0, set y 0, set z 1, set w 1, eval, output; set x 0, set y 1, set z 0, set w 0, eval, output; set x 0, set y 1, set z 0, set w 1, eval, output; set x 0, set y 1, set z 1, set w 0, eval, output; set x 0, set y 1, set z 1, set w 1, eval, output; set x 1, set y 0, set z 0, set w 0, eval, output; set x 1, set y 0, set z 0, set w 1, eval, output;
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## Copyright (C) 2006-2017 John W. Eaton ## ## This file is part of Octave. ## ## Octave is free software; you can redistribute it and/or modify it ## under the terms of the GNU General Public License as published by ## the Free Software Foundation; either version 3 of the License, or (at ## your option) any later version. ## ## Octave is distributed in the hope that it will be useful, but ## WITHOUT ANY WARRANTY; without even the implied warranty of ## MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU ## General Public License for more details. ## ## You should have received a copy of the GNU General Public License ## along with Octave; see the file COPYING. If not, see ## <http://www.gnu.org/licenses/>. %!shared x, a, b %! x = [1,2]; %! a = 1; %! b = 2; %!test %! y = [a... # comments here ok %! b]; %! assert (y, x); ## FIXME: Next 3 tests use '\' continuation outside of a double-quoted string ## This behavior is deprecated and will be removed at some point. ## When it does these %!test %! x = [1;2]; %! y = [a... # comments here ok %! ;\ %! %! b]; %! assert (y, x); %!assert (1 + ... %! 2 - \# comments here ok %! 3 / ... # comments here ok %! -1,6); %!function y = f (a,... %! b, ... %! c, ... % comments ok %! x, # continuation characters not required in parens %! y, \# but they should work too. %! z) %! %! y = 1; %!endfunction %! %!assert (f (), 1) # String continuation using '\' %!assert (["abc\ %! def"], "abc def") %!test %!assert (1 == 1 %! && 2 == 2 %! || 3 == 5); %!test %! x = [1, ... %! %! ... %! %! 2]; %! y = [1;2]; %! assert (y, x); %!test %! x = [1 ,... %! 2]; %! y = [1,2]; %! assert (y, x); %!test %! x = [ 1 , ... %! 2]; %! y = [1,2]; %! assert (y, x); %!test %! x = [ 1 , ...anything after the ... is ignored %! 2]; %! y = [1,2]; %! assert (y, x);
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// test3: // Código Scilab para graficar el resultado del test3, está escrito para el // caso de 20000 casos de prueba (n=20000). Si se desea modificar esta // cantidad se debe altirar el valor de n // clear() n = 20000 [fd,err] = mopen("ejercicioC.data",'r') for i=1:n [n,A(i,1),A(i,2),A(i,3)] = mfscanf(fd,"%f,%f,%d."); if A(i,3) == 1 then C(i,1) = A(i,1); C(i,2) = A(i,2); else B(i,1) = A(i,1); B(i,2) = A(i,2); end end mclose(fd) plot(C(:,1),C(:,2),'dr') plot(B(:,1),B(:,2),'dg')
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//Example 1_6 page no:24 clc; Vs=30; R1=5; R2=4; R3=2; R4=4; R5=1/((1/(R2))+(1/(R3))+(1/(R4))); Rt=R1+R5; It=Vs/Rt;//calculating the total current disp(It,"the total current is (in A)");
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//Example 3-3, Page No - 106 clear clc Pc = 30 m=0.85 Pt = Pc*(1+ (m^2/2)) Psb_both =Pt-Pc Psb_one = Psb_both/2 printf('The total power is %.1f watt \n The power in one sideband is %.1f watt',Pt,Psb_one)
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// Modified by Minho Kim (9 Oct 2014) load Decoder.hdl, output-file Decoder.out, compare-to Decoder.cmp, output-list in%B3.1.3 out%B2.2.1; set in 0, eval, output; set in 1, eval, output;
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// Grob's Basic Electronics 11e // Chapter No. 19 // Example No. 19_3 clc; clear; // How much is the inductance of a coil that induces 40 V when its current changes at the rate of 4 A/s? // Given data Vl = 40; // Induced voltage=40 Volts R = 4 // Current changing rate=di/dt=4 A/s L = Vl/R; disp (L,'The Value of Inductance in Henry')
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clc; p1=11; // Initial pressure in bar T1=40; // Initial temperature in degree celcius p2=60; // Final pressure in bar R_1=8.3143; // Universal gas constant in kJ/kmol K // The crictical properties for natural gas Tc=161; // Temperature in kelvin Pc=46.4; // Pressure in bar // Reduced properties are Pr1=p1/Pc; Pr2=p2/Pc; Tr1=(T1+273)/Tc; // T2=T1, The ideal gas enthalpy h2*=h1*=h1 h21=-47.5; // From generalized enthalpy departure chart M=16; // Molecular weight Sp2_1=(R_1/M)*log (p2/p1)// for the difference in ideal gas entropies Sp2_Sp_2=-0.1125; Sp_2_Sp_1=-2.1276; // Entropies in kJ/kg K s2_s1=(Sp2_Sp_2)+(Sp_2_Sp_1); q=(T1+273)*s2_s1; // Heat transfer w=q-h21; // Work of compression disp ("kJ/kg",w,"Work of compression = ","kJ/kg",q,"Heat transfer = ");
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//Example 27_8 clc(); clear; //To calculate the decay constant and half life of substance n_no=0.9 //Units in constant t=12 //Units in h lamda=log(1/n_no)/t //Units in h^-1 t1=round(0.693/lamda) //Units in h printf("The decay constant is lamda=%.7f h^-1\n The Half life is t0.5=%d h",lamda,t1)
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//Example 5_5 clc(); clear; //To find the lattice parameter of lead theta=30 //units in degrees n=1 l=1.54*10^-10 //units in meters d=(n*l)/(2*sin(theta*%pi/180)) h=2 k=2 l=0 a=d*(sqrt(h^2+k^2+l^2)) //units in meters a=a*10^10 //units in Armstrongs printf("Lattice parameter is a=%.1f A",a) //in text book the answer is printed wrong as 4.1A The answer is 4.4A nm
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clear; clc; disp("--------------Example 3.28---------------") dB1=-3; // signal is attenuated dB2=7; // signal is amplified dB3=-3; // signal is attenuated dB=dB1+dB2+dB3; // add to get final dB printf("The final decibel value is +%d dB . Hence the signal has gained in power.",dB); //display result
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clear; clc; close; t=0:1/100:10; w=1; theta=%pi/3; T=2*%pi/w; x=cos(t*w+theta); y=cos((t+T)*w+theta); if ceil(x)==ceil(y) then disp('cos(wo*t+theta) is periodic with T=2*pi/W0') else disp('nonperiodic') end
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// chapter 5 // example 5.6 // fig. E 5.6 // Determine power loss // page-182-183 clear; clc; // given t_r=2; // in us (rise time) R_DS_on=0.2; // in ohm (drain to source resistance when MOSFET is ON) D=0.7; // duty cycle f=30; // in kHz (frequency) V_DS=100; // in V (DC power supply) R_L=12; // in ohm (load resistance) // calculate I_D=V_DS/(R_L+R_DS_on); // calculation of drain current f=f*1E3; // changing unit from kHz to Hz T=1/f; // calculation of switching period t_on=D*T; // calculation of on-time W_on=I_D^2*R_DS_on*t_on; // calculation of energy loss during on-time P_on=W_on*f; // calculation of power loss during on-time printf("\nThe power loss in the on-state is \t\t P_on=%.2f W",P_on); t_r=t_r*1E-6; // changing unit from us to s W_ON=V_DS*I_D*t_r/6; // calculation of energy loss during turn-on interval P_ON=W_ON*f; // calculation of power loss during turn-on interval printf("\nThe power loss during the turn-on interval is \t P_ON=%.1f W",P_ON);
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clc //initialisation of variables clear T1= 100 //C T2= 90 //C p= 76 //cm of hg H= 542*18.02 //cal mole^-1 //CALCULATIONS p1= p/10^((H/4.576)*((T1-T2)/((273.2+T1)*(273.2+T2)))) //RESULTS printf ('Final vapour pressure of water = %.1f cm',p1)
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Name=Motemote Aimer Hard PlayerCharacters=Aimer BotCharacters=BOT1.bot;BOT2.bot IsChallenge=true Timelimit=30.0 PlayerProfile=Aimer AddedBots=BOT1.bot;BOT1.bot;BOT1.bot PlayerMaxLives=1 BotMaxLives=0;0;0 PlayerTeam=1 BotTeams=2;2;2 MapName=mote.map MapScale=2.5 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.1 ScoreToWin=1000.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Fortnite,Apex, OW, Click-Timing, Flick,Valorant WeaponHeroTag=Revolver DifficultyTag=2 AuthorsTag=@Lac0caL BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=true Description=EZ GameVersion=2.0.1.2 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=true LockedFOVMin=75.0 LockedFOVMax=110.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=Aimbot MinReactionTime=0.1 MaxReactionTime=0.1 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=90.0 FlickSpeed=10.0 FlickError=0.0 TrackSpeed=10.0 TrackError=0.0 MaxTurnAngleFromPadCenter=90.0 MinRecenterTime=0.0 MaxRecenterTime=0.0 OptimalAimFOV=90.0 OuterAimPenalty=0.0 MaxError=0.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=BOT1 DodgeProfileNames=Long Strafes DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=3.0 WeaponProfileWeights=100.0;100.0;100.0;100.0;100.0;100.0;100.0;100.0 AimingProfileNames=Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=BOT1 SeeThroughWalls=true NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=BOT2 DodgeProfileNames=Long Strafes DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=3.0 WeaponProfileWeights=100.0;100.0;100.0;100.0;100.0;100.0;100.0;100.0 AimingProfileNames=Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot;Aimbot WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=BOT2 SeeThroughWalls=true NoDodging=false NoAiming=true AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=Aimer MaxHealth=1.0 WeaponProfileNames=Revolver;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=0.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=50.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=500.0 Acceleration=0.0 AirAcceleration=16000.0 Friction=0.0 BrakingFrictionFactor=0.0 JumpVelocity=0.0 Gravity=1.0 AirControl=0.0 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=Cuboid MainBBHeight=270.0 MainBBRadius=60.0 MainBBHasHead=true MainBBHeadRadius=30.0 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=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=false BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=0.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=Endo CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=BOT1 MaxHealth=3.0 WeaponProfileNames=Shotgun;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=30.0 MovementType=Base MaxSpeed=3200.0 MaxCrouchSpeed=500.0 Acceleration=3000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=7.0 AirControl=0.0 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=true AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cuboid MainBBHeight=300.0 MainBBRadius=60.0 MainBBHasHead=true MainBBHeadRadius=30.0 MainBBHeadOffset=0.0 MainBBHide=true 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=999.0 BlockSpawnFOV=30.0 BlockSpawnDistance=333.0 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 TerminalVelocity=0.0 CharacterModel=Endo CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=true ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=BOT2 MaxHealth=3.0 WeaponProfileNames=BB 3;;;;;;; MinRespawnDelay=60.0 MaxRespawnDelay=60.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=30.0 MovementType=Base MaxSpeed=600.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 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=Cuboid MainBBHeight=300.0 MainBBRadius=60.0 MainBBHasHead=true MainBBHeadRadius=30.0 MainBBHeadOffset=0.0 MainBBHide=true 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=999.0 BlockSpawnFOV=0.0 BlockSpawnDistance=333.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=true 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 TerminalVelocity=0.0 CharacterModel=Endo CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=true ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Long Strafes MaxTargetDistance=0.0 MinTargetDistance=0.0 ToggleLeftRight=false ToggleForwardBack=false MinLRTimeChange=1000.0 MaxLRTimeChange=1000.0 MinFBTimeChange=1.0 MaxFBTimeChange=1.0 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=TargetShootingSoon TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.75 MaxJumpTime=0.75 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.025 BlockedMovementReactionMax=0.05 WaypointLogic=Ignore WaypointTurnRate=0.1 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Weapon Profile] Name=Revolver Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=90.0 TimeBetweenShots=0.2 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=5.0 MagazineMax=7 AmmoPerShot=1 ReloadTimeFromEmpty=2.0 ReloadTimeFromPartial=2.0 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.5 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=true ADSZoomDelay=0.1 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=30.0 RecoilNegatable=false DecalType=0 DecalSize=200.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=1.0 FlatKnockbackVertical=1.0 HitscanRadius=0.0 HitscanVisualRadius=1.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=2.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=3 CancelReloadOnKill=false FlatKnockbackHorizontalMin=1.0 FlatKnockbackVerticalMin=1.0 ADSScope=No Scope ADSFOVOverride=80.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Law Bringer WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=1.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Bolt Action Sniper 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=Bullet ParticleWallImpact=None ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=Bullet ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=5.0 ParticleBodyImpactScale=10.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=10000.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=4.0 MinRecoilUp=2.0 MinRecoilHoriz=1.0 MaxRecoilHoriz=1.5 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.03 TimeToRecoilReset=0.2 AAMode=0 AAPreferClosestPlayer=true AAAlpha=1.0 AAMaxSpeed=360.0 AADeadZone=0.0 AAFOV=120.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=Shotgun Type=Projectile ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.1 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=0.1 MaxHitscanRange=100000.0 GravityScale=10.0 HeadshotCapable=false HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=2.0 ReloadTimeFromPartial=2.0 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=3.0 DelayBeforeShot=0.0 ProjectileGraphic=Shuriken VisualLifetime=0.1 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=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=3.0 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=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=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=6 CancelReloadOnKill=true 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=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=111.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Minigun 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=Blood ParticleProjectileTrail=None ParticleHitscanTrace=Tracer ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=100.0 ParticleProjectileTrailScale=30.0 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=0.0,0.1,0.0,0.0 SpreadSCA=0.0,0.1,0.0,0.0 SpreadMSA=0.0,0.1,0.0,0.0 SpreadMCA=0.0,0.1,0.0,0.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=0.0,0.1,0.0,0.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=0.0,0.1,0.0,0.0 MaxRecoilUp=4.0 MinRecoilUp=4.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.45 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 [Weapon Profile] Name=BB 3 Type=Projectile ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=30.0 TimeBetweenShots=5.0 Pierces=true Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=1000.000 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=10.0 MaxHitscanRange=100000.0 GravityScale=0.07 HeadshotCapable=false HeadshotMultiplier=10.0 MagazineMax=3 AmmoPerShot=1 ReloadTimeFromEmpty=2.0 ReloadTimeFromPartial=2.0 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=50.0 DelayBeforeShot=0.0 ProjectileGraphic=Arrow VisualLifetime=0.3 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=1.0 ProjectileEnemyHitRadius=0.75 CanAimDownSight=true ADSZoomDelay=0.1 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=30.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=1111.0 FlatKnockbackVertical=1111.0 HitscanRadius=30.0 HitscanVisualRadius=7.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=25.0 AimPunchResetTime=0.05 AimPunchCooldown=0.1 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=5.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=1111.0 FlatKnockbackVerticalMin=1111.0 ADSScope=No Scope ADSFOVOverride=70.0 ADSFOVScale=Clamped Horizontal ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Stud Gun WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Minigun 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=Rocket ParticleHitscanTrace=Bullet ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=0.9 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=3.0 MinRecoilUp=1.0 MinRecoilHoriz=0.5 MaxRecoilHoriz=1.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.03 TimeToRecoilReset=0.55 AAMode=0 AAPreferClosestPlayer=true AAAlpha=1.0 AAMaxSpeed=360.0 AADeadZone=0.0 AAFOV=360.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 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//A Textbook of Chemical Engineering Thermodynamics //Chapter 6 //Thermodynamic Properties of Pure Fluids //Example 27 clear; clc; //Given: T = 473; //temperature in K P = 50*10^5; //pressure in Pa d = 24.3; //density of ammonia (kg/m^3) m = 17; //molecular wt of ammonia R = 8.314; //ideal gas constant //To estimate the fugacity of ammonia V = m/(d*1000); //molar volume of ammonia (m^3/kmol) //Using eq. 6.142 (Page no. 234) f = (V*(P^2))/(R*T); mprintf('The fugacity of ammonia is %f bar',f/10^5); //end
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// Calculate the values of resistance R1 and R2 clc; E_20=0.112*10^-3;// emf at 20degree C E_900=8.446*10^-3; E_1200=11.946*10^-3; E1=E_900-E_20; E2=E_1200-E_20; disp('E1=1.08*R1/(R1+2.5+R2); (i)') disp('E2=1.08*(R1+2.5)/(R1+2.5+R2); (ii)') disp('on solving (i) and (ii)') R1=5.95; R2=762.6; disp(R1,'value of resistance R1 (ohm)=') disp(R2,'value of resistance R2 (ohm)=')
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//Example 5.16 //To Find out Bilinear Transformation of HS=2/((s+1)*(s+2)) clear; clc ; close ; s=%s; z=%z; HS=2/((s+1)*(s+2)); T=1; HZ=horner(HS,(2/T)*(z-1)/(z+1)); disp(HZ,'H(z) =');
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// chapter 7 , Example 7.7 , pg 211 rho=2300 //resistivity (in ohm*m) for Si (value given in book is wrong) ni=1.6*10^16 //intrinsic concentration (in m^-3) Ue=0.15 //electron mobility (in m^2/(V*s)) e=1.6*10^-19 //charge of electron (in C) // assuming 1*1*1 (in cm) dimension of Si crystal l=10^-2 //length (in m) b=10^-2 //breadth (in m) w=10^-2 //width (in m) Nsi=5*10^28 // (in atoms/m^3) x=1/10^9 //doping concentration A=l*b //area (in m^2) R1=(rho*l)/A //resistance of pure Si crystal (in ohm) Nd=Nsi*x //donor concentration (in m^-3) p=ni^2/Nd //concentration of hole (in m^-3) sigma=Nd*Ue*e //coductivity of doped Si (in ohm^-1*m^-1) R=l/(sigma*A) //resistance of doped Si crystal (in ohm) printf("Resistance of pure Si crystal (in ohm)") disp(R1) printf("Resistance of doped Si crystal (in ohm)") disp(R) //answer given is wrong
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// test the foc funcprot(0); exec('foc.sci'); Id_back = 0; Iq_back = 0; theta = 0; Vdc = 12; Id = 0; Iq = 5; R = 2; Ed = 0; Eq = 0; ed = 0; eq = 0; [Id_back, Iq_back, theta, Ed, ed, Eq, eq] = foc(Id, Iq, Vdc, R, theta, Id_back, Iq_back, Ed, Eq, ed, eq);
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load Compl2.hdl, output-file Compl2.out, output-list s%B1.16.1; set ah %B1010010101011010, eval; set al %B0110101101011010, eval;
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//fiber optic communications by joseph c. palais //example 7.2 //OS=Windows XP sp3 //Scilab version 5.4.1 clc; clear all; //given eta=0.01//quantum efficiency of a detector lambda=0.8*(10^-6)//wavelength in m e=1.6*10^-19//charge of an electron in columb h=6.63*10^-34//plancks constant c=3*10^8//velocity of light in m/s // to find Row=(eta*e*lambda)/(h*c)//responsivity of detector in mA/W mprintf("Responsivity of detector=%f mA/W",Row*10^3)//multiplication with 10^3 converts the unit from A/W to mA/W
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// Y.V.C.Rao ,1997.Chemical Engineering Thermodynamics.Universities Press,Hyderabad,India. //Chapter-4,Example 10,Page 105 //Title:Final temperature //================================================================================================================ clear clc //INPUT N=100;//number of moles of carbon dioxide in mol T1=298;//initial temperature in K Q=1;//energy added as heat in MJ a=45.369;//coefficient in the specific heat capacity expression where Cp=a+bT+eT^-2 b=8.688*10^-3;//coefficient in the specific heat capacity expression where Cp=a+bT+eT^-2 e=-9.619*10^5;//coefficient in the specific heat capacity expression where Cp=a+bT+eT^-2 //Where Cp is in J/molK //CALCULATION delh=Q*10^6/N;//calculation of enthalpy in J Tguess=520;//The final temperature guess value in K used for solving the system of equations //The system of equations are defined by : //T2=T1+(delh/Cpm)--->A //Cpm=a+(b*Tm)+(e/T1T2)--->B Cpm_guess=a+(b*((T1+Tguess)/2))+(e/(T1*Tguess));//calculation of Cpm guess (in J/molK) to be used to determine T2 from Equation A T2_guess=T1+(delh/Cpm_guess);//calculation of T2 using Equation A (in K) based on the value of Cpm guess computed using Equation B tolerance=1e-6;//defining the tolerance limit to obtain convergence while abs(T2_guess-Tguess)>tolerance Tguess=T2_guess; Cpm_guess=a+(b*((T1+Tguess)/2))+(e/(T1*Tguess)); T2_guess=T1+(delh/Cpm_guess);//the iteration process to solve the system of equations end T2=T2_guess;//value of the final temperature of CO2 obtained upon solving the system of equations(A and B) in K //OUTPUT mprintf('\n The final temperature= %0.1f K\n',T2); //===============================================END OF PROGRAM===================================================
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// Exa 6.8 clc; clear; close; // Given data P=1000;// in ohm Q=1000;// in ohm S=100;// in ohm E=2;// in volt Rg=50;// in ohm R_desh= 101;// in ohm R=Q*S/P;// in ohm del_R= R_desh-R;// in ohm E_Th= E*[(R+del_R)/(R+del_R+S)- P/(P+Q)];// in volt R_Th= [(R+del_R)*S/(R+del_R+S)+ P*Q/(P+Q)];//in ohm Ig= E_Th/(R_Th+Rg);// in amp Ig=Ig*10^+6;// in micro amp disp(Ig,"The galvanometer current in micro amp")
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function builder_cpp() src_cpp_path = get_absolute_file_path("builder_cpp.sce"); lib_name = "xls_link"; entry_points = ["getObjExcelLink"; .. "destroyObjExcelLink"; .. "setOutputArgument"; .. "getInputArgument"; .. "getVariant"; .. "getXlFileFormatName"; .. "getXlFileFormat"; .. "IndToStr"]; file_names = ["AutomationHelper.cpp" "ExcelLink.cpp"; .. "MainObject.cpp"; .. "getInputArgument.cpp"; .. "setOutputArgument.cpp"; .. "xlFileFormat.c"; .. "Excel_utils.c"]; CFLAGS = "-DXLS_LINK_EXPORTS"; CFLAGS = CFLAGS + " " + ilib_include_flag(src_cpp_path); CC = ""; LIBS = ""; LDFLAGS = "ole32.lib oleaut32.lib user32.lib"; FFLAGS = ""; tbx_build_src(entry_points, .. file_names, .. "cpp", .. src_cpp_path, .. LIBS, .. LDFLAGS, .. CFLAGS, .. FFLAGS, .. CC, .. lib_name); endfunction builder_cpp(); clear builder_cpp;
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// // 08.08.24 // 09.08.12 // 09.08.13 // 13.11.30 Directon supported function Bowname(varargin) global BOWMIDDLE; Nargs=length(varargin); Siki=varargin(Nargs); Nargs=Nargs-1; // 13.11.30 Dr="c"; if Nargs>=1 then Tmp=varargin(Nargs); if type(Tmp)==10 Dr=Tmp; Nargs=Nargs-1; end end if Nargs==0 // 13.11.30 P=Mixop(1,BOWMIDDLE); elseif Nargs==1 // 13.11.30 Bdata=varargin(1); P=Bowmiddle(Bdata); else A=varargin(1); B=varargin(2); D=1/2*Vecnagasa(B-A); Tmp=varargin(3); if type(Tmp)==10 H=D*0.2; else H=Tmp*D*0.2; end; H=min(H,D); Ydata=MakeBowdata(A,B,H); Tmp=Bowmiddle(Ydata); P=Mixop(1,Tmp); end Expr(P,Dr,Siki); //13.11.30 endfunction
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//Solution 10-9 WD=get_absolute_file_path('10_09_solution.sce'); datafile=WD+filesep()+'10_09_example.sci'; clc; exec(datafile) //unit conversions V = V * 1000 / 3600; //from [km/hr] to [m/s] nu = mu / rho_water; Re = V * c / nu; printf("Reynolds number is %1.2e", Re); if Re < Re_cr then printf("\nHence the flow is laminar"); elseif Re >= Re_cr & Re < Re_tran printf("\nHence the flow is transitional"); else printf("\nHence the flow is turbulent"); end
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//Tested on Windows 7 Ultimate 32-bit //Chapter 3 Semiconductor Diodes and Miscellaneous Devices Pg no. 89 clear; clc; //Given Data r=1.0;//Diode resistance in ohms Rl=100;//Load resistance in ohms Ep=30;//Input supply voltage in volts peak //Solution disp("(a)"); Ip=Ep/(Rl+r)*1000;//peak current in milli-amperes Irms=Ip/sqrt(2);//rms current in milli-amperes Iavg=Ip/%pi;//average or d.c. value of current in in milli-amperes printf("The peak value of current = Ip=%d mA\n",Ip); printf("The rms value of current = Irms=%.1f mA\n",Irms); printf("The average or d.c. value of current = Iav=%.1f mA\n",Iavg); disp("(b)"); Pdc=(Iavg/1000)^2*Rl//d.c. output power in watts printf("The d.c. output power = Pdc=%.3f watts\n",Pdc); disp("(c)"); Pac=(Irms/1000)^2*(Rl+r);//input ac power in watts printf("The a.c. input power = Pin=%.2f watts\n",Pac); disp("(d)"); n=Pdc/Pac;//Rectification efficiency is output dc power over input ac power printf("Rectification efficiency= %d percentage",n*100); //Error in textbook as Irms=Ip/sqrt(2) and not Ip/2
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//determine the base and collector current and exact and approax dc alpha clear; clc; //soltion //given Ie=8.4*10^-3//A//emitter current Icbo=0.1*10^-6;//A//reverse leakage current Ib=0.008*Ie;//A//base current Ic=Ie-Ib; Icinj=Ic-Icbo; a0=Icinj/Ie; a=Ic/Ie; printf("Base current is %.1f uA\n",Ib*10^6); printf("Collector current %.4f mA\n",Ic*1000); printf("Exact value of alphha = %.7f\n",a0); printf("Approax value of alpha = %.3f",a);
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//practical interpolation //example 3.11 //page 99 clc;clear;close; x=[0.61 0.62 0.63 0.64 0.65 0.66 0.67]; y=[1.840431 1.858928 1.877610 1.896481 1.915541 1.934792 1.954237]; h=0.01//interval between values of x c=1; for i=1:6 d1(c)=y(i+1)-y(i); c=c+1; end c=1; for i=1:5 d2(c)=d1(i+1)-d1(i); c=c+1 end c=1; for i=1:4 d3(c)=d2(i+1)-d2(i); c=c+1; end c=1; for i=1:3 d4(c)=d3(i+1)-d3(i); c=c+1; end d=[d1(1) d2(1) d3(1) d4(1)]; x0=0.638; p=(x0-x(4))/h; y_x=y(4); y_x=y_x+p*(d1(3)+d1(4))/2+p^2*(d2(2))/2;//stirling formula printf(' the value at %f by stirling formula is : %f\n\n',x0,y_x); y_x=y(3); p=(x0-x(3))/h; y_x=y_x+p*d1(3)+p*(p-1)*(d2(2)/2); printf(' the value at %f by bessels formula is : %f\n\n',x0,y_x);
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clc; funcprot(0); // Initialization of Variable C=79.0;//in mm ra=11.42;//elevarion in image in mm rb=15.65;//elevarion in image in mm hb=651;//height of B in mm H=1500;//height in m //calculation delp=ra-rb;//pa=ra+c and pb=rb+c so ra-rb=pa-pb pa=ra+C; ha=hb+delp/pa*(H-hb); disp(ha,"height of A in m") clear()
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check_installed: module_and_function: pkg.version args: - salt assertion: assertNotEmpty
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// Exa 4.21 format('v',6) clc; clear; close; // Given data V_CC = 10;// in V R_C = 10;// in k ohm R_C = R_C * 10^3;// in ohm R_B = 100*10^3;// in ohm Beta_dc = 100; V_BE = 0.7;// in V // Applying KVL to input section, V_CC = (I_E*R_E) + (I_B*R_B) + V_BE or I_C = (V_CC-V_BE)/( R_C + (R_B/Beta_dc) );// in A V_CE =V_CC - (I_C*R_C);// in V I_C=I_C*10^3;// in mA disp("DC load line shown in figure.") disp("Q-points : "+string(V_CE)+" V, "+string(I_C)+" mA") I_Csat =V_CC/R_C*10^3;// in mA V_CEcutoff = V_CC;// in V plot([V_CEcutoff ,0],[0,I_Csat]); xlabel("V_CE in volts"); ylabel("I_C in mA") title("DC load line")
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//Chapter-14, Example 14.4, Page 583 //============================================================================= clc clear //INPUT DATA T=27;//Temperature of swimming pool in degree C h=0.4;//Relative humidity v=2;//Speed of wind in m/s v1=(15.89*10^-6);//Kinematic viscosity in m^2/s p=0.0436;//Density in kg/m^3 DAB=(0.26*10^-4)//DAB value in m^2/s L=15;//Length in m //CALCULATIONS Sc=(v1/DAB);//Schmidt number Re=(v*L)/v1;//Reynolds number ShL=(((0.037*Re^(4/5))-870)*Sc^(1/3));//Equivalent Schmidt number h1=(ShL*(DAB/L))/10^-3;//Mass transfer coefficient for evaporation in mm/s //OUTPUT mprintf('Mass transfer coefficient for evaporation is %3.1f*10^-3 m/s',h1) //=================================END OF PROGRAM==============================
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// Scilab Code Ex6.6: Page-197 (2006) clc; clear; e = 1.6e-019; // Electronic charge, C n_i = 2.15e+013; // Carrier density of Ge at room temperature, per cc mu_e = 3900; // Mobility of electron, cm-square/V-s mu_h = 1900; // Mobility of hole, cm-square/V-s sigma_i = e*(mu_e+mu_h)*n_i; // Intrinsic conductivity of Ge, mho per m rho_i = 1/sigma_i; // Intrinsic resistivity of Ge at room temperature, ohm-m printf("\nThe intrinsic resistivity of Ge at room temperature = %2d ohm-cm", rho_i); // Result // The intrinsic resistivity of Ge at room temperature = 50 ohm-cm
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s=%s sys=syslin('c',(k)*(s+1)*(s+4)/(s*(s+3)*(s+5))) evans(sys)
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// Scilab Code Ex3a.b.4: Page-140 (2008) clc; clear; m = 1; // Mass of the suspended body, kg s = 25; // Stifness constant of the spring, N/m r = poly(0, 'r'); // As f0/f_prime = 2/sqrt(3), solving for r r = roots(4*(s/m-r^2/(4*m^2))-3*s/m); // Damping factor, kg/sec printf("\nThe damping factor of damped oscillations = %d kg/sec", r(1)); // Result // The damping factor of damped oscillations = 5 kg/sec
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clc disp("Example 2.58") printf("\n") disp("Design a voltage regulator using zener diode to meet following specification") printf("Given\n") printf("1 Resistance are in ohms \n 2 Current are in ampere \n 3 voltage sources are in volt\n") //unregulated dc input voltage Vimin=20 Vimax=30 //regulated dc output voltage Vo=10 //minimum zener current Izmin=2*10^-3 //maximum zener current Izmax=100*10^-3 //load current ILmin=0 ILmax=25*10^-3 //load resistance RL=Vo/ILmax //maximum Resistance Rmax=(Vimin-Vo)/(Izmin+ILmax) //minimum resistance Rmin=(Vimax-Vo)/(Izmax+ILmin) //Required resistance R=(Rmax+Rmin)/2 printf("minimum resistance %d ohm \n",Rmin) printf("maximum resistance %d ohm \n",Rmax) printf("required resistance %d ohm \n",R) printf("load resistance %d ohm \n",RL)
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// Given:- // Applying the conservation of mass principle, the overall dissociation reaction is described by // CO2 --- zCO2 + (1-z)CO + ((1-z)/2)O2 p = 1.0 // in atm pref = 1.0 // in atm // At 3200 K, Table A-27 gives log10k = -.189 // Solving k = ((1-z)/2)*((1-z)/(3-z))^.5 gives z = 0.422 // Calculations k = 10**log10k // From tables A-25 and A-23 hfbarCO2 = -393520.0 // in kj/kmol deltahbarCO2 = 174695-9364 // in kj/kmol hfbarCO = -110530.0 // in kj/kmol deltahbarCO = 109667-8669 // in kj/kmol hfbarO2 = 0 // in kj/kmol deltahbarO2 = 114809-8682 // in kj/kmol hfbarCO2r = -393520.0 // in kj/kmol deltahbarCO2r = 0 // in kj/kmol Qcvdot = 0.422*(hfbarCO2 + deltahbarCO2) + 0.578*(hfbarCO + deltahbarCO) + 0.289*(hfbarO2 + deltahbarO2)- (hfbarCO2r + deltahbarCO2r) // Result printf( ' The heat transfer to the reactor, in kJ per kmol of CO2 entering is: %f', Qcvdot);
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60002190043_SCILAB 5_inverse z transform (1).sce
//Programs to find the inverse z transform using the //long division method_2 clear; z=%z; num=3*(z^2)+2*z+1; den=z^2-3*z+2; h=ldiv(num,den,16); disp("First sixteen terms of the series:",h)
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// ============================================================================= // gfx4scilab - ui // dgerod@xyz-lab.org.es // ============================================================================= dir_path = get_absolute_file_path("loader.sce"); getd(dir_path); // =============================================================================
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clc; r=0.1; //in metre H=3/(2*(%pi)*r); //calculating H field intensity disp(H,"H field intensity in A/metre = "); //displaying result
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//example 4.1 (pg 149) //2x1 + 3x2 - x3 = 5 //-2x2 - x3 = -7 //-5x3 = -15 A = [2 3 -1;0 -2 -1;0 0 -5] b = [5 -7 -15]' a=[A b] [nA,mA]=size(A) n=nA //Backward substitution x(3) = a(n,n+1)/a(n,n); for i = n-1:-1:1 sumk=0; for k=i+1:n sumk=sumk+a(i,k)*x(k); end x(i)=(a(i,n+1)-sumk)/a(i,i); end disp(x)
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{% import "20300/UKA/Workflow/vars.sls" as base %} check_kafka_service_running: module_and_function: service.status args: - kafka assertion: assertTrue {% for package in ["java-1.8.0"] %} jinja_test_{{ package }}_latest: module_and_function: pkg.upgrade_available args: - {{ package }} assertion: assertFalse {% endfor %} validate_user_{{ base.kafka_user }}: module_and_function: user.info assertion_section: shell args: - {{ base.kafka_user }} assertion: assertEqual expected-return: /bin/bash check listener values{{base.zookeeper_ip_string}}: module_and_function: file.search args: - {{ base.kafka_config_path }} - SASL_PLAINTEXT://* assertion: assertTrue output_details: True
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// Case Study:-Chapter 4 ,Page No:106 // 1.Inventory Report ITEMS=4; i=1; printf("[Enter in single line seperated be spaces]\n"); while(i <= 4) printf("Enter code,quantity, and rate:"); [code(i),quantity(i),rate(i)]=scanf("%s %d %f"); i=i+1; end printf("INVENTORY REPORT\n"); printf("----------------------------------------------\n"); printf("Code Quantity Rate Value\n"); printf("----------------------------------------------\n"); total_value=0; i=1; while(i<=ITEMS) value=quantity(i)*rate(i); printf("%6s %10d %10.2f %e\n",code(i),quantity(i),rate(i),value); total_value= total_value+value; i=i+1; end printf("----------------------------------------------\n"); printf(" Total Value = %e\n",total_value); printf("----------------------------------------------\n");
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Data label index: 0 Data label contents: Common AN Vgroup Successful!
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tst
NGP-TC-16675 login when offline and Guest as true.tst
<?xml version="1.0" ?> <TestCase name="NGP-TC-16675 login when offline and Guest as true" version="5"> <meta> <create version="9.5.1" buildNumber="9.5.1.6" author="admin" date="04/21/2017" host="CACDTL02RK216W" /> <lastEdited version="9.5.1" buildNumber="9.5.1.6" author="admin" date="04/21/2017" host="CACDTL02RK216W" /> </meta> <id>9DF4DF2426E011E7B8B20CB120524153</id> <Documentation>Put documentation of the Test Case here.</Documentation> <IsInProject>true</IsInProject> <sig>ZWQ9NSZ0Y3Y9LTEmbGlzYXY9OS41LjEgKDkuNS4xLjYpJm5vZGVzPS02OTY5Mjk2NzE=</sig> <subprocess>false</subprocess> <initState> </initState> <resultState> </resultState> <Node name="Read file config.js" log="" type="com.itko.lisa.test.FileNode" version="1" uid="A903AEE126E011E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="true" next="Java Script Step" > <!-- Assertions --> <CheckResult assertTrue="false" name="Ensure Result Equals" type="com.ca.lisa.apptest.json.AssertJSONEquals2"> <log>Assertion name: Ensure Result Equals checks for: false is of type: Ensure Result Equals.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <jsonPath>$.offline</jsonPath> <expectedValue>false</expectedValue> <ignoreArrayOrder>false</ignoreArrayOrder> </CheckResult> <CheckResult assertTrue="false" name="Ensure Result Equals~1" type="com.ca.lisa.apptest.json.AssertJSONEquals2"> <log>Assertion name: Ensure Result Equals~1 checks for: false is of type: Ensure Result Equals.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <jsonPath>$.guest</jsonPath> <expectedValue>true</expectedValue> <ignoreArrayOrder>false</ignoreArrayOrder> </CheckResult> <Loc>{{LISA_RELATIVE_PROJ_ROOT}}/Data/Login Expired At N Minutes/demo/config/config.js</Loc> <charset>DEFAULT</charset> <PropKey></PropKey> <onFail>abort</onFail> </Node> <Node name="Java Script Step" log="" type="com.itko.lisa.test.ScriptNode" version="1" uid="1998A28626E111E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="false" next="Read file config.js~1" > <!-- Assertions --> <CheckResult assertTrue="true" name="Any Exception Then Fail" type="com.itko.lisa.dynexec.CheckInvocationEx"> <log>Assertion name: Any Exception Then Fail checks for: true is of type: Assert on Invocation Exception.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <param>.*</param> </CheckResult> <onerror>abort</onerror> <script>import java.io.RandomAccessFile;&#13;&#10;RandomAccessFile raf = new RandomAccessFile(&quot;{{LISA_RELATIVE_PROJ_ROOT}}/Data/Login Expired At N Minutes/demo/config/config.js&quot;, &quot;rw&quot;);&#13;&#10;String line = &quot;&quot;;&#13;&#10;long num = 0;&#13;&#10;while ((line = raf.readLine()) != null) {&#13;&#10;if(line.contains(&quot;\&quot;offline\&quot;&quot;)) {&#13;&#10; num = raf.getFilePointer();&#13;&#10; num = num - 21;&#13;&#10; break;&#13;&#10; }&#13;&#10; } &#13;&#10;raf.seek(num);&#13;&#10;raf.write(&quot; \&quot;offline\&quot;: true&quot;.getBytes());&#13;&#10;raf.close();&#13;&#10;</script> </Node> <Node name="Read file config.js~1" log="" type="com.itko.lisa.test.FileNode" version="1" uid="E8BF732226E011E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="true" next="Open the web component login page" > <!-- Assertions --> <CheckResult assertTrue="false" name="Ensure Result Equals" type="com.ca.lisa.apptest.json.AssertJSONEquals2"> <log>Assertion name: Ensure Result Equals checks for: false is of type: Ensure Result Equals.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <jsonPath>$.offline</jsonPath> <expectedValue>true</expectedValue> <ignoreArrayOrder>false</ignoreArrayOrder> </CheckResult> <CheckResult assertTrue="false" name="Ensure Result Equals~1" type="com.ca.lisa.apptest.json.AssertJSONEquals2"> <log>Assertion name: Ensure Result Equals~1 checks for: false is of type: Ensure Result Equals.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <jsonPath>$.guest</jsonPath> <expectedValue>true</expectedValue> <ignoreArrayOrder>false</ignoreArrayOrder> </CheckResult> <Loc>{{LISA_RELATIVE_PROJ_ROOT}}/Data/Login Expired At N Minutes/demo/config/config.js</Loc> <charset>DEFAULT</charset> <PropKey></PropKey> <onFail>abort</onFail> </Node> <Node name="Open the web component login page" log="" type="lisa.ui.uiMethods.uiMethods" version="1" uid="8184F22B26E111E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="false" next="Click on Demo" > <classname>GoToUrl</classname> <BROWSER>firefox</BROWSER> <URL>http://radhika.dtveng.net:8080/components/dfw-login/</URL> <OS>windows</OS> </Node> <Node name="Click on Demo" log="" type="lisa.ui.actions.uiNode" version="1" uid="864B7AFB26E111E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="false" next="Switching the iframe to xpath" > <xPath>xPath</xPath> <actions>click</actions> <parameter1>{{Demo}}</parameter1> <false>false</false> <checkboxOnError>false</checkboxOnError> </Node> <Node name="Switching the iframe to xpath" log="" type="lisa.ui.uiMethods.uiMethods" version="1" uid="54C1F10226E211E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="false" next="Verify Offline user is there" > <classname>SwitchToFrameByXpath</classname> <Xpath>//iframe[@class=&apos;style-scope iron-component-page&apos;]</Xpath> </Node> <Node name="Verify Offline user is there" log="" type="lisa.ui.actions.uiNode" version="1" uid="8EFAAFAB26E111E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="false" next="Verify login otion is not there" > <!-- Assertions --> <CheckResult assertTrue="false" name="Ensure Result Contains String~5" type="com.itko.lisa.test.CheckResultContains"> <log>Assertion name: Ensure Result Contains String~5 checks for: false is of type: Result as String Contains Given String.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <param>Offline User</param> </CheckResult> <xPath>xPath</xPath> <actions>getText</actions> <parameter1>/html/body/div/demo-snippet/div[1]/div[1]/div/span[2]</parameter1> <parameter2></parameter2> <false>false</false> <checkboxOnError>false</checkboxOnError> </Node> <Node name="Verify login otion is not there" log="" type="lisa.ui.actions.uiNode" version="1" uid="A2FC732226E111E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="false" next="Java Script Step~1" > <!-- Assertions --> <CheckResult assertTrue="false" name="Ensure Result Contains String" type="com.itko.lisa.test.CheckResultContains"> <log></log> <then>fail</then> <param>Logout</param> </CheckResult> <xPath>xPath</xPath> <actions>getText</actions> <parameter1>/html/body/div/demo-snippet/div[1]/div[1]/div/span[1]/a</parameter1> <parameter2></parameter2> <false>false</false> <checkboxOnError>false</checkboxOnError> </Node> <Node name="Java Script Step~1" log="" type="com.itko.lisa.test.ScriptNode" version="1" uid="CCC8AD2626E111E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="false" next="Read file config.js~2" > <!-- Assertions --> <CheckResult assertTrue="true" name="Any Exception Then Fail" type="com.itko.lisa.dynexec.CheckInvocationEx"> <log>Assertion name: Any Exception Then Fail checks for: true is of type: Assert on Invocation Exception.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <param>.*</param> </CheckResult> <onerror>abort</onerror> <script>import java.io.RandomAccessFile;&#13;&#10;RandomAccessFile raf = new RandomAccessFile(&quot;{{LISA_RELATIVE_PROJ_ROOT}}/Data/Login Expired At N Minutes/demo/config/config.js&quot;, &quot;rw&quot;);&#13;&#10;String line = &quot;&quot;;&#13;&#10;long num = 0;&#13;&#10;while ((line = raf.readLine()) != null) {&#13;&#10;if(line.contains(&quot;\&quot;offline\&quot;&quot;)) {&#13;&#10; num = raf.getFilePointer();&#13;&#10; num = num - 21;&#13;&#10; break;&#13;&#10; }&#13;&#10; } &#13;&#10;raf.seek(num);&#13;&#10;raf.write(&quot; \&quot;offline\&quot;: false&quot;.getBytes());&#13;&#10;raf.close();&#13;&#10;</script> </Node> <Node name="Read file config.js~2" log="" type="com.itko.lisa.test.FileNode" version="1" uid="DADE2D1E26E111E7B8B20CB120524153" think="500-1S" useFilters="true" quiet="true" next="end" > <!-- Assertions --> <CheckResult assertTrue="false" name="Ensure Result Equals" type="com.ca.lisa.apptest.json.AssertJSONEquals2"> <log>Assertion name: Ensure Result Equals checks for: false is of type: Ensure Result Equals.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <jsonPath>$.offline</jsonPath> <expectedValue>false</expectedValue> <ignoreArrayOrder>false</ignoreArrayOrder> </CheckResult> <CheckResult assertTrue="false" name="Ensure Result Equals~1" type="com.ca.lisa.apptest.json.AssertJSONEquals2"> <log>Assertion name: Ensure Result Equals~1 checks for: false is of type: Ensure Result Equals.</log> <then>fail</then> <valueToAssertKey></valueToAssertKey> <jsonPath>$.guest</jsonPath> <expectedValue>true</expectedValue> <ignoreArrayOrder>false</ignoreArrayOrder> </CheckResult> <Loc>{{LISA_RELATIVE_PROJ_ROOT}}/Data/Login Expired At N Minutes/demo/config/config.js</Loc> <charset>DEFAULT</charset> <PropKey></PropKey> <onFail>abort</onFail> </Node> <Node name="end" log="" type="com.itko.lisa.test.NormalEnd" version="1" uid="9DF4DF2A26E011E7B8B20CB120524153" think="0h" useFilters="true" quiet="true" next="fail" > </Node> <Node name="fail" log="" type="com.itko.lisa.test.Abend" version="1" uid="9DF4DF2826E011E7B8B20CB120524153" think="0h" useFilters="true" quiet="true" next="abort" > </Node> <Node name="abort" log="" type="com.itko.lisa.test.AbortStep" version="1" uid="9DF4DF2626E011E7B8B20CB120524153" think="0h" useFilters="true" quiet="true" next="" > </Node> </TestCase>
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clc //initialisation of variables t=65//B.Th.U per lb n=0.98//dry p=105//lb/in^2 a=14//Degree C b=20//Degree C p1=800//ft/sec v=0.80//ft/lb p2=3.5//lb/sec q=1400//in V=sqrt(2*32.2*778*t)//ft/sec W=(p1)*(1750-b)/32.2//ft lb/lb stream/sec H=(W*p2/550)//ft/lb E=1/64.4*[(1053)^2-(825)^2]//ft.lb steam /sec //CALCULATIONS Hd=(E/q)//C.H.U //RESULTS printf('the steam as it leaves the blades and hourse power=% f C.H.U',Hd)
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// Example 13.3 //Write a program to create a linear linked list interactively //and print the list and total number of items in the list. funcprot(0); NULL=0;i=1; //Create the list function [List]=create(list1) global List; //Create the current node in the list list1.number=input("Input a number(Type -999 to end); ") if list1.number==-999 then list1.next=NULL; list1.add=NULL; else //Create the next node in the list list1.add=list1.add+1; list1.next=NULL; List(i)=list1; if(i==1) then else List(i-1).next=List(i).add end i=i+1; create(list1); //Call create() function end return; endfunction //Function to print the numbers of list function []=print1(list1) if list1(i)(1).next~=NULL then printf("%d--->",list1(i)(1).number);//Print current item i=i+1; if list1(i)(1).next==NULL then printf("%d",list1(i)(1).number); end print1(list1);//Move to next item end return; endfunction //Function to count the number of items in the list function []=count(list1) global c; if list1(i)(1).next==NULL then return; else i=i+1; c=i; count(list1); end return; endfunction //Create the structure i.e. node node=struct('number',0,'add',0,'next',0); head=node; global List; //Calling the functions List=create(head); print1(List); global c; c=1; count(List); //Print the total number of items printf("\nNumber of items = %d",c);
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clc // initialization of variables clear sigma_x=1000 //kg/cm^2 sigma_y=-500 //kg/cm^2 sigma_z=0 //kg/cm^2 tau_xy=500 //kg/cm^2 E=2*10^6 // kg/cm^2 nu=0.25 //calculations ep_x=1/E*(sigma_x-nu*(sigma_y+sigma_z)) ep_y=1/E*(sigma_y-nu*(sigma_x+sigma_z)) ep_z=1/E*(sigma_z-nu*(sigma_y+sigma_x)) J1=ep_x+ep_y+ep_z sigma_1=(sigma_x+sigma_y)/2+sqrt((1/2*(sigma_x-sigma_y))^2+tau_xy^2) sigma_2=(sigma_x+sigma_y)/2-sqrt((1/2*(sigma_x-sigma_y))^2+tau_xy^2) th=1/2*atan(2*tau_xy/(sigma_x-sigma_y)) th=th*180/%pi ep_1=1/E*(sigma_1-nu*sigma_2) ep_2=1/E*(sigma_2-nu*sigma_1) ep_3=-1/E*nu*(sigma_1+sigma_2) //results printf('The magnitude of principal strain are %.8f, %.8f, %.8f',abs(ep_1),abs(ep_2),abs(ep_3)) printf('\n and the diection is given by theta=%.2f degrees',th) printf('\n J1 is %.6f',J1)
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//Ex:1.12 clc; clear; close; // dl=y/50 // then dl/y=((y/50)/y=1/50) dl_y=1/50;// the value of dl/y Rr=80*%pi^2*(dl_y^2);// Radiation resistance in ohm printf("The radiation resistance = %f ohm", Rr);
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// Exa 2.9 clc; clear; close; format('v',6) // Given data bita = 200; V_CEQ = 3;// in V V_CC = 6;// in V V_BB= -6;// in V V_BE= 0.7;// in V Vo = 0;// in V R1= 90*10^3;// in ohm R2= 90*10^3;// in ohm // V_CC - I_CR_C - V_CEQ - I_ER_E-V_BB = 0 (i) // Vo = V_CEQ + I_E*R_E - V_CC or I_ER_E= Vo+V_CC-V_CEQ;// in V // From eq(i) I_CR_C= V_CC - I_ER_E - V_CEQ - V_BB;// in V // Applying KVL to the input side of circuit //V_CEQ-[(R1 || R2)*I_B]-V_BE-I_ER_E+V_CC=0 or I_B= (V_CEQ-V_BE-I_ER_E+V_CC)/((R1*R2)/(R1+R2));// in A I_E= (1+bita)*I_B;//in A R_E= I_ER_E/I_E;// in ohm I_C= bita*I_B;// in A R_C= I_CR_C/I_C;// in ohm disp("Part (a) : ") disp(R_E,"The value of R_E in ohm is : ") disp(R_C,"The value of R_C in ohm is : ") disp("Parb (b) :") bita= 100; I_E= (1+bita)*I_B;//in A I_C= bita*I_B;// in A Vo_new= V_CEQ+I_E*R_E-V_CC;// in V Change_in_Vo= Vo_new-Vo;// in V disp(Change_in_Vo,"The change in Vo in volts is : ")
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//Chapter-4, Illustration 14, Page 146 //Title: Gears and Gear Drivers //============================================================================= clc clear //Input data d=216;//Ring diameter in mm m=4;//Module in mm //Calculations Td=(d/m);//Teeth of wheel D Tb=Td/4;//Teeth of wheel B Tb1=ceil(Tb);//Teeth of wheel B Td1=4*Tb1;//Teeth of wheel D Tc1=(Td1-Tb1)/2;//Teeth of wheel C d1=m*Td1;//Pitch circle diameter in mm //Output mprintf('Teeth of wheel B is %3.0f \n Teeth of wheel C is %3.0f \n Teeth of wheel D is %3.0f \n Exact pitch circle diameter is %3.0f mm',Tb1,Tc1,Td1,d1)
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clc disp("Example 1.76") printf("\n") disp("Find the diode current and power dissipation") Vdc=12 Vz=4.3 //zener voltage R=820 Iz=(Vdc-Vz)/R Pd=Vz*Iz printf("the diode current=\n%f ampere\n",Iz) printf("the power dissipation=\n%f watt\n",Pd)
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sci
phaseInputParseAs_ab.sci
function [a,b,w,cas1,fs]=phaseInputParseAs_ab(arg,nargin) fs=0; if nargin<2 then error('no. of inputs not valid'); end v=size(arg(2)); if size(v)>2 then error ('invalid input dimension'); end a=arg(1); b=arg(2); [n,k]=size(arg(2)) if nargin==2 then //(a,b) is the input w=[0:(1/512):(511/512)]*%pi; cas1=1; elseif nargin==3 then //(a,b,n) or (a,b,w) or (a,b,'whole') cas1=1; v=size(arg(3)); if type(arg(3))==10 then if arg(3)=='whole' then n=512; w=[0:(1/n):((n-1)/n)]*(2*%pi); cas1=1; else error('invalid input'); end elseif (type(arg(3))==1) if (v==[1,1])&(floor(arg(3))==arg(3))&(arg(3)>0) then //i.e. the entry is a single integer n=arg(3); w=[0:(1/n):((n-1)/n)]*%pi; elseif (v(1)==1) then //(sos,w) w must be one dimensional w=arg(3); elseif (v(2)==1) then //w to row matrix w=(arg(3))'; else error ('dimension of input is invalid'); end else error ('invalid input'); end elseif nargin==4 then //(a,b,n,fs) or (a,b,f,fs) or (a,b,n,'whole') if type(arg(4))==10 then cas1=1; if (arg(4)=='whole') then v=size(arg(3)); if (v==[1,1])&(floor(arg(3))==arg(3))&(arg(3)>0) then //i.e. the entry is a single integer n=arg(3); w=[0:(1/n):((n-1)/n)]*(2*%pi); else error ('dimension of input is invalid'); end else error('invalid input'); end elseif (type(arg(4))==1) then v=size(arg(4)); if v~=[1,1] then error ('dimension of input is invalid'); end cas1=2; fs=arg(4); v=size(arg(3)); if (v==[1,1])&(floor(arg(3))==arg(3))&(arg(3)>0) then //i.e. the entry is a single integer n=arg(3); w=[0:(1/n):((n-1)/n)]*(%pi); elseif (v(1)==1) then //(sos,w) w must be one dimensional w=2*arg(3)*%pi/fs; elseif (v(2)==1) then //w to row matrix w=2*%pi*(arg(3))'/fs; else error ('dimension of input is invalid'); end else error ('input format is invalid'); end elseif nargin==5 //(a,b,n,fs,'whole') or (a,b,f,fs,'whole') if arg(5)=='whole' then v=size(arg(4)); if v~=[1,1] then error ('dimension of input is invalid'); end cas1=2; v=size(arg(3)); if (v==[1,1])&(floor(arg(3))==arg(3))&(arg(3)>0) then //i.e. the entry is a single integer n=arg(3); w=[0:(1/n):((n-1)/n)]*(2*%pi); elseif (v(1)==1) then //(sos,w) w must be one dimensional w=2*arg(3)*%pi/fs; elseif (v(2)==1) then //w to row matrix w=2*%pi*(arg(3))'/fs; else error ('dimension of input is invalid'); end else error ('input format is invalid'); end end //so that a,b are row vectors [n,k]=size(a); if k==1 then a=a'; end [n,k]=size(b); if k==1 then b=b'; end endfunction