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//Example 5.18 clc disp("P = 8, f = 50 Hz, f_s = 1.5 Hz") disp("f_s = s*f") s=1.5/50 format(5) disp(s,"Therefore, s = ...Slip") ns=(120*50)/8 format(4) disp(ns,"N_s(in r.p.m) = 120f/P =") n=750*(1-0.03) format(6) disp(n,"N(in r.p.m) = N_s*(1-s_m) = ...Speed of the motor")
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clc; // page no 328 // prob no 8.6 //2 kHz tone is present on channel 5 of group 3 of supergroup //signal is lower sided so fc_channel_5=92*10^3; fg=fc_channel_5 - (2*10^3);// 2MHz baseband signal // we know group 3 in the supergroup is moved to the range 408-456 kHz with a suppressed carrier frequency of 516kHz f_s_carr=516*10^3; fsg=f_s_carr - fg; disp(fsg);
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errcatch(-1,"stop");mode(2);//Example 7_13 ; ; //To calculate the refractive index of the core NA=0.39 delta=0.05 n1=NA/sqrt(2*delta) printf("The refractive index of the core is %.3f",n1) exit();
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clear // // // //Variable declaration e=1.6*10^-19; //charge(coulomb) c=3*10^8; //velocity of matter wave(m/s) h=6.62*10^-34; //plank's constant(Js) lamda=6328*10^-10; //wavelength(m) //Calculation E=h*c/(lamda*e); //energy of photon(eV) p=h/lamda; //momentum of photon(kg m/s) //Result printf("\n energy of photon is %0.2f eV",E) printf("\n momentum of photon is %0.2f *10^-27 kg m/s",p*10^27)
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clc clear //Input data L1=0.225;//Thickness of the brick in m K1=4.984;//Thermal conductivity of brick in kJ/hr m C/m L2=0.125;//Thickness of insulating brick in m K2=0.623;//Thermal conductivity of insulating brick in kJ/hr m C /m Ti=1650;//Temperature inside the furnace in degree centigrade hl=245.28;//Conductance at inside wall in kJ/hr m^2 C ho=40.88;//Conductance at outside wall in kJ/hr m^2 C To=27;//Temperature of surrounding atmosphere in degree centigrade //Calculations R=((1/hl)+(L1/K1)+(L2/K2)+(1/ho));//Total resistance of the wall in C hr/kJ q=(Ti-To)/R;//Rate of heat loss per m^2 of the wall in kJ/hr m^2 T1=Ti-(q*(1/hl));//Inner surface temperature in degree centigrade T3=Ti-(q*((1/hl)+(L1/K1)+(L2/K2)));//Outer surface temperature in degree centigrade //Output printf('(a)The rate of heat loss per sq m of the wall q = %3.2f kJ/hr m^2 \n (b)The temperature at the inner surface T1 = %3.2f degree centigrade \n (c)The temperature at the outer surface T3 = %3.2f degree centigrade ',q,T1,T3)
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function x=distancia(vo,alfa,t),x=vo*cos(alfa)*t,endfunction function y=altura(vo,alfa,g,t),y=vo*sin(alfa)*t-g*t^2/2,endfunction vo=10; g=10; alfa1=%pi/6; alfa2=%pi/3; t1=0:0.01:1; x1=distancia(vo,alfa1,t1); y1=altura(vo,alfa1,g,t1); t2=0:0.01:sqrt(3); x2=distancia(vo,alfa2,t2); y2=altura(vo,alfa2,g,t2); plot(x1,y1,x2,y2) title('Tiro parabólico rasante (en azul) y por elevación (en verde)') xlabel('x') ylabel('y')
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//Variable declaration: t = 273 //Standard temperature (K) v = 0.0224 //Volume of air occupied by 1 gmol of ideal gas (m^3) V = 1100 //Volume of heat exchanger (m^3) T = 22+273 //Temperature of heat exchanger (K) x1 = 0.75 //gmols of hydrocarbon leaking from the exchanger (gmol) //Calculation: n = V*(1/v)*(t/T) //Total number of gmols of air in the room (gmol) xHC = (x1/(n+x1))*10**6 //The mole fraction of hydrocarbon in the room (ppm) ans = round((xHC*1000)*10**-1)/10**-1 //Result: printf("1. The mole fraction of hydrocarbon in the room is : %f ppb .",ans)
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// Scilab code Ex6.6: Pg.255 (2008) clc; clear; h = 6.626e-034; // Planck's constant, Js m = 9.1e-031; // Mass of the electron, kg h_cross = h/(2*%pi); // Reduced Planck's constant, Js V_0 = 2*1.6e-019; // Height of potential step, J E = 0.1*V_0; // Energy of incident electron, J C = 2*sqrt(E)/(sqrt(E)+sqrt(E-V_0)); // Wave equation constant alpha = sqrt(2*m*(V_0-E))/h_cross; psi_square = zeros(100); i = 1; // Index for array for index = 0:0.1e-010:10e-010 x(i) = index psi_square(i) = abs(C)^2*exp(-2*alpha*x(i)); i = i + 1; end clf() plot2d(x, psi_square); // Plot psi_square vs x title('Plot of |psi_square| vs x', 'fontsize', 4); xlabel('x', 'fontsize', 3); ylabel('|psi_square|', 'fontsize', 3); // The attached graph shows the phenomenon
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clc //given that del_x = 2e-9 // Uncertainty in position in m h = 6.63e-34 // Plank constant m = 9.1e-31 // mass of electron in Kg printf("Example 2.13") h_bar = h / (2*%pi) // constant del_p = h_bar/(2*del_x) // Calculation of uncertainty in momentum del_v = del_p/m printf("\n Uncertainty in velocity of particle is %e m/s.\n\n\n",del_v)
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//pagenumber 37 example 20 clear un=1300;//centimetre square per velocity second //at 300kelvin ni=1.5*10^10; u=500;//centimetre square per velocity second conduc=1.6*10^-19*1.5*10^10*(un+u); q=1/conduc; //impurity of 1 atom included per 10^5 atoms disp("resistivity at 300kelvin = "+string((q))+"ohm centimetre"); n=5*10^22/10^5; p=ni^2/n; q=1/(1.6*10^-19*(un*n+(u*p))); disp("resistivity at impurity of 1 atom included per 10^5 atoms = "+string((q))+"ohm centimetre");
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clc; clear all; n1 = 1.55; // Refractive index of core n2 = 1.50; // Refractice index of clad NA = sqrt(n1^2-n2^2); // Numerical Aperture disp('',NA,'The numerical aperture of fiber is')
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//Obtain path of solution file path = get_absolute_file_path('solution12_10.sce') //Obtain path of data file datapath = path + filesep() + 'data12_10.sci' //Clear all clc //Execute the data file exec(datapath) //Calculate the tension in the band on tight side P1 (N) P1 = sigmat * w * t //Calculate the tension in the band on the loose side P2 (N) P2 = P1/(%e^(mu * theta * %pi/180)) //Calculate the actuating force on the lever P (N) P = (P2 * d1 - P1 * d2)/(d3 + d1) //Calculate the torque capacity of the brake Mt (N-m) Mt = (P1 - P2)*R //Check self-locking if ((d1 / d2)>(%e^(mu * theta * %pi/180))) printf("\nThe brake is not self-locking\n") else printf("\nThe brake is self-locking\n") end //Print results printf("\nTension in the band on the tight side(P1) = %f N\n",P1) printf("\nTension in the band on the loose side(P2) = %f N\n",P2) printf("\nActuating force(P) = %f N\n",P) printf("\nTorque capacity of the brake(Mt) = %f N-m\n",Mt/1000)
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//Example 1.31 //Add //Page no. 26 clc;clear;close; a=0.4532e5;b=0.5427e7; c=a+b printf('Addition of %.4g and %.6g = %.6g',a,b,c)
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funcprot(0); // Initialization of Variable function[dms]=degtodms(deg) d = int(deg) md = abs(deg - d) * 60 m = int(md) sd = (md - m) * 60 sd=(round(sd*100)/100) dms=[d m sd] endfunction del1=75+14.0/60+20.0/3600;//declination in degrees del2=70+12.0/60+30.0/3600;//declination in degrees d=del1-del2;//difference in degrees //calculation k=cos(del1*%pi/180)/cos(del2*%pi/180); A2=%pi/2-atan((cos(d*%pi/180)-k)/sin(d*%pi/180)); A2=A2*180/%pi; A2=120+15.0/60+10.0/3600-A2; CR=360-A2; A2=degtodms(A2); CR=degtodms(CR); disp(A2,"azimuth of angle R in degree,minites,seconds respectively"); disp(CR,"true bearing of CR in degree,minites,seconds respectively"); clear()
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//Example 7.3 clc clear x = 0:4; y = [6.9897 7.4036 7.7815 8.1281 8.451]; n = length(x); del = %nan*ones(n,5); del(:,1) = y'; for j = 2:6 for i = 1:n-j+1 del(i,j) = del(i+1,j-1) - del(i,j-1); end end del(:,1) = []; n0 = length(del(1,:)); X = 2; i = find(x==X); dowy = 0; for j = 1:n0 if j==2*int(j/2) then add = del(i,j); else add = (del(i-1,j) + del(i,j))/2; i = i-1; if i==0 then break end end if add == %nan then break else dowy(j) = add; end end mprintf("%5s %6s %10s %9s %9s %9s",'x','y','dy','d2y','d3y','d4y') disp([x' y' del]) mu = 1; h = x(2) - x(1); dy2 = mu/h*(dowy(1) - 1/6*dowy(3)); d2y2 = mu/h^2*(dowy(2)-1/12*dowy(4)); dy2 = round(dy2*10^4)/10^4; d2y2 = round(d2y2*10^4)/10^4; disp(dy2,"y''(2) = ") disp(d2y2,"y''''(2) = ")
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errcatch(-1,"stop");mode(2);//page 238 ; ; A=[1 0 1 6 2;0 1 1 0 3]; b=[8 9]'; c=[0 0 7 -1 -3]'; lb=[0 0 0 0 0]' ub=[]; [x,lagr,f]=linpro(c,A,b,lb,ub); disp(x,'New corner:'); disp(f,'Minimum cost:'); //end exit();
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//Variable declaration epsilon0=8.85*10**-12; epsilonr=1.0000684; //dielectric constant of material N=2.7*10**25; //number of atoms(per m**3) E=10**6; //electric field(V/m) e=1.6*10**-19; Z=2; //atomic number //Calculation alpha_e=epsilon0*(epsilonr-1)/N; //electronic polarizability(F m**2) r=(alpha_e/(4*%pi*epsilon0))**(1/3); //radius(m) d=alpha_e*E/(Z*e); //displacement(m) //Result printf('radius is %0.3f *10**-11 m \n',(r*10**11)) printf('answer varies due to approximating off errors\n') printf('displacement is %0.3f *10**-16 m \n',(d*10**16))
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// ***************************************** // * Universidad Católica del Uruguay // * Cálculo Numérico 2016 // * Laboratorio 5 // * Eduardo Senturión - Federico González // ***************************************** // Esta función se utiliza para saber quienes son los participantes del grupo function Grupo=AlumnosDelGrupo() Grupo = {}; Grupo.Nombre1 = "FernandoTorterolo"; Grupo.Nombre2 = "MartinDaRosa"; Grupo.Nombre3 = "PabloFernandez"; endfunction // Implementacion de método iterativo general para sistemas lineales. // A Matriz sparse [nxn] // b Vector [nx1] // x resultado de Ax = b function x = ResolverTridiagonal(A, b) [n m] = size(A) AA = A bb = b for i=2:n AA(i,2) = AA(i,2) - AA(i,1) * AA(i-1,3) / AA(i-1,2) bb(i) = bb(i) - AA(i,1) * bb(i-1) / AA(i-1,2) end x(n) = bb(n) / AA(n,2); for i = n-1:-1:1 x(i) = (bb(i)-AA(i,3)*x(i+1)) / AA(i,2) end x endfunction
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// Initilization of variables M=10 // kg // Here M=M_1=M_2 g=9.81 // m/s^2 // acc due to gravity // Calculations // Consider the respective F.B.D // Applying the principle of conservation of energy and by equating the total energies at position 1 & position 2 we get v as, v=sqrt((M*g*4)/(25)) // m/s // Results clc printf('The velocity of mass M_2 is %f m/s \n',v)
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//Example 2.4 clc;clear;close; A=1;T=2; w0=2*%pi/T; //Calculation of trignometric fourier series co-efficients a0=4*A/T*(integrate('t-0.5*T','t',-T/2,-T/4)+integrate('t','t',-T/4,T/4)+integrate('-t+0.5*T','t',T/4,T/2)); for n=1:10; a(1,n)=2*4*A/T*(integrate('(t-0.5*T)*cos(n*w0*t)','t',-T/2,-T/4)+integrate('t*cos(n*w0*t)','t',-T/4,T/4)+integrate('(-t+0.5*T)*cos(n*w0*t)','t',T/4,T/2)); b(1,n)=2*4*A/T*(integrate('(t-0.5*T)*sin(n*w0*t)','t',-T/2,-T/4)+integrate('t*sin(n*w0*t)','t',-T/4,T/4)+integrate('(-t+0.5*T)*sin(n*w0*t)','t',T/4,T/2)); end //Displaying fourier coefficients disp(T,'fundamental period T= ',A,'Assumption: Amplitude A= '); disp('Tignometric fourier series co-efficients:'); disp(a0,'a0= ');disp(a,'an= ');disp(b,'bn= '); t=-T/2:0.01*T:T/2; x=[-4*A/T*t(1:25)-2*A 4*A/T*t(26:75) -4*A/T*t(76:101)+2*A]; subplot(311);plot(t,x); title('x(t)');xlabel('time t'); subplot(312);plot2d3(a); title('Coefficients an');xlabel('n'); subplot(313);plot2d3(b); title('Coefficients bn');xlabel('n');
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// Mvt d'une particule dans un chp E et B // // Technique : application de la RFD // méthode d'Euler // par Sébastien CELLES // Commencé le 06/02/2004 // // Hyp : Terre = réf gali // Système : particule chg // Forces : Fe=qE // Fm->=q v-> vectoriel B-> // Système de coordonnées : cartésien [ux uy uz] // Horloge : t // // z // / \ | -> // / | \ \|/ g // | // | y // | \ // +------------ // / O / // | / // |/ // x --- // clear function [v]=crossP(v1,v2) // le produit vectoriel en vectoriel... // v1 et v2 doivent etre des matrices (3,n) v=zeros(v1) v(1,:) = v1(2,:).*v2(3,:) - v1(3,:).*v2(2,:) v(2,:) = v2(1,:).*v1(3,:) - v2(3,:).*v1(1,:) v(3,:) = v1(1,:).*v2(2,:) - v1(2,:).*v2(1,:) endfunction printf("\n"); printf("\n"); printf("Resolution d un probleme de mecanique terrestre en 3 dimensions \n"); printf("\n"); printf("\n"); printf("Calcul en cours... Patientez !\n"); printf("\n"); t_ini=0; // MODIFIABLE defaut : t_ini=0; t_pas=1E-13; // MODIFIABLE defaut : t_pas=0.1; t_fin=1E-10; // MODIFIABLE defaut : t_fin=10; // Testé sur ATHLON-XP-2100 avec 2000 pts en même pas 1 seconde ! // Exemples // Obus dang g // t_ini = 0; // t_pas = 0.001; // t_fin = 1.2; // m=1; // q=0; // g=9.81; // OM_ini=[0 0 0]; // V0=10; // %alfa=30; // v_ini = [0 V0*cos(%alfa*2*%pi/360); V0*sin(%alfa*2*%pi/360)]; // e- dans B // t_ini = 0; // t_pas = 0.001; // t_fin = 1.2; // m = me; // q = qe; // h1 = 0; // h2 = 0; // g0 = 0; // OM_ini = [0 0 0]; // V0 = 10 // %alfa = 5 // v_ini = [V0*sin(%alfa*2*%pi/360) 0 V0*cos(%alfa*2*%pi/360)]; // B=[0 0 1]; // A faire // e- dans E // e- dans E et B t=[t_ini:t_pas:t_fin]'; // le prime sert à transposer pour avoir un vecteur colonne N=size(t,'r'); // Constantes g0 = 0; //9.81 g = [0 0 -g0]; // Accélération de la pesanteur MODIFIABLE defaut : g=[0 0 -9.81]; (9.81m*s^-2) h1 = 0; // Coefficient de frottement visqueux Fv=h1*v h2 = 0; // Coefficient de frottement fluide Ff=h2*v^2 qe = 1.6E-19; // Charge élémentaire me = 9.109389E-31; // Masse d'un électron mp = 1.672623E-27; // Masse d'un proton mn = 1.676928E-27; // Masse d'un neutron // k = ; // Constante de raideur du ressort Fr=k*(l-l0) // l0 = 0.10; // Longueur à vide du ressort // Gc = 6.67259E-11; // Constante de la loi de gravitation // R1 = // Rayon de la planète 1 // M1 = // Masse de la planète 1 // R2 = // Rayon de la planète 2 // M2 = // Masse de la planète 2 // %epsilon_0 = 1/(4*%pi*8.98755178737E9); // %mu_0 = 4*%pi*100E-9 // Système m = me; // Masse MODIFIABLE defaut : m=1; (1kg) q = qe; // Conditions initiales OM_ini = [0 0 0]; // Position initiale (MODIFIABLE) V0 = 10; %alfa = 5; // degré //v_ini = [0 V0*cos(%alfa*2*%pi/360) V0*sin(%alfa*2*%pi/360)]; // Vitesse initiale (MODIFIABLE) v_ini = [V0*sin(%alfa*2*%pi/360) 0 V0*cos(%alfa*2*%pi/360)]; F_ini = [0 0 0]; //m*g; // Penser à modifier la "force initiale" F(t=0) pour plus de précision et surtout dans la boucle a_ini = F_ini/m; // RFD // Initialisation t_0=t_ini; // Instant courant OM_t0=OM_ini; // Position courante v_t0=v_ini; // Vitesse courante a_t0=a_ini; // Accélération courante F_t0=F_ini; // Force courante OM_tm1=OM_ini; // Position précédente (t moins 1) v_tm1=v_ini; // Vitesse précédente (t moins 1) a_tm1=a_ini; // Accélération précédente (t moins 1) F_tm1=F_ini; // Force précédente (t moins 1) OM_tm2=OM_ini; // Position précédente (t moins 2) v_tm2=v_ini; // Vitesse précédente (t moins 2) a_tm2=a_ini; // Accélération précédente (t moins 2) F_tm2=F_ini; // Force précédente (t moins 2) OM_tp1=[0 0 0]; // Position suivante (t plus 1) v_tp1=[0 0 0]; // Vitesse suivante (t plus 1) a_tp1=[0 0 0]; // Accélération suivante (t plus 1) F_tp1=[0 0 0]; // Force suivante (t plus 1) OM=OM_ini; // Matrice des positions [x_0 y_0 z_0] // [x_1 y_1 z_1] // [x_2 y_2 z_2] // [ . . . ] v=v_ini; // Matrice des vitesses [vx_0 vy_0 vz_0] // [vx_1 vy_1 vz_1] // [vx_2 vy_2 vz_2] // [ . . . ] a=a_ini; // Matrice des accélérations [ax_0 ay_0 az_0] // A voir // [ax_1 ay_1 az_1] // [ax_2 ay_2 az_2] // [ . . . ] F=F_ini; // Matrice des forces [Fx_0 Fy_0 Fz_0] // [Fx_1 Fy_1 Fz_1] // [Fx_2 Fy_2 Fz_2] // [ . . . ] // Boucle sur la durée de l'expérience k=0; while N <> size(OM,'r') //t_0<=t_fin, //****printf("*********** Nouvel instant t ***********\n"); t_0 = t_0 + t_pas; k = k+1; printf("."); //****t_0 // Forces (MODIFIABLE mais ATTENTION !) // Poids P = m*g; // Force de frottement visqueux // Fv=-h1*v Fv = - h1*v_t0; // Force de frottement fluide // Ff=-h2*v^2 if norm(v_t0)<>0 uv_t0 = v_t0/norm(v_t0); // Vecteur unitaire selon la direction de v à l'instant courant else uv_t0 = [0 0 0]; // cas où norm(v_t0) = 0 end Ff = - h2*(v_t0*v_t0')*uv_t0; // Force EM Fe + Fb // Fe = q * E E = [0 0 0]; // Champ électrique Fe = q*E; // Fb = q * (v vectoriel B) // Le produit vectoriel n'existe pas dans SciLab il faut "le faire" voir crossP B = [0 0 1]; // Champ magnétique Fb = q*((crossP(v_t0',B'))'); // Somme des forces F_t0 = P + Fv + Ff + Fe + Fb; // Relation Fondamentale de la Dynamique // Somme des forces = m * accélération // F=m*a // a=F/m a_t0=F_t0/m; // Intégration 1 : vitesse // a = (v_tp1-v_t0)/t_pas v_tp1 = a_t0*t_pas + v_t0; // Intégration 2 : position // v = (M_tp1-M_t0)/t_pas OM_tp1 = v_t0*t_pas + OM_t0; // Mise à jour des matrices position, vitesse, force // // // OM = [OM ; OM_tp1]; v = [v ; v_tp1]; a = [a ; a_t0]; F = [F ; F_t0]; // Décalage OM_t0=OM_tp1; v_t0=v_tp1; // a_t0=a_tp1; // F_t0=F_tp1; OM_tm1=OM_t0; v_tm1=v_t0; // a_tm1=a_t0; // F_tm1=F_t0; OM_tm2=OM_tm1; v_tm2=v_tm1; // a_tm2=a_tm1 // F_tm2=F_tm1; end // Fin de boucle printf("\n"); // Retour à la ligne printf("\n"); // Saut de ligne printf("Fin des calculs !\n"); printf("\n"); // Mise en forme des résultats // t (déja mis en forme) xbasc() // ou xclear() permet d'effacer l'écran graphique // x y z x=OM(:,1); // (rem sur TI on ne peut pas récupérer les colonnes mais uniquement les lignes y=OM(:,2); // alors (astuce !) on transpose on recupère une ligne et on retranspose) z=OM(:,3); //printf("\n"); //printf("Trajectoire dans le plan yz\n"); //plot2d(y,z); //halt() //c'est une pause mais ça ne s'appelle pas pause() ! //xbasc() // ou xclear() permet d'effacer l'écran graphique printf("\n"); printf("Trajectoire dans l espace\n"); // bizarrement SciLab n'aime pas l'aspostrophe param3d(x,y,z); //plot3d(x,y,z); Trace des surfaces halt() //c'est une pause mais ça ne s'appelle pas pause() ! xbasc() // ou xclear() permet d'effacer l'écran graphique // vx vy vz vx=v(:,1); vy=v(:,2); vz=v(:,3); printf("\n"); printf("Hodographe\n"); param3d(vx,vy,vz); //printf("Hodographe dans le plan yz\n"); //plot2d(vy,vz) //plot3d(vx,vy,vz); halt() //c'est une pause mais ça ne s'appelle pas pause() ! xbasc() // ou xclear() permet d'effacer l'écran graphique // ax ay az ax=a(:,1); ay=a(:,2); az=a(:,3); printf("\n"); printf("az = f(ax,ay)\n"); param3d(ax,ay,az); //printf("az = f(ay)\n"); //plot2d(ay,az); //plot3d(ax,ay,az); halt() //c'est une pause mais ça ne s'appelle pas pause() ! xbasc() // ou xclear() permet d'effacer l'écran graphique // Plan de phase x.=f(x) // sqrt(vx^2+vy^2+vz^2) donne ||v->|| en fonction de t // sqrt(x^2+y^2+z^2) donne ||M->|| en fonction de t printf("\n"); printf("Plan de Phase\n"); NormV = sqrt(vx^2+vy^2+vz^2); NormM = sqrt(x^2+y^2+z^2); plot2d(NormM,NormV) GLOBAL = [t,x,y,z,vx,vy,vz,ax,ay,az]; // Construction d'une variable contenant tous les résultats halt() printf("\n"); printf("\n"); printf("Tous les résultats sont dans les variables t,x,y,z,vx,vy,vz,ax,ay,az et GLOBAL\n"); printf("\n"); printf("\n"); printf("Sebastien CELLES\n"); printf("sebastien.celles@ac-limoges.fr\n"); xbasc()
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//The answer given in book for this question is wrong. clc; P=4;//No of poles Ia=120;//armature current A=4;//No of parallel paths for armature conductor L=0.02//inductance in mH //Et=L*(di/dt),Transformer emf in coil //di=2*Ia/A,change of current during commutation //dt=Tc,time of commutation //Et=0.02*0.001*(60/Tc) ....(1) //Er=2*(Bav*l*v),rotational emf in single turn coil //Er=2*(phi_c/Tc) ....(2),phi_c is the avg value of flux in the commutating zone //For linear commutation, Er=Et, from equation (1)&(2) phi_c=60*0.02*0.001/2;//phi_c is the avg value of flux in the commutating zone printf('THE AVG. VALUE OF FLUX IN THE COMMUTATING ZONE IS %f Wb.',phi_c)
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function pontoY = gregoryNewton(eixoX, eixoY, pontoX) tamanho = length(eixoX); vetor = eixoY; for i = 1: tamanho -1 for j = tamanho : -1 : i+1 vetor(j) = vetor(j) - vetor(j-1); end end u = ((pontoX - eixoX(1))/(eixoX(2) - x(1))) pontoY = vetor(tamanho); for i = tamanho-1 : -1: 1 pontoY = pontoY * (u - i + 1)/ i + vetor(i); end endfunction x = 1 : 2 : 20; y = x.**3 + x - 1; resposta = gregoryNewton(x, y, 4); disp(resposta); x = 0 : 1 : 5; y = [1 2 21 76 185 366]; resposta = gregoryNewton(x, y, 3.2); disp(resposta); x = [1.1 1.3 1.4 1.6 1.7 1.9]; y = [0.9048 0.7408 0.6703 0.5488 0.4966 0.4066]; resposta = gregoryNewton(x, y, 1.33); disp(resposta);
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//Example 3_9 clc;clear;funcprot(0); // Properties rho=1000; // The density of water in kg/m^3 g=9.81; // The acceleration due to gravity in m/s^2 // Given values R=0.8;// Radius of solid cylinder in m h_bottom=5;// m A=0.8*1;// m^2 s=4.2; h_c=s+R/2;// m // Calculation // (a) F_x=(rho*g*h_c*A)/1000;//kN printf('(a)Horizontal force on vertical surface F_x=%0.1f kN\n',F_x); F_y=(rho*g*h_bottom*A)/1000;// kN V=(R^2-(%pi*(R^2)/4))*1;// m^3 W=(rho*g*V)/1000;// kN F_v=F_y-W;// kN F_r=sqrt(F_x^2+F_v^2);// kN theta=atand(F_v/F_x);// degree printf('The hydrostatic force acting on the cylinder,F_r=%0.1f kN\n',F_r); printf('The direction of the hydrostatic force acting on the cylindrical surface,theta=%0.1f degree\n',theta); //(b) W_cyl=F_r*sind(theta);// kN printf('(b)The weight of the cylinder per m length,W_cyl=%0.1f kN\n',W_cyl);
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// // 08.05.22 // 08.08.24 function Pd=Bowdata(varargin) global BOWMIDDLE BOWSTART BOWEND Nargs=length(varargin); PA=varargin(1); PB=varargin(2); Cut=0; D=1/2*Vecnagasa(PB-PA); if Nargs>=3 H=varargin(3)*D*0.2; else H=D*0.2; end H=min(H,D); if Nargs>=4 Cut=varargin(4); end Ydata=MakeBowdata(PA,PB,H); C=Mixop(1,Ydata); r=Mixop(2,Ydata); R1=Mixop(3,Ydata); R2=Mixop(4,Ydata); Rng='R=['+string(R1)+','+string(R2)+']'; Theta=(R1+R2)*0.5; BOWMIDDLE=MixS([C(1)+r*cos(Theta),C(2)+r*sin(Theta)],Theta); M=Mixop(1,BOWMIDDLE); ThetaM=Mixop(2,BOWMIDDLE); BOWSTART=PA; BOWEND=PB; if Cut==0 Pd=Circledata(C,r,Rng); else Alpha=R1; Beta=ThetaM-Cut/(2*r); Rng='R=['+string(Alpha)+','+string(Beta)+']'; Pd=Circledata(C,r,Rng); Alpha=ThetaM+Cut/(2*r); Beta=R2; Rng='R=['+string(Alpha)+','+string(Beta)+']'; Tmp=Circledata(C,r,Rng); Pd=[Pd;%inf,%inf;Tmp]; end endfunction
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// exa 7.10 Pg 212 clc;clear;close; // Given Data d=35;// mm d2=125;// mm n=6;// factor of safety T=800;// N.m N=350;// rpm tau_s=63;// MPa tau_b=56;// MPa tau_CI=10;// MPa tau_k=46;// MPa // Diameter of bolts: F=2*T*10**3/d2/n;// N //%pi/4*db**2*tau_b=F db=sqrt(F/(%pi/4*tau_b));// mm printf('\n (i) Diameter of bolts = %.2f mm. Use 8 mm.',db) // Flange thickness d1=2*d;// mm //T=%pi/2*d1**2*t2*tau_CI t2=T*1000/(%pi/2*d1**2*tau_CI);// mm printf('\n (ii) Flange thickness = %.1f mm. Use t2 = 12 mm',t2) t2=12;// mm //Key dimensions b=10;// mm (width of key) t=7;// mm (from tables) //T=l*b*tau_k*d/2 l=T*10**3/(b*tau_k*d/2);// mm l=ceil(l);// mm printf('\n (iii) Length of key = %.f mm\n\t\td=%.f mm\n\t\tb=%.f mm',l,d,b) // Hub length lh=l;// mm (length of hub) printf('\n (iv) Hub length = %.f mm',l) tau_c=T*10**3/(%pi/16*(d1**4-d**4)/d1);// N/mm.sq. printf('\n shear stress in hub = %.2f N/mm.sq.',tau_c) printf('It is nearly equal to %.f N/mm.sq.',tau_CI) printf('\n hence design parameters are fine.') // Power transmitted P=2*%pi*N*T/60/10**3;// kW printf('\n (v) Power transmitted = %.2f kW',P)
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//data Zin=45 //ohm ZL=20 //ohm b=0.5/2 //cm Er=2.1 L=200*10^-9 //H f=3*10^9 //Hz C=55.63*Er*10^-12 //F //formulas and result printf("\nresult:-") Zo=sqrt(Zin*ZL) printf("\nZo=%.0f ohm",Zo) k=30/sqrt(200*10^-9/(55.63*Er*10^-12)) a=b/exp(k) printf("\na=%f cm",a) lambda=1/(f*sqrt(L*C)) printf("\nlambda=%f m",lambda) d=lambda/4 printf("\nd=%f m =%f cm",d,d*100)
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//simplify (a+b)/(a^2-b^2) clear; clc; close; //as, by formula,(a^2-b^2)=(a+b)(a-b) mprintf("\n (a+b)/((a+b)(a-b)) => 1/(a-b) \n")
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// Example 1.3 clear; clc; close; format('v',6); // Given data P=4;//No. of poles f=50;//in Hz N=1470;//in rpm //Calculations Ns=120*f/P;//in rpm S=(Ns-N)/Ns;//Slip fr=S*f;//induced emf frequency in Hz disp(fr,"Induced emf frequency in Hz : ");
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Introduction to heat transfer by S.K.Som, Chapter 6, Example 10") //Wind at a speed of U=36km/hr blows over a flat plate of length,L=6m .If the density and kinematic viscosity of air are rho=1.2kg/m^3 and mu=1.5*10^-5m^2/s respectively. U=36; L=6; rho=1.2; mu=1.5*10^-5; //Wind velocity in m/s is Uinf disp("Wind velocity(Uinf)in m/s is") Uinf=U*1000/3600 //Reynolds number is given by ReL=L*Uinf/mu disp("Reynolds number is") ReL=L*Uinf/mu //We consider that transition of boundary layer takes place from laminar to turbulent takes place at ReL=5*10^5. //Therfore the corresponding friction coefficient is given by CbarfL=(0.074-ReL^(1/5))-(1742/ReL) disp("Friction coefficient is") CbarfL=(0.074/ReL^(1/5))-(1742/ReL) //Drag force on one side of the plate per unit metre width is given by FD=CbarfL*rho*Uinf^2*L/2 disp("Drag force on one side of the plate per unit metre width in Newton is ") FD=CbarfL*rho*Uinf^2*L/2 //The turbulent boundary layer thickness at the trailing edge is given by delta=L*(0.379/ReL^(1/5)) disp("The turbulent boundary layer thickness at the trailing edge in metre is ") delta=L*(0.379/ReL^(1/5))
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//Chapter 2, Exmaple 8, page 70 //Calculate the volume of the insulator clc clear //Thinkness of graded design V = 150*sqrt(2) Ebd = 50 T = V/Ebd printf("\nThickness of graded design= %e cm \n",T) //Based on figure 2.24 r = 2 // radius of the conductor l = 10 //length of graded cylinder; The textbook uses 10 instead of 20 zr = l*(T+r) printf("Curve = %e cm^2 \n",zr) //Volume of graded design V1 V1 = 4*%pi*zr*(zr-r) printf("V1 = %e cm^3 \n",V1) //Unit is wrong in the textbook //Thickness of regular design as obtained form Eq.2.77 pow = V/(2*Ebd) t = 2*(%e^pow-1) printf("Thickness of regular design = %e cm \n",t) //Volume of regular design V2 V2 = %pi*((2+t)^2-4) printf("V2 = %e cm^3 \n",V2)//unit not mentioned in textbook //Answers may vary due to round off error
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expr 12 \| 34 \| 12 \| 34 expr 12 \| 34 \| \( 12 \| 34 \) expr \( 12 \| 34 \) \| 12 \| 34 expr \( 12 \| 34 \) \| \( 12 \| 34 \) expr 12 \| 34 \& 34 \& 13 expr 12 \| 34 \& \( 34 \& 13 \) expr \( 12 \| 34 \) \& 34 \& 13 expr \( 12 \| 34 \) \& \( 34 \& 13 \) expr 12 \| 34 != 12 = 34 expr 12 \| 34 != \( 12 = 34 \) expr \( 12 \| 34 \) != 12 = 34 expr \( 12 \| 34 \) != \( 12 = 34 \) expr 34 \& 13 \& 34 \& 13 expr 34 \& 13 \& \( 34 \& 13 \) expr \( 34 \& 13 \) \& 34 \& 13 expr \( 34 \& 13 \) \& \( 34 \& 13 \) expr 34 \& 13 != 12 = 34 expr 34 \& 13 != \( 12 = 34 \) expr \( 34 \& 13 \) != 12 = 34 expr \( 34 \& 13 \) != \( 12 = 34 \) expr 34 \& 13 - 12 + 34 expr 34 \& 13 - \( 12 + 34 \) expr \( 34 \& 13 \) - 12 + 34 expr \( 34 \& 13 \) - \( 12 + 34 \) expr 12 = 34 != 12 = 34 expr 12 = 34 != \( 12 = 34 \) expr \( 12 = 34 \) != 12 = 34 expr \( 12 = 34 \) != \( 12 = 34 \) expr 12 = 34 - 12 + 34 expr 12 = 34 - \( 12 + 34 \) expr \( 12 = 34 \) - 12 + 34 expr \( 12 = 34 \) - \( 12 + 34 \) expr 12 = 34 / 4 \* 6 expr 12 = 34 / \( 4 \* 6 \) expr \( 12 = 34 \) / 4 \* 6 expr \( 12 = 34 \) / \( 4 \* 6 \) expr 12 + 34 - 12 + 34 expr 12 + 34 - \( 12 + 34 \) expr \( 12 + 34 \) - 12 + 34 expr \( 12 + 34 \) - \( 12 + 34 \) expr 12 + 34 / 4 \* 6 expr 12 + 34 / \( 4 \* 6 \) expr \( 12 + 34 \) / 4 \* 6 expr \( 12 + 34 \) / \( 4 \* 6 \)
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//sum of naturals between x and y clc; clear; x=70; y=25; (x*(x+1)/2) - (y*(y+1)/2) + y
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imgaussfilt3.sci
// Copyright (C) 2015 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author: Shreyash Sharma // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in function [outputImg]=imgaussfilt3(inputImage, filter_height, filter_width, sigmaX, sigmaY) // This function is used for 3-D Gaussian filtering of 3-D images // // Calling Sequence // B=imgaussfilt3(A, filter_height, filter_width, sigmaX, sigmaY) // // Parameters // A: image matrix of the source image. // filter_height: height of the Gaussian filter, specified as a scalar // filter_width: width of the Gaussian filter, specified as a scalar // sigmax: Standard deviation in x of the Gaussian distribution, specified as a numeric, real, positive scalar. // sigmay: Standard deviation in y of the Gaussian distribution, specified as a numeric, real, positive scalar // B : output image with it's histogram matching similar to a given reference image. // // Description // imgaussfilt3(___,Value,...) filters 3-D image A with a 3-D Gaussian smoothing kernel with parameters used to control aspects of the filtering. // // Examples // img = imread("lena.jpeg"); // imshow(img); // filtered_img = imgaussfilt3(img, 9, 9, 3, 3); // imshow(filtered_img); // inputList=mattolist(inputImage); outputList=raw_imgaussfilt3(inputList, filter_height, filter_width, sigmaX, sigmaY); for i=1:size(outputList) outputImg(:,:,i)=outputList(i) end endfunction
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//Divided difference for the functin = ln(x) clc; clear; close(); format('v',9); x = [1 1.5 1.75 2]; fx = [0 0.40547 0.55962 0.69315]; fab(1) = (fx(2)-fx(1))/(x(2)-x(1)); fab(2) = (fx(3)-fx(2))/(x(3)-x(2)); fab(3) = (fx(4)-fx(3))/(x(4)-x(3)); fabc(1)= (fab(2)-fab(1))/(x(3)-x(1)); fabc(2)= (fab(3)-fab(2))/(x(4)-x(2)); fabcd(1)= (fabc(2)-fabc(1))/(x(4)-x(1)); disp(fx',fab,fabc,fabcd,'Divided difference columns : ') //We can redraw the table, the existing entries does not change x(5)=1.1; fx(5)=0.09531; fab(4) = (fx(5)-fx(4))/(x(5)-x(4)); fabc(3)= (fab(4)-fab(3))/(x(5)-x(3)); fabcd(2)= (fabc(3)-fabc(2))/(x(5)-x(2)); fabcde(1)=(fabcd(2)-fabcd(1))/(x(5)-x(1)); disp(fx',fab,fabc,fabcd,fabcde,'Divided difference columns after addition of an entry : ')
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// Find Id,Vgs,Vds,region of operation // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 6-9 in page 277 clear; clc; close; // Given data Idss=4*10^-3; // Drain current in mA Vp=-2; // Peak voltage in V Vdd=10; // Supply voltage in V Vgs=0; // Gate source voltage in V // Calculation Id=Idss*(1-(Vgs/Vp)); printf("(a)Id = %0.0e A\n",Id); printf("(b)Since Id=Idss, Vgs=0 V\n"); Vds=10-Vgs; printf("(c)Vds = %0.0f V\n",Vds); printf("Since Vds=10V>Vgs-Vp=2V,Active region operation of upper JFET is confirmed"); // Result // (a) Id = 4 mA, // (b) Vgs = 0 V, // (c) Vds = 10 V
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//To calculate the power delivered by the source in the given circuit. clc; Z=[3+%i*1 -%i -2;-%i 2+%i*3 -%i*2;-2 %i*2 3+%i*1] D=det(Z) Z_1=[15.7 -%i -2;0 2+%i*3 -%i*2;0 %i*2 3+%i*1] D_1=det(Z_1) V_1=D_1/D //Power delivered =V_1*I*cos(theta)=Real(V_1*I),which on simplification equals 100 watts.
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clc; //page no 8-52 //Example 8.14 //Let Csmax/Csmin be denoted by C fmin=500;//in kHz fmax=1600;//in kHz IF=465;//in kHz C=(fmax/fmin)^2; fomin=fmin+IF; fomax=fmax+IF; disp(C,'Csmax/Csmin='); disp(+'kHz',fomin,'fomin='); disp(+'kHz',fomax,'fomax='); //Let Comax/Comin be denoted by C1 C1=(fomax/fomin)^2; disp(C1,'Comax/Comin='); Csmax=350//in pF Csmin=Csmax/C; disp(+'pF',Csmin,'Csmin='); //We know that //C=[Csmax(Csmin+Cp)/Csmin(Csmax+Cp)] //4.58=350/34.2*((34.2+Cp)/(350+Cp)) Cp=221.3;//in pF Comax=(Csmax*Cp)/(Csmax+Cp); Comin=(Csmin*Cp)/(Csmin+Cp); disp(+'pF',Comax,'Comax='); disp(+'pF',Comin,'Comin='); //Rounding Comax Comax1=135.5; //The oscillator coil frequency can be calculated as Lo=[1/[(2*%pi*(fomin*10^3))^2*(Comax1*10^-12)]]*10^6;//Answer was given wrong in the text book disp(+'microHenry',Lo,'Oscillator coil frequency is'); //At 1000 kHz f=1000;//in kHz fomid=f+IF; Comid=Comax/(fomax/fomid)^2; Comid1=68.2; disp(+'pF',Comid,'Comid='); Csmid=1/[(1/Comid1)-(1/Cp)]; disp(+'pF',Csmid,'Csmid='); fsmid=fmax/sqrt(Csmax/Csmid); disp(+'kHz',fsmid,'fs"'mid="); Terr=fsmid-f; disp(+'kHz',Terr,'Tracking error is');
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clear clc K1=1;// K2=1.66*10^6;//in dm^3/mol Keq=(K1/K2);//equilibrium constant in mol/dm^3 RT_F=0.05913;//in V n=1;// Ecell=RT_F/n*(log10(Keq)) printf('Ecell=%.4f V',Ecell) E_h=0.337;// n2=2 Ecell_2=n2*E_h printf('\nEcell_2=%.3f V',Ecell_2) //page 544
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clc //initialisation of variables l= 5 //ft h= 20 //in n= 1/15 AG= 50 //in x= 30 //in w= 62.4 //lb/ft^3 //CALCULATIONS AG1= AG/(1+n) G1G2= n*x/(1+n) W= l^2*w*(l/2) h1= 32 //in BK= h1/2 GK= 10 //in G1K= (AG+GK)-AG1 BG1= BK-G1K BM= (l^4/12)*2*12/(l^3*BK*n) G1M= BM+BG1 o= atand(G1G2/G1M) //RESULTS printf ('angle through which the cube will tilt = %.f degrees ',o)
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//pathname=get_absolute_file_path('11.20.sce') //filename=pathname+filesep()+'11.20-data.sci' //exec(filename) //Height of chimney(in m): H=45 //Temperature of burnt gases(in K): Tg=630 //Air requirement(in kg air per kg of fuel burnt): m=15 //Ambient air temperature(in K): Ta=300 //Minimum temperatre of artificial draught(in K): Tga=150+273 //Specific heat of flue gases(in kJ/kg.K): Cpg=1.005 //Calorific value of fuel(in kJ/kg): C=30000 //Draught (in mm of water column): hw=353*H*(1/Ta-(m+1)/(m*Tg)) //Draught (in metres of hot gas column): hg=H*(m/(m+1)*Tg/Ta-1) //Temperature of chimney for maximum discharge(in K): Tgmax=Ta*2*(m+1)/m //Chimney efficiency: n=9.81*H*(m/(m+1)*Tg/Ta-1)/(Cpg*(Tg-Tga)*10^3)*100 //Extra heat carried away by flue gases(in kJ): Q=(m+1)*Cpg*(Tg-Tga) //Percentage heat spent in natural draught: nn=Q/C*100 printf("\n RESULT \n") printf("\nDraught = %f mm of water",hw) printf("\nDraught = %f metres of hotgas column",hg) printf("\nTemperature of chimney gases for maximum discharge = %d K",Tgmax) printf("\nChimney efficiency = %f percent",n) printf("\nExtra heat carried away by flue gases per kg of fuel burnt = %f kJ",Q) printf("\nPercentage heat carried away in natural draught = %f percent",nn)
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function[x,y] = myfun(a,b) m=a^2+b^2 x = m+b; y = m-b; endfunction
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///////////////////////////////////////////////////////////////// // LA FONCTION ETUDIE : EGGHOLDER ///////////////////////////////////////////////////////////////// function [y]=f_eh(x) x1 = x(1) x2 = x(2) //y=-(x2-47)*sin(sqrt(abs(x2+x1/2+47))) - x1*sin(sqrt(abs(x1-(x2+47)))) y=-(x(2,:)+47).*sin(sqrt(abs(x(1,:)./2 + x(2,:) + 47))) - x(1,:).*sin(sqrt(abs(x(1,:) - x(2,:) - 47))) // c'est bon pour le moral //y=-20*exp(-.2*sqrt(.5*(x1*x1 + x2*x2)) ) - exp(.5*cos(2*%pi*x1+2*%pi*x2)) + %e + 20 endfunction B_eh=[-512 512;-512 512]; //B_eh=[-5 5;-5 5]; sol_eh=[512 ; 404.2319]; ///////////////////////////////////////////////////////////////// // CREATION D ECHANTILLON ///////////////////////////////////////////////////////////////// // Créer un ensemble aléatoire de n vecteurs dans l'espace bornés défini par B // INPUT // B : matrice d*2 : bornes de l'ensemble de la forme B=[xmin xmax ; ymin ymax ; ...] // n : nombre de vecteurs aléatoires créer // OUTPUT // X : matrice d*N : ensemble des vecteurs aléatoires créés function [X]=samp_alea(B,n) [d,_]=size(B); X=zeros(d,n); for li=1:d do X(li,:)=B(li,1)+(B(li,2)-B(li,1))*rand(1,n); end endfunction // Créer un ensemble aléatoire de n points dans l'espace bornés défini par B respectant // les conditions d'un carré latin : même espacement selon coords, coordonnées uniques // INPUT // B : matrice d*2 : bornes de l'ensemble de la forme B=[xmin xmax ; ymin ymax ; ...] // n : nombre de vecteurs aléatoires créer // OUTPUT // X : matrice d*N : ensemble des vecteurs aléatoires créés function [X]=LatinHypercube(B,n) [d,_]=size(B); X=zeros(d,n); for li=1:d do X(li,:) = samwr( n , 1 , linspace(B(li,1),B(li,2),n) )'; end endfunction function test_LatinHypercube() n=5; B=[0 10 ; 0 5]; LH=LatinHypercube(B,n); clf gca().tight_limits=['on','on']; gca().data_bounds= [B(1,1)-1 B(2,1)-1 ; B(1,2)+1 B(2,2)+1]; gca().isoview='on'; gca().auto_scale='off'; plot(LH(1,:),LH(2,:), "+"); for i=1:n do // ligne horizontale plot( B(1,:) , [LH(2,i),LH(2,i)] ); // ligne verticale plot( [LH(1,i),LH(1,i)] , B(2,:) ); end endfunction //////////////////////////////////////////////////// // DDELETE TOUS LES TAGS //////////////////////////////////////////////// // Permet de supprimer tous les éléments graphiques d'un certain tag // INPUT // tag : le tag rechercher function destroy(tag) f = findobj(tag); while f<>[] do delete(f); f=findobj(tag); end endfunction ///////////////////////////////////////////////////////////////// // CALCUL DE LA PSO ///////////////////////////////////////////////////////////////// // RECHERCHE MINIMUM //////////////////////////// function [a,b] = mincol(x,f) [n,m]=size(x) a=x(:,1) b=1 for i = 1:m if f(a) > f(x(:,i)) then a=x(:,i) b=i end end endfunction function [a,b] = mincol_abs(x,f) // [n,m]=size(x) a=x(:,1) b=1 for i = 1:m if abs(f(a)) > abs(f(x(:,i))) then a=x(:,i) b=i end end endfunction ///////////////////////////////////// // CRITERE CONVERGENCE //////////////////////////// // Calcul le centre gravité d'un nuage de points P de poids W // INPUT // P : matrice d*n : les n vecteurs colonnes de dim d // W : matrice 1*n : les poids des vecteurs // OUTPUT // G : matrice d*1 : position du centre de gravité function G=GravityCenter(P,W) // somme des poids p=sum(W) // pondération des points Ppond=P*diag(W) // somme pondérée sumPond=sum(Ppond,"c") // moyenne pondere G=sumPond/p endfunction // Calculer le cercle de centre le centre de gravité d'un nuage de point et qui // encercle tous les points // INPUT // P : matrice d*n : les n vecteurs de dim d à encercler // OUTPUT // G : matrice d*1 : position du centre de gravité // r : rayon du cercle entourant tous les points function [G,r]=Surround(P) // [d,n]=size(P) // définit le centre de masse // par défaut, poids à 1 -> donner masse plus importante aux sols proches ? W=ones(n,1) G=GravityCenter(P,W) // on calcule la distance (carré entre les points et le centre du cercle à la recherche // de la distance maximale, qui donnera rayon cercle // R2 : liste des rayons au carré dif = P-kron(ones(1,n),G) R2 = sum(dif.*dif, "r") r = sqrt(max(R2)) endfunction ////////////////////////////////////// // BORNER LES POINTS ////////////////////////// // x : matrice d,n : les n points de dimensions d à borner // b : matrice d,2 : pour chaque coef, la borne inf et sup function bx=bound_x(x,b) bx=x [d,n]=size(bx) for li=1:d do bx(li,:)=min(b(li,2),max(b(li,1),bx(li,:))) end endfunction
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Example4_6.sce
// Example 4.6 clear; clc; close; format('v',9); // Given data lm=6*10^-3;//magnet length in m g=2*10^-3;//in m Tph=200;//turns Br=0.3;//in T l=50*10^-3;//in m n=25*10^-3;//in m I=10*10^-3;//in A N=200;//turns mo=4*%pi*10^-7;//permittivity //Calculations Am=(2/3)*%pi*[n-g-lm/2]*l;//in m^2 Ag=[(2/3)*%pi*(n-g/2)+2*g]*(l+2*g);//in m^2 Cfi=Am/Ag;//unitless //For normal BLDG motor, HC=606 KA/M HC=606;//in KA/M Hm=N*I/l;//KA/M Bm=Br*[1-Hm/HC];//in T Mrec=(Br-Bm)*10^-3/(4*%pi*10^-7*40); Pmo=mo*Mrec*Am/lm;//in m-Wb/AT Pmo=Pmo*10^-3;//in Wb/AT Kc=1.05;//given constant g_dash=Kc*g;//in m Rg=g_dash/mo/Am; Bg=Cfi*Br/(1+Pmo*Rg);//in T Torque=2*Tph*Bg*l*n*I;//in N-m disp(Torque,"Torque per phase in N-m : ");
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// Example A-7-12 // Nyquist plot for positive omega clear; clc; xdel(winsid()); //close all windows s = %s /2 /%pi; num = 20 * ( s^2 + s + 0.5); den = s * (s + 1) * (s + 10); G = syslin('c',num,den); a = gca(); a.clip_state = 'on'; nyquist(G,0.01,1000); xgrid(color('gray')); a.data_bounds = [-3 -5 ; 3 1]; a.box = 'on';
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//ques-5.5 //Calculating activity of solution clc C=0.992;//molarity of NaCl y=0.782;//activity coefficient a=y*C;//activity printf("The activity of solution is %.3f M.",a);
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//Example4.2// a=4;//body-centered cubic as given in table 3.3 b=sqrt(3); //body-centered cubic as given in table 3.3 c=1;// as we take R common from the equation ri=(1/2)*(a/b)-c mprintf("ri = %f R",ri) //from the appendix 2, R=0.124nm giving R=0.124;//nm //atomic radius of iron ri1=ri*R mprintf("\nri1 = %f nm",ri1) rC=0.077;//nm //atomic radius of carbon from the appendix 2 R1=rC/ri1 mprintf("\nR1 = %f ",R1)
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// Problem no 14.12,Page No.340 clc;clear; close; H=6 //m //height of dam a=1.5 //m //top width b=3.5 //m //Bottom width rho_s=16 //KN/m**3 //density of soil rho_mason=22.5 //KN/m**3 //density of mason phi=30 //Degree //angle of repose //Calculations //Let Length of dam ,L=1 m L=1 //m //weight of dam W=(a+b)*2**-1*L*H*rho_mason //Rankine's coeff earth pressure K=((1-sin(30*%pi*180**-1))*(1+sin(phi*%pi*180**-1))**-1) //Lateral thrust P=rho_s*H**2*L*2**-1*K //Distance of Line of action from vertical base x_bar=(b**2+b*a+a**2)*(3*(b+a))**-1 //distance of pt where resultant cuts the base x=P*W**-1*H*3**-1 //Eccentricity e=x_bar+x-b*2**-1 //Pressure at heel B sigma1=W*b**-1*(1-6*e*b**-1) //Pressure at heel C sigma2=W*b**-1*(1+6*e*b**-1) //Result printf("The Max Intensities of soil at the wall is %.2f",sigma2);printf(" KN/m**2") printf("\n The Min Intensities of soil at the wall is %.2f",sigma1);printf(" KN/m**2") //Plotting the Shear Force Diagram X1=[0,L,L] Y1=[sigma2,sigma1,0] Z1=[0,0,0] plot(X1,Y1,X1,Z1) xlabel("Length x in m") ylabel("Shear Force in kN") title("the Shear Force Diagram")
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clear clc n=11 disp('the first row denotes the boy no. ') A(1,:)=[1 2 3 4 5 6 7 8 9 10 11]; disp('the second row denotes the marks in test I (x1) ') A(2,:)=[23 20 19 21 18 20 18 17 23 16 19]; disp('the third row denotes the marks in test I (x2) ') A(3,:)=[24 19 22 18 20 22 20 20 23 20 17]; disp('the fourth row denotes the difference of marks in two tests (d)') for i=1:11 A(4,i)=A(3,i)-A(2,i); end disp('the fifth row denotes the (d-1) ') for i=1:11 A(5,i)=A(4,i)-1; end disp('the sixth row denotes the square of elements of fourth row') for i=1:11 A(6,i)=A(4,i)^2; end A a=0; disp('the sum of elements of fourth row= ') for i=1:11 a=a+A(4,i); end a b=0; disp('the sum of elements of sixth row= ') for i=1:11 b=b+A(6,i); end b disp('standard deviation') d=(b/(n-1))^0.5 t=(1-0)*(n)^0.5/2.24
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//Example 4.19.5: resistance clc; clear; close; //given data : V1=1;//in V I=1.5*10^-3;//in A rd=200*10^3;// in ohm Rm=50;// in ohm Rs=600*10^3;// in ohm gm=0.005;//in mho rd1=rd/((gm*rd)+1); V0=gm*((rd1*Rs)/(rd1+Rs))*V1 R0=(2*Rs*rd1)/(Rs+rd1) R_cal=(V0/I)-Rm-R0; disp(R_cal,"resistance ,R_cal(ohm) = ") // answer is wrong in book
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clear; clc; close; x=poly(0,'x'); //let x be amount of increase in pence mans_new_wage=480+x; womens_new_wage=370+x; for x=1:500 if((480+x) == (6*(370+x)/5))//by given data mprintf("the weekly increase is %ip \n",x) end end
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//Example 5.11 //To Design the Filter using Impulse Invarient Method clear; clc ; close ; s=%s; T=1; HS=(2)/(s^2+3*s+2); elts=pfss(HS); disp(elts,'Factorized HS = '); //The poles comes out to be at -2 and -1 p1=-2; p2=-1; z=%z; HZ=(2/(1-%e^(p2*T)*z^(-1)))-(2/(1-%e^(p1*T)*z^(-1))) disp(HZ,'HZ = ');
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errcatch(-1,"stop");mode(2);//example 1.11 //page 31 ; funcprot(0); //initialisation of variable sigma=0.022//from table Gamma=9789//unit weight S=0.79;//from table d=2/1000;//diameter h=4*sigma/Gamma/S/d; disp(h*1000,"rise of height of alcohol(mm):"); exit();
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//Example 2.3 //computing initial value using scilab clear;clc; xdel(winsid()); s=%s n3=(3*s+2) d3=s*(s^2+4*s+5) F=n3/d3 //Applying initial value theorem //when limit "s" tends to infinity, final value of "F" becomes "0" disp(0,"Final value=")
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Example8_7.sce
clear ; clc; // Example 8.7 printf('Example 8.7\n\n'); // Page no. 213 // Solution // Write given data B_in = 1.1 ;// Flow rate in of blood -[L/min] B_out = 1.2;// Flow rate out of blood -[L/min] S_in = 1.7;// Flow rate in of solution -[L/min] // Composition of input blood B_in_CR = 2.72 ;//[g/L] B_in_UR = 1.16 ;//[g/L] B_in_U = 18 ;//[g/L] B_in_P = 0.77 ;//[g/L] B_in_K = 5.77 ;//[g/L] B_in_Na = 13.0 ;//[g/L] B_in_water = 1100 ;//[mL/min] // Composition of output blood B_out_CR = 0.120 ;//[g/L] B_out_UR = 0.060;//[g/L] B_out_U = 1.51 ;//[g/L] B_out_P = 0.040 ;//[g/L] B_out_K = 0.120 ;//[g/L] B_out_Na = 3.21 ;//[g/L] B_out_water = 1200 ;//[mL/min] n_un = 7 ;// Number of unknowns in the given problem n_ie = 7 ;// Number of independent equations d_o_f = n_un-n_ie ;// Number of degree of freedom printf('Number of degree of freedom for the given system is %i .\n\n',d_o_f); // Water balance in grams, assuming 1 ml is equivalent to 1 g S_in_water = 1700 ;//[ml/min] S_out_water = B_in_water+ S_in_water - B_out_water; S_out = S_out_water/1000 ;//[L/min] printf(' Flow rate of water in output solution is %.2f L/min.\n\n',S_out); // The component balance in grams for CR,UR,U,P,K and Na are S_out_CR = (B_in*B_in_CR - B_out*B_out_CR)/S_out; S_out_UR = (B_in*B_in_UR - B_out*B_out_UR)/S_out; S_out_U = (B_in*B_in_U - B_out*B_out_U)/S_out; S_out_P = (B_in*B_in_P - B_out*B_out_P)/S_out; S_out_K = (B_in*B_in_K - B_out*B_out_K)/S_out; S_out_Na = (B_in*B_in_Na - B_out*B_out_Na)/S_out; printf(' Component Concentration(g/L) in output Dialysis solution \n'); printf(' UR %.2f \n',S_out_UR); printf(' CR %.2f \n',S_out_CR); printf(' U %.2f \n',S_out_U); printf(' P %.2f \n',S_out_P); printf(' K %.2f \n',S_out_K); printf(' Na %.2f \n',S_out_Na);
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<start> <upsFile>BurnRate.ups</upsFile> <!-- NOTE....... plotScript2 is hard coded!!!!!--> <gnuplot> <script>plotScript.gp</script> <title>Burn Rates vs Pressure At 298K</title> <ylabel>Burn Rate (m/s)</ylabel> <xlabel>Pressure (Pa)</xlabel> </gnuplot> <AllTests> </AllTests> <Test> <Title>VolumeFraction1</Title> <sus_cmd>mpirun -np 1 ./sus -svnDiff -svnStat </sus_cmd> <postProcess_cmd>compare_burn_rates.m -pDir 1 -mat 1 -rho_CC 1832 </postProcess_cmd> <x>25</x> <replace_values> /Uintah_specification/MaterialProperties/MPM/material/geom_object/volumeFraction :1.0 /Uintah_specification/MaterialProperties/ICE/material/geom_object/volumeFraction :0.0 </replace_values> </Test> <Test> <Title>VolumeFraction0.9</Title> <sus_cmd>mpirun -np 1 ./sus -svnDiff -svnStat </sus_cmd> <postProcess_cmd>compare_burn_rates.m -pDir 1 -mat 1 -rho_CC 1832 </postProcess_cmd> <x>25</x> <replace_values> /Uintah_specification/MaterialProperties/MPM/material/geom_object/volumeFraction :0.9 /Uintah_specification/MaterialProperties/ICE/material/geom_object/volumeFraction :0.1 </replace_values> </Test> <Test> <Title>VolumeFraction0.8</Title> <sus_cmd>mpirun -np 1 ./sus -svnDiff -svnStat </sus_cmd> <postProcess_cmd>compare_burn_rates.m -pDir 1 -mat 1 -rho_CC 1832 </postProcess_cmd> <x>25</x> <replace_values> /Uintah_specification/MaterialProperties/MPM/material/geom_object/volumeFraction :0.8 /Uintah_specification/MaterialProperties/ICE/material/geom_object/volumeFraction :0.2 </replace_values> </Test> <Test> <Title>VolumeFraction0.7</Title> <sus_cmd>mpirun -np 1 ./sus -svnDiff -svnStat </sus_cmd> <postProcess_cmd>compare_burn_rates.m -pDir 1 -mat 1 -rho_CC 1832 </postProcess_cmd> <x>25</x> <replace_values> /Uintah_specification/MaterialProperties/MPM/material/geom_object/volumeFraction :0.7 /Uintah_specification/MaterialProperties/ICE/material/geom_object/volumeFraction :0.3 </replace_values> </Test> <Test> <Title>VolumeFraction0.6</Title> <sus_cmd>mpirun -np 1 ./sus -svnDiff -svnStat </sus_cmd> <postProcess_cmd>compare_burn_rates.m -pDir 1 -mat 1 -rho_CC 1832 </postProcess_cmd> <x>25</x> <replace_values> /Uintah_specification/MaterialProperties/MPM/material/geom_object/volumeFraction :0.6 /Uintah_specification/MaterialProperties/ICE/material/geom_object/volumeFraction :0.4 </replace_values> </Test> </start>
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function teoriaDeColas(lamda, s, u, n, pob, c)//n = capacidad del sistema, pob = poblacion if(c <> 0) if(s == 1) cn = CnServicioCambiante(lamda, u, c) else cn = CnServicioCambianteMS(lamda, s, u, c) end else if(n == %inf && pob == %inf) cn = Cn(lamda, s, u, n); else if(n <= s && pob == %inf) cn = Cn(lamda, s, u, n); else if(pob <> %inf) cn = CnPoblacionFinita(lamda, s, u, n, pob); else printf("Caso aun no definido\n"); return; end end end end pn = Pn(cn); printf("Eficiencia = %.7f\n", lamda/(s*u)); printf("P0 = %.7f\n", P0(cn)); l = sum(L(pn)); printf("L = %.7f\n", l); vlq = Lq(pn, s); printf("Lq = %.7f\n", sum(vlq)); printf("W = %.7f\n", l/lamda); printf("Wq = %.7f\n", sum(Wq(vlq,lamda))); printf("P{Wq > 0} = %.7f\n", 1-sum(pn(1:s))); endfunction function x=CnPoblacionFinita(lamda, s, u, N, pob) n = 0:s; x = (factorial(N)./(factorial(N-n).*factorial(n))).*((lamda/u).^n); epsilon = 1e-7; aux = s+1; while(%t) p = factorial(N)/(factorial(N-aux)*factorial(s)*(s^(aux-s))); p = p * ((lamda/u)^aux); aux = aux + 1; if(p < epsilon || aux > N) break; end x = [x,p]; if(p == %nan || p == %inf || p == -%inf) x = [0]; return; end end endfunction function x=CnServicioCambiante(lamda, u, c)// n = 0; x = []; epsilon = 1e-7; while(%t) p = ((lamda/u)^n)/(factorial(n)^c); if(p < epsilon) break; end x = [x,p]; n = n + 1; if(p == %nan || p == %inf || p == -%inf) x = [0]; return; end end endfunction function redesDeColas(lamdas, ss, us, p)//vector de lamdas, servidores y u, matriz de transicion lamdaT = sum(lamdas); for i=1:length(ss) lamdai = lamdas(i) + sum(p(:,i)'.*lamdas); printf("### Para sub-sistema %d\n", i); teoriaDeColas(lamdai, ss(i), us(i),%inf,%inf,0); printf("\n"); end endfunction function x=CnServicioCambianteMS(lamda, s, u, c) n = 0:s; x = ((lamda/u).^n)./factorial(n); epsilon = 1e-7; aux = s + 1; while(%t) p = (lamda/u)^aux; p = p/(factorial(s)* ((factorial(aux)/factorial(s))^c)* (s^((1-c)*(aux-s))) ); if(p < epsilon) break; end x = [x,p]; n = n + 1; if(p == %nan || p == %inf || p == -%inf) x = [0]; return; end aux = aux + 1; end endfunction function x=Cn(lamda, s, u, capacidad)// aux = 0:s; x = (lamda.^aux)./(factorial(aux).*(u.^aux)) if(capacidad <= s) return; end n = s+1; epsilon = 1e-7; while(%t) p = (lamda^n)/(factorial(s).*(u^s).*((s*u)^(n-s))); if(p < epsilon) break; end x = [x,p]; n = n + 1; if(p == %nan || p == %inf || p == -%inf) x = [0]; return; end end endfunction function y=P0(cn) sumatoria = sum(cn); y = 1/(sumatoria); endfunction function z=Pn(cn) p0 = 1/sum(cn); z = p0.*cn; endfunction function z=L(pn) n = 0:length(pn)-1; z = pn.*n; endfunction function z=Lq(pn, s) ini = length(pn); pn = pn(s+1:length(pn)); n = s:ini-1; z = (n-s).*pn; endfunction function z=Wq(lq, lamda) z = lq/lamda; endfunction
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//Exam:11.3 clc; clear; close; D=0.002;//Grain diameter(in mm) d=D*10^(-3);//Grain diameter(in m) K=0.63;//Constant(in MNm^(-3/2)) sigma_i=80;//in MNm^-2 sigma_y=sigma_i+K*d^(-1/2);//Yield stress for a polycrystalline alloy disp(sigma_y,'Yield stress for a polycrystalline alloy(in MN/m^2)');
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// Gravimetric Analysis clear; clc; printf("\t Example 4.9\n"); mSample=0.5662;//mass of sample, g Cl=35.5;//mol mass of Cl, g AgCl=143.4;//mol mass of AgCl, g mAgCl=1.0882;//mass of AgCl formed, g %Cl(AgCl)=Cl/AgCl*100;//percent Cl in AgCl mCl=%Cl(AgCl)*mAgCl/100;//mass of Cl in AgCl, g //the same amount of Cl is present in initial sample %Cl=mCl/mSample*100;//percent Cl in initial sample printf("\t the percentage of Cl in sample is : %4.2f percent\n",%Cl); //End
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// A Texbook on POWER SYSTEM ENGINEERING // A.Chakrabarti, M.L.Soni, P.V.Gupta, U.S.Bhatnagar // DHANPAT RAI & Co. // SECOND EDITION // PART I : GENERATION // CHAPTER 7: TARIFFS AND ECONOMIC ASPECTS IN POWER GENERATION // EXAMPLE : 7.1 : // Page number 73 clear ; clc ; close ; // Clear the work space and console // Given data connected_load = 450.0*10**3 // Connected load(kW) maximum_demand = 250.0*10**3 // Maximum demand(kW) units_generated = 615.0*10**6 // Units generated per annum(kWh) // Calculations // Case(i) demand_factor = maximum_demand/connected_load // Demand factor // Case(ii) hours_year = 365.0*24 // Total hours in a year average_demand = units_generated/hours_year // Average demand(kW) load_factor = average_demand/maximum_demand*100 // Load factor(%) // Results disp("PART I - EXAMPLE : 7.1 : SOLUTION :-") printf("\nCase(i) : Demand factor = %.3f ", demand_factor) printf("\nCase(ii): Load factor = %.1f percent", load_factor)
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//chapter12 //example12.2 //page236 Vcc=13 // V V_knee=1 // V Rc=4 // kilo ohm gain_beta=100 V_Rc=Vcc-V_knee Ic=V_Rc/Rc Ib=Ic/gain_beta Vs=Ic/5 // since Ic/Vs = 5 mA/V given printf("maximum input signal voltage = %.3f V or %.3f mV \n",Vs,Vs*1000)
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// Exa 11.7 clc; clear; close; format('v',6) // Given data V_L = 230;// in V f = 50;// in Hz N = 950;// in rpm E2 = 100;// in V Ns =1000;// in rpm // Ns = 120*f/P; P = (120*f)/Ns; disp(P,"The Number of ploes is"); s = ((Ns-N)/Ns)*100;// %s in % disp(s,"The percentage of full load slip in % is"); // The rotor induced voltage at full load E2r = (s/100)*E2;// in V disp(E2r,"The rotor induced voltage in V is"); // The rotor frequency at full load f_r = (s/100)*f;// in Hz disp(f_r,"The frequency at full load in Hz is");
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Yesterday, all my troubles seemed so far away Now it looks as though they're here to stay Oh, I believe in yesterday Suddenly, I'm not half the man I used to be There's a shadow hanging over me Oh, yesterday came suddenly
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-- The intellectual and technical concepts contained herein are proprietary to Fuzzy Logix, LLC. -- and may be covered by U.S. and Foreign Patents, patents in process, and are protected by trade -- secret or copyright law. Dissemination of this information or reproduction of this material is -- strictly forbidden unless prior written permission is obtained from Fuzzy Logix, LLC. -- Functional Test Specifications: -- -- Test Category: Statistical Functions -- -- Last Updated: 05-30-2017 -- -- Author: <kamlesh.meena@fuzzyl.com> -- -- BEGIN: TEST SCRIPT -- BEGIN: TEST(s) -----******************************************************************************************************************************* -----**************************************************************** ---SP_Perc -----**************************************************************** DROP TABLE FinStockPricePerc; EXEC SP_Perc('FinStockPrice', 'CLOSEPRICE', 'TICKERSYMBOL', '0.1,0.3,0.5,0.7,0.9', 'FinStockPricePerc'); SELECT * FROM FinStockPricePerc LIMIT 20;
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clc //Chapter1 //Ex_1.5 //Given L=100*10^-6//in Henry C=100 *10^-12 //in Farad T=300 // in Kelvin R=200*10^3 //in ohms k=1.38*10^-23 //in J/K fo=1/(2*%pi*sqrt(L*C))//resonant frequency Q=2*%pi*fo*C*R//quality factor B=fo/Q //Bandwidth of tuned RLC //Acc. to Johnson resistor noise equation Vrms=sqrt(4*k*T*R*B) //in volts Vrms=Vrms/10^-6 //in micro volts disp(Vrms," Minimum rms radio signal that can be detected in micro volts is")
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clc //Variable initialisation V=400//Supply voltage in volts f=50//Supply Frequency in Hz P=6//No of poles Rs=0.2//stator resistance in ohm Rr=0.07//Rotor resistance in ohm Xs=0.4//Stator impedance in ohm Xr=0.4//Rotor impedance in ohm Sm1=0.25//Maximum Slip at 25% speed range N1=750//Speed in rpm a1=130 am=150//maximum Firing Angle n=2//Stator to rotor turns ratio Rd=0.02//Dc link resistance in ohm N2=950//Speed in rpm N3=850//Speed in rpm //Solution V1=V/sqrt(3) Ns=120*f/P//Synchronous speed in rpm Wms=Ns*2*%pi/60 a=-Sm1/cosd(am)//At 25% speed Range m=2/a//Transformer Turns Ratio S1=(Ns-N1)/Ns Vd11=3*sqrt(6)*S1*V1/(%pi*n) Vd21=3*sqrt(6)*V1*cosd(a1)/(%pi*m) Rs1=Rs/(n^2) Rr1=Rr/(n^2) Id1=(Vd11+Vd21)/(2*((S1*Rs1)+Rr1)+Rd)//The answers vary due to round off error T1=abs(Vd21)*Id1/(S1*Wms)//The answers vary due to round off error S2=(Ns-N2)/Ns Tr=(3/Wms)*V1^2*(Rr/S2)/((Rs+(Rr/S2))^2+(Xs+Xr)^2)//Rated torque in N-m Thr=Tr/2//Half rated Torque in N-m S3=(Ns-N3)/Ns X=poly(0,'X')//let X=cos(a2) Vd12=3*sqrt(6)*S3*V1/(%pi*n) Vd22=3*sqrt(6)*V1*X/(%pi*m) Id2=(Vd12+Vd22)/(2*((S3*Rs1)+Rr1)+Rd) T2=abs(Vd22)*Id2/(S3*Wms) //Equating T2 to Thr 0==5547.31*X^2-2878.788*X+349.52//Polynomial Equation in X X1=(2878.788+sqrt((2878.788^2)-4*5547.31*349.52))/(2*5547.31)//Roots of polynomial eqn X2=(2878.788-sqrt((2878.788^2)-4*5547.31*349.52))/(2*5547.31)//Roots of polynomial eqn a11=acosd(-X1) a22=acosd(-X2) printf('\n\n Transformer Turns Ratio=%0.1f \n\n',m) printf('\n\n Torque for 750rpm and alpha 130=%0.1f N-m\n\n',T1) printf('\n\n The Field Current=%0.1f \n\n',a11) printf('\n\n The Field Current=%0.1f \n\n',a22) //The answers vary due to round off error
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//To calculate the miller indices of a plane //plane intercepts at a,b/2,3*c //therefore intercepts are (1 1/2 3) //reciprocal of the intercepts is (1/2 2 1/3) //thus miller indices are (3 6 1) printf("miller indices of the plane are (3 6 1)");
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function stlwrite(t, filename, fmt) [lhs,rhs] = argn(0); if rhs < 3 then error("Not enough input argument") end if type(t) <> 16 then error("First argument must be a typed list (tlist)") end if strcmp(typeof(t), 'stldata') <> 0 then error("First argument must be a stldata tlist") end if type(filename) <> 10 then error("File name must be a string") end if type(fmt) <> 10 then error("STL file format must be a string") end if members(fmt, ["ascii" "binary"]) == 0 then error("...") end if strcmp(fileext(filename), ".stl") <> 0 then filename = filename + ".stl" end if strcmp(fmt, "ascii", "i") == 0 then fd = mopen(filename, "wt") [err, msg] = merror(fd) if (err <> 0) then error(msg) end if strcmp(part(t.header, 1:5), "solid") <> 0 then mfprintf(fd, "solid %s\n", t.header) else mfprintf(fd, "%s\n", t.header) end for n = 1:size(t.x, "c") mfprintf(fd, .. " facet normal %f %f %f\n outer loop\n vertex %f %f %f\n vertex %f %f %f\n vertex %f %f %f\n endloop\n endfacet\n", .. t.normals(1,n), t.normals(2,n), t.normals(3,n), .. t.x(1,n), t.y(1,n), t.z(1,n), .. t.x(2,n), t.y(2,n), t.z(2,n), .. t.x(3,n), t.y(3,n), t.z(3,n)) end mfprintf(fd, "endsolid") mclose(fd) else fd = mopen(filename,"wb") [err, msg] = merror(fd) if (err <> 0) then error(msg) end if strcmp(part(t.header, 1:5), "solid") == 0 then t.header = part(t.header, 7:$) mputstr(part(t.header, 7:86), fd) else mputstr(part(t.header, 1:80), fd) end mput(size(t.x, "c"), "ui", fd) for n = 1:size(t.x, "c") mput([t.normals(1,n) t.normals(2,n) t.normals(3,n)], "f", fd) mput([t.x(1,n) t.y(1,n) t.z(1,n)], "f", fd) mput([t.x(2,n) t.y(2,n) t.z(2,n)], "f", fd) mput([t.x(3,n) t.y(3,n) t.z(3,n)], "f", fd) mput(0 , "us", fd) end mclose(fd) end endfunction
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EXAMPLE11_17.SCE
//ANALOG AND DIGITAL COMMUNICATION //BY Dr.SANJAY SHARMA //CHAPTER 11 //Information Theory clear all; clc; printf("EXAMPLE 11.17(PAGENO 498)"); //given Px_1 = 1/2;//probability of first symbol Px_2 = 1/4;//probability of second symbol Px_3 = 1/8;//probability of third symbol Px_4 = 1/16;//probability of fourth symbol Px_5 = 1/16;//probability of fifth symbol r = 16//outcomes per second //calculations H_X = Px_1*log2(1/Px_1) + Px_2*log2(1/Px_2) + Px_3*log2(1/Px_3) + Px_4*log2(1/Px_4) + Px_5*log2(1/Px_5); R = r*H_X;//information rate //result printf("\n\nRate of information = %.2f bits/sec",R);
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@relation coil2000 @attribute MOSTYPE integer[1,41] @attribute MAANTHUI integer[1,10] @attribute MGEMOMV integer[1,6] @attribute MGEMLEEF integer[1,6] @attribute MOSHOOFD integer[1,10] @attribute MGODRK integer[0,9] @attribute MGODPR integer[0,9] @attribute MGODOV integer[0,5] @attribute MGODGE integer[0,9] @attribute MRELGE integer[0,9] @attribute MRELSA integer[0,7] @attribute MRELOV integer[0,9] @attribute MFALLEEN integer[0,9] @attribute MFGEKIND integer[0,9] @attribute MFWEKIND integer[0,9] @attribute MOPLHOOG integer[0,9] @attribute MOPLMIDD integer[0,9] @attribute MOPLLAAG integer[0,9] @attribute MBERHOOG integer[0,9] @attribute MBERZELF integer[0,5] @attribute MBERBOER integer[0,9] @attribute MBERMIDD integer[0,9] @attribute MBERARBG integer[0,9] @attribute MBERARBO integer[0,9] @attribute MSKA integer[0,9] @attribute MSKB1 integer[0,9] @attribute MSKB2 integer[0,9] @attribute MSKC integer[0,9] @attribute MSKD integer[0,9] @attribute MHHUUR integer[0,9] @attribute MHKOOP integer[0,9] @attribute MAUT1 integer[0,9] @attribute MAUT2 integer[0,9] @attribute MAUT0 integer[0,9] @attribute MZFONDS integer[0,9] @attribute MZPART integer[0,9] @attribute MINKM30 integer[0,9] @attribute MINK3045 integer[0,9] @attribute MINK4575 integer[0,9] @attribute MINK7512 integer[0,9] @attribute MINK123M integer[0,9] @attribute MINKGEM integer[0,9] @attribute MKOOPKLA integer[1,8] @attribute PWAPART integer[0,3] @attribute PWABEDR integer[0,6] @attribute PWALAND integer[0,4] @attribute PPERSAUT integer[0,9] @attribute PBESAUT integer[0,7] @attribute PMOTSCO integer[0,7] @attribute PVRAAUT integer[0,9] @attribute PAANHANG integer[0,5] @attribute PTRACTOR integer[0,7] @attribute PWERKT integer[0,6] @attribute PBROM integer[0,6] @attribute PLEVEN integer[0,9] @attribute PPERSONG integer[0,6] @attribute PGEZONG integer[0,3] @attribute PWAOREG integer[0,7] @attribute PBRAND integer[0,8] @attribute PZEILPL integer[0,3] @attribute PPLEZIER integer[0,6] @attribute PFIETS integer[0,1] @attribute PINBOED integer[0,6] @attribute PBYSTAND integer[0,5] @attribute AWAPART integer[0,2] @attribute AWABEDR integer[0,5] @attribute AWALAND integer[0,1] @attribute APERSAUT integer[0,12] @attribute ABESAUT integer[0,5] @attribute AMOTSCO integer[0,8] @attribute AVRAAUT integer[0,4] @attribute AAANHANG integer[0,3] @attribute ATRACTOR integer[0,6] @attribute AWERKT integer[0,6] @attribute ABROM integer[0,3] @attribute ALEVEN integer[0,8] @attribute APERSONG integer[0,1] @attribute AGEZONG integer[0,1] @attribute AWAOREG integer[0,2] @attribute ABRAND integer[0,7] @attribute AZEILPL integer[0,1] @attribute APLEZIER integer[0,2] @attribute AFIETS integer[0,4] @attribute AINBOED integer[0,2] @attribute ABYSTAND integer[0,2] @attribute CARAVAN{0,1} @inputs MOSTYPE,MAANTHUI,MGEMOMV,MGEMLEEF,MOSHOOFD,MGODRK,MGODPR,MGODOV,MGODGE,MRELGE,MRELSA,MRELOV,MFALLEEN,MFGEKIND,MFWEKIND,MOPLHOOG,MOPLMIDD,MOPLLAAG,MBERHOOG,MBERZELF,MBERBOER,MBERMIDD,MBERARBG,MBERARBO,MSKA,MSKB1,MSKB2,MSKC,MSKD,MHHUUR,MHKOOP,MAUT1,MAUT2,MAUT0,MZFONDS,MZPART,MINKM30,MINK3045,MINK4575,MINK7512,MINK123M,MINKGEM,MKOOPKLA,PWAPART,PWABEDR,PWALAND,PPERSAUT,PBESAUT,PMOTSCO,PVRAAUT,PAANHANG,PTRACTOR,PWERKT,PBROM,PLEVEN,PPERSONG,PGEZONG,PWAOREG,PBRAND,PZEILPL,PPLEZIER,PFIETS,PINBOED,PBYSTAND,AWAPART,AWABEDR,AWALAND,APERSAUT,ABESAUT,AMOTSCO,AVRAAUT,AAANHANG,ATRACTOR,AWERKT,ABROM,ALEVEN,APERSONG,AGEZONG,AWAOREG,ABRAND,AZEILPL,APLEZIER,AFIETS,AINBOED,ABYSTAND @outputs CARAVAN @data 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 1 1 1 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 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//Chapter 6 Example 2// clc clear //total discharge during weeks=td// w1=500;w2=500;w3=350;w4=200;w5=300;w6=800;w7=1100;w8=900;w9=400;w10=200; // these are the weekly discharges respectively for 10 weeks// td=w1+w2+w3+w4+w5+w6+w7+w8+w9+w10; printf("\n Total Discharge = %.2f m^3/sec\n",td); //average weekly discharge=wd// wd=td/10; printf("\n Average weekly discharge = %.2f m^3/sec\n",wd); // to plot the hydrograph// x=[1,2,3,4,5,6,7,8,9,10]; y=[500,500,350,200,300,800,1100,900,400,200]; plot2d(x,y,style=2,rect=[0,0,10,1100]); xtitle("Hydrograph","Time(Weeks)","Q(m^3/sec)"); xset('window',1); // to plot flow duration graph// a=[10,20,30,50,60,70,90,100]; b=[1100,900,800,500,400,350,300,200]; plot2d(a,b,style=3,rect=[0,0,100,1100]); xtitle("Flow duration curve","Percentage of time","Q(m^3/sec)"); // to plot mass curve// xset('window',2); c=[1,2,3,4,5,6,7,8,9,10]; d=[3500,7000,9450,10850,12950,18550,26250,32550,35350,36750]; plot2d(c,d,style=4,rect=[0,0,10,40000]); xtitle("Mass Curve","Time(weeks)","Cumulative flow(day-sec-metre)"); legend("Mass Curve","Ordinary Curve");
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//Example number 8.10, Page number 173 clc;clear; close; //Variable declaration h=200; //hysteresis loss per cycle(J/m**3) M=7650; //atomic weight(kg/m**3) n=100; //magnetisation cycles per second //Calculation hpl=h*n; //hysteresis power loss per second(watt/m**3) pl=hpl/M; //power loss(watt/kg) //Result printf("hysteresis power loss per second is %.f W/m^3",hpl) printf("\n power loss is %.3f W/kg",pl)
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clc; clear; mprintf('MACHINE DESIGN \n Timothy H. Wentzell, P.E. \n EXAMPLE-3.2 Page No.43\n'); b=2; //[in] Width of beam h=2; //[in] Height of beam I=(b*h^3)/12; //[in^4] Moment of inertia F=3000; //[lb] Load applied to beam L=36; //[in] Length of beam c=1; //[in] Distance of outer most fiber from neutral axis E=30*10^6; //[lb/in^2] Modulus of elasticity Sy=30000; //[lb/in^2] Yield strength Su=55000; //[lb/in^2] Ultimate strength SF=2; //[] Safety factor based on ultimate stress M=F*L/4; //[lb*in] Bending moment S=(M/I)*c; //[lb/in^2] Bending stress //Note-In the book I=1.33 in^4 is used instead of I=1.3333333 in^2 mprintf('\na. The maximum stress in beam is %f lb/in^2',S); delta=-F*L^3/(48*E*I); //[in] Maximum deflection in this beam mprintf('\nb. The maximum deflection in this beam is %f in.',delta); if Sy>S then mprintf('\nc. Yes, the stress of %f lb/in^2 is less than the yield of Sy=%f lb/in^2.',S,Sy); else mprintf('\nc. No, the stress of %f lb/in^2 is greater than the yield of Sy=%f lb/in^2',S,Sy); end Sall=Su/SF; //[lb/in^2] Allowable stress if Sall>S then mprintf('\nd. It is acceptable because allowable stress is greater than the acttual stress of %f lb/in^2.',S); else mprintf('\nd. Design is not acceptable because allowable stress is less than the actual stress of %f lb/in^2.',S) end //Note: The deviation of answer from the answer given in the book is due to round off error.(In the book values are rounded while in scilab actual values are taken)
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function [varargout] = retrieveImages(QueryImage, IndexImage, varargin) /// varargout(1) = index /// varargout(2) = score /// varargout(3) = Imageword [ lhs rhs ] = argn(0) if rhs > 6 then error(msprintf("Too many input arguments")) end if lhs > 3 then error(msprintf("Too many output arguments")) end QueryImage_list = mattolist(QueryImage) if lhs == 1 then select rhs case 2 then index = opencv_retrieveImages(QueryImage_list, IndexImage) case 4 then index = opencv_retrieveImages(QueryImage_list, IndexImage, varargin(1), varargin(2)) case 6 then index = opencv_retrieveImages(QueryImage_list, IndexImage, varargin(1), varargin(2), varagin(3), varargin(4)) end varargout(1) = index elseif lhs == 2 then select rhs case 2 then [index, score] = opencv_retrieveImages(QueryImage_list, IndexImage) case 4 then [index, score] = opencv_retrieveImages(QueryImage_list, IndexImage, varargin(1), varargin(2)) case 6 then [index, score] = opencv_retrieveImages(QueryImage_list, IndexImage, varargin(1), varargin(2), varagin(3), varargin(4)) end varargout(1) = temp varargout(2) = score elseif lhs == 3 then select rhs case 2 then [index, score, Imageword] = opencv_retrieveImages(QueryImage_list, IndexImage) case 4 then [index, score, Imageword] = opencv_retrieveImages(QueryImage_list, IndexImage, varargin(1), varargin(2)) case 6 then [index, score, Imageword] = opencv_retrieveImages(QueryImage_list, IndexImage, varargin(1), varargin(2), varagin(3), varargin(4)) end varargout(1) = index varargout(2) = score del = struct("WordIndex", Imageword(1), "Location", Imageword(2), "Vocab_size", Imageword(3), "Count", Imageword(4)) varargout(3) = del end endfunction
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//Chapter7,Ex7.5,Pg7.15 clc; B=50 Ib=20 //Base current in microamperes Ic=B*Ib printf("\n Ic=%.0f mA \n",Ic*10^-3) Ie=Ic+Ib printf("\n Ie=%.2f mA \n",Ie*10^-3)
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//Example 9.2: clc; clear; close; //given data : Va=300;// in V Vm=300*sqrt(2);//in V Rl=50;//in ohm theta1=90;//firing angle in degree idc=((Vm/(2*%pi*Rl))*(1+cosd(theta1)));//in A format('v',6) disp((idc),"(i) the dc load current is ,(A)=") irms=Va/(2*Rl);//in A format('v',4) disp(round(irms),"(ii) the rms load current is ,(A)=") P=irms^2*Rl;//in W format('v',5) disp(round(P),"(iii) the power dissipated by the load is ,(W)=")
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clc clear D=0.3; L=0.6; N=60; Hs=5; Hd=10; Ep=0.8; Qa=0.075; A=(22/7)*(1/4)*D*D; Rho=1000; g=9.81; F1=Rho*g*Hs*A; F2=Rho*g*Hd*A; TF=F1+F2; printf('Total Force Required: %2.2f kN',TF/1000); printf('\n'); Q=(2*L*A*N)/60; Qa=0.075; Slip=(Q-Qa)/Q; printf('Percentage Slip: %2.2f Percent',Slip*100); printf('\n'); Cd=Qa/Q; P=(Rho*g*Qa*(Hs+Hd))/Ep; printf('Power input: %2.2f kW',P/1000); printf('\n');
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clc //finite difference method disp("the solution of eg 5.1-->Discretization in 1-D space"); //given d2y_by_dx2-2=0 hence it is dirichlet's problem x_1=0, y_1=0 //initial boundary conditions x_3=1, y_3=0 delta_x=.5 //since we have to find y_2 at x=.5 so x_2=.5 //in the central difference method substituting i=2 we have //(y_3-2*y_2+y_1)/(delta_x)^2=2 //since y_1 & y_3=0 as per B.C. y_2=(y_3+y_1-2*delta_x^2)/2 disp(y_2,"the value of y at x=.5 from finite difference method is"); x=.5 y_exact=x^2-x disp(y_exact,"the value of y from exact soln at x=.5 is");
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// Example 5.7: Analyse the circuit to find node voltages and branch currents V_CC=-10; // (V) R_E=2000; // (ohm) R_C=1000; // (ohm) V_EE=10; // (V) V_E=0.7; // (V) emitter base junction will be forward biased with V_E=V_EB=0.7V disp(V_E,"Emitter base junction is forward biased with V_E (V)") I_E=(V_EE-V_E)/R_E; disp(I_E,"Emitter current (A)") B=100; // Assuming beta 100 a=B/(B+1); I_C=a*I_E; // Assuming the transistor to operate in active mode disp(I_C,"Collector current (A)") V_C=V_CC+I_C*R_C; disp(V_C,"Collector voltage (V)") I_B=I_E/(B+1); disp(I_B,"Base current (A)")
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clc //given s1=26 s2=24 s3=23 sr=31 i1=70 i2=72 i3=61 ir=71 t=1500//lb in k1=-i3/s3//Ns3-Ni2/(Ni3-Ni2)=k //S3 is fixed thus k2=1-(1/k1)//k2=Ni3/Ni2 k3=-i2/s2//k3=Ns2-Ni3/(Ni2-Ni3) k4=(1/k2-1)*k3+1//k4=Ns2/Ni3 ; reducing using k2 and k3 k5=-i1/s1//Ns1-Nf/(Ni1-Nf) k6=(1-k5)/(1-k5/k4)//k6=Ns1/Nf printf("\n Ns1/Nf = %.2f",k6)
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clc; clear all; t = 12.5e-6; // Thickness in meters d = 0.01; // Difference in principal refractive index (uo-ue) lambda = 2*t*d;//The wavelength of light disp('m',lambda,'The wavelength of light is') //rounding off due to scilab
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function [y, i, j] = moc_unique (x,param) // Return the unique elements of x, sorted in ascending order. // Calling Sequence // moc_unique (x) // moc_unique (x, "rows") // moc_unique (..., "first") // umoc_nique (..., "last") // [y, i, j] = moc_unique (...) // Description // If x is a row vector, return a row vector, but if x // is a column vector or a matrix return a column vector. // // If the optional argument "rows" is supplied, return the unique // rows of x, sorted in ascending order. // // If requested, return index vectors i and j such that // x(i)==y and y(j)==x. // // Additionally, one of "first" or "last" may be given as // an argument. If "last" is specified, return the highest // possible indices in i, otherwise, if "first" is // specified, return the lowest. The default is "last". // See also // moc_ismember // Authors // Copyright (C) 2008, 2009 Jaroslav Hajek // Copyright (C) 2000, 2001, 2005, 2006, 2007 Paul Kienzle // H. Nahrstaedt 2010,2011 // // 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/>. [nargout,nargin]=argn(0); if (nargin < 1) error ("One Argument is needed!"); end if nargin==1 optfirst = 0; optrows = 0; else optfirst = (param=="first"); optlast = param=="last" optrows = param=="rows" & size (x, 2) > 1; end if (optrows) n = size (x, 1); dim = 1; else n = size (x,'*'); dim = (size (x, 1) == 1) + 1; end y = x; if (n < 1) i = []; j = []; return; elseif (n < 2) i = 1; j = 1; return; end if (optrows) [y, i] = gsort(y,'r','i'); match = and (y(1:n-1,:) == y(2:n,:), 2); idx = find (match); y(idx,:) = []; else if (size (y, 1) ~= 1) y = y(:); end //[y, i] = mtlb_sort (y); [y, i] = gsort (y,'g','i') match = (y(1:n-1) == y(2:n)); idx = find (match); y(idx) = []; end if (nargout >= 3) j = i; if (dim == 1) j(i) = cumsum ([1; ~match]); else j(i) = cumsum ([1, ~match]); end end if (optfirst) i(idx+1) = []; else i(idx) = []; end endfunction //assert(unique([1 1 2; 1 2 1; 1 1 2]),[1;2]) //assert(unique([1 1 2; 1 0 1; 1 1 2],'rows'),[1 0 1; 1 1 2]) //assert(unique([]),[]) //assert(unique([1]),[1]) //assert(unique([1 2]),[1 2]) //assert(unique([1;2]),[1;2]) //assert(unique([1,NaN,Inf,NaN,Inf]),[1,Inf,NaN,NaN]) //assert(unique({'Foo','Bar','Foo'}),{'Bar','Foo'}) //assert(unique({'Foo','Bar','FooBar'}'),{'Bar','Foo','FooBar'}') //test // [a,i,j] = unique([1,1,2,3,3,3,4]); // assert(a,[1,2,3,4]) // assert(i,[2,3,6,7]) // assert(j,[1,1,2,3,3,3,4]) // //test // [a,i,j] = unique([1,1,2,3,3,3,4]','first'); // assert(a,[1,2,3,4]') // assert(i,[1,3,4,7]') // assert(j,[1,1,2,3,3,3,4]') // //test // [a,i,j] = unique({'z'; 'z'; 'z'}); // assert(a,{'z'}) // assert(i,[3]') // assert(j,[1,1,1]') // //test // A=[1,2,3;1,2,3]; // [a,i,j] = unique(A,'rows'); // assert(a,[1,2,3]) // assert(A(i,:),a) // assert(a(j,:),A)
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s = poly(0,'s'); t = 0:.001:10; // PART A h1 = 1/s^2; h2 = 50*s/(s^2+s+100); h3 = s-2; h4 = h1*h2*h3; Heq = syslin('c', h4/(1+h4)); // PART B h1 = s; h2 = 1/s; h3 = h1*h1+h2; // inner series + parallel connection h4 = h3/(h3+1)*h2; // taking care of upper feedback loop Heq_b = syslin('c', h1*h4/(1+h1*h4)); // very similar to a part (just there is additional multiplication in feedback loop), this Heq itslf works like a syslin object would //PART C h1 = s; h2 = 2*s; h3 = 1/(s+1); h4 = 4; G1 = h1+h2; G2 = h1/(1+h1); G3 = h1/(G1); // 1/s+2 G4 = G1*G2+ h2; G5 = 4*G3/(1+4*G3); G6 = G4*G5; Heq = syslin('c', G6/(1+G6));
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sce
bowtie.sce
Name=bowtie PlayerCharacters=1 BotCharacters=2.bot IsChallenge=true Timelimit=90.0 PlayerProfile=1 AddedBots=2.bot PlayerMaxLives=0 BotMaxLives=10 PlayerTeam=1 BotTeams=2 MapName=vertex.map MapScale=4.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=1.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Tracking WeaponHeroTag=Tracking Beam DifficultyTag=2 AuthorsTag=faiNt` BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=HEADSHOTS ONLY // ADS GameVersion=1.0.7.2 ScorePerDistance=0.0 [Aim Profile] Name=At Feet MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Low Skill At Feet MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Low Skill MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Bot Profile] Name=2 DodgeProfileNames=Long Strafe FB DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=2.0 DodgeProfileMinChangeTime=1.5 WeaponProfileWeights=1.0;1.0;2.0;1.0;0.0;0.0;0.0;0.0 AimingProfileNames=At Feet;Low Skill At Feet;Low Skill;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Watcher SeeThroughWalls=false NoDodging=false NoAiming=false [Character Profile] Name=1 MaxHealth=300.0 WeaponProfileNames=gun;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=700.0 MaxCrouchSpeed=500.0 Acceleration=5000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=320.0 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=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 [Character Profile] Name=Watcher MaxHealth=100.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.1 MaxRespawnDelay=5.0 StepUpHeight=45.0 CrouchHeightModifier=0.69 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=20.000 HeadshotOnly=true DamageKnockbackFactor=3.0 MovementType=Base MaxSpeed=200.0 MaxCrouchSpeed=270.0 Acceleration=10000.0 AirAcceleration=16000.0 Friction=100.0 BrakingFrictionFactor=0.0 JumpVelocity=300.0 Gravity=1.0 AirControl=0.16 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.000 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=0.888 Z=0.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=130.0 MainBBRadius=18.0 MainBBHasHead=true MainBBHeadRadius=10.0 MainBBHeadOffset=40.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=160.0 ProjBBRadius=26.0 ProjBBHasHead=false ProjBBHeadRadius=20.0 ProjBBHeadOffset=15.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.1 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 [Dodge Profile] Name=Long Strafe FB MaxTargetDistance=100000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.5 MaxLRTimeChange=2.0 MinFBTimeChange=1.0 MaxFBTimeChange=2.0 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.15 DamageReactionMaximumDelay=0.18 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.8 BlockedMovementReactionMin=0.05 BlockedMovementReactionMax=0.1 [Weapon Profile] Name=gun Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.046 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=1.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=7.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.05 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=true 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=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=1.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.1 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=77.139999 ADSFOVScale=Apex Legends ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 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,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=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=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -150.000000 710.000000 1854.000000 -86.000000 710.000000 1854.000000 -86.000000 710.000000 336.000000 -150.000000 710.000000 336.000000 -150.000000 -8.000000 1854.000000 -86.000000 -8.000000 1854.000000 -86.000000 -8.000000 336.000000 -150.000000 -8.000000 336.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 0 1 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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/08/FunctionCalls/SimpleFunction/SimpleFunctionVME.tst load SimpleFunction.vm, output-file SimpleFunction.out, compare-to SimpleFunction.cmp, output-list RAM[0]%D1.6.1 RAM[1]%D1.6.1 RAM[2]%D1.6.1 RAM[3]%D1.6.1 RAM[4]%D1.6.1 RAM[310]%D1.6.1; set sp 317, set local 317, set argument 310, set this 3000, set that 4000, set argument[0] 1234, set argument[1] 37, set argument[2] 9, set argument[3] 305, set argument[4] 300, set argument[5] 3010, set argument[6] 4010, repeat 10 { vmstep; } output;
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// // t1=80-70 l=50 k=1/(cos(20*(%pi/180))) k1=k*(sin(t1*(%pi/180))) t3=asin(k1) t3=t3*(180/(%pi)) printf("\n theta 3= %0.3f ",t3) t3=180-t3 t2=180-(t3+t1) r=l*(sin(t1*(%pi/180)))/(sin(0.6*(%pi/180))) printf("\n Radius R= %0.3f ",r)
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//Determine the critical angle of incidence between two substances with different refractive indexes n1 = 1.5; n2 = 1.46; thetaC = asind((1.46*n2)/(1.5*n1)); disp(thetaC, 'Critical angle is (in degrees)')
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clc;clear; //Example 15.10 //calculation of crosssection //given values t=.01*10^-3;//thickness in m n=10^13;//no of protons bombarding target per s NA=6.02*10^26;//avogadro's number M=7;//atomic mass of lithium in kg d=500;//density of lithium in kg/m^3 n0=10^8;//no of neutrons produced per s //calculation n1=d*NA/M;//no of target nuclei per unit volume n2=n1*t;//no of target nuclei per area A=n0/(n*n2); disp(A,'crosssection(in m^2) for this reaction is');
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clear // // // //Variable declaration e=1.6*10^-19; //charge(coulomb) x=9*10^9; r0=3.56*10^-10; //equilibrium distance(m) A=1.763; //madelung constant n=10.5; //repulsive exponent value IE=3.89; //ionisation energy(eV) EA=-3.61; //electron affinity(eV) //Calculations U0=-(x*A*e/r0)*(1-1/n); //ionic cohesive energy(eV) U=U0+IE+EA; //atomic cohesive energy(eV) //Result printf("\n ionic cohesive energy is %0.2f eV",U0) printf("\n atomic cohesive energy is %0.2f eV",U)
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clc //Given that c = 3e8 // speed of light in m/s v = 0.9 * c // velocity of rod wrt laboratory proper_time = 2.5e-8 // proper mean life time of mesons // sample problem 16 page No. 228 printf("\n \n\n # Problem 16 # \n") printf("\n Standard formula used \n t = t_o /sqrt ( 1- (v/c)^2)") t = proper_time / sqrt (1 - (v / c)^2) // calculation of New mean life time printf ("\n New mean life time is %e s.",t )
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Introduction to heat transfer by S.K.Som, Chapter 6, Example 7") //A flat plate B=1.2m wide and of length L is kept parallel to a uniform stream of air of velocity Uinf=3m/s in a wind tunnel. Uinf=3; B=1.2; //If it is desired to have a laminar boundary layer only on the plate //Assume that the laminar flow exists up to a reynold number(ReL)=5*10^5.Take density of air as rhoair=1.2kg/m^3 and viscosity of air as nuair=1.5*10^-5 m^2/s. nuair=1.5*10^-5; rhoair=1.2; ReL=5*10^5; //For maximum length of the plate reynolds number is ReL=Uinf*L/nuair //so L=ReL*nuair/Uinf disp("The maximum length of plate in m is ") L=ReL*nuair/Uinf //The average skin friction coefficient is cfL=1.328/(ReL)^(1/2) disp("The average skin friction coefficient is") cfL=1.328/(ReL)^(1/2) //Fd is drag force disp("Drag force on one side of plate in N is") Fd=cfL*(rhoair*Uinf^2/2)*B*L
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units VMG $thermo = VirtualMaterials.IdealLiquid/Ideal/HC / -> $thermo /LiquidPhases = 2 /thermo + TOLUENE ETHYLBENZENE STYRENE MESITYLENE alpha-METHYLSTYRENE n-PROPYLBENZENE #Feed S1 = Stream.Stream_Material() /S1.In.T = 317.75 K /S1.In.P = 220 mmHg /S1.In.Fraction = 0.80 51.00 47.77 0.06 0.13 0.20 /S1.In.MoleFlow = 99.96 kgmole/h #Tower 1 T1 = Tower.DistillationColumn() /T1.TryToSolve = 0 /S1.Out -> /T1.Feed_1_feed /T1.Stage_0 + 49 /T1.Stage_50.feed.ParentStage = 9 #Total cond and P prof delete /T1.Stage_0.condenserV /T1.LiquidDraw_0_condenserL.P = 40 mmHg /T1.LiquidDraw_51_reboilerL.P = 270 mmHg #More specs and solve /T1.LiquidDraw_0_condenserL.MoleFlow = 52 kgmole/h /T1.Variable_0_Reflux.Generic = 2.5 /T1.TryToRestart = 0 /T1.TryToSolve = 1 /T1.TryToRestart = 1 /T1.TryToSolve = 0 #Add liquid draw and solve /T1.Stage_20.L = Tower.LiquidDraw() /T1.LiquidDraw_20_L.MoleFlow = 11 kgmole/h /T1.TryToRestart = 1 /T1.TryToSolve = 1 #Energy, distillate, draw and bottoms streams for T1 S2 = Stream.Stream_Material() /T1.LiquidDraw_0_condenserL -> /S2.In S3 = Stream.Stream_Material() /T1.LiquidDraw_20_L -> /S3.In S4 = Stream.Stream_Material() /T1.LiquidDraw_51_reboilerL -> /S4.In Q1 = Stream.Stream_Energy() /T1.EnergyFeed_0_condenserQ -> /Q1.In Q2 = Stream.Stream_Energy() /Q2.Out -> /T1.EnergyFeed_51_reboilerQ #Tower2 T2 = Tower.DistillationColumn() /T2.TryToSolve = 0 /S4.Out -> /T2.Feed_1_feed /T2.Stage_0 + 49 /T2.Stage_50.feed.ParentStage = 30 #Total cond and P prof delete /T2.Stage_0.condenserV /T2.LiquidDraw_0_condenserL.P = 40 mmHg /T2.LiquidDraw_51_reboilerL.P = 250 mmHg #more specs and solve /T2.LiquidDraw_0_condenserL.MoleFlow = 16 kgmole/h /T2.Variable_0_Reflux.Generic = 2.5 /T2.TryToRestart = 0 /T2.TryToSolve = 1 /T2.TryToRestart = 1 /T2.TryToSolve = 0 #Add liquid draw and solve /T2.Stage_20.L = Tower.LiquidDraw() /T2.LiquidDraw_20_L.MoleFlow = 7 kgmole/h /T2.TryToRestart = 0 /T2.TryToSolve = 1 /T2.TryToRestart = 1 /T2.TryToSolve = 0 #Energy, distillate, draw and bottoms streams for T2 S5 = Stream.Stream_Material() /T2.LiquidDraw_0_condenserL -> /S5.In S6 = Stream.Stream_Material() /T2.LiquidDraw_20_L -> /S6.In S7 = Stream.Stream_Material() /T2.LiquidDraw_51_reboilerL -> /S7.In Q3 = Stream.Stream_Energy() /Q3.Out -> /T2.EnergyFeed_51_reboilerQ Q4 = Stream.Stream_Energy() /T2.EnergyFeed_0_condenserQ -> /Q4.In #Connect recycle and spec estimates /T2.LiquidDraw_0_condenserL -> /T1.Stage_44.feed = Tower.Feed() /T1.Feed_44_feed -> /S5.Out /S5.In.T ~= 350 K /S5.In.P ~= 26.6644 /S5.In.MoleFlow ~= 0 /S5.In.Fraction ~= 1 0 0 0 0 0 /T2.LiquidDraw_0_condenserL -> /S5.In #Final solve /T1.TryToRestart = 1 /T1.TryToSolve = 1 /T2.TryToRestart = 1 /T2.TryToSolve = 1
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//ANSWER GIVEN IN THE BOOK FOR THIS QUESTION IS INCORRECT. clc; //Neglecting armature reaction & magnetic saturation //Assuming rotational losses to remain constant V=230;//Supply voltage P=15000;//power rating of dc series motor in watts Il_1=80;//line current rated Il_2=40;//line current assuming that motor draws half the rated current at rated voltage Ia_1=Il_1;//armature current at line current equal to 80 A. Ia_2=Il_2;//armature current at line current equal to 40 A. n1=1000;//rated speed in rpm //Full load losses expressed as percentage of motor input:- //Armature ohmic loss=2.8%(including brush loss) //Field ohmic loss=2.2% //Rotational loss=2.2% P_ip=V*Il_1;//full load input P_ohmic=P_ip*(5.4/100)//As percent of total ohmic losses=2.2+2.8=5.4% //But P_ohmic=Il*Il*(Ra+Rs); where (Ra+Rs)=(armature + series field) resistance //(Ra+Rs)=P_ohmic/(Il*Il)=0.115 ohms //Let, r=(Ra+Rs) r=0.115; //PART(a)- Ea1=V-(Ia_1*r);//counter emf at line current = 80 A Ea2=V-(Ia_2*r);//counter emf at line current = 40 A //Since the magnetic saturation is neglected, phi_1=k*80 & phi_2=k*40; where k=constant & phi_1 & phi_2 are flux per pole at line currents 80 & 40 A respectively. //(Ea1/Ea2)=(n1*phi_1)/(n2*phi_2) or (220.8/225.4)=(1000*80)/(n2*40); where Ea1=220.8 V Ea2=225.4 V. n2=(1000*80*225.4)/(40*220.8);//speed in rpm printf('The speed of rotation of motor when the motor draws half the rated current at rated voltage is %f rpm.',round(n2)); //PART(b)- Pr=P_ip*(2.2/100);//rotational losses Psh=Ea2*Ia_2-Pr; printf('\nThe shaft output power is %f W.',Psh);
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player_keep_win_list = list() player_switch_win_list = list() player_keep_win = 0 player_switch_win = 0 doors = 3 clf title("Mounty Hall Problem: " + string(doors) + " doors") xlabel("Games") ylabel("% Win") for n = 1:1000 car = int(rand() * doors) + 1 door = int(rand() * doors) + 1 openned_door = int(rand() * doors) + 1 while openned_door == car | openned_door == door do openned_door = int(rand() * doors) + 1 end if door == car then player_keep_win = player_keep_win + 1 end player_keep_win_list($ + 1) = player_keep_win new_door = int(rand() * doors) + 1 while new_door == door | new_door == openned_door do new_door = int(rand() * doors) + 1 end if new_door == car then player_switch_win = player_switch_win + 1 end player_switch_win_list($ + 1) = player_switch_win x = 1:length(player_switch_win_list) plot(list2vec(player_switch_win_list)'./x, "r") plot(list2vec(player_keep_win_list)'./x, "g") hl=legend(['Switch door';'Keep door']); end
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clc; clear; close; t=10;//in years A=2*(10^7);//in hr-cm^2/amp delH=0.85;//in eV T=398;//in kelvin t50=10*t*365*24; k=8.62*(10^(-5)); Jmax=sqrt(A*exp(delH/(k*T))/t50); disp(Jmax,'max tolerable current density for electromigration(in A/cm^2)='); //the answer given in the textbook is wrong
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clear; clc; // Illustration 9.1 // Page: 508 printf('Illustration 9.1 - Page: 508\n\n'); // solution //*****Data*****// // A-solute B-solvent ci_f = 50; // [feed side concentration, mole/cubic m] ci_p = 15; // [permeate side concentration, mole/cubic m] t = 2*10^-4; // [membrane thickness, cm] q_A = 176; // [permeability, barrer] D = 4*10^-1; // [tube inside diameter, cm] D_A = 5*10^-5; // [diffusuvity, square cm/s] Re = 20000; // [reynolds number] Sc = 450; // [Schmidt number] mtc_p = 0.12; // [square cm/s] //*****// // From equation 9.6, 1 barrer = 8.3*10^-9 square cm/s // Therefore q_A = q_A*8.3*10^-9; // [square cm/s] Q_A = q_A/t; // [permeance, cm/s] // The mass-transfer coefficient on the feed side is from equation (2-75) for turbulent flow of a liquid inside a circular pipe: Sh = 0.023*Re^0.83*Sc^(1/3); // Now mass transfer coefficient k_af = Sh*D_A/D; // [cm/s] // Total resistance to mass transfer res_total = (1/k_af)+(1/Q_A)+(1/mtc_p); // [s/cm] // Transmembrane flux of solute A N_A = (ci_f-ci_p)/(res_total*100); // [mole/square m.s] printf("The transmembrane flux of solute A is %e mole/square m.s\n\n",N_A); percent_mem_res = ((1/Q_A)/res_total)*100; // [%] printf("Membrane resistance is %f percent of the total\n\n",percent_mem_res);
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//No of cylinders k=6 //Speed (in rpm) s=720 //Diameter (in cm) d=(20*10^(-2)); //Stroke Lenght (in cm) l=(25*(10^(-2))); //Compression ratio cr=20; //Exhaust Pressure (in bar) ep=(1.04*(10^5)); //Ambient temperature (in kelvin) t=300; //Universal gas constant r=287; //Scavanger Efficiency nsc=0.85 //Scavanger ratio Rsc=1.2 //Specific heat of gas at constant pressure cp=1.005 //Brake Power bp = (120*k) //bsfc in kg/kWh bsfc = 0.21 //Calorific Value (in calorie) CV = 44000/3600
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clc; //from tables; v_a=0.1115;//m^3/kg p_b=20;//bar v_d=0.4743;//m^3/kg hf=763;//kJ/kg h=2650;//kJ/kg h_fg=2015;//kJ/kg x=(h-hf)/h_fg; vg=0.1944;//m^3/kg v_c=x*vg; clf(); x=linspace(0.05,0.5,1000); y=(0.09957*20)*((x)^(-1)); plot2d(x,y,style=1); y=20; plot(x,y) y=10; plot(x,y); y=(0.4743*6)*((x)^(-1)); plot2d(x,y,style=4); y=(0.1115*20)*((x)^(-1)); plot2d(x,y,style=2); y=6; plot2d(x,y,style=4)
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function a=f2t(S,fs) N=length(S); T=1/fs*N; t=[-(T/2):1/fs:(T/2-1/fs)]; temp1=fft(S)/T; temp2=N*ifft(S)/T; a(1:N/2)=temp1(N/2+1:-1:2); a(N/2+1:N)=temp2(1:N/2); a=a.*exp((-%i*%pi)*fs*t); endfunction