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s = %s sysl = syslin('c',1,(s*s+0.3*2*s+1)); xtitle( 'Second order step response with damping factor 0.3', 'X axis', 'Y axis' ) ; t =0:0.1:10; y = csim('step',t,sysl) plot(t,y)
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////Given W=3 //ev h=6.63*10**-34 e=1.6*10**-19 lembda=3.0*10**-7 //m c=3*10**8 //m/s //Calculation v0=(W*e)/h v=c/lembda E=h*(v-v0) E1=(h*(v-v0))/(1.6*10**-19) V0=E/e //Result printf("\n (a) Threshold frequency %0.2f *10**15 HZ",v0*10**-15) printf("\n (b) Maximum energy of photoelectron %0.2f eV",E1) printf("\n (c) Stopping potential %0.2f V",V0)
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function contourf(x,y,z,nv,style,strf,leg,rect,nax) [nout,nin]=argn(0); if nin==0, s_mat=['t=-%pi:0.1:%pi;m=sin(t)''*cos(t);contourf(t,t,m);']; write(%io(2),s_mat);execstr(s_mat); return; end; if nin <= 8 then nax=[1,10,1,10];end if nin <= 7 then rect=[0,0,1,1];end if nin <= 6 then leg=" ";end if nin <= 5 then strf="121";end if nin <= 3 then nv=linspace(mini(z),maxi(z),10);end if nin <= 2 then z=rand(size(x,'*'),size(y,'*'));end if nin <= 1 then y=1:10;end if nin <= 0 then x=1:10;end if x==[] then x=1:size(z,'r');end if y==[] then y=1:size(z,'c');end nvs=size(nv,'*') ; if nvs==1 then nvs=nv;nv=linspace(mini(z),maxi(z),nv);end if nin <= 4 then style = -1*ones(1,nvs);end if nin <= 7 then rect=[mini(x),mini(y),maxi(x),maxi(y)]; end [mz,nz] = size(z); minz = min(z); maxz = max(z); // Surround the matrix by a very low region to get closed contours, and // replace any NaN with low numbers as well. zz=[ %nan*ones(1,nz+2); %nan*ones(mz,1),z,%nan*ones(mz,1);%nan*ones(1,nz+2)]; kk=find(isnan(zz(:))); zz(kk)=minz-1e4*(maxz-minz)+zeros(kk); xx = [2*x(1)-x(2); x(:); 2*x(mz)-x(mz-1)]; yy = [2*y(1)-y(2); y(:); 2*y(nz)-y(nz-1)]; // Internal call to get the contours contour2di(xx,yy,zz,nv,style,strf,leg,rect,nax); [x1,y1]=c2dex(); CS=[x1;y1]; // Find the indices of the curves in the c matrix, and get the // area of closed curves in order to draw patches correctly. ii = 1; ncurves = 0; I = []; Area=[]; while (ii < size(CS,2)), nl=CS(2,ii); ncurves = ncurves + 1; I(ncurves) = ii; xp=CS(1,ii+(1:nl)); // First patch yp=CS(2,ii+(1:nl)); Area(ncurves)=sum( mtlb_diff(xp).*(yp(1:nl-1)+yp(2:nl))/2 ); ii = ii + nl + 1; end lp=xget('lastpattern'); if nv > lp ; write(%io(2),'Colormap too small');return ;end min_nv=mini(nv); max_nv=maxi(nv); plot2d([mini(xx);maxi(xx)],[mini(yy);maxi(yy)],0,strf,leg,rect,nax); // Plot patches in order of decreasing size. This makes sure that // all the lev1es get drawn, not matter if we are going up a hill or // down into a hole. When going down we shift levels though, you can // tell whether we are going up or down by checking the sign of the // area (since curves are oriented so that the high side is always // the same side). Lowest curve is largest and encloses higher data // always. draw_min=1; H=[]; [FA,IA]=sort(abs(Area)); pat=xget('pattern'); for jj=IA', nl=CS(2,I(jj)); lev1=CS(1,I(jj)); if (lev1 ~= minz | draw_min), xp=CS(1,I(jj)+(1:nl)); yp=CS(2,I(jj)+(1:nl)); pat=size(find( nv <= lev1),'*'); xset("pattern",pat); xfpoly(xp,yp) end; end xset('pattern',pat); if style(1)<>-1 then contour2d(xx,yy,zz,nv,style,"000",leg,rect,nax); end
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//Chapter 3 : Systems of Linear Equations //Example 3.6 //Scilab 6.0.1 //Windows 10 clear; clc; lambda=3 //assume lambda to be 3 P=[1 lambda 0;0 1 0;0 0 1]; A=[1 3;5 7;9 11]; //let A be any 4*2 matrix disp(P,'P:') disp(A,'A:') disp(lambda,'lambda:') PA=P*A; disp(PA,'PA') mprintf('the effect of multiplying A on the left by P is to add \n lambda times the second row of A to the first row')
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//Example number 7.7, Page number 148 clc;clear; close; //Variable declaration epsilonr=1.0000684; //dielectric constant Na=2.7*10**25; //number of atoms x=1/(9*10**9); E=10**6; //electric field(V/m) e=1.6*10**-19; //charge(c) Z=2; //atomic number //Calculation r0=((epsilonr-1)/(4*%pi*Na))**(1/3); //radius of electron cloud(m) X=x*E*r0**3/(Z*e); //displacement(m) //Result printf("radius of electron cloud is %.2e m",r0) printf("\n displacement is %.4e m",X)
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clc; clear; y=5;//ft angle=40;//degree l=12;//ft rate=1.4;//ft per 1000 ft of length K=1.49; A=(l*y)+(y*y/tan(angle*%pi/180));//ft P=(l+(2*y/sin(angle*%pi/180)));//ft Rh=A/P; S0=rate/1000; x=K*(A)*(Rh^(2/3))*(S0^0.5);//where Rh=Q*n n=0.012; Q=x/n;//cfs disp("cfs",Q,"The flowrate=") V=Q/A;//ft/sec Fr=V/(32.2*y)^0.5; disp(Fr,"Froude number=")
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//Example 8.6 //current clc; clear; close; V=220;// in volts I=60;// in amperes rpm=728;//turns Ts=150;//shaft torque in N-m nc=80;//commercial efficiency in percentge I=((Ts*2*%pi*rpm*746)/(60*746*(nc/100)*V));// CURRENT TAKEN IN AMPERES disp(round(I),"current taken in amperes is")
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clc m=1; //kg p=8; //bar s1=6.55; //kJ/kg.K T=200; //0C s_f1=2.0457; //kJ/kg.K s_fg1=4.6139; //kJ/kg.K h_f1=720.9; //kJ/kg h_fg1=2046.5; //kJ/kg h2=2839.3; //kJ/kg x1=(s1-s_f1)/s_fg1; h1=h_f1+x1*h_fg1; Q=h2-h1; disp("Heat supplied=") disp(Q) disp("kJ/kg") // For T-s diagram s=0:0.01:10; T=(-(s-5)^2+298); plot(s,T) T=[295.44 295.44]; s=[6.6 3.45]; plot(s,T,'g') s=[6.6 7]; T=[295.44 300]; plot(s,T,'g') s=[6.55 6.55]; T=[270 295.44]; plot(s,T,'r') s=[6.6 6.6]; T=[270 295.44]; plot(s,T,'--r') s=[6.66 6.66]; T=[270 295.44]; plot(s,T,'r') xtitle("T-s diagram", "s(kJ/kg K)", "T(K)") //The area in red represents the heat flow and it goes upto x-axis
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// Test avec la matrice suivante : K3 = [ 5 0 0 0 0 0 0 0 0 0 0 0 0 -1 0 -1 0 0 0 -1 0 0 0 -1 -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 8 0 -1 0 0 0 0 0 0 0 0 0 -1 -1 0 0 0 0 0 -1 -1 0 0 0 -1 -1 -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 8 -1 0 0 0 0 0 0 0 0 0 0 0 -1 -1 0 0 0 0 0 0 0 0 0 0 0 0 0 -1 -1 -1 0 -1 -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 -1 -1 24 -1 0 -1 0 0 0 0 0 0 -1 -1 -1 -1 0 0 0 -1 -1 0 0 -1 -1 -1 -1 -1 0 -1 -1 -1 -1 -1 -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 -1 13 0 -1 -1 0 0 0 0 0 0 -1 0 0 0 0 0 0 0 -1 0 0 0 0 -1 -1 -1 0 0 0 -1 0 0 -1 -1 -1 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 8 -1 0 0 0 0 0 0 0 0 0 -1 -1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 -1 -1 -1 0 -1 -1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 ; 0 0 0 -1 -1 -1 21 -1 0 -1 0 0 0 0 0 0 -1 -1 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 -1 0 -1 -1 -1 -1 -1 -1 -1 -1 -1 -1 -1 -1 0 0 -1 0 0 0 0 0 0 0 0 0 0 0 ; 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sigma = 'SM'; [d, v] = eigs(K3, B, k, sigma); Xx = v(:,2); Yy = v(:,3); Zz = v(:,4); // calcul matrice Zz2 unitaire = ones(dim); Zz2 = Zz*unitaire; Zz2 = eye(Zz2).*Zz2; // fin calcul matrice Zz2 //param3d1(Xx, Yy, Zz); a = get("current_axes"); h = a.children; h.line_mode = "off"; h.mark_mode = "on"; h.mark_size = 1; h.mark_foreground = 5; // affichage des aretes for i = 1:dim for j = 1:dim if K3(i,j) == -1 then // tracer l'arete i j // x1 = [ Xx(i); Xx(j) ]; // y1 = [ Yy(i); Yy(j) ]; //z1 = [ Zz(i); Zz(j) ]; printf('\n{ { %ff, %ff, %ff } , { 0.0f, 0.0f, 1.0f } },', Xx(i), Yy(i), Zz(i)); printf('\n{ { %ff, %ff, %ff } , { 0.0f, 0.0f, 1.0f } },', Xx(j), Yy(j), Zz(j)); // xarrows(x1, y1, z1, 0, 2); end end end
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//CAPTION: Linear_Magnetron //chapter_no.-10, page_no.-459 //Example_no.10-1-2a clc; //(a) Calculate_the_electron_velocity_at_the_hub_surface em=1.759*(10^11);//em=e/m Bo=.015;//Magnetic_flux_density d=5*(10^-2);//Distance_between_cathode_and_anode h=2.77*(10^-2);//hub_thickness V=em*Bo*h; disp(V,'the_electron_velocity_at_the_hub_surface(in m/s)is ='); //(b) Calculate_the_phase_velocity_for_synchronism disp(V,'the_phase_velocity_for_synchronism is Vph=w/B ='); //(c) Calculate_the_Hartree_anode_voltage wB=V;//wB=w/B Voh=((V*Bo*d))-((1/2)*(1/em)*(V^2)); Voh=Voh/1000;//in KV disp(Voh,'the_Hartree_anode_voltage (in KV) is =');
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//23.3 p=30//in cm f=10//in cm x=(1/f)-(1/p) q=1/x M=-(q/p) disp("part a") disp(q,"The position of final image in cm=") disp(M,"The magnification=") p=5//in cm f=10//in cm x=(1/f)-(1/p) q=1/x M=-(q/p) disp("part b") disp(q,"The position of final image in cm=") disp(M,"The magnification=")
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clc clear //Input data n=1.66*10^-4;//The viscosity of the gas in dynes/cm^2 C=4.5*10^4;//The R.M.S velocity of the molecules in cm/s d=1.25*10^-3;//The density of the gas in g/cc N=6.023*10^23;//The Avogadro number V=22400;//The volume of a gas at N.T.P in cc pi=3.142;//The mathematical constant of pi //Calculations L=(3*n)/(d*C);//The mean free path of the molecules of the gas in cm F=(C/L);//The frequency collision in per sec n=N/V;//Number of molecules per cc D=1/((1.414*pi*n*L)^(1/2));//Molecular diameter of the gas molecules in cm //Output printf('(1)The mean free path of the molecules of the gas is %3.0g cm \n (2)The frequency of collision is N = %3.0g /sec \n (3)Molecular diameter of the gas molecules is d = %3.0g cm ',L,F,D)
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//Euler's Method clc; clear; close(); format('v',8); funcprot(0); deff('[g]=f(x,y)','g= -y^2/(1+x)'); y = 1; x = 0; h = 0.05; while x<0.2 y = y - 0.05*y^2/(1+x); x = x + h; disp(y,x,'Value of y at x :'); end disp(y,'The calculated value of y(0.2):'); x = 0.2; act = 1/(1+log(1+x)); disp(act,'The exact value is of y(0.2): '); err = act - y; disp(err,'The error is :');
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//Exa 7.11 clc; clear; close; //Given data : format('v',7); l=600;//in meter VA=440;//in volt VB=400;//in volt R=0.01;//in ohm/100m RAC=(R/100)*300;//in ohm RCD=(R/100)*300;//in ohm RDE=(R/100)*100;//in ohm REF=(R/100)*200;//in ohm RFB=(R/100)*300;//in ohm //VA-VB=VAC+VCD+VDE+VEF+VFB;//in volt IA=(VA-VB+42.5)/(0.12);//in Ampere IAC=IA;ICD=IA-100;IDE=IA-300;IFE=IA-550;IFB=IA-850;//in Ampere disp(IAC,"Current fed at A, IA(in A):"); disp(-IFB,"Current fed at B, IB(in A):");
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clc // Given that lambda = 6.6e-7 // wavelength of light in meter L = 1.32e-5 // coherence length in meter // Sample Problem 1 on page no. 1.40 printf("\n # PROBLEM 1 # \n") printf("\n Standard formulae used \n delta_L = c * delta_t \n") coherence_time = L / (3 * 10 ^ 8)//calculation for coherence time printf("\n Coherence time = %e sec",coherence_time)
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//Chapter 9 : Eigenvalues and Eigenvectors //Example 9.11 //Scilab 6.0.1 //Windows 10 clear; clc; A=[2 1;1 0] disp(A,'A=') eig=spec(A) disp(eig,'eigen values are') P=[1 1;-eig(1) -eig(2)] disp(P,'P=') pap=inv(P)*A*P pap(1,2)=round(pap(1,2)) pap(2,1)=round(pap(2,1)) disp(pap,'P^-1AP=') invp=(1/(2*sqrt(2)))*[eig(2) 1;-eig(1) -1] disp(invp,'P^-1')
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//Chapter-3,Example 5,Page 57 clc; close; //Part (a) t_half= 1620 //half life of radium lamda= 0.693/t_half //as radium lose one centigram mass N_0=100 // in centigram N_1=N_0-1 t_1=log10(N_0/N_1)/(lamda*log10(%e)) printf('Part (a)---total number of years required are %.2f years ',t_1) // Part (b) N_2= 1 t_2=log10(N_0/N_2)/(lamda*log10(%e)) printf('\n Part (b)---total number of years required are %.2f years ',t_2)
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clc //Initialzation of variables T1=298//K T2=273//K //Calculations factor=sqrt(T2/T1) percentage=(1-factor)*100 //Results printf('Percentage loss of speed of air molecules = %.2f',percentage)
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clc clear //input data N=3600//Running speed of blower in rpm Dt=0.2//The rotor tip diameter in m Dh=0.125//The rotor hub diameter in m P1=1.013//The atmospheric pressure in bar T1=298//The atmospheric temperature in K m=0.5//Mass flow rate of air in kg/s db=20//The turning angle of the rotor in degree b1=55//The inlet blade angle in degree R=287//The universal gas constant in J/kg.K nc=0.9//Total-to-total efficiency P=0.25//Total pressure drop across the intake in cm of water Cp=1005//The specific heat of air at constant pressure in J/kg.K r=1.4//The ratio of specific heats of air g=9.81//Acceleration due to gravity in m/s^2 ns=0.75//The stator efficiency dw=1000//Density of water in kg/m^3 //calculations d1=(P1*10^5)/(R*T1)//The density of air at inlet in kg/m^3 A=(3.141/4)*((Dt^2)-(Dh^2))//The area of flow in m^2 Ca=m/(d1*A)//The axial velocity of air in m/s U=((3.141*(Dt+Dh)*N)/(2*60))//Mean rotor blade velocity in m/s b2=b1-db//The outlet blade angle in degree Cx2=U-(Ca*tand(b2))//The whirl velocity at exit in m/s Cx1=0//The whirl velocity at entry in m/s as flow at inlet is axial dh0r=U*(Cx2-Cx1)//The actual total enthalpy rise across the rotor in J/kg dh0sr=nc*dh0r//The isentropic total enthalpy rise across the rotor in J/kg dP0r=(d1*dh0sr)*((10^-1)/(g))//The total pressure rise across the rotor in cm of water P0=dP0r-P//Stagnation pressure at the rotor exit in cm of water C2=((Ca^2)+(Cx2^2))^(1/2)//The absolute velocity at the exit in m/s dPr=dP0r-((d1*((C2^2)-(Ca^2)))/2)*((10^-1)/g)//The static pressure across the rotor in cm of water dhs=((C2^2)-(Ca^2))/2//The actual enthalpy change across the stator in J/kg dhss=ns*dhs//The theoretical enthalpy change across the stator in J/kg dPs=(d1*dhss)*((10^-1)/g)//The static pressure rise across the stator in cm of water dP0s=-((dPs/((10^-1)/g))+((d1/2)*(Ca^2-C2^2)))*(10^-1/g)//The change in total pressure across the stator in cm of water P03=P0-dP0s//Total pressure at stator inlet in cm of water dh0ss=((dw*g*(P03/100))/d1)//Theoretical total enthalpy change across the stage in J/kg ntt=dh0ss/dh0r//The overall total-to-total efiiciency DR=dPr/(dPr+dPs)//The degree of reaction for the stage //output printf('(a)Total pressure of air exit of rotor is %3.2f cm of water\n(b)The static pressure rise across the rotor is %3.2f cm of water\n(c)The static pressure rise across the stator os %3.2f cm of water\n(d)The change in total pressure across the stator is %3.2f cm of water\n(e)The overall total-to-total efficiency is %3.3f\n(f)The degree of reaction for the stage is %3.3f',P0,dPr,dPs,dP0s,ntt,DR)
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//Example 6.19 //PID compensation design for spacecraft attitude control. xdel(winsid())//close all graphics Windows clear; clc; //------------------------------------------------------------------ //System transfer function s=poly(0,'s'); G1=(0.9/s^2); G2=(2/(s+2)); G=G1*G2; Gs=syslin('c',G); // PID controller parameters Td_inv=0.1; // Td_inv=1/Td=0.1 Kd=1/Td_inv; //Kd=Td=Td_inv (derivative gain) Ti_inv=0.005; // Ti_inv=1/Ti=0.005 Ki=Ti_inv; //Ki=Ti_inv (integral gain) Kp=0.05 //Kp (Proportional gain) D=Kp*(Kd*s+1)*(Ki/s+1); //PID Compensator Dsc=syslin('c',D); Ds=syslin('c',D/Kp); //PID Compensator with Kp=1 // Compensated system with Kp=1 GDs=Gs*Ds; //PID compensated system Kp=0.05; GDsc=Gs*Dsc; //------------------------------------------------------------------ //The bode plots bode([Gs;GDs;GDsc],0.01/2/%pi,100/2/%pi,... ['G(s)';'D(s)G(s) with (Kp=1)';'D(s)G(s) with (Kp=0.05)'],"rad"); exec .\fig_settings.sci; //custom script for setting figure properties title('Compensation for PID design','fontsize',3) //Phase margin of pid compensated system with Kp=0.05; [pm wcp]=p_margin(GDsc); //------------------------------------------------------------------ //closed loop system //step response Gc=GDsc/(GDsc+1); figure; t=0:0.05:40; y=csim('step',t,Gc); plot(t,y,2) //Title, labels and grid to the figure exec .\fig_settings.sci; //custom script for setting figure properties title('Step response for PID compensation of spacecraft'... ,'fontsize',3) xlabel('Time t (sec.)','fontsize',2) ylabel('$theta$','fontsize',2) //------------------------------------------------------------------ //step disturbance response Gc=G1/((G1*G2*D)+1); Gcs=syslin('c',Gc); figure; t=0:0.5:1000; u=0.1*ones(1,length(t)); y=csim(u,t,Gcs) plot(t,y,2) //Title, labels and grid to the figure exec .\fig_settings.sci; // custom script for setting figure properties title('Step disturbance response for PID compensation... of spacecraft','fontsize',3) xlabel('Time t (sec.)','fontsize',2) ylabel('$theta$','fontsize',2) //------------------------------------------------------------------
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//EXAMPLE 8.1 //MAXIMA SCILAB TOOLBOX REQUIRED FOR THIS EXAMPLE //Digital filter structure clear; clc; syms W1 W2 W3 X Y a d B y E z; //Equations obtained are as follows: W1 = X - a*W3/z; W2 = W1 - d*W2/z; W3 = W2/z + E*W2; Y = B*W1 +y*W3/z; //Solving the above equations: Hz=(B + (B*d+y*E)/z + y/(z^2))/(1 + (d+a*E)/z + a/(z^2)) disp(Hz,'Hz = ');
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errcatch(-1,"stop");mode(2);// Example 5.16: Io , bta=100; VBE=0.7; // in volts // From Fig. 5.30 // Writing KVL for the indicated loop I_ref=(10-VBE)/10; // in mili-amperes Io=bta*I_ref/(2*(1+bta)); // in mili-amperes disp(Io,"Io (mA) ="); exit();
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clc disp("the soln of eg 10.1-->2-D steady heat conduction-Gauss Seidel method "); for i=1:9,tnew(i)=101,e(i)=1 //assumed values end t=1e-6 //since all the nodes are interior nodes so discretized eqn used is eqn 10.10 while e(1)>t&e(2)>t&e(3)>t&e(4)>t&e(5)>t &e(6)>t& e(7)>t& e(8)>t & e(9)>t do for i=1:9, told(i)=tnew(i),end tnew(1)=(told(2)+40+told(4))/4 //on solving eqns for various nodes we get, tnew(2)=(tnew(1)+told(3)+told(5)+20)/4 tnew(3)=(tnew(2)+told(6)+420)/4 tnew(4)=(told(5)+tnew(1)+told(7)+20)/4 tnew(5)=(tnew(2)+told(8)+told(6)+tnew(4))/4 tnew(6)=(tnew(3)+tnew(5)+told(9)+400)/4 tnew(7)=(tnew(4)+told(8)+40)/4 tnew(8)=(tnew(5)+tnew(7)+told(9)+20)/4 tnew(9)=(tnew(6)+420+tnew(8))/4 for i=1:9,e(i)=abs(tnew(i)-told(i)) end end disp("the values of T from 1st element to last is"); for i=1:9,disp(tnew(i)); end
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clc; v=230; // rated voltage of dc shunt motor n=1000; // rated speed of motor rf=115; // field resistance ra=0.5; // armature resistance ia=4; // no load armature current k=(v-ia*ra)/(2*%pi*n/60); // constant term in formula of back EMF disp('case a'); t=80; // load torque ia2=t/k; // armature load current Ea2=v-ia2*ra; // counter EMF corresponding to load armature current printf('Armature current for given load is %f A\n',ia2); n2=(Ea2*60)/(k*2*%pi); printf('Speed of motor at given load is %f rpm\n',n2); disp('case b'); pd=8000; // power developed by motor n3=1250; // speed at power is developed // determining value of armature current corresponding to power by solving quadratic equation whose terms are t1=ra; t2=-v; t3=pd; p=[ t1 t2 t3]; ia3=roots(p); Ea3=v-ia3(2)*ra; // counter EMF for load armature current k1=k/(v/rf); // constant term in formula of back EMF for field current = 1 A ifn=(Ea3*60)/(2*%pi*n3*k1); rfn=v/ifn; printf('External resistance that must be inserted in series with field winding is %f ohms',rfn-rf);
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Example_6_21_3.sce
// Example 6.21.3 page 6.60 clc; clear; tr=50; //radiative recombination lifetime tnr=110; //non-radiative recombination lifetime h=6.624d-34; //plank's constant c=3d8; //speed of light q=1.6d-19; //charge of electron i=40d-3; //current lamda=0.87d-6; //wavelength t=tr*tnr/(tr+tnr); //computing total recombination time eta=t/tr; //computing internal quantum efficiency Pint=eta*h*c*i/(q*lamda); //computing internally generated power Pint=Pint*10^3 printf("\nTotal recombinaiton time is %.2f ns.\nInternal quantum efficiency is %.4f.\nInternally generated power is %.2f mW.",t,eta,Pint); //answers in the book with slight deviaitons //Total recombinaiton time is 34.37 ns, deviation of 0.01ns. //Internal quantum efficiency is 0.6874, deviaiton of 0.0001. //Internally generated power is 39.24 mW, deviation of 0.02mW.
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clc; //page 185 //problem 3.7 //Given input inmedance of matching networkis R1 = 10 ohm & output impedance of matching networ is R2 = 50 ohm & carrier frequency is fc = 500 KHz R1 = 10 R2 = 50 fc = 500000 //Wc = 2*pi*fc Wc = 2*%pi*fc //AS R1 = R2*(X2^2)/[(R2^2)+(X2^2)], X2 = 25ohm X2 = 25 //AS X1 = (R2^2)*X2/[(R2^2)+(X2^2)] & R1>R2, X1 = -20ohm X1 = -20 //|X1| = |jwL| = wL = 20 & |X2| = |1/jwC| = 1/wC = 25, so |X1*X2| = L/C = 500 denotes as LC_div LC_div = 500 //Wc^2 = 1/(L*C). LC is denoted as LC_prod LC_prod = 1/(Wc^2) //In the textbook the calculated LC = 10^-3, in reality the value of LC = 1.013D-13 L = sqrt(LC_div*LC_prod) //In the textbook the calculated L^2 = 50*10^-14, in reality the value of L^2 = 5.066D-11 C = L/500 //In the textbook the calculated C = 1.4*10^-9, in reality the value of C = 1.424D-08 disp('Inductance '+string(L)+' H') disp('Capacitance '+string(C)+' F')
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// (Distortion in CT system) // Exercise 5 clear; clf; dt = 1/10000; t = -0.01:dt:0.01; x1 = sin(2*%pi*100*t) subplot(231) plot(t,x1,'y'); title("x1 vs time","fontsize",3) x2 = sin(2*%pi*200*t) subplot(232) plot(t,x2,'r'); title("x2 vs time","fontsize",3) x = x1 + x2; // input signal subplot(233) plot(t,x,'m') title("x vs time","fontsize",3) // Same Amplitude & Same time diff. results into no distortion A1 = 2; A2 = 2; t1 = 0.004; t2 = 0.004; c = A1*sin(2*%pi*100*(t-t1)) + A2*sin(2*%pi*200*(t-t2)); subplot(234) plot(t,c,'g') title("y vs time (No distortion)","fontsize",3) // Same Amplitude & Different time diff. results into Time distortion t1 = 0.002; t2 = 0.004; A1 = 2; A2 = 2; d = A1*sin(2*%pi*100*(t-t1)) + A2*sin(2*%pi*200*(t-t2)); subplot(235) plot(t,d,'b') title("y vs time (Time distortion)","fontsize",3) // Different Amplitude & same time diff. results into Amplitude distortion A1 = 2; A2 = 4; t1 = 0.004; t2 = 0.004; e = A1*sin(2*%pi*100*(t-t1)) + A2*sin(2*%pi*200*(t-t2)); subplot(236) plot(t,e,'r') title("y vs time (Amplitude distortion)","fontsize",3)
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Example12_2.sce
//Example 12.2 //Program to determine the required electrical and optical SNR clear; clc ; close ; //Given data BER=10^(-9); //BIT ERROR RATE //Optical SNR SNR_op=(erfinv(1-2*BER))*2*sqrt(2); //erfc(x)=1-erf(x) //Electrical SNR SNR_el=((erfinv(1-2*BER))*2*sqrt(2))^2; //erfc(x)=1-erf(x) //Displaying the Results in Command Window printf("\n\n\t Optical SNR is %1.0f or %0.1f dB.",SNR_op,10*log10(SNR_op)); printf("\n\n\t Electrical SNR is %1.0f or %0.1f dB.",SNR_el,10*log10(SNR_el));
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clc clear //At 7 bar pressure P1=7; //in bar P2=1; //in bar n=1.1; //Now according to law of expansion P(V)^1.1= Constant Vg1=0.273; //in m^3/kg V1=Vg1; V2=((P1/P2)^(1/n))*V1; W=((P1*100*V1)-(P2*100*V2))/(n-1); printf('Work Done: %3.1f kJ/kg',W); printf('\n'); Hg=2763.5; //in kJ/kg H1=Hg; Vg=1.694; //At 1 bar, Vg=1.694 and as V2<Vg steam is wet x=V2/Vg; Hf=417.5; //in kJ/kg Hfg=2258; //in kJ/kg H2=Hf+(x*Hfg); U2=H2-(P2*100*V2); U1=H1-(P1*100*V1); U=U2-U1; printf('Change in Internal Energy: %3.2f kJ/kg',U); printf('\n'); Q=U+W; printf('Heat transferred during the process: %3.2f kJ/kg',Q); printf('\n');
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// Y.V.C.Rao ,1997.Chemical Engineering Thermodynamics.Universities Press,Hyderabad,India. //Chapter-4,Example 14,Page 113 //Title:Final state and mass of steam that entered the tank //================================================================================================================ clear clc //INPUT V=3;//volume of tank in m^3 T0=100;//initial temperature of steam in degree celsius T=300;//temperature of superheated steam in the pipeline in degree celsius P=3;//pressure of superheated steam in the pipeline in MPa R=8.314;//universal gas constant in J/molK //CALCULATION Ps=101.33;//pressure of saturated steam in kPa from steam tables corresponding to T0 vg=1.673;//specific volume of saturated vapour in m^3/kg obtained from steam tables corresponding to T0 hg=2676.0;//specific enthalpy of saturated vapour in kJ/kg obtained from steam tables corresponding to T0 h=2995.1;//specific enthalpy of superheated steam in kJ/kg obtained from superheated steam tables corresponding to T and P u0=((hg*10^3)-(Ps*10^3*vg))*10^-3;//calculation of initial internal energy of steam in kJ/mol using the first law of thermodynamics for the adiabatic charging of a tank m0=V/vg;//calculation of mass of steam initially in the tank in kg //The first law of thermodynamics for the adiabatic charging of a tank is given by: //mfuf-m0u0=(mf-m0)h. This equation is to be solved to determine mf Tf=418;// assuming final temperature of superheated steam in degree celsius //For superheated steam at P and Tf vf=0.102329;//specific volume of superheated steam in m^3/kg uf=2965.78;//internal energy of the superheated steam in kJ/kg mf_guess=V/vf;//taking a guess value for the mass of steam inside the tank at the end of the charging operation,in kg function[fn]=solver_func(ui) //Function defined for solving the system to determine the internal energy of steam inside the tank at the end of the charging operation in kJ/kg using Eq.(4.44, where Q=0 as the process is adiabatic) fn=(mf_guess*ui)-(m0*u0)-((mf_guess-m0)*h); endfunction [uf_solved]=fsolve(mf_guess,solver_func,1e-6)//using inbuilt function fsolve for solving the system of equations mf=mf_guess//mass of the steam inside the tank at the end of the charging operation, in kg mass=mf-m0;//calculation of mass of steam that entered the tank in kg //OUTPUT mprintf("\n The final state of steam(superheated),Pressure=%d MPa\n",P); mprintf("\n The final state of steam(superheated),Temperature=%d degree celsius\n",Tf); mprintf("\n The mass of steam that entered the tank=%0.3f kg\n",mass); //===============================================END OF PROGRAM===================================================
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## Test of tag deletion by regexp set echo read <snarl.svn tag /INITIAL_IMPORT/ delete write -
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clc; m = input('enter row'); n = input('enter col'); a = zeros(m,n); b = zeros(m,n); c = zeros(m,n); disp('enter elements'); for i = 1:m for j = 1:n a(i,j) = input(''); end end disp('enter elements'); for i = 1:m for j = 1:n b(i,j) = input(''); end end for i = 1:n for j = 1:m c(i,j) = a(i,j)+b(i,j); end end disp(a); disp(b); disp(c);
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// To determine the short circuit capacity of each station clear clc; X=1200*100/800;// percent reactance of other generating station Xc=.5*1200/(11*11); Sc=1200*100/86.59;// short circuit MVA of the bus Xf=119.84;// equivalent fault impedence between F and neutral bus MVA=1200*100/Xf; mprintf("short circuit capacity of each station=%.0f MVA\n",MVA);
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clear clc //to find kinetic energy // GIVEN:: //distance travelled by neutron d = 6.2//in meters //time for neutron travel t = 160//in micrometers //mass of neutron m = 1.67e-27//in kg // SOLUTION: //speed of neutron v = d/(t*10^-6)//in m/s //applying formula for kinetic energy //kinetic energy of neutron K = (1/2)*m*v^2//in J K1 = K*(6.242e18)//in eV K = nearfloat("succ",1.26e-18) K1 = nearfloat("succ",7.9) printf ("\n\n Speed of neutron v = \n\n %.2e m/s",v); printf ("\n\n Kinetic energy of neutron in J K = \n\n %.2e J",K); printf ("\n\n Kinetic energy of neutron in eV K = \n\n %.1f eV",K1);
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// Scilab code Exa 4.5.5 : Checking whether the reaction is spontaneous or exoergic : page no. 185 (2011) // Cf-252 > Zr-98 +Ce-145 + 9*n-1 is the given reaction M_Cf = 252.081621; // Atomic mass of Cf, amu M_Zr = 97.912735; // Atomic mass of Zr, amu M_Ce = 144.917230; // Atomic mass of Ce, amu M_n = 3.0160294; // Atomic mass of neutron, amu r_sum = M_Cf+M_Zr; // Sum of reactant, amu p_sum = M_Ce+M_n; // Sum of product, amu // Declare the function which check the Q-value function Q = check_Qvalue(r_sum,p_sum) if r_sum >= p_sum then Q = 1; else Q = 0; end endfunction // Reaction if (check_Qvalue(r_sum,p_sum) == 1) then printf("\n Reaction : \n\n\t Cf(256) ----> Zr(98)+Ce(145)+9*n(1)") printf("\n\n\t\tThis reaction is spontaneous") elseif (check_Qvalue(r_sum,p_sum) == 0) then printf("\n Reaction : \n\n\t Cf(256) ----> Zr(98)+Ce(145)+9*n(1)") printf("\n\n\t\tThis reaction is not spontaneous") end // Reaction : // Cf(256) ----> Zr(98)+Ce(145)+9*n(1) // This reaction is spontaneous
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// Exa 5.22 format('v',6) clc; clear; close; // Given data V_T = 1;// in V k = 160*10^-6;// in A/V^2 I_DQ = 160*10^-6;// in A V_GS = V_T + sqrt(I_DQ/k);// in V V_DD = 5;// in V V_DSQ = 3;// in V R_D = (V_DD - V_DSQ)/(I_DQ);// in ohm R_D = R_D * 10^-3;// in k ohm disp(R_D,"The value of R_D in k ohm is");
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l=30*10^(-3); r=200; v=10; f=1000; disp("Part a"); x_l=2*%pi*f*l; z=sqrt(r^2+x_l^2); disp("the impedance (in Ω) of the circuit is"); disp(z); disp("Part b"); i=v/z; disp("the current (in A) in the circuit is"); disp(i); disp("Part c"); deg=atan(x_l/r)*180/%pi; disp("the phase angle (in deg) between applied voltage and current is"); disp(deg);
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// Exa 9.31 clc; clear; close; // Given data V_DD = 5;// in V V_T= 1;// in V k= 1;// in mA/V^2 R1 = 1;// in M ohm R2 = 1;// in M ohm R_S= 2;// in k ohm R_D= 2;// in k ohm I1 = V_DD/(R1+R2);// in A disp(I1,"The value of I1 in µA is : ") V_A = (R2/(R2+R1))*V_DD;// in V disp(V_A,"The value of V_A and V_G in volts is : ") I_D= poly(0,'I_D'); V_C= I_D*R_S;// in V V_GS= V_A-V_C;// in V I_D= I_D-k*(V_GS-V_T)^2; I_D= roots(I_D);// in mA I_D= I_D(2);// in mA disp(I_D,"The value of I_D in mA is : ") V_B= V_DD-I_D*R_D;// in V V_C= I_D*R_S;// in V V_DS= V_B-V_C;// in V disp(V_B,"The value of V_B in volts is : ") disp(V_C,"The value of V_C in volts is : ") disp(V_DS,"The value of V_DS in volts is : ") // Note: In the book, the calculated values are wrong, this is why the answer in the book is wrong.
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clear // //Given //Variable declaration sigma1=100 //Major principal stress in N/sq.mm sigma2=-40 //Minor principal stress in N/sq.mm theta=90-60 //Angle of inclination in degrees //Calculation sigman=((sigma1+sigma2)/2)+(((sigma1-sigma2)/2)*cos((%pi/180)*(2*theta))) sigmat=((sigma1-sigma2)/2*(sin((%pi/180)*(2*theta)))) sigmaR=(sqrt(sigman**2+sigmat**2)) sigmat_max=int((sigma1-sigma2)/2) phi=int((180/%pi)*(atan(sigmat/sigman))) //Result printf("\n Resultant stress in magnitude = %0.3f N/mm^2",sigmaR) printf("\n Direction of resultant stress = %0.3f degrees",phi) printf("\n Maximum shear stress = %0.3f N/mm^2",sigmat_max)
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Ex12_4.sce
// Example 12_4 clc;funcprot(0); // Given data X_O_2=0.2095;// The mole fraction for oxygen p_m=0.1013;// MN/m^2 d=100;// m M_O_2=32.00;// The molecular mass of oxygen M_He=4.003;// The molecular mass of helium R=8.3143;// kJ/(kgmole.K) // Calculation // (a) p_O_2=X_O_2*p_m;// MN/m^2 p_m=1.08;// MN/m^2 X_O_2=p_O_2/p_m;// The mole fraction for oxygen Shi_O_2=X_O_2;// The volume fraction for oxygen pi_O_2=X_O_2;// The pressure fraction for oxygen X_He=1-X_O_2;// The mole fraction for helium Shi_He=X_He;// The volume fraction for oxygen M_m=(X_O_2*M_O_2)+(X_He*M_He);// kg/kgmole w_O_2=X_O_2*(M_O_2/M_m);// The mass fraction for oxygen w_He=1-w_O_2;// The mass fraction for helium printf("\n(a)The mole and volume fraction of oxygen,X_O2=Shi_O2=pi_O2=%0.4f \n The helium mole and volume fractions,X_He=Shi_He=%0.3f \n The mixture equivalent molecular mass,M_m=%1.2f kg/kgmole",X_O_2,X_He,M_m); // (b) R_m=R/M_m;// kJ/(kg.K) c_vO_2=0.657;// kJ/(kg.K) c_vHe=3.123;// kJ/(kg.K) c_pO_2=0.917;// kJ/(kg.K) c_pHe=5.200;// kJ/(kg.K) c_vm=(w_O_2*c_vO_2)+(w_He*c_vHe);// kJ/(kg.K) c_pm=(w_O_2*c_pO_2)+(w_He*c_pHe);// kJ/(kg.K) k_m=c_pm/c_vm;// The specific heat ratio of the mixture printf("\n(b)The mixture equivalent gas constant,R_m=%1.2f kJ/(kg.K) \n The mixture specific heats,c_vm=%1.2f kJ/(kg.K) & c_pm=%1.2f kJ/(kg.K) \n The specific heat ratio of the mixture,k_m=%1.2f",R_m,c_vm,c_pm,k_m);
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//Example 7.2: Diffusion potential clc; clear; close; format('v',6) //given data : Na=5*10^23;// in m^-3 Nd=5*10^21;// in m^-3 T=300;// in K e=1.6*10^-19;// in J k=1.38*10^-23;// in JK^-1 V=(k*T)/e; ni=2.2*10^12;// in m^-3 Vd=V*log((Na*Nd)/ni^2); disp(Vd,"Diffusion potential,Vd(V) = ")
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// Calculate width of Gating pulse // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 8-3 in page 377 clear; clc; close; // Given Data Il=4*10^-3; // Latching current of SCR in A V=100; // DC voltage of the circuit in V L=0.1; // Inductance of the circuit in H // Calculations t=(L/V)*Il; printf("Required width of the gating pulse is %0.2e s",t); // Results // Required width of the gating pulse is 4 mu-s
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Tint 0 0 0 0 TintAlphaChange 100 1 Linear Wait 1 TintAlphaChange 0 1 Linear Wait 1 Loop
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// Example 9.4.2 page 9.12 clc; clear; output=3; //laser output sensitivity=-54; //APD sensitivity coupling_loss=17.5; L=6; //length in km sl=1.1; //loss correspond to one splice in dB n=3; //number of splices fl=5; //fiber loss in dB/km connector_loss=0.8; allowed_loss=output-sensitivity; splices_loss=n*sl; fiber_loss=L*fl; margin=allowed_loss-(splices_loss+fiber_loss+coupling_loss+connector_loss); printf("\nFinal margin is %.1f dB.",margin);
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Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00 Iteration = 0 Energy = 0.000E+00
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clc //initialisation of variables d= 10 //in h= 3.5 //in g= 32.2 //ft/sec^2 //CALCULATIONS A= (%pi/4)*(d^2/144) V= sqrt(2*g*(h/12)) vm= (2/3)*V Q= vm*A*60 //RESULTS printf (' Quantity flowing per minute = %.1f ft^3 ',Q)
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[]
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FOSSEE/Scilab-TBC-Uploads
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//pathname=get_absolute_file_path('12.03.sce') //filename=pathname+filesep()+'12.03-data.sci' //exec(filename) //Diameter of the bore(in m): d=0.3 //Length of the stroke(in m): L=0.6 //Occerance od cut-off: r1=0.4 //Pressure at which steam enters(in bar): p1=7.5 //Pressure at exhaust(in bar): p3=0.1 //Rpm of the engine: n=180 //Diagram factor: d1=0.6 //Expansion ratio: r=1/r1 //Hypothetical mean effective pressure(in bar): mep=p1/r*(1+log(r))-p3 //Actual mean effective pressure(in bar): mepa=mep*d1 //Indicated power(in kW): IP=mepa*L*%pi*d^2*2*n*10^2/(4*60) printf("\n RESULT \n") printf("\nIndicated power = %f kW",IP)
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ex_32_5.sce
//find clc //solution //given BP=5000//W N=1200//rpm n=N/2 pm=0.35//N/mm^2 effm=0.8 //let D bebore dia IP=BP/effm//W //IP=pm*l*A*n/60 //A=%pi*D^2/4,l=1.5D //IP=4.12*10^-3 *D^3 D=(IP*1000/4.12)^(1/3)//mm printf("dia of bore dis,%f mm\n",D) l=1.5*D L=1.15*l ft=42 printf("stroke length is,%f mm\n",L) p=9*pm C=0.1 th=D*sqrt(C*p/ft) printf("thickness of head is,%f mm\n",th) Fc=(%pi/4)*D^2*p//N//force on cylinder...eq1 //let ns be nu,mbr of studs ns=6//...assume ///let dc be core dia ft1=65//N/mm^2 //d be nominal dia //Fs=ns*(%pi/4)*dc^2*ft1=216*d^2....eq2...//dc=0.84*d //using eq1 and eq2 //we get //d=sqrt(Fc/216) printf("nominal dia is ,%f mm\n",sqrt(Fc/216)) printf("nominal dia is,say 14 mm\n") d=14//mm
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Example9_39.sce
//Example 9.39 clc disp("From equation(3) we get") qe=(4.095/(4095*2))*10^3 format(4) disp(qe,"Q_E(in mV) = 4.095 / (4096-1)*2 =")
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clc; clear; m=68.1;//kg v=40;//m/s t=10;//s g=9.8;//m/s^2 function y=f(c) y=g*m*(1-exp(-c*t/m))/c - v; endfunction x1=12; x2=16; xt=14.7802;//true value e=input("enter the tolerable true percent error=") xr=x1-(f(x1)*(x2-x1))/(f(x2)-f(x1)); etemp=abs(xr-xt)/xt*100;//error while etemp>e if f(x1)*f(xr)>0 then x1=xr; xr=x1-(f(x1)*(x2-x1))/(f(x2)-f(x1)); etemp=abs(xr-xt)/xt*100; end if f(x1)*f(xr)<0 then x2=xr; xr=x1-(f(x1)*(x2-x1))/(f(x2)-f(x1)); etemp=abs(xr-xt)/xt*100; end if f(x1)*f(xr)==0 then break; end end disp(xr,"The result is=")
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err_bv.tst
; checks bit vector sorts (set-logic QF_BV) (declare-fun x () (_ BitVec 4)) (declare-fun y () (_ BitVec 1)) (declare-fun z () (_ BitVec 4)) (declare-fun k () (_ BitVec 0)) (declare-fun k () (_ BitVecx 0)) (declare-fun k () (_ BitVec -1)) (declare-fun k () (_ BitVec)) (declare-fun k () (_ BitVec 1 2)) (assert (= x #b010 )) (assert (= z #xab )) (assert (= z y ))
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clc // C_aH_bO_cN_dS_e a=60/12; b=20; c=5/16; d=10/14; e=5/32; // C_5 H_20 O_0.3125 N_0.7143 S_0.1562 + x O2 + x*(79/21)N2 → p CO2 + q H2O + r SO2 + s N2 p=5; q=20/2; r=0.1562; x=(2*p+q+2*r-0.3125)/2; s=(0.7143+2*x*79/21)/2; air=(9.92*32+x*79/21*28)/100; disp("Stoichiometric air required =") disp(air) disp("kg/kg of fuel")
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Exercise_18.sce
clc; clear; //clears the console and all previously stored variables function V0 = BS_EuCall_FFT (S0, r, sigma, T, K, R, N, M) //defining initial parameters delta=M/N; m=1:N; kappa_1=0; //f_tilde_0 for European Call for K=e^kappa function y = f_tilde(z) y = 1/ (z*(z-1)); //since kappa=0 endfunction //Characteristic function for the BS model function x = chi(u) x=exp(%i*u*(log(S0)+r*T)-(%i*u+u^2)*sigma^2/2*T); endfunction //defining the g function function y = g(u) y=f_tilde(R+%i*u) * chi(u-%i*R); endfunction //computing x_n vector for n=1,...,N for n=m x_n(n)=g((n-1/2)*delta)*delta*exp(-%i*(n-1)*delta*kappa_1) kappa_m(n)=kappa_1+(n-1)*2*%pi/M end //applying Fast Fourier Transform to compute x_hat_m from x_n for m=1,...,N x_hat_all=fft(x_n) //defining function for computation of option Values for different kappas (4.16) function y = V0_k(x) y = exp(-r*T+(1-R).*kappa_m)/%pi.*real(x.*exp(-%i/2*delta.*kappa_m)) endfunction //initializing matrix with dimension of Nx2, to store all results //computed for option value and strike V0_km=zeros(N,2) //Storing option price values for a range of strike prices (kappas) V0_km(:,2)=V0_k(x_hat_all) //Storing strike prices V0_km(:,1)=exp(kappa_m) //matrix transpose for later use in the interpln function (needed in this form) V0_km=V0_km' //linear interpolation of the results, compute option prices for needed strike prices V0=interpln(V0_km, K) endfunction S0=100; r=0.05; sigma=0.2; T=1; K=80:130; R=1.1; N=2^11; M=50; V0 = BS_EuCall_FFT (S0, r, sigma, T, K, R, N, M) disp("V0 = " + string(V0) + " K = " + string(K))
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Ex8_9.sce
//Ex8_9 clc Ai = -60 Ri = 2.0*10^3 RL = 15*10^3 disp("Ai = "+string(Ai))//current gain disp("Ri = "+string(Ri)+"ohm")//input resistance disp("RL = "+string(RL)+"ohm")//load resistance Av = Ai*RL/Ri disp("Av = Ai*RL/Ri = "+string(Av))//voltage gain //note : in textbook, // author notify LOAD RESISTANCE as 'Rc' in question BUT 'RL' in solution. // I have work with "load resistance notified as RL".
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function [a,b]=foo(x,y) u=x+y // u is a local variable v=x*y // v is a local variable a=u+c // c is an external variable b=u*exp(v) // exp is an external functions endfunction L=macrovar(foo) // L=list(in,out,nolocal,called,local)
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Baptiste Distance FS Dodge.sce
Name=Baptiste Distance FS Dodge PlayerCharacters=Quaker BotCharacters=Quaker Bot Hard.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Quaker AddedBots=Quaker Bot Hard.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=2 BotTeams=1 MapName=Dodgingg.map MapScale=5.3 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=3.5 ScorePerKill=100.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Reflex, Quake WeaponHeroTag=LG, Lightning Gun DifficultyTag=3 AuthorsTag=Aestheticgoose BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Dodge Training against hard to hit bots from a midrange distance. GameVersion=2.0.0.2 ScorePerDistance=0.025 MBSEnable=true MBSTime1=0.1 MBSTime2=0.08 MBSTime3=1.0 MBSTime1Mult=0.1 MBSTime2Mult=20.0 MBSTime3Mult=45.0 MBSFBInstead=false MBSRequireEnemyAlive=false [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=Quaker Bot Hard DodgeProfileNames=ADAD;Short Strafes DodgeProfileWeights=1.0;1.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;0.25;2.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Quaker Bot SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=Quaker MaxHealth=300.0 WeaponProfileNames=Triple Tap Rifle;;;;;;; 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=1300.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=false CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=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 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=Quaker Bot MaxHealth=200.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=3200.0 MaxCrouchSpeed=500.0 Acceleration=18000.0 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=488.0 MainBBRadius=88.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=50.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 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 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=ADAD MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.16 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.1 MaxCrouchTime=0.1 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 [Dodge Profile] Name=Short Strafes MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.0 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=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 [Weapon Profile] Name=Triple Tap Rifle Type=Hitscan ShotsPerClick=1 DamagePerShot=25.0 KnockbackFactor=0.1 TimeBetweenShots=0.65 Pierces=false Category=FullyAuto BurstShotCount=3 TimeBetweenBursts=0.1166 ChargeStartDamage=0.0 ChargeStartVelocity=X=0.100 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=0.1 ChargeTimeToCap=0.1 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=0.100 Y=0.000 Z=0.000 MuzzleVelocityMax=X=0.100 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=10.0 MaxHitscanRange=999999.0 GravityScale=0.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=44 AmmoPerShot=1 ReloadTimeFromEmpty=1.968635 ReloadTimeFromPartial=1.968635 DamageFalloffStartDistance=2333.333252 DamageFalloffStopDistance=4666.666504 DamageAtMaxRange=12.5 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.379403 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=true 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ForceFirstPersonInADS=true ZoomBlockedInAir=true ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=None ParticleHitscanTrace=None ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=0.1 DamageAtCenter=0.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.0 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.116853,0.878543,0.016692,0.600939 SpreadSCA=0.116853,0.878543,0.016692,0.600939 SpreadMSA=0.116853,0.878543,0.016692,0.600939 SpreadMCA=0.116853,0.878543,0.016692,0.600939 SpreadSSH=0.116853,0.878543,0.016692,0.600939 SpreadSCH=0.116853,0.878543,0.016692,0.600939 SpreadMSH=0.116853,0.878543,0.016692,0.600939 SpreadMCH=0.116853,0.878543,0.016692,0.600939 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.066733 TimeToRecoilReset=0.2002 AAMode=2 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=1.5 AADeadZone=0.0 AAFOV=75.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=true AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.01 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=true PSRLoopStartIndex=0 PSRViewRecoilTracking=1.0 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 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//CHAPTER 2- STEADY-STATE ANALYSIS OF SINGLE-PHASE A.C. CIRCUIT //Example 20 // read it as example 19 in the book on page 2.72 disp("CHAPTER 2"); disp("EXAMPLE 20"); //VARIABLE INITIALIZATION L=0.5 //in Henry C=5 //in mf, multiply by 10^-6 to convert to f R=25 //in ohms //SOLUTION //solution (i) //Resonance frequency f = (1/2π)sqrt((1/LC)-R^2/L^2) fr=(1/(2*%pi))*sqrt((1/(L*C*10^-6))-(R^2)/(L^2)); disp("SOLUTION (i)"); disp(sprintf("For parallel circuit,Resonant frquency is %3f Hz", fr)); disp(" "); //solution (ii) //Total circuit impedance at resonance is Z=L/RC z=L/(R*C*10^-6); disp("SOLUTION (ii)"); disp(sprintf("Total impedence at resonance is %3f kΩ", z/1000)); // //solution (iii) //Bandwidth (f2-f1)=R/(2.π.L) bw=R/(2*%pi*L); disp("SOLUTION (iii)"); disp(sprintf("Bandwidth is %3f Hz", bw)); // //solution (iv) //Quality factor Q=1/R.sqrt(L/C) Q=(1/R)*sqrt(L/(C*10^-6)); disp("SOLUTION (iv)"); disp(sprintf("Quality Factor is %3f", Q)); //solution in the book is wrong as there is a total mistake in imaginery part 7.2+0.798=11.598 // //END
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// Exa 2.15 clc; clear; close; // Given data miu_n= 1300;// in cm^2/Vs q=1.6*10^-19;// in C ni= 4.3*10^-6;// in /cm^3 V= 1;// in volt L=8;// in cm A=0.8*0.8;// in cm^2 I=4*10^-3;// in A // R= rho*L/A = V/I R= V/I;// in Ω sigma= L/(R*A);// in (Ωcm)^-1 // sigma= q*n*miu_n n= sigma/(q*miu_n); N_D= n; disp(N_D,"The value of N_D is :") // Part (b) d=L; E= V/d; vd=miu_n*E;// in cm/s disp(vd,"Drift velocity in cm/s is : ")
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load AND1250918.hdl; output-file AND1250918.out; output-list a b out; set a %B1011001011101001 , set b %B1011111010110010, eval , output; set a %B1101001101100101 , set b %B1011011001011010, eval , output; set a %B1011001101011010 , set b %B1011011010100010, eval , output; set a %B0101101100101110 , set b %B1011011101000101, eval , output; set a %B1011110011101001 , set b %B1101010110101011, eval , output; set a %B1011001011100111 , set b %B1110101101010101, eval , output;
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ex_19_3.sce
//Example 19.3 // position of fermi level clc; clear; //given data : Eo=.3;// initial position in eV T=300;//initially temperature in kelvin T1=330;// final temperature in kelvin E=Eo*T1/T;// (formula to calculate) final position in eV disp(E,"new position of fermi level in eV")
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clear; clc; N = 2640;//rigidity modulus in tons/in^2 d = 3/8;//diameter of the rod in inches P = 1/2;//axial pull in tons del_d = 0.000078;//change in diameter in inches A = 0.25*%pi*d^2;//section area in in^2 p = P/A ;//stress tons/in^2 LS = del_d/d;//lateral strain m = p/(LS*2*N) - 1; E = 2*N*(1 + 1/m);//modulus of elasticity in ton/in^2 PR = 1/m;//poisson's ratio printf('Poisson ratio 1/m = %.3f',PR); printf('\n E = %d ton/in^2',E); //there is an error in the answer given in textbook.
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// Chapter 5 additional Example 12 //============================================================================== clc; clear; //input data h = 1; // miller indice k = 1; // miller indice l = 0; // miller indice d = 2.86*10^-10 // interplanar distance in m // Calculations a = d*sqrt((h^2)+(k^2)+(l^2)); // interplanar distance // Output mprintf('Lattice constant a = %3.3e m',a); //==============================================================================
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I=../images/tilesets/tileset.png; 0,0,0,1,0,1,2,1; 0,0,3,0,0,0,2,2; 3,1,1,1,2,0,0,4; 1,3,1,0,3,1,2,0; 1,1,1,3,2,1,1,0; 2,0,0,17,2,2,2,3; 0,0,0,1,2,0,1,1; 0,2,2,2,0,0,0,1; 1,1,0,2,0,0,0,4; 0,0,1,2,0,0,1,2; 0,2,1,0,0,0,0,3; 1,0,0,0,0,0,0,1; 3,2,0,2,0,0,0,2; 2,0,0,0,1,2,2,3; 1,1,1,0,0,0,0,1;
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clc clear //Input data C=800*(5/18) //Velocity in m/s Po=105 //Stagnation pressure in kPa To=35+273 //Stagnation temperature in K Cp=1005 //Specific heat capacity at constant pressure in J/kg-K k=1.4 //Adiabatic Constant R=287 //Specific gas constant in J/kg-k //Calculation T=To-(C^2/(2*Cp)) //Static temperature in K P=Po*(T/To)^(k/(k-1)) //Static pressure in kPa a=sqrt(k*R*T) //Sound Velocity in m/s M=C/a //Mach number //Output printf('(A)Static conditions:\n Pressure is %3.2f kPa\n Temperature is %3.2f K\n Sound Velocity is %3.2f m/s\n (B)Mach number is %3.2f',P,T,a,M)
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Ex3_7.sce
//Tested on Windows 7 Ultimate 32-bit //Chapter 3 Semiconductor Diodes and Miscellaneous Devices Pg no. 91 clear; clc; //Given Data Rl=200;//Load resistance in ohms esf=50;//Input signal frequncy in hertz RF=5/100;//Ripple Factor //Solution C=1/(esf*Rl*2*RF)*10^6;//Capacitance in micro faraday; printf("The size of shunt capacitor is C = %d μF",C);
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[ "Apache-2.0", "LicenseRef-scancode-unknown-license-reference" ]
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( - a^2 - 2*a*b - b^2 + x^2).getIsolatedSignature() = null
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Ex1_7.sce
clc // Example 1.7.py // A flat plate with a chord length of 3 ft and an infinite span(perpendicular to // the page in fig 1.5) is immersed in a Mach 2 flow at standard sea level // conditions at an angle of attack of 10 degrees. The pressure distribution // over the plate is as follows: upper surface, p2=constant=1132 lb/ft^2 lower // surface, p3=constant=3568 lb/ft^2. The local shear stress is given by tau_w = // 13/xeta^0.2, where tau_w is in pounds per square feet and xeta is the distance // in feet along the plate from the leading edge. Assume the distribution of // tau_w over the top and bottom surfaces is the same. Both the pressure and // shear disributions are sketched qualitatively in fig. 1.5. Calculate the lift // and drag per unit span on the plate. // // Variable declaration M1 = 2.0 // mach number freestream p1 = 2116.0 // pressure at sea level (in lb/ft^2) l = 3.0 // chord of plate (in ft) alpha = 10.0 // angle of attack in degrees p2 = 1132.0 // pressure on the upper surface (in lb/ft^2) p3 = 3568.0 // pressure on the lower surface (in lb/ft^2) // Calculations // assuming unit span pds = -p2*l + p3*l // integral p.ds from leading edge to trailing edge (in lb/ft) L = pds*cos(alpha*%pi/180.0) // lift per unit span (in lb/ft), alpha is converted to radians Dw = pds*sin(alpha*%pi/180.0) // pressure drag per unit span (in lb/ft), alpha is converted to radians Df = 16.25 * (l** 4.0/5.0) // skin friction drag per unit span (in lb/ft) // from integral tau.d(xeta) Df = 2 * Df * cos(alpha*%pi/180.0) // since skin friction acts on both the side D = Df + Dw // total drag per unit span (in lb/ft) // Result printf("\n Total Lift per unit span = %.0f lb", L) printf("\n Total Drag per unit span = %.0f lb", D)
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Example_5_21.sce
//A Textbook of Chemical Engineering Thermodynamics //Chapter 5 //Some Applications of the Laws of Thermodynamics //Example 21 clear; clc; //Given: P2 = 2800; //pressure of superheated steam (kPa) P1 = 275; //pressure of withdrawn steam (kPa) V = 1.070*10^-3; //specific volume of saturated liquid at 275 kPa //From steam tables: H6 = 138; //enthalpy of saturated liquid at 5 kPa S6 = 0.4764; //entropy of saturated liquid at 5 kPa H_v1 = 2562; //enthalpy of saturated vapour at 5 kPa S_v1 = 8.3951; //entropy of saturated vapour at 5 kPa H1 = 549; //enthalpy of saturated liquid at 275 kPa S1 = 1.6408; //entropy of saturated liquid at 275 kPa H_v2 = 2721; //enthalpy of saturated vapour at 275 kPa S_v2 = 7.0209; //entropy of saturated vapour at 275 kPa H3 = 3063; //enthalpy of superheated steam at 2800 kPa and 598 K S3 = 6.6875; //entropy of superheated steam at 2800 kPa and 598 K //To determine the fraction of steam withdrawn and thermal efficiency of cycle //Referring fig. 5.23 (Page no.161) S4 = S3; //isentropic expansion x = (S4-S1)/(S_v2-S1); //quality of steam H4 = H1 + x*(H_v2-H1); H7 = H6; //as the power input to the condensate pump is neglegible //Applying energy balance around feed water heater m = (H1-H7)/(H4-H7); //fraction of steam extracted mprintf('Fraction of steam withdrawn is %f',m); W_in = V*(P2-P1); //work input to the feed water pump H2 = H1+W_in; //Considering isentropic expansion in turbine S5 = S3; x = (S5-S6)/(S_v1-S6); H5 = H6 + x*(H_v1-H6); //Using eq. 5.85 (Page no.162) eff = ((H3-H2)-(1-m)*(H5-H6))/(H3-H2); mprintf('\n Thermal efficiency is %f percent',eff*100); //end
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Ex3_6.sce
clear // // // //Variable declaration d=0.4086*10^-10; //lattice spacing(m) theta=65; //glancing angle(degree) h=6.6*10^-34; //plank's constant(Js) m=9.1*10^-31; //mass(kg) n=1; //Calculation theta=theta*%pi/180; //angle(radian) lamda=2*d*sin(theta)/n; //debroglie wavelength(m) v=h/(m*lamda); //velocity(m/sec) //Result printf("\n debroglie wavelength is %0.4f *10^-10 metre",lamda*10^10) printf("\n velocity is %0.3f *10^6 m/sec",v/10^6) printf("\n answer in the book is wrong")
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float a[][]; /* ошибка */
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//=========================================================================== //chapter 3 example 13 clc;clear all; //variable declaration R1 = 1000; //resistance in Ω R2 = 500; //resistance in Ω eR1 = 1; //error resistance eR2 = 1; //error resistance //calculations R = (R1*R2)/(R1+R2); //resistance in Ω X = R1*R2; Y = R1+R2; dX = (eR1+eR2); //error in X //dY = (dR1/Y)+(dR2/Y); //dY = (R1/Y)*(dR1/R1)+((R2/Y)*(dR2/R2) dY = ((R1/(Y))*(eR1))+((R2/(Y))*(eR2)); //error in Y eP = dX+dY; //percentage error in equivaent parallel resistance in % e = R*(eP/(100)); //error(maximum ossible) in equivalent parallel resistance in Ω //result mprintf("percentage error = %3.2f percentage",eP); mprintf("\nerror in equivalent parallel resistance = %3.2f Ω",e);
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// Updated(18-7-07) // 4.1 a = 0.9; n = -10:20; y = zeros(1,size(n,'*')); for i = 1:length(n) if n(i)>=0, y(i) = a^n(i); end end stem(n,y) label('u1',4,'Time(n)','0.9^n1(n)',4)
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//trace asteroid clc; clear; x=[-5:0.01:5]; a=4; y1=(a^(2/3) - (x.^2).^(1/3)).^(3/2); //for some odd reason, x^(2/3) != (x^2)^(1/3) y2=-y1; plot2d(x,y1); plot2d(x,y2); xlabel("X-Axis") ylabel("Y-Axis") title("Asteroid")
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clc clear //INPUT DATA r1=0.1258*10^-9//atomic radii of the iron atom in BCC structure in m r2=0.1292*10^-9//atomic radii of the iron atom in FCC structure in m T=910//metallic iron changes from BCC to FCC in centigrade //CALCULATION a1=((4*r1)/sqrt(3))//lattice constant of BCC structure in m v1=((a1*a1*a1)/2)//The volume occupied by one BCC atom in m^3 a2=((4*r2)/sqrt(2))//lattice constant of FCC structure in m v2=((a2*a2*a2)/4)//The volume occupied by one FCC atom in m^3 V=((v1-v2)/v1)*100//The change in volume percentage //OUTPUT printf('The change in volume percentage is %3.5f',V)
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//Problem 9.03: A conductor moves with a velocity of 15 m/s at an angle of (a) 90°, (b) 60° and (c) 30° to a magnetic field produced between two square-faced poles of side length 2 cm. If the flux leaving a pole face is 5 μWb, find the magnitude of the induced e.m.f. in each case. //initializing the variables: l = 0.02; // in m b = 0.02; // in m v = 15; // in m/s R = 20; // in ohms Phi = 5E-6; // in Wb u0 = 4*%pi*1E-7; a1 = 90; // in degrees a2 = 60; // in degrees a3 = 30; // in degrees //calculation: A = l*b B = Phi/A E90 = B*l*v*sin(a1*%pi/180) E60 = B*l*v*sin(a2*%pi/180) E30 = B*l*v*sin(a3*%pi/180) printf("\n\nResult\n\n") printf("\n Induced e.m.f. at angles 90°, 60°, 30° are %.2E V, %.2E V, %.3E V respectively\n",E90,E60,E30)
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// Scilab Code Ex4.3: Page-234 (2008) clc; clear; c = 3e+008; // Speed of light in vacuum, m/s v = [c c/sqrt(2) sqrt(3)/2*c c/2 0.8*c]; // Different speeds of metre rod, m/s L0 = 100; // Actual length of the rod, cm for i = 1:1:5 L = L0*sqrt(1-v(i)^2/c^2); // Apparent length of rod from Lorentz transformation, m printf("\nFor v = %4.2e m/s, L = %4.1f cm", v(i), L); end // Result // For v = 3.00e+008 m/s, L = 0.0 cm // For v = 2.12e+008 m/s, L = 70.7 cm // For v = 2.60e+008 m/s, L = 50.0 cm // For v = 1.50e+008 m/s, L = 86.6 cm // For v = 2.40e+008 m/s, L = 60.0 cm
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res_log=read('../data/gps_kalman_log.m',-1,16); [r_n,c_n]=size(res_log); idx=[1:r_n]; // First plot KF state //xset('color',3); //xset('background', 1); xbasc(); xset('window',0); // plot pos_x result subplot(511); plot2d(res_log(:,2)); xtitle("ECEF_x",'100ms','m'); xset('background', 4); // plot pos_y result subplot(512); plot2d(res_log(:,3)); xtitle("ECEF_y",'100ms','m'); xset('background', 4); // plot pos_z result subplot(513); plot2d(res_log(:,4)); xtitle("ECEF_z", '100ms','m'); xset('background', 4); // plot clk_bias result subplot(514); plot2d(res_log(:,5)); xtitle("clk_bias", '100ms','m'); xset('background', 4); // plot clk_drift result subplot(515); plot2d(res_log(:,6)); xtitle("clk_drift", '100ms','m/s'); xset('background', 4); // Then plot corrections xset('window',1); // plot corr_pos_x result subplot(511); plot2d(res_log(:,7)); xtitle("ECEF_x correction",'100ms','m'); xset('background', 4); // plot corr_pos_y result subplot(512); plot2d(res_log(:,8)); xtitle("ECEF_y_correction",'100ms','m'); xset('background', 4); // plot corr_pos_z result subplot(513); plot2d(res_log(:,9)); xtitle("ECEF_z_correction", '100ms','m'); xset('background', 4); // plot corr_bias result subplot(514); plot2d(res_log(:,10)); xtitle("clk_bias_correction", '100ms','m'); xset('background', 4); // plot corr_drift result subplot(515); plot2d(res_log(:,11)); xtitle("clk_drift_correction", '100ms','m/s'); xset('background', 4); // Then plot diag of P_matrix xset('window',2); // plot p_pos_x result subplot(511); plot2d(res_log(:,12)); xtitle("ECEF_x_cov",'100ms','m^2'); xset('background', 4); // plot p_pos_y result subplot(512); plot2d(res_log(:,13)); xtitle("ECEF_y_cov",'100ms','m^2'); xset('background', 4); // plot p_pos_z result subplot(513); plot2d(res_log(:,14)); xtitle("ECEF_z_cov", '100ms','m^2'); xset('background', 4); // plot p_bias result subplot(514); plot2d(res_log(:,15)); xtitle("clk_bias_cov", '100ms','m^2'); xset('background', 4); // plot p_drift result subplot(515); plot2d(res_log(:,16)); xtitle("clk_drift_cov", '100ms','(m/s)^2'); xset('background', 4);
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//Example 4.17. clc format(6) Io1=7.5*10^-6 T1=27 T2=127 disp("The saturation current at 400 K is,") disp("Io2 = Io1 * 2^((T2-T1)/10)") disp(" = 7.5*10^-6 * 2^(127-27/10)") Io2=Io1*(2^((T2-T1)/10)) I=Io2*10^3 disp(I,"Io2(mA) = ")
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#define your files scenario = "EP"; pcl_file = "EP.pcl"; #standard settings scenario_type = trials; active_buttons = 5; button_codes = 1,2,3,4,5; response_logging = log_active; #log only if response is expected response_matching = simple_matching; default_output_port = 1; #parallel port response_port_output = false; write_codes = true; pulse_width = 100; #duration of shock default_background_color = 0,0,0; default_font_size = 40; default_text_color = 255,255,255; default_font = "Tahoma"; ##################################################### begin; ##################################################### #Stimuli picture {} default; picture {text {caption = "+"; font_size=100; font_color = 255,255,255,;}; x=0;y=0;} fixation_cross; TEMPLATE "template.tem"; text { caption = "XXX"; font_size =20; preload = false; } gap; # RANGE OF RATING SCALE # array{ text {caption = "0";}; text {caption = "100";}; } number; # QUESTION ABOVE RATING SCALE # array{ text { caption = "Skatta din upplevda smärtintensitet";}; text { caption = "Skatta ditt upplevda obehag";}; } questions; # RATING SCALE # picture { box { height = 10; width = 200; color = 255,255,255; }; x = 0; y = 0; box { height = 50; width = 5;color = 255,255,255; }; x = 0; y = 0; text gap; x = -200; y = 0; text gap; x = 200; y = 0; text gap; x=0; y=150; }scale; ####################################################### #Define trialtypes ####################################################### # FIXATION CROSS # trial { all_responses = false; trial_duration = stimuli_length; trial_type = fixed; stimulus_event{ picture fixation_cross; time = 0; duration = 4000; code="fixation_cross"; } ev_fixation_cross; } tr_fixation_cross; # CONDITION TRIAL # trial { trial_duration = stimuli_length; trial_type = fixed; all_responses = false; stimulus_event{ #condition picture { text {caption = "condition";}; x = 0; y = 0; } pic_condition; time=0; duration = 500; code = "condition"; } ev_condition; }tr_condition; # PORT OUTPUT # trial{ trial_duration = stimuli_length; trial_type = fixed; all_responses = false; stimulus_event{ nothing {}; port_code = 99; code = "port_output"; } ev_port_output; }tr_port_output; # SHOCK # trial { trial_duration = stimuli_length; trial_type = fixed; all_responses = false; stimulus_event{ #shock picture picture { text {caption = "condition";}; x = 0; y = 0; } pic_shock; time=0; duration = 2000; code = "shockpic"; } ev_shockpic; stimulus_event{ nothing {}; code = "Shock"; deltat = 0; port_code = 1; } ev_shock; stimulus_event{ picture fixation_cross; time = 2000; code = "shockpic"; } ev_shockcross; } tr_shock; # RATING SCALE # trial { all_responses = true; trial_duration = stimuli_length; trial_type = fixed; } tr_rate; #########################
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//Chapter 1, Example 1.7 clc //Initialisation v1=10 //voltage v2=0 //voltage r1=200 //resistance in ohm r2=300 //resistance in ohm //Calculation v=v1*(r2/(r1+r2)) //voltage //Results printf("Voltage, V = %d V",v)
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//Caption: Entropy //Example 9.9 //page no 398 //Find Entropy,Amount of information clc; clear; px1=0.4; px2=0.3; px3=0.2; px4=0.1; HX=-px1*log2(px1)-px2*log2(px2)-px3*log2(px3)-px4*log2(px4); printf(" \n Entropy \n \n\t i) H(X) = %.2f bits/symbol,\n",HX); Px1x2x1x3=px1*px2*px1*px3; Ix1x2x1x3=-log2(Px1x2x1x3); printf(" \n Amount of information \n \n\t ii) I(x1x2x1x3) = %.2f bits/symbol,\n",Ix1x2x1x3); Px4x3x3x2=px4*px3*px3*px2; Ix4x3x3x2=-log2(Px4x3x3x2); printf(" \n \t \n \t I(x4x3x3x2) = %.2f bits/symbol.\n",Ix4x3x3x2);
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//Example 3.7 // total resistance clc; clear; close; //given data : r1=6; // resistance in ohm r2=10; // resistance in ohm r3=15; // resistance in ohm r=(1/r1)+(1/r2)+(1/r3); R=1/r; disp(R,"equivalent resistance,R(ohm) = ")
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h1=2//m h2=0.5//m S=0.85//specific gravity of oil
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// Example 4.20.a;//delay clc; clear; close; d=0.02;// Change in refractive index n1=1.5;//Core refrctive index L=3*10^3;//Length in meter C=2.998*10^8;//Speed of light in m/s dts=round(((L*n1*d)/C)*10^9);//DELAY IN NS disp(dts,"DELAY IN NS")
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//Example 12.3;no. of subscribers clc; clear; close; pt=1;//mW pn=-40;//dBm pn1=10^(pn/10);// c=0.05;// d=0.11;// x=((pn1)/(pt*c));// y=((log10(x))/(log10((1-d)*(1-c))));// n=y+1;// disp(round(n),"no. of subscribers are")
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[[-1,2,-1,0,0],[1,2,-1,1,0],[2,-2,1,-1,0],[2,-1,2,0,0]] [-1,9,-6,8] [-4,25,-22,17] [-2,41,-17,40]*2 [-3,19,-18,10]*3 [-3,115,-34,114]*3 [-16,111,-108,47] [-6,41,-33,32]*6 [-12,167,-86,159]*3 [-4,249,-57,248]*4 [-25,193,-190,68] [-5,461,-86,460]*5 [-12,103,-102,31]*3 [-50,309,-285,184]*2 [-48,349,-268,285]*3 [-12,145,-81,136]*12 [-20,573,-198,565]*5 [-6,769,-121,768]*6 [[-1,2,1,1,0],[1,2,1,0,0],[2,1,2,0,0],[2,2,1,1,0]] [5,3,4,6]*3 [41,16,23,44] [61,50,64,85]*2 [87,25,38,90] [157,147,186,238]*3 [53,12,19,54]*3 [207,98,136,231]*2 [263,192,249,344]*3 [107,108,136,171]*12 [263,49,80,266] [571,605,760,946]*5 [405,64,107,408] [163,54,80,171]*6 [589,300,411,670]*3 [699,484,632,891]*4 [271,240,305,396]*15 [925,1014,1272,1573]*6 [[0,-1,2,-1,0],[0,1,2,-1,1],[0,2,-2,1,-1],[0,2,-1,2,0]] [-1,9,-6,8]*2 [-4,25,-22,17]*3 [-2,41,-17,40]*3 [-3,19,-18,10]*12 [-3,115,-34,114]*4 [-16,111,-108,47]*5 [-6,41,-33,32]*15 [-12,167,-86,159]*5 [-4,249,-57,248]*5 [-25,193,-190,68]*6 [-5,461,-86,460]*6 [-12,103,-102,31]*21 [-50,309,-285,184]*7 [-48,349,-268,285]*7 [-12,145,-81,136]*21 [-20,573,-198,565]*7 [-6,769,-121,768]*7 [[0,-1,2,1,1],[0,1,2,1,0],[0,2,1,2,0],[0,2,2,1,1]] [5,3,4,6]*6 [41,16,23,44]*3 [61,50,64,85]*3 [87,25,38,90]*4 [157,147,186,238]*4 [53,12,19,54]*15 [207,98,136,231]*5 [263,192,249,344]*5 [107,108,136,171]*15 [263,49,80,266]*6 [571,605,760,946]*6 [405,64,107,408]*7 [163,54,80,171]*21 [589,300,411,670]*7 [699,484,632,891]*7 [271,240,305,396]*21 [925,1014,1272,1573]*7 [[0,0,1,-2,1],[0,0,2,-1,2],[0,1,-1,2,-2],[0,1,-1,2,1]] [2,16,-9,15]*2 [12,51,-38,43]*3 [3,60,-22,59]*3 [12,40,-33,31]*12 [4,152,-41,151]*4 [80,235,-204,171]*5 [15,80,-54,71]*15 [20,265,-118,257]*5 [5,310,-66,309]*5 [150,408,-365,283]*6 [6,552,-97,551]*6 [84,217,-198,145]*21 [175,644,-510,519]*7 [112,665,-428,601]*7 [21,238,-114,229]*21 [28,791,-246,783]*7 [7,896,-134,895]*7 [[0,0,1,2,1],[0,0,2,1,2],[0,1,1,2,-1],[0,1,1,2,2]] [6,8,1,9]*6 [48,69,-5,76]*3 [75,96,29,110]*3 [100,152,-27,165]*4 [196,248,95,287]*4 [60,95,-23,102]*15 [245,340,3,378]*5 [320,415,97,472]*5 [135,170,73,198]*15 [294,480,-137,511]*6 [726,912,419,1067]*6 [448,749,-237,792]*7 [189,280,-37,306]*21 [700,959,41,1070]*7 [847,1106,225,1254]*7 [336,427,149,492]*21 [1183,1484,713,1742]*7 [[0,1,0,0,-1],[0,2,0,0,1],[1,0,0,-1,0],[1,0,0,2,0]] [-14,20,-7,17] [-78,87,-26,55] [-57,129,-38,124] [-84,88,-21,43]*3 [-148,472,-111,465] [-620,635,-124,251] [-195,235,-78,172]*3 [-490,895,-294,831] [-305,1265,-244,1256] [-1290,1308,-215,433] [-546,2796,-455,2785] [-798,805,-114,229]*3 [-2345,2513,-670,1388] [-2212,2779,-948,2139] [-651,1099,-372,1000]*3 [-1526,4151,-1090,4055] [-889,5425,-762,5412] [[0,1,-2,-1,-1],[0,2,2,1,1],[1,1,2,-1,0],[1,1,2,2,0]] [-10,12,1,9]*3 [-123,132,-5,76] [-183,255,58,220] [-116,120,-9,55]*3 [-628,952,285,861] [-265,270,-23,102]*3 [-345,385,2,252]*3 [-1315,1720,291,1416] [-535,855,292,792]*3 [-1578,1596,-137,511] [-3426,5676,2095,5335] [-945,952,-79,264]*3 [-1141,1197,-74,612]*3 [-4123,4690,123,3210] [-1631,2079,300,1672]*3 [-1897,2772,745,2460]*3 [-6475,11011,4278,10452] [[0,1,-2,1,0],[0,2,-1,2,0],[1,-1,2,-2,0],[1,-1,2,1,0]] [2,16,-9,15] [12,51,-38,43] [3,60,-22,59]*2 [12,40,-33,31]*3 [4,152,-41,151]*3 [80,235,-204,171] [15,80,-54,71]*6 [20,265,-118,257]*3 [5,310,-66,309]*4 [150,408,-365,283] [6,552,-97,551]*5 [84,217,-198,145]*3 [175,644,-510,519]*2 [112,665,-428,601]*3 [21,238,-114,229]*12 [28,791,-246,783]*5 [7,896,-134,895]*6 [[0,1,2,1,0],[0,2,1,2,0],[1,1,2,-1,0],[1,1,2,2,0]] [6,8,1,9]*3 [48,69,-5,76] [75,96,29,110]*2 [100,152,-27,165] [196,248,95,287]*3 [60,95,-23,102]*3 [245,340,3,378]*2 [320,415,97,472]*3 [135,170,73,198]*12 [294,480,-137,511] [726,912,419,1067]*5 [448,749,-237,792] [189,280,-37,306]*6 [700,959,41,1070]*3 [847,1106,225,1254]*4 [336,427,149,492]*15 [1183,1484,713,1742]*6 [[0,1,2,-1,1],[0,2,-2,1,-1],[1,-1,2,-2,0],[1,-1,2,1,0]] [6,-4,-3,5]*3 [75,-66,-38,43] [123,-51,-44,118] [76,-72,-33,31]*3 [460,-136,-123,453] [185,-180,-68,57]*3 [205,-165,-108,142]*3 [835,-430,-354,771] [415,-95,-88,412]*3 [1158,-1140,-365,283] [2766,-516,-485,2755] [721,-714,-198,145]*3 [721,-665,-340,346]*3 [2443,-1876,-1284,1803] [1015,-567,-456,916]*3 [1337,-462,-410,1305]*3 [5383,-847,-804,5370] [[0,1,0,0,1],[0,2,0,0,-1],[1,0,0,-2,0],[1,0,0,1,0]] [6,-4,-5,3]*3 [84,-75,-53,28] [105,-33,-92,70] [260,-248,-127,65] [364,-40,-303,273] [210,-205,-83,42]*3 [665,-545,-484,266] [760,-355,-669,456] [315,5,-248,252]*3 [1302,-1284,-431,217] [2046,204,-1535,1705] [2408,-2387,-685,344] [819,-763,-452,234]*3 [2590,-2023,-1977,1110] [2849,-1505,-2488,1628] [1092,-217,-935,780]*3 [3913,623,-2820,3354] #---> reslines=12
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//8.7 clc; f_unity=10^6; Av=100000; open_loop_upper_cutoff_f=f_unity/Av; printf("open loop upper cutoff frequency=%.0f Hz", open_loop_upper_cutoff_f) disp('when beta=0.001') beta=0.001; Closed_loop_gain=Av/(1+Av*beta); printf("\nClosed loop gain=%.1f ",Closed_loop_gain) upper_cutoff_frequency=f_unity/Closed_loop_gain; printf("\nUpper cutoff frequency=%.0f Hz", upper_cutoff_frequency) disp('when beta=0.01') beta=0.01; Closed_loop_gain=Av/(1+Av*beta); printf("\nClosed loop gain=%.1f ",Closed_loop_gain) upper_cutoff_frequency=f_unity/Closed_loop_gain; printf("\nUpper cutoff frequency=%.0f Hz", upper_cutoff_frequency) disp('when beta=0.1') beta=0.1; Closed_loop_gain=Av/(1+Av*beta); printf("\nClosed loop gain=%.3f ",Closed_loop_gain) upper_cutoff_frequency=f_unity/Closed_loop_gain; printf("\nUpper cutoff frequency=%.0f Hz", upper_cutoff_frequency)
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//Motor boat crossing river //refer fig. 14.11 and 14.12 //let the motor boat start from A and reaches C vrx=15 //kmph //distance to be moved in x direction=1 km //time required t is t=4 //min //boat will move down the stream vy=5 //kmph //Distance moved in downstream direction (d) d=333.33 //m //Let the direction of boat be set at theta to x-direction theta=asind(1/3) //degree printf("The boat should be set in the direction theta=%.2f degree and time required is t=%.2f min\nDistance moved in downstream direction=%.2f m",theta,t,d)
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Example_5_15.sce
//A Textbook of Chemical Engineering Thermodynamics //Chapter 5 //Some Applications of the Laws of Thermodynamics //Example 15 clear; clc; //Given: T1 = 300; //indoor temperatur (K) T2 = 290; //outside temperature (K) W_input = 1; //1 kW heat pump W_output = 30; //given output (kW) //To verify that given heat pump is equivalent to 30 kW heater Q2 = (T2/(T1-T2))*W_input; //heat absorbed Q1 = Q2 + W_input; //heat rejected if(Q1==W_output) mprintf('1 kW pump if operated reversibly, is equivalent to a 30 kW heater'); else mprintf('The given heat pump is not equivalent to a 30 kW heater'); end //end
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variables.sce
function y=f1( x ) y = 0.5^x - 3 + ( x + 1 ) ^ 2 endfunction function y=f2( x ) y = x .* log10( x + 1 ) - 1; endfunction function y=f3( x ) y = x + log10( x ) - 0.5; endfunction density = 0.0001;
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// Mission X1 // Chargement de l'image au format .dat dans la mémoire load("C:\Users\Jean-Guillaume P\Documents\Exia\A2\Projets\Imagerie\ExoLife\Images\Mission_X\Asellus Secundus.dat"); // Utilisation de l'inverse de la transformée de Fourrier img_out = ifft(imgT); // Affichage figure; display_gray(img_out); // Sauvegarde de l'image writepbm(img_out, "C:\Users\Jean-Guillaume P\Documents\Exia\A2\Projets\Imagerie\ExoLife\Rendus\MissionX1.pbm");
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Ex9_3.sce
// Chapter 9 example 3 //------------------------------------------------------------------------------ clc; clear; // Given Data f = 10*10^9; // radar Tx frequency PRF = 2000; // Pulse repetitive frequency in Hz Vr = 0.5; // radial vel in Mach c = 3*10^8; // velocity of EM waves in m/s vs = 330; // velocity of sound in m/s // Calculations lamda = c/f; // wavelength in m max_unamb_fd = PRF/2; // maximum unambiguous doppler shift Vrunamb = (lamda*max_unamb_fd)/2; // doppler shift Vaircraft = 0.5*vs; // Converting from Mach to m/s fd_desired = (2*Vaircraft)/lamda; PRF_desired = 2*fd_desired; // desired PRF // Output if Vrunamb < Vaircraft then mprintf('The radar is not capable of determining unambiguously the velocity of the approaching aircraft\n'); end mprintf(' Desired Pulse Repetition Rate = %d Khz',PRF_desired/1000); //------------------------------------------------------------------------------
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FallschirmspringerDGL.sci
function zp = FallschirmspringerDGL(t, z) g = 9,81; m = 100; cw = 1,4; p = 1,2; r = 5; zp = [z(2); -g*m + 0,5*cw*p*%pi*r^2*z(2).^2/m]; endfunction
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hakesh729/Project_hack
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load MantissaMUL.hdl, output-file MantissaMUL.out, output-list a%B1.8.1 a%D1.8.1 b%D1.8.1 b%B1.8.1 out%B1.16.1 out%D1.16.1; //170(10101010) * 187(10111011) = 31,790(01111100 00101110) set a %B10101010 , set b %B10111011 , eval, output; //139(10001011) * 138(10001010) = 19182(01001010 11101110) set a %B10001011 , set b %B10001010 , eval, output;
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q2.sce
s = poly(0,'s'); G = 10/(s*(s+2)*(s+4)); // PART A k = 4; // any arbitrary value chosen H = k*G/(1+k*G); disp(H); // PART B k_range = .1:.1:100.1; // excluding k =0 case // for each k we get 3 poles since denominator of H is cubic poles = zeros(3,length(k_range)); for i = 1:length(k_range) k = k_range(i); H = syslin('c',k*G/(1+k*G)); [_,p, _] = tf2zp(H) poles(:,i) = p; end plot2d(real(poles'), imag(poles'), [-2,-3,-4]); a = gca() a.data_bounds = [-12,-9;4,9]; title('Loci of closed loop poles as K varies') xlabel('Real (poles)'); ylabel('Imaginary (poles)'); // PART C k1 = k_range(find(real(poles(2,:))>= 0))(1); k2 = k_range(find(real(poles(3,:))>= 0))(1); k3 = k_range(find(real(poles(1,:))>= 0))(1); k_critical = min(k1,k2,k3);
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20_1.sce
//Find fracture strength and ratio //Ex:20.1 clc; clear; close; l=1.5*10^-6;//crack length in m e=70*10^9;//Young's modulous in N/m^2 y_e=1.05;//specific surface energy in j/m^2 a_f=sqrt((2*y_e*e)/(3.14*l)); a_f1=a_f*10^-6;//in MPa disp(a_f1,"Fracture strength (in MPa) = "); r=a_f/e;//ratio disp(r,"Ratio of fracture strength to Youngs modulous = " );
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examplesec10_1_1.sce
//Example sec 10.1.1 //mass, dashpot, spring arrangement. clear;clc; xdel(winsid()); M=1 K=2 F=2 A=[0 1;-2 -2] C=eye(A) s=%s D=s*C-A X=inv(D)*[1;1] //taking the laplace transform of X disp("X(t)=sqrt(5)*sin(t+inv(tan 0.5));sqrt(10)*sin(t+inv(tan -1/3))") disp("The system is asymptotically stable")