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// Scilab code Ex13.8: Pg 486 (2005) clc; clear; M_X = 226.025406; // Atomic mass of Ra-226, u M_Y = 222.017574; // Atomic mass of Rn-222, u M_alpha = 4.002603; // Mass of alpha particle, u Q = (M_X - M_Y - M_alpha)*931.494; // Q-value for Radium Decay, MeV/u printf("\nThe Q-value for Radium Decay = %4.2f MeV", Q); // Result // The Q-value for Radium Decay = 4.87 MeV
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// Scilab code Ex17.11 : Pg:894 (2011) clc;clear; e = 1.6e-019; // Energy equivalent of 1 eV, J/eV N_A = 6.023e+026; // Avogadro's number, per kmol P = 2; // Power produced by the fission of U235, watt E_f = 200*1e+06*e; // Energy released per fission, J FR = P/E_f; // Fission rate of U235, fission/sec N = 0.5/235*N_A; // Number of U235 nuclei in 0.5 kg of U235 E = 200*N; // Energy released in the complete fissioning of 0.5 kg of U235, MeV printf("\nThe fission rate of U235 = %4.2e fissions/sec", FR); printf("\nThe energy released in the complete fissioning of 0.5 kg of U235 = %1.0e kcal", E*1e+06*e/(1000*4.186)); // Result // The fission rate of U235 = 6.25e+010 fissions/sec // The energy released in the complete fissioning of 0.5 kg of U235 = 1e+010 kcal
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bula ngibula V;SG;1;FUT reka bayareka V;SG;1;PST e sizoe V;PL;2;PST rekisa uzorekisa V;PL;1;PST qala bazoqala V;PL;3;PST haufi bazohaufi V;PL;3;PST reka sizoreka V;PL;2;PST thusa nithusa V;PL;2;FUT haufi uhaufi V;SG;3;FUT hulaa ngihulaa V;SG;1;FUT ebe siyaebe V;PL;2;PRS tloo batloo V;PL;3;FUT haufi uyahaufi V;SG;2;PRS lumela bazolumela V;PL;3;PST qala niyaqala V;PL;3;PRS ithute ithuteea V;NFIN qete uzoqete V;PL;1;PST rekisa bazorekisa V;PL;3;PST phomolo niphomolo V;PL;2;FUT ema ngiema V;SG;1;FUT boroko uzoboroko V;SG;3;PST ebe sizoebe V;PL;2;PST hulaa ngizohulaa V;SG;2;PST ebe uyaebe V;SG;2;PRS phomolo sizophomolo V;PL;2;PST qala niqala V;PL;2;FUT bala uyabala V;PL;1;PRS tloo sitloo V;PL;1;FUT lula nilula V;PL;2;FUT lumela balumela V;PL;3;FUT utloa siutloa V;PL;1;FUT bula uzobula V;PL;1;PST etsa uzoetsa V;SG;3;PST ebe ngiebe V;SG;1;FUT phomolo uphomolo V;SG;3;FUT lumela uyalumela V;SG;3;PRS lumela ngiyalumela V;SG;1;PRS tloo ngitloo V;SG;1;FUT utloa uzoutloa V;PL;1;PST sututsa bazosututsa V;PL;3;PST bala sizobala V;PL;2;PST hulaa uyahulaa V;SG;2;PRS etsa uyaetsa V;PL;1;PRS thusa bathusa V;PL;3;FUT qete siqete V;PL;1;FUT bula nibula V;SG;2;FUT fofa ngifofa V;SG;1;FUT etsa uyaetsa V;SG;2;PRS qala uyaqala V;SG;3;PRS qala siyaqala V;PL;2;PRS bula niyabula V;PL;3;PRS utloa ngiutloa V;SG;1;FUT rekisa uyarekisa V;SG;2;PRS ebe ngiyaebe V;SG;1;PRS fofa bazofofa V;PL;3;PST ya niyaya V;PL;3;PRS bula sibula V;PL;1;FUT reka uyareka V;SG;3;PRS thusa uzothusa V;PL;1;PST boroko siyaboroko V;PL;2;PRS utloa ngizoutloa V;SG;2;PST ya yaea V;NFIN lula siyalula V;PL;2;PRS thusa ngiyathusa V;SG;1;PRS qala sizoqala V;PL;2;PST lumela uyalumela V;PL;1;PRS ema niema V;SG;2;FUT sututsa ngizosututsa V;SG;2;PST fofa uyafofa V;PL;1;PRS lula nilula V;SG;2;FUT fofa sifofa V;PL;1;FUT lula uyalula V;SG;3;PRS ema bazoema V;PL;3;PST boroko ngiboroko V;SG;1;FUT lumela uzolumela V;PL;1;PST ngola ngizongola V;SG;2;PST lumela uyalumela V;SG;2;PRS reka nireka V;SG;2;FUT ithute uyaithute V;PL;1;PRS bula bayabula V;SG;1;PST bala bazobala V;PL;3;PST e uzoe V;PL;1;PST lumela siyalumela V;PL;2;PRS bala balaea V;NFIN fofa uyafofa V;SG;3;PRS lula uzolula V;PL;1;PST ithute sizoithute V;PL;2;PST rekisa uyarekisa V;PL;1;PRS ngola niyangola V;PL;3;PRS qala ngizoqala V;SG;2;PST bula bazobula V;PL;3;PST lula bazolula V;PL;3;PST bala babala V;PL;3;FUT boroko niyaboroko V;PL;3;PRS ja uzoja V;SG;3;PST utloa utloaea V;NFIN rekisa urekisa V;SG;3;FUT lula ulula V;SG;3;FUT hulaa nihulaa V;SG;2;FUT
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//=============================================================================================== // chapter 1 example 9 clc; clear; // Variable Declaration r = 0.175*10^-9; //radius in m h = 2; //miller indices k = 3; //miller indices l = 1; //miller indices //calculation a = (4*r)/sqrt(2); dhkl = a/sqrt((h^2)+(k^2)+(l^2)); //result mprintf('inter planar spacing =%3.2e m\n',dhkl); mprintf('Note : calculation mistake in textbook in calculating dhkl value '); //=============================================================================================
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A000008 sage 1 - x - x^2 + x^3 - x^5 + x^6 + x^7 - x^8 - x^10 + x^11 + x^12 - x^13 + x^15 - x^16 - x^17 + x^18 + 1 A000008 vect [1],[1,-1,-1,1,0,-1,1,1,-1,0,-1,1,1,-1,0,1,-1,-1,1] A000008 coef [1,1,2,2,3,4,5,6,7,8,11,12,15,16,19,22] A000012 sage 1 - x + 1 A000012 vect [1],[1,-1] A000012 coef [1,1,1,1,1,1,1,1,1,1,1,1,1,1,1,1] A000027 sage x - 2*x + x^2 + 1 A000027 vect [0,1],[1,-2,1] A000027 coef [0,1,2,3,4,5,6,7,8,9,10,11,12,13,14,15] A000032 sage - x + 2 - x - x^2 + 1 A000032 vect [2,-1],[1,-1,-1] A000032 coef [2,1,3,4,7,11,18,29,47,76,123,199,322,521,843,1364]
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// Ex4_35 clc; // Given: t1=2.7;// h t2=3.6;// h // Solution: k1=0.693/t1; k2=.693/t2; tmax=(log(k2/k1))/(k2-k1); printf("The time when daughter activity reaches maximum is %f and this is same when activities of both are equal.",tmax)
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scenario = "WM fMRI expt"; #scenario_type = trials; scenario_type = fMRI; #scenario_type = fMRI_emulation; scan_period = 2000; pulses_per_scan = 1; pulse_code = 7; pcl_file="WMfmri.pcl"; active_buttons = 3; button_codes = 1, 2, 9; #left mouse button, right mouse button #write_codes=true; # use if sending codes out through a port default_background_color=0,0,0; default_font="arial"; default_font_size = 40; #default_text_color = 255,255,255; default_text_color=255,255,255; begin; picture { }default; bitmap {filename="WMscreenshot.bmp";} screenshot; picture{text {caption="debug"; }debug_txt; x=0; y=0;}debug_pic; picture{ bitmap screenshot; x=0; y=0; text {caption="Index finger for yes"; font_size=14; font="arial"; }instructions_txtL; x=-100; y=-100; text {caption="Middle finger for no"; font_size=14; font="arial"; }instructions_txtR; x=100; y=-100; text {caption="INSTRUCTIONS"; font_size=14; font="arial"; }instrct; x = 0; y = 100; }instructions_pic1; picture{ bitmap screenshot; x=0; y=0; text instructions_txtL; x=-100; y=-100; text instructions_txtR; x=100; y=-100; text {caption="STARTING..."; font_size=16; font="arial"; }starting; x = 0; y = 100; }instructions_pic2; ######################################################## trial{ trial_type = specific_response; trial_duration = forever; terminator_button = 3; stimulus_event{ picture instructions_pic1; }instructions_event; }instructions_trial; trial { picture instructions_pic2; code = "start_trial"; duration = 1000; mri_pulse = 1; # set for testing }start_trial; trial{ all_responses = false; # responses made in this trial will be ignored stimulus_event{ picture {text{caption = "5"; font_size = 40;} five; x = 0; y = 0;}; duration = 1000;}; stimulus_event{ picture {text{caption = "4"; font_size = 40;} four; x = 0; y = 0;}; deltat = 1000; duration = 1000;}; stimulus_event{ picture {text{caption = "3"; font_size = 40;} three; x = 0; y = 0;}; deltat = 1000; duration = 1000;}; stimulus_event{ picture {text{caption = "2"; font_size = 40;} two; x = 0; y = 0;}; deltat = 1000; duration = 1000;}; stimulus_event{ picture {text {caption = "1"; font_size = 40;} one; x = 0; y = 0;}; deltat = 1000; duration = 1000;}; }countdown_trial; trial{ # stimulus_event{ # picture {text{caption="+";}iti_txt; x=0; y=0; }fixn_pic; # duration=500; # code="fixn"; # }fixn_event; stimulus_event{ picture {text{caption="DEBUG";}encode_txt; x=0; y=0; }encode_pic; #deltat=500; duration=4000; code="encode"; }encode_event; stimulus_event{ picture {text{caption=" ";}delay_txt; x=0; y=0; }delay_pic; deltat=4000; duration=4000; # will be set in pcl to be 0 or 4 sec code="delay"; }delay_event; stimulus_event{ picture {text{caption="A";}probe_txt; x=0; y=0; }probe_pic; deltat=4000; duration=2000; code="probe"; }probe_event; stimulus_event{ picture {text{caption="*";}iti_txt; x=0; y=0; }iti_pic; deltat=2000; duration=2000; # will be set in pcl to be 2, 4, 6, or 12 sec code="iti"; }iti_event; }wm_trial; trial{ stimulus_event{ picture default; duration=27000; code="rest_break_blankscreen"; }rest_blank_event; }rest_break_blank; trial { all_responses = false; # responses made in this trial will be ignored picture {text{caption = "Thank you. Please remember to stay still until the scanner stops.";}; x = 0; y = 0;}finished; code = "thanks"; duration = 10000; }end_trial;
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//Ex 3.3 clc;clear;close; G=-10;//Gain Ri=100;//kohm(input resistance) R1=Ri;//kohm R2=-G*R1;//kohm disp(R1,"Value of R1(kohm)"); disp(R2/1000,"Value of R2(Mohm)");
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Chapter6_example2.sce
clc clear //Input data n=181*10^-6//Coefficient of viscosity of a gas in p v=3*10^4//Average speed of molecules in cm/s d=1.2929*10^-3//Density in g/cm^3 //Calculations lemda=((3*n)/(d*v))/10^-6//Mean free path in cm*10^-6 //Output printf('Mean free path is %3.0f * 10^-6 cm',lemda)
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//Example 1.9://error clc; clear; close; v=95;//volts r=40;//ohms i=v/r;//amperes err=-0.2;//error in resistance err1=(err/r)*100;//percentage error evv=0.95;//error in voltage evv1=(evv/v)*100;//percentage error x=evv1-err1;// ei=(x/100)*i;// disp(i,"current in the circuit is,(A)=") disp(ei,"error in current is,(A)=") disp(x,"percentage error in current is,(%)=")
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//chapter 17 //example 17.1 //page 518 clear; clc ; //given //dc load line Vcc=13;//supply voltage R1=4.7;R2=3.7;RE=1; Rpy=40; N1=74;N2=14; Rl=56; //plot point A(Vce,Ic)=(Vcc,0) VB=Vcc*R2/(R1+R2); VE=VB; VBE=VB-0.7; IE=VE/RE; IC=IE; VCE=Vcc-IC*(Rpy+RE);//plot point Q(VCE,IC)=(8,5) VCE=[13,8]; IC=[0,5]; plot(VCE,IC) xtitle('dc load line','VCE in V','IC in mA') //ac load line Rl'==(N1/N2)^2*Rl; //total ac load Rlac=(Rpy+Rl')/1000; deltaIC=5; deltaVCE=deltaIC*Rlac; //point B(VCE,IC)=(16,0) VCE=[8,16]; IC=[5,0]; figure,plot(VCE,IC,'r-.'); xtitle('ac load line','VCE in V','IC in mA')
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example13.sce
clc clear //input data b2=10//Rotor blade air angle at exit in degree Dt=0.6//The tip diameter in m Dh=0.3//The hub diameter in m N=960//The speed of the fan in rpm P=1//Power required by the fan in kW pi=0.245//The flow coefficient P1=1.02//The inlet pressure in bar T1=316//The inlet temperature in K R=287//The universal gas constant in J/kg.K Cp=1.005//The specific heat of air at constant pressure in kJ/kg.K r=1.4//The ratio of specific heats of air g=9.81//Acceleration due to gravity in m/s^2 //calculations A=(3.141/4)*((Dt^2)-(Dh^2))//Area of the fan at inlet in m^2 Dm=(Dt+Dh)/2//The mean rotor diameter in m U=(3.141*Dm*N)/60//The mean blade speed in m/s Ca=pi*U//The axial velocity in m/s Q=A*Ca//The flow rate of air in m^3/s d=(P1*10^5)/(R*T1)//Density of air in kg/m^3 dPst=((d*(U^2)*(1-((pi*tand(b2))^2)))/2)*((10^5)/(g*(10^3)))*10^-5//Static pressure across the stage in m W.G Wm=U*(U-(Ca*tand(b2)))//Work done per unit mass in J/kg m=d*Q//Mass flow rate in kg/s W=m*Wm//Work done in W no=W/(P*10^3)//Overall efficiency //output printf('(a)THe flow rate is %3.3f m^3/s\n(b)Static pressure rise across the stage is %3.3f m W.G\n(c)The overall efficiency is %3.4f',Q,dPst,no)
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Ex9_7.sce
//EX9_7 PG-9.21 clc C=1000e-12; C1=C; C2=C; f=500e3; Ceq=(C1*C2)/(C1+C2); L=1/(4*%pi^2*f^2*Ceq);//since f=1/(2*%pi*sqrt(L*Ceq)); L=L*1e6; printf("\n Therefore L=%.3f micro H \n",L)
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4_12.sce
clear; clc; close; Re = 1.2*10^(3); Rc = 4.7*10^(3); Rb = 250*10^(3); Vcc = 10; Vbe = 0.7; Beta = 135; Ib = (Vcc - Vbe)/(Rb + (Beta)*(Re+Rc)); Icq = Beta*Ib; Vceq = Vcc - Icq*(Rc+Re); disp(Icq,'Value of Icq(Amperes) is : '); disp(Vceq,'Value of Vceq(Volts) : ');
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Ex46.sce
//Ex:46 clc; clear; close; p_ts=10*log(20)/log(10);//saturated transponder power in dbw b=2;//back_off in db p_b=p_ts-b;//power becomes with back_off in db p_B=floor(p_b); P_b=10^(p_B/10);//Power becomes with back_off n_c=P_b/1;//no. of channels n_cs=floor(n_c); printf("The max no. of VSAT channels=%f",n_cs);
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Ex3_1.sce
clc; clear all; //chapter 3 //page no 75 //example 3.1 A=1 //arbitrary value provided T=10 //T represents tau (arbitrary value provided) //plot for non periodic pulse t=-2*T:.001:2*T; vt=[zeros(-2*T:.001:-T/2) A*ones(-T/2+.001:.001:T/2-.001) zeros(T/2:.001:2*T)] clf subplot(211) plot2d(t,vt,[2],rect=[-2*T,0,2*T,A+1]) xtitle('(a) Non periodic pulse','t','v(t)') //plot for amplitude spectum f=-4/T:.001:4/T; Vf=[] for i=1:length(f) if f(i)==0 then Vf=[Vf A*T]; //according to L'Hopitals rule sin(x)/x=1 at lim x->0 else Vf=[Vf A*T*sin(%pi*f(i)*T)/(%pi*f(i)*T)] end end subplot(212) plot2d(f,Vf,[5]) xtitle('(b) Amplitude spectrum','f','V(f)') xgrid
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Exa5_4.sce
// Exa 5.4 clc; clear; close; // given data Ton=100;//in mSEC Toff=200;//in mSEC BETA=0.2;//unitless //Let R1=1 Kohm R1=1;//in Kohm R2=R1*(1-BETA)/BETA;//in Kohm // Assuming C=10 uF C=10;//in uF R3=Ton*10^-3/(C*10^-6*0.41);//in Kohm R4=Toff*10^-3/(C*10^-6*0.41);// in Kohm disp(R1,"Value of R1 in Kohm is ; ") disp(R2,"Value of R2 in Kohm is ; ") disp(R3/1000,"Value of R3 in Kohm is ; ") disp(R4/1000,"Value of R4 in Kohm is ; ") disp(C,"Value of C in uF is ; ")
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Chapter5_Example9.sce
//Hougen O.A., Watson K.M., Ragatz R.A., 2004. Chemical process principles Part-1: Material and Energy Balances(II Edition). CBS Publishers & Distributors, New Delhi, pp 504 //Chapter-5, Illustration 9, Page 124 //Title: Estimation of dry bulb and wet bulb temperature //============================================================================= clear clc //INPUT m = [12.1 0.1 7.6 80.2]; //Composition of CO2, CO, O2, N2 in percentage //DATA FROM GRAPH //Part(a) T1 = 87; //Wet bulb temperature obtained from Fig 19, Page 120 & Fig 20, 122 //Part(b) T2 = 140; //Dry bulb temperature obtained from Fig 19, Page 120 & Fig 20, 122 //OUTPUT // Console output mprintf('\n (a) Wet bulb temperature = %2.0f degree F \n (b) Dry bulb temperature = %3.0f degree F',T1,T2); // File output fd= mopen('.\Chapter5_Example9_Output.txt','w'); mfprintf(fd,'\n (a) Wet bulb temperature = %2.0f degree F \n (b) Dry bulb temperature = %3.0f degree F',T1,T2); mclose(fd); //=========================END OF PROGRAM======================================
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EX3_13.sce
//Calculate current and power input //Chapter 3 //Example 3.13 //page 216 clear; clc; disp("Example 3.13") R1=0.21; //primary resistance in ohms X1=1; //primary reactance in ohms R2=2.72*10^(-4); //secondary resistance in ohms X2=1.3*10^(-3); //secondary reactanced in ohms V1=6600; //primary voltage in volts V2=250; //secondary voltage in volts r=V1/V2; //turns ratio Re=R1+(r^2*R2); printf("Equivalent resistance referred to primary side=%fohms",Re); Xe=X1+(r^2*X2); printf("\nEquivalent reactance referred to primary side=%fohms",Xe); Ze=sqrt(Re^2+Xe^2); printf("\nequivalent impedance reffered to primary,Ze=%fohms",Ze); V=400; //voltage in volts I1=V/Ze; printf("\nI1=%f",I1); printf("\nPower input=%fW",(I1^2*Re));
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prob1_18.sce
// Prob 1.18 clc; clear; close; format('v',6); // Given data : Poles=2;//no. of poles m=3;//no. of phase f=50;//in Hz Ep=5700;//in volt Xs=1.5;//in ohm/phase Iphase=Ep/Xs;//in Ampere IL=Iphase;//in Ampere disp(IL,"Line current in Ampere : ");
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p5.sce
function x1 = metodoJacobi(A, x0, b, eps) [m, n] = size(A) x1 = zeros(n, 1) for i = 1:n suma = 0 for j = 1:n if j <> i then suma = suma + A(i, j)*x0(j) end end x1(i) = (b(i) - suma)/A(i,i) end while (norm(x0 - x1) > eps) x0 = x1 for i = 1:n suma = 0 for j = 1:n if j <> i then suma = suma + A(i, j)*x0(j) end end x1(i) = (b(i) - suma)/A(i,i) end end endfunction function x1 = metodoGaussSeidel(A, x0, b, eps) [m, n] = size(A) x1 = zeros(n, 1) for i = 1:n suma = 0 for j = 1:n if j <> i then suma = suma + A(i, j)*x1(j) end end x1(i) = (b(i) - suma)/A(i,i) end while (norm(x0 - x1) > eps) x0 = x1 for i = 1:n suma = 0 for j = 1:n if j <> i then suma = suma + A(i, j)*x1(j) end end x1(i) = (b(i) - suma)/A(i,i) end end endfunction function x1 = metodoRelajacion(A, x0, b, w, eps) [m, n] = size(A) x1 = zeros(n, 1) for i = 1:n suma = 0 for j = 1:n if j <> i then suma = suma + A(i, j)*x1(j) end end x1(i) = (1-w) * x1(i) + w*(b(i) - suma)/A(i,i) end while (norm(x0 - x1) > eps) x0 = x1 for i = 1:n suma = 0 for j = 1:n if j <> i then suma = suma + A(i, j)*x1(j) end end x1(i) = (1-w) * x1(i) + w*(b(i) - suma)/A(i,i) end end endfunction function x1 = metodoRelajacionTridiagonal(A, x0, b, eps) [m, n] = size(A) x1 = zeros(n, 1) Tj = eye(A) - inv(diag(diag(A)))*A w = 2/(1 + sqrt(1 - (max(abs(spec(Tj))) ** 2 ))) for i = 1:n suma = 0 for j = 1:n if j <> i then suma = suma + A(i, j)*x1(j) end end x1(i) = (1-w) * x1(i) + w*(b(i) - suma)/A(i,i) end while (norm(x0 - x1) > eps) x0 = x1 for i = 1:n suma = 0 for j = 1:n if j <> i then suma = suma + A(i, j)*x1(j) end end x1(i) = (1-w) * x1(i) + w*(b(i) - suma)/A(i,i) end end endfunction
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Example_21_2.sce
//clear// clear; clc; //Example 21.2 //Given K = 273.16 T = 100+K ; //[K] P = 10; //[atm] //From Table 21.1 TcA = 198+K; //[K] TcB = -147+K; //[K] rho_cA = 0.552; //[g/cm^3] rho_cB = 0.311; //[g/cm^3] MA = 137.5; MB = 28; //Solution VcA = MA/rho_cA //[cm^3/g mol] VcB = MB/rho_cB //[cm^3/g mol] //Substituing in Eq.(21.25) Dv = (0.01498*T^1.81*(1/MA+1/MB)^0.5)/(P*(TcA*TcB)^0.1405*(VcA^0.4+VcB^0.4)^2); //[cm^2/s] disp('cm^2/s',Dv,'Volumetric Diffusivity (Dv) = ')
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Ex8_7.sce
clc; clear; Wb=0.5*10^-6 //width of base region in m Dp=15*10^-4 // in m^2/s //Calculation tau_n=Wb^2/(2*Dp) //in s tau_B=tau_n //in s fT=1/(2*%pi*tau_B) mprintf("a) upper frequency limit= %1.2e Hz",fT)
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Example4_2.sce
clear ; clc; // Example 4.2 printf('Example 4.2\n\n'); // Page no. 93 // Solution // Given // Heat capacity = 139.1 + (1.56*10^-1)Tc J/(g mol* degree C), T is in degree C // First convert Tc (Temperature in degree celsius) to TR (in degree R) to get c + dTR, where c = 139.1 + (1.56*10^-1)*(-460-32)/1.8 ; d = (1.56*10^-1)/1.8; //Now convert c +dTR to (Btu/lb mol*degree R) to get answer of form a + bTR,where a = c*(454/(1055*1.8)) ; b = d*(454/(1055*1.8)) ; printf('The required answer is %.2f + (%.2e)T Btu/(lb mol*degree R) , where T is in degree R . \n',a,b);
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Ex4_3.sce
//Exa 4.3 clc;clear;close; format('v',5); P=5;//MVA V=1000;//V speed=1500;//rpm//speed ns=speed/60;//rps f=50;//Hz pf=0.8;//Power factor Lagging Xs=20;//%//synchronous reluctance Xs=Xs/100;///p.u. disp("Part(a)"); V=1;//p.u.//on no load E=1;//p.u.//on no load Ps=V*E/Xs;//p.u. Ps=Ps*P;//MW per elect. radian Ps=Ps*1000;//kW per elect. radian //1 mech. radian=%pi/90 elect. radian Ps=Ps*%pi/90;//kW per mech. degree disp(Ps,"Synchronising power per mech. degree(kW)"); d=0.5;//degree////displacement Ts=Ps*1000*d/2/%pi/ns;//N-m format('v',6); disp(Ts,"Synchronising torque(N-m)"); disp("Part(b)"); theta=acosd(pf);//degree E=V+(cosd(theta)-%i*sind(theta))*%i*Xs;//p.u. Ps=V*E/Xs;//p.u. Ps=Ps*P;//MW per elect. radian Ps=Ps*1000;//kW per elect. radian //1 mech. radian=%pi/90 elect. radian Ps=Ps*%pi/90;//kW per mech. degree Ps=abs(Ps);//kW per mech. degree disp(Ps,"Synchronising power per mech. degree(kW)"); d=0.5;//degree////displacement Ts=abs(Ps)*1000*d/2/%pi/ns;//N-m disp(Ts,"Synchronising torque(N-m)"); //Answer in the textbook is not accurate.
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Ex5_5.sce
//pagenumber 288 example 5 clear av=12480; fedbac=8;//decibel volgai=20*log10(av);//gain without fedback volga1=volgai-fedbac; beta1=((av/5000)-1)/av; disp("voltage gain with fedback = "+string((volga1))+"decibel"); disp("beta = "+string((beta1)));
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//Example 10.15 m=50*10^-3;//Mass of the disc (kg) v=30;//Initial velocity of the disc (m/s) M=2;//Mass of the stick (kg) r=1.2;//Length of the stick (m) I_prime=(m+M/3)*r^2;//Moment of inertia of the stick and disc stuck together, See Equation 10.128 (kg.m^2) omega_prime=m*v*r/I_prime;//Angular velocity (rad/s) printf('a.Angular velocity of the two (stick and disc) after collision = %0.2f rad/s',omega_prime) KE=(1/2)*m*v^2;//Initial kinetic energy (translational) (J) printf('\nb.Initial kinetic energy = %0.1f J',KE) KE_prime=(1/2)*I_prime*omega_prime^2;//Final kinetic energy (rotational) (J) printf('\n Final kinetic energy = %0.2f J',KE_prime) p=m*v;//Linear momentum before collision (kg.m/s) printf('\nc.Total linear momentum before collision = %0.2f kg.m/s',p) v_prime=r*omega_prime;//New velocity of the disk (m/s) p_prime=(m+M/2)*v_prime;//Linear momentum after collision (kg.m/s) printf('\n Total linear momentum after collision = %0.2f kg.m/s',p_prime) //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest
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void main () { int i = 1 ; print ("i " , i , "\n"); }
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// Problema 2 function [x, ea, iter] = GaussSeidelR(A,b,lambda,es,maxit) //GaussSeidel: Gauss Seidel method //x = GaussSeidel(A,b): Gauss Seidel without relaxation //input: //A = coefficient matrix //b = right hand side vector //es = stop criterion (default = 0.00001%) //maxit = max iterations (default = 50) //output: //x = solution vector //mode(2) if argn(2)<2,error('at least 2 input arguments required'),end if argn(2)<5|isempty(maxit),maxit=50;end if argn(2)<4|isempty(es),es=0.00001;end if argn(2)<3|isempty(lambda),lambda=1;end [m,n] = size(A); if m~=n, error('Matrix A must be square'); end C = A; for i = 1:n C(i,i) = 0; x(i) = 0; end for i = 1:n C(i,1:n) = C(i,1:n)/A(i,i); end for i = 1:n d(i) = b(i)/A(i,i); end iter = 0; while (1) xold = x; for i = 1:n xoldi = x(i); x(i) = d(i)-C(i,:)*x; x(i) = lambda*x(i) + (1-lambda)*xoldi; if x(i) ~= 0 ea(i) = abs((x(i) - xold(i))/x(i)) * 100; end end iter = iter+1; if max(ea)<=es | iter >= maxit, break, end end endfunction ///////////////////////////////////////////////////////// // A = [10 -2;-3 12] // b = [8 9]'; // lambda = 1.2 // [x, ea, iter] = GaussSeidelR(A,b,lambda,0.0001,50) ///////////////////////////////////////////////////////// // A = [0.8 -0.4 0; -0.4 0.8 -0.4; 0 -0.4 0.8] // b = [41 25 105]' // lambda = 1.2 // [x, ea, iter] = GaussSeidelR(A,b,lambda,0.0001,50)
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// convert into norton circuit // Electronic Principles // By Albert Malvino , David Bates // Seventh Edition // The McGraw-Hill Companies // Example 1-6, page 19 clear;clc; close; // Given data Vth=10;// Thevenin voltage in volts Rth=2000;// Thevenin resistance in ohms // Calculations In=Vth/Rth;// Norton current in amperes disp("Amperes",In,"Norton Current=") // Result // Norton current is 5 milliAmperes
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// Exa 2.25 format('v',7);clc;clear;close; // Given data Wrange= 500;//wattmeter range in W del_A= 1.5*Wrange/100;//limiting error at full scale in W P= 50;//power in W Pmin= P-del_A;// minimum power in W Pmax= P+del_A;// maximum power in W disp("The range of the reading is : "+string(Pmin)+" watts to "+string(Pmax)+" watts");
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clc;clear; //Example 13.7 //calculation of uncertainty in position //1)given values h=6.626*10^-34;//Planck's constant in Js v1=220;//velocity of e in m/s m=9.1*10^-31;//mass of e in kg A=0.065/100;//accuracy //1)calculation v2=v1*A;//uncertainty in speed x1=h/(2*%pi*m*v2);// disp(x1,'uncertainty in position of e (in m)is'); //2)given values m1=150/1000;//mass of object in kg x2=h/(2*%pi*m1*v2); disp(x2,'uncertainty in position of baseball(in m) is');
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clc //Initialization of variables L=50 Fm=0.02 //N Vm=1 //m/s //calculations Fp=L^3 *Fm Fp=Fp*0.2248 Vp=sqrt(L) *Vm Vp=Vp*3.28 Hp=Fp*Vp/550 //results printf("Required horsepower = %.1f hp",Hp)
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function[] = realimentador(A, B, C, polos) U = zeros(length(polos), length(polos)); for i=1:length(polos), U(:,i) = (A^(i-1))*B; end printf("Matriz U/Wc ------------------------\n"); disp(U); if(rank(U) == size(U, 'r')) then printf("\nSistema é controlável\n"); else halt("\nSistema NÃO é controlável \n"); end delta = poly(polos, 't'); printf("\nDelta ------------------------\n"); disp(delta); qc = zeros(length(polos), length(polos)); for i=0:length(polos), qc = qc+(A^i)*coeff(delta, i); end printf("\nMatriz qc(A)/qc(G)---------------------\n"); disp(qc); U_1 = inv(U); printf("\nMatriz U^(-1)/Wc^(-1)---------------------\n"); disp(U_1); t = zeros(1, length(polos)); t(1, $) = 1; K = -t*U_1*qc; printf("\nK---------------------\n"); disp(K); endfunction //Se function[] = sr_d(G, H, C, polos) Ga = zeros(size(G, 'r')+1, size(G,'c')+size(H, 'c')); Ga(1:$-1, 1:size(G,'c')) = G; Ga(1:$-1, size(G, 'c')+1:$) = H; Ha = zeros(size(Ga, 'r'), 1); Ha($, 1) = 1; printf("Matriz Ga -------------------------- \n"); disp(Ga); printf("\nMatriz Ha -------------------------- \n"); disp(Ha); Wc = zeros(length(Ha), length(Ha)); for i=1:length(Ha), Wc(:, i) = (Ga^(i-1))*Ha; end printf("\nMatrix Wc ------------------------ \n"); disp(Wc); if(rank(Wc) == length(Ha)) then printf("\nRank cheio \n"); else halt("\nNão tem Rank cheio \n"); end printf("\nPolinomio delta -------------------- \n"); delta = poly(polos, 'G'); disp(delta); qc = zeros(size(Ga, 'r'), size(Ga, 'c')); coeficientes = coeff(delta); for i=1:length(coeficientes), qc = qc + (Ga^(i-1))*coeficientes(i); end printf("\nqc(Ga) ------------------------- \n"); disp(qc); printf("\nWc inversa ---------------------- \n"); disp(inv(Wc)); m = zeros(1, size(qc, 'c')); m($) = 1; ka = m*inv(Wc)*qc; printf("\nKa ------------------ \n"); disp(ka); t1 = [G-eye(size(G, 'r'), size(G, 'r')) H; C*G C*H]; t2 = zeros(1, length(ka)); t2(1, $) = 1; k = (ka+t2)*inv(t1); printf("\nK ------------------ \n"); disp(k); endfunction
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// Scilab Code Ex3c.7: Page-185 (2008) clc; clear; D = 1.2; // Distance between the source and the slit, m d = 7.5e-004; // Separation between the two slits, cm n = 20; // Number of fringes crossed in the field of view bita = 1.888e-002/n; // Fringe width, cm lambda = bita*d/D; // Wavelength of light, cm printf("\nThe wavelength of the light used in biprism experiment = %4d angstrom", lambda/1e-010); // Result // The wavelength of the light used in biprism experiment = 5900 angstrom
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//Example 2-16, page No-49 clear clc fr=28*10^6 Q=70 bandwidth = fr/Q printf('The bandwidth is %.3f Khz',bandwidth/10^3)
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clc; warning('off'); printf("\n\n example2.3 - pg30"); // given tauyx=-0.003; //[N/m^2] - momentum flux dely=0.1; //[m] - distance between two parralel plates mu=0.01; //[kg/m*sec] - viscosity // using the formula tauyx=F/A=-mu*(delUx/dely) delUx=-((tauyx*dely)/mu)*100; printf("\n\n Velocity of the top plate is \n deltaUx=%fcm/sec",delUx);
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//Chapter7,Pg7.4,Ex7.2 clc; Bdc=90 // Ic=15 //Collector current Ib=Ic/Bdc printf("\n Ib=%.2f uA \n",Ib*10^3) Ie=Ib+Ic printf("\n Emitter current Ie=%.2f mA \n",Ie) Adc=Bdc/(Bdc+1) printf("\n Adc=%.2f \n",Adc)
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Chapter12_Example6.sce
clc clear //INPUT d=0.35;//diameter of the mirror in m t=5;//time in min T=16;//temperature of water found to be in deg.C m=60;//mass of water in gm mc=30;//mass of calorimeter in gm cp=0.1;//specific heat of copper in cal/gm/deg.C //CALCULATIONS q=(m+cp*mc)*T*4/(5*3.14*d^2);//amount of heat received by earth in cal //OUTPUT mprintf('amount of heat received by earth is %3.2f cal',q)
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clc //initialisation of variables h1= 3892.2 //kJ/kg h2= 4102.2 //kJ/kg dh= 1015.4 //kJ/kg dh1= 448 //kJ/kg h3= 2151.1 //kJ/kg h4= 3081.1 //kJ/kg //RESULTS printf (' Specific Enthalpy= %.1f kJ/kg',h1) printf (' \n Specific Enthalpy= %.1f kJ/kg',h2) printf (' \n Specific Enthalpy= %.1f kJ/kg',h3) printf (' \n Specific Enthalpy= %.1f kJ/kg',h4) printf (' \n Enthalpy difference= %.f kJ/kg',dh) printf (' \n Enthalpy difference= %.f kJ/kg',dh1)
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// Example1.3. A coil consists of 2000 turns of copper wire having a cross sectional area of 0.8 mm^2. The mean length per turn is 80 cm and resistivity of copper is 0.02 micro-ohm- metre. Find the resistance of the coil and power absorbed by the coil when connected across 110 V d.c. supply. //1 millimetre = 10^-3 metre // 1 micro-ohm = 10^-6 ohms N = 2000; // number of turns A = 0.8*10^-6;// crossectional area (m^2) l = 80*10^-2;// mean length(m) p = 0.02*10^-6;// resistivity (ohm-m) V = 110; // supply voltage(V) // Let R ohms be the resistance of the coil and P watts be the power absorbed // FORMULAE: R=p*L/A , where L is the length of the coil ; P= V^2/R L= prod([l,N]);// length of the coil(m) R =prod([p,L])/A;// calculation of resisrance (ohms) P = (V^2)/R;// power absorbed by the coil (Watts) disp(R,"resistance of the coil (in ohms)= ") disp(P,"power absorbed by the coil(in watts)=")
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//Chemical Engineering Thermodynamics //Chapter 13 //Thermodynamics in Phase Equilibria //Example 13.15 clear; clc; //Given T = [146.2 142.3 126.1 115.9 95.0 98.0 100];//Temperature in deg cel P1 = [760.0 685.0 450.3 313.0];//Vapour pressure of 1,1,2,2-tetrachloroethane at the coressponding temperature in mm Hg P2_5 = 648.0;//Vapour pressure of water at 95 deg cel in mm Hg P2_6 = 711.0;//Vapour pressure of water at 98 deg cel in mm Hg P = 760;//Total pressure of mixture in mm Hg x1 = [0 0 0 0 0 0 0]; //To plot a graph between temperature and vapour phase composition for i = 1:4 x1(i) = P1(i)/P;//mole fraction of 1,1,2,2-tetrachloroethane end x2_5 = P2_5/P;//mole fraction of water at 95 deg cel x2_6 = P2_6/P;//mole fraction of water at 98 deg cel x1(5) = 1-x2_5; x1(6) = 1-x2_6; clf; plot(x1,T); xtitle("","mole fraction of 1,1,2,2-tetrachloroethane","Temperature in deg cel"); mprintf('The required graph has been ploted in the graphic window'); //end
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// Implementation of example 7.2 // Basic and Applied Thermodynamics by P.K.Nag clc clear // T for temperature,m for mass,S for entropy,dS is change in entropy t1=273 // K t2=373 // K m=1 // kg c=4.187 // (a) dSw=m*c*log(t2/t1); // reservoir's temperature remains constant so dS=Q/T Q=m*c*(t2-t1); dSr=-(Q/t2); dSu=dSw+dSr; printf("entropy change of universe = %.3f kJ/K \n",dSu); // (b) // now water is heated in stages from two reservoirs.. t3=323 // K dSw=m*c*log(t3/t1)+m*c*log(t2/t3); dSr1=-[m*c*(t3-t1)/t3]; dSr2=-[m*c*(t2-t3)/t2]; dSu2=dSw+dSr1+dSr2; printf("entropy change of universe in 2nd case = %.3f kJ/K \n",dSu2); // the entropy change of universe would be less & less if water is heated in more & more stages...it will be zero if water is heated reversibly... // end
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clc; v1=10; // voltage applied to primary when secondary is short circuited ip=60; // primary current when secondary is short circuited k=0.8; // turns ratio E1=250; // input voltage for load voltage has to be calculated E2=200; // rated voltage of secondary il=100; // load current pfo=0.24; // power factor during short circuit test f=(1-k)^2/k^2; // factor by which secondary impedance has to be multiplied for referring it to primary // ze1=z1+f*z2 therefore by ohm s law ze1=v1/ip; // total impedance referred to primary re1=ze1*pfo; // total resistance referred to primary xe1=ze1*sqrt(1-pfo^2); // total leakage reactance referred to primary disp('case a'); pf=0.8; // lagging power factor of load Ip=(E2*il)/E1; // current in primary due to load current v2=(E1-Ip*(re1*pf+xe1*sqrt(1-pf^2)))*k; printf('Secondary terminal voltage at %f lagging power factor is %f v\n',pf,v2); disp('case b') pf=1; // unity power factor v2=(E1-Ip*(re1*pf+xe1*sqrt(1-pf^2)))*k; printf('Secondary terminal voltage at unity power factor is %f v',v2);
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function [y,y1]=convol(h,x,y0) [lhs,rhs]=argn(0), n=prod(size(x)), m=prod(size(h)), m1=n+m-1; x(m1)=0;h(m1)=0; if norm(imag(x))==0&norm(imag(h))==0 then y=real(fft(fft(matrix(x,1,m1),-1).*fft(matrix(h,1,m1),-1),1)), else y=fft(fft(matrix(x,1,m1),-1).*fft(matrix(h,1,m1),-1),1), end if lhs+rhs=5 then, y0(n)=0;//update carried from left to right y1=y(n+1:n+m-1); y=y(1:n)+y0; elseif lhs+rhs=4 then, if rhs=2 then, y1=y(n+1:n+m-1); y=y(1:n);//initial update else, y0(n+m-1)=0;//final update y=y(1:n+m-1)+y0; end, else, y=y(1:n+m-1);//no update end,
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// // "vib-res2.sce" // clear; clf(); load("vib_res.dat","om1","xxmax"); // vib-res.sce で保存したデータ m=1; c=0.2; k=1; P=1; zeta = c/( 2*sqrt(m*k) ); // 表3.1 omn = sqrt(k/m); // 表3.1 function y = K(Om) global zeta; y=1/sqrt((1-Om^2)^2 +(2*zeta*Om)^2); endfunction om2 = linspace(0.2,1.6,100); A = P/(m*omn^2); for i=1:100 R(i) = A*K(om2(i)/omn); end plot(om1, xxmax,"o", om2, R,"-" ); xlabel("om"); ylabel("Amplitude"); xtitle("Response Curve (o max(x); - R)"); xgrid(); g=gca(); g.data_bounds=[0.2,0;1.6,6]; xgrid(); //座標軸の設定
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ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 0.309980D+00 2 -0.179830D-02 0.283944D-02 3 -0.898948D-04 -0.237995D-04 0.213876D-02 4 0.498176D+00 -0.211740D-01 0.181332D+00 0.165172D+03 5 0.475384D+00 0.279603D-01 0.169884D+00 0.131769D+02 0.634357D+02 6 -0.430338D+00 0.345828D-01 -0.214359D+00 -0.741504D+02 -0.345789D+02 7 0.211363D-01 0.324385D-02 -0.853563D-03 0.149496D+00 -0.148024D+00 8 0.401090D-02 0.269219D-03 -0.206836D-03 0.261971D-01 0.618253D-02 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 ________ ________ ________ 6 0.318120D+03 7 0.295132D+01 0.364494D+00 8 -0.141413D+01 -0.338507D-01 0.137069D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.061 1.000 3 -0.003 -0.010 1.000 4 0.070 -0.031 0.305 1.000 5 0.107 0.066 0.461 0.129 1.000 6 -0.043 0.036 -0.260 -0.323 -0.243 7 0.063 0.101 -0.031 0.019 -0.031 8 0.062 0.043 -0.038 0.017 0.007 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 ________ ________ ________ 6 1.000 7 0.274 1.000 8 -0.677 -0.479 1.000
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function y =fa(x) y = -481 +408 +589.64 * x + (-2349.163 * x^2)/2 endfunction a = 0 b = 0.3 x= a contador = 0 while(1) xOld = x; x= (a+b)/2; Er = abs((x-xOld)/x) contador = contador + 1 if (Er < 10^-4) then break end if(fa(a)*fa(x) < 0) b= x else a=x end end
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clear all; clc; disp("Scilab Code Ex 13.12 : ") //Given: L = 1600; //mm K = 2; l = 80; //mm b = 40; //mm e = 20; //mm c = 40; //mm //Calculations: I1 = (1/12)*(l*b^3); A = l*b; r = sqrt(I1/A); sl_ratio = (K*L)/(r); //Eqn 13.26: sigma_allow = (378125)/(sl_ratio^2); I2 = (1/12)*(b*l^3); coefficient = (1/A) + (e*c)/I2; sigma_max = sigma_allow; P = sigma_max/coefficient; P = P/1000; //Display: printf('\n\nThe load that can be supported if the column is fixed at its base = %1.2f kN',P); //------------------------------------------------------------------------END-----------------------------------------------------------------------------------
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load Larc.hdl, set RAM16K[0] %X8101, // 1. li R1 1 R1 <-- 1 set RAM16K[1] %X8202, // 2. li R2 2 R2 <-- 2 set RAM16K[2] %X9FFF, // 3. lui R15 -1 R15 <-- -256 set RAM16K[3] %X0312, // 4. add R3 R1 R2 R3 <-- 3 set RAM16K[4] %X141F, // 5. sub R4 R1 R15 R4 <-- 257 set RAM16K[5] %X6512, // 6. nor R5 R1 R2 R5 <-- -4 set RAM16K[6] %X7612, // 7. slt R6 R1 R2 R6 <-- 1 set RAM16K[7] %X7621, // 8. slt R6 R2 R1 R6 <-- 0 set RAM16K[8] %X7F22, // 9. slt R15 R2 R2 R15 <-- 0 set RAM16K[9] %XF000 // 10. halt ; repeat 100 { tick, tock; }
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// Example 7.6, page no-272 clear clc L=1.778 //Loss factor of the feeder 2.5dB equivalent ts=30 //Noise temperature of sattelite receiver in K t=50 //Noise temperature in K ti=290 // reference temperature in K x=t/L y=ti*(L-1)/L Te=x+y+ts F1=1+(ts/ti) F2=1+(Te/ti) printf("contribution of antenna noise temperature when\n referred to the input of the receiver is %.1f K",x) printf("\n\n Contribution of feeder noise when referred to the\n input of the receiver is %.1f",y) printf("\n\n1. Noise figure in first case = %.3f = %.3f dB",F1,10*log10(F1))//answer in book is different 0.426dB printf("\n\n2. Noise figure in second case = %.3f = %.2f dB",F2,10*log10(F2))
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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 13.3w //calculation of the height of the water coloumn //given data h1=2*10^-2//difference in the height(in m) s=13.6//specific gravity of mercury //calculation //P = P0 + (h*rho*g)........using this equation h=h1*s//height of the water coloumn printf('the height of the water coloumn is %d cm',h*10^2)
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errcatch(-1,"stop");mode(2);//Example 4.16 (b) //Program to Evaluate and Compare the 8-point DFT of the given Sequence //x2[n]=1, 0<=n<=6 using DIT-FFT Algorithm. ; ; ; x2=[1,1,1,1,1,1,1,0]; //FFT Computation X2 = fft (x2 , -1); disp(X2,'X2(k) = '); exit();
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clear ; clc; // Example 10.6 printf('Example 10.6\n\n'); // Page no. 281 // Solution // Basis: P=100 // Product from the reactor-[g mol] P=100 ;//Product from the reactor-[g mol] // Composition of product C3H8 = 0.195*P ;// [g mol] C4H10 = 0.594*P ;// [g mol] C5H12 = 0.211*P;// [g mol] n_un = 3 ;// Number of unknowns in the given problem(excluding extent of reaction) n_ie = 3 ;// 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',d_o_f); C = C3H8*3+C4H10*4+C5H12*5 ;// moles of C on product side H = C3H8*8+C4H10*10+C5H12*12 ;// moles of H on product side // Solve following eqn.( obtained by element balance of C & H) for F and G //8F+0G = C //18F+2G = H a = [8 0;18 2] ;// matrix formed by coefficients of unknowns b = [C;H] ;//matrix formed by constant x = a\b ;// matrix of solution R = x(2)/x(1) ;// Ratio of H2 consumed to C8H18 reacted = G/F printf(' Molar ratio of H2 consumed to C8H18 reacted is %.3f \n',R);
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clc(); clear; // To calculate the relaxation time of conduction electrons rho=1.54*10^-8; //resistivity in ohm-m n=5.8*10^28; //electron/m^3 m=9.108*10^-31; //mass in kg e=1.602*10^-19; //charge in coulomb tow=m/(n*(e^2)*rho); printf("relaxation time of conduction electrons in sec is"); disp(tow);
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//debug clc; V1=420; //supply voltage r1=2.95; x1=6.82; r2=2.08; x2=4.11; Iml=6.7; //magnetizing line current Pw=269; //core loss s=0.03; //slip P=12; f=50; N=(120*f)/P; Ns=(120*f)/P; Im=Iml/sqrt(3); //V1=E1+Im(r1+jx1) //Above equation on solving gives the solution as E1*E1+52.8E1-175572.65 Q=[1 52.8 -175572.62]; R=roots(Q); E1=R(2); Xm=E1/Im; //As per the circuit diagram a=r2/s; Zf=(((r2/s)+x2*%i)*Xm*%i)/((r2/s)+((x2+Xm)*%i)); Rf=real(Zf); Zab=complex((real(Zf)+r1),(imag(Zf)+x1)); I1=420/Zab; I1M=sqrt((real(I1)*real(I1))+(imag(I1)*imag(I1))); an1=atand(imag(I1),real(I1)); pf=cosd(atand(imag(I1)/real(I1))); I2=I1*(Xm*%i)*(1/((r2/s)+((x2+Xm)*%i))); an2=atand(imag(I2),real(I2)); I2M=sqrt((real(I2)*real(I2))+(imag(I2)*imag(I2))); T=3*(60/(2*%pi*N))*I1M*I1M*Rf; mprintf('The power factor is %f Lag\n The input current is %f A lagging by an angle of %f degrees \n The output rotor current is %f A lagging by an angle of %f degrees \n The Torque developed is %f Nm \n',pf,I1M,-an1,I2M,-an2,T); //For maximun Torque X1=x1+Xm; Re=(r1*Xm)/X1; Xe=(x1*Xm)/X1; smT=r2/(sqrt((Re)*(Re)+(x2+Xe)*(x2+Xe))); Nm=Ns*(1-smT); Tem=3*(E1)*(E1)*(1/(Re+(sqrt((Re)*(Re)+(x2+Xe)*(x2+Xe)))))*(1/2)*(1/(2*%pi*(N/60))); mprintf('maximum torque developed is %f Nm \n corresponding speed is %f rpm',Tem,Nm);
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/tests/test_diff_3_i.tst
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test_diff_3_i.tst
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FOSSEE/Scilab-TBC-Uploads
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Ex4_25.sce
// Calculating the amount of oil and amount of water clc; disp('Example 4.25, Page No. = 4.51') // Given Data MVA = 40;// MVA rating of transformer Q = 200;// Total losses (in kW) Q_oil = 0.8*Q;// Since 20% of losses are dissipated by tank walls Heat taken up by oil (in kW) // Calculation of the amount of oil T = 20;// Temperature rise of oil (in degree celsius) cp = 0.4;// by assuming Vo = 0.24*Q_oil/(cp*T);// Amount of oil (in litre per second) disp(Vo,'Amount of oil (litre per second)='); // Calculation of the amount of water T = 10;// Temperature rise of water (in degree celsius) Vw = 0.24*Q_oil/T;// Amount of water (in litre per second) disp(Vw,'Amount of water (litre per second)='); //in book Vo is equal to 4.8 (litre per second) and Vw is equal to 3.84 (litre per second). The answers vary due to round off error
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8_4.sce
//All the quantities are expressed in SI units M = 2.79; //Mach number T = 320; //static temperature from ex. 7.3 p = 1; //static pressure in atm gam = 1.4; //from eq. (8.40) T0 = T*(1+((gam-1)/2*M*M)); //from eq. (8.42) p0 = p*((1+((gam-1)/2*M*M))^(gam/(gam-1))); printf("\nRESULTS\n---------\nThe total temperature and pressure are:\n T0 = %3.0f K\n P0 = %2.1f atm\n",T0,p0)
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Ahmad6543/Scenarios
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sce
Colosseum Aimbotz.sce
Name=Colosseum Aimbotz PlayerCharacters=Roman BotCharacters=Barbarian.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Roman AddedBots=Barbarian.bot;Barbarian.bot;Barbarian.bot;Barbarian.bot;Barbarian.bot;Barbarian.bot;Barbarian.bot;Barbarian.bot PlayerMaxLives=0 BotMaxLives=0;0;0;0;0;0;0;0 PlayerTeam=2 BotTeams=1;1;1;1;1;1;1;1 MapName=colopit.map MapScale=6.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=true TimeRefilledByKill=0.0 ScoreToWin=10.0 ScorePerDamage=0.0 ScorePerKill=1.0 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=Target Switch, Flick, Apex, Overwatch, ADS WeaponHeroTag=Pistol, Deagle, McCree DifficultyTag=1 AuthorsTag=PPV, Sn0wFly BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=false Description=Relentless waves of bots assault your position. Kill as many as you can! GameVersion=1.0.7.2 ScorePerDistance=0.0 [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=Barbarian DodgeProfileNames=Long Strafe FB;Long Strafe;Rushdown;Straight Rushdown DodgeProfileWeights=5.0;3.0;15.0;6.0 DodgeProfileMaxChangeTime=1.5 DodgeProfileMinChangeTime=0.9 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Barbarian SeeThroughWalls=true NoDodging=false NoAiming=false [Character Profile] Name=Roman MaxHealth=300.0 WeaponProfileNames=Almost-Six Shooter;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=0.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 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=160.0 MainBBRadius=58.0 MainBBHasHead=true MainBBHeadRadius=40.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=160.0 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=3.0 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=20.0 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=Barbarian MaxHealth=300.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.3 MaxRespawnDelay=5.0 StepUpHeight=5.0 CrouchHeightModifier=0.69 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=20.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=600.0 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=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=0.584 Z=0.004 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=160.0 MainBBRadius=32.0 MainBBHasHead=true MainBBHeadRadius=32.0 MainBBHeadOffset=-30.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=160.0 ProjBBRadius=32.0 ProjBBHasHead=true ProjBBHeadRadius=32.0 ProjBBHeadOffset=-30.0 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=300.0 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=-150.0 [Dodge Profile] Name=Long Strafe FB MaxTargetDistance=800.0 MinTargetDistance=60.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.5 MaxLRTimeChange=0.6 MinFBTimeChange=0.5 MaxFBTimeChange=0.8 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.02 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=0.25 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Long Strafe MaxTargetDistance=800.0 MinTargetDistance=60.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.5 MaxLRTimeChange=0.9 MinFBTimeChange=0.8 MaxFBTimeChange=1.0 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.15 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=0.25 BlockedMovementPercent=0.8 BlockedMovementReactionMin=0.05 BlockedMovementReactionMax=0.1 [Dodge Profile] Name=Rushdown MaxTargetDistance=100.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.2 MaxLRTimeChange=0.6 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.06 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=0.25 BlockedMovementPercent=0.8 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Straight Rushdown MaxTargetDistance=100.0 MinTargetDistance=0.0 ToggleLeftRight=false ToggleForwardBack=true MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.3 MaxFBTimeChange=0.6 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.1 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=0.25 BlockedMovementPercent=0.8 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Almost-Six Shooter Type=Hitscan ShotsPerClick=1 DamagePerShot=200.0 KnockbackFactor=4.0 TimeBetweenShots=0.2 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=7 AmmoPerShot=1 ReloadTimeFromEmpty=1.5 ReloadTimeFromPartial=1.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.00001 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 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=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.2 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=7 CancelReloadOnKill=true FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=103.0 ADSFOVScale=Clamped Horizontal 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=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 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=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Map Data] reflex map version 8 global entity 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clc clear //input c=4*(10^-6);//capacitance of a capacitor by which a resistive-inductive load is shunted in farad v=2;//supply voltage in volts f=5000;//supply frequency in hertz q=10;//Q factor of the circuit //calculations vwc=2*2*%pi*f*c;//capacitor current in amperes it=vwc/q;//total current in amperes i1=((vwc^2)+(it^2))^0.5;//load current in amperes z1=v/i1;//load impedance in ohms r1=z1*(it/i1);//resistance of load in ohms x1=q*r1;//reactance of load in ohms l=(x1*(10^6))/(2*%pi*f);//load inductance in microhenry //output mprintf('the load has a resistance of %3.3f ohms and an inductance of %3.0f microhenry',r1,l)
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//program to solve differential equation using euler's method function []=euler(x0,y0,xn,h) deff('y1=f(x,y)','y1=(y-x)/(y+x)') y1=y0+(h)*f(x0,y0) x0=x0+h y0=y1 while x0<xn y1=y0+(h)*f(x0,y0) x0=x0+h y0=y1 end disp(y1) endfunction
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//Chapter 12 : Solutions to the Exercises //Scilab 6.0.1 //Windows 10 clear; clc; //Solution for 1.18 A=[0 1;0 1] B=[-1 -1;0 0] AB=A*B disp(AB,'AB=') A2=A^2 disp(A2,'A^2=') B2=B^2 disp(B2,'B^2=') AB2=(A+B)^2 disp(AB2,'(A+B)^2=') e1=A2+2*AB+B2 disp(e1,'A2+2*AB+B2=') e2=(A+B)*((A+B)^2) disp(e2,'(A+B)*((A+B)^2)=') e3=(A^3)+(3*(A^2)*B)+(3*A*(B^2))+(B^3) disp(e3,'A^3+3*A^2*B+3*A+B^2+B^3=')
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clc; m=30; // mass flow rate in kg/s N=15000; // Speed in rpm r2=0.3; // Radius in m D2=r2*2; // Diameter in m w2=100; // Relative velocity in m/s beta_1=80; // in degrees p01=1; // Inlet pressure in bar T01=300 // Inlet temperature in kelvin Cp=1.005; // specific heat at constant pressure in kJ/kg K r=1.4; // Specific heat ratio R=287; // Characteristic gas constant in J/kg K u2=3.14*D2*N/60; ct2=u2-(w2*cosd (beta_1)); Fr=m*ct2*r2; P=Fr*(2*3.14*N/60); W=u2*ct2; P02=p01*(1+(W*10^-3/(Cp*T01)))^(r/(r-1)); disp ("Nm",Fr,"Torque = "); disp ("kW",P/1000,"Power = "); disp ("bar",P02,"Head Developed = ");
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clc //initialisation of variables Dp= 1 //in Dr= 10 //in R= 12 W= 15 //tons //CALCULATIONS Ar= %pi*Dr^2/4 Ap= %pi*Dp^2/4 P= W*2240/((Ar/Ap)*R) //RESULTS printf ('power applied to lever = %.f lbs',P)
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// 6.5 clc; R=10*10^3; Ri=100*10^3; Rt=100*10^3; Rp=(Ri*R)/(Ri+R); Attenuation=Rp/Rt; Attenuation_factor=1/Attenuation; printf("\nAttenuation factor=%.1f ",Attenuation_factor)
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clc //to calculate strength of solution theta=11 //degree l=20 //length in cm alpha=66 //specific rotation of sugar in degree c=10*theta/(l*alpha) disp("strength of solution is c="+string(c)+"gm/cm^3")
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errcatch(-1,"stop");mode(2);//Chapter 8, Problem 7 ; Q=1.6*10^-19; //charge in coulombs v=3*10^7; //velocity of charge B=18.5*10^-6; //flux density F=Q*v*B; //Calculating force printf("Force = %f x10^−17 N",F*10^17); exit();
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//Exam:3.27 clc; clear; close; //Miller indices of plane h=1; k=1; l=1; wavelength=0.54;//in angstrom a=3.57;//size of a cube n=1; d_111=a/(h^2+k^2+l^2)^(1/2);//interplanar spacing(in Angstrom) angle=asind(n*wavelength/(2*d_111)); disp(angle,'Bragg angle(in degree)=');
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//Example 1.7 clc; clear; close; t =0:0.01:10 F=1000; x=sin(2*%pi*F*t); P={integrate('(sin(2*180*F*t)^2)','t',-0.001,+0.001)}/(2*1/F); disp(P,"Power of signal= "); disp("Since the given signal has a finite power, it is a POWER signal");
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//Scilab Code for Example 1.7 of Signals and systems by //P.Ramakrishna Rao clear; clc; n=1; for t=-10:0.1:10; //Function for Even signal y1(n)=0.5*(exp(-t)*u(t)+exp(t)*u(-t)); n=n+1; end a=gca(); a.x_location="origin"; a.y_location="origin"; t=-10:0.1:10; //Plot of Even Signal plot(t,y1); title('y1(t)'); xlabel('Time in seconds'); n=1; for t=-1:0.01:1; //Function for Odd signal y2(n)=0.5*(exp(-t)*u(t)-exp(t)*u(-t)); n=n+1; end figure(1); a=gca(); a.x_location="origin"; a.y_location="origin"; t=-1:0.01:1; //Plot of Odd Signal plot(t,y2) disp('plotted the signal both in even and odd forms'); title('y2(t)'); xlabel('Time in seconds');
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//Example 2.6 //Integration //Page no. 36 clc;clear;close; disp(integrate('1/x','x',exp(-4),1),'Integration Value='); //performing integration with respect to dx
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//Example 13_4 clc;clear; // Given values S_0=0.003;// Bottom slope n_1=0.030; n_2=0.050; // Calculation s=sqrt(3^2+3^2); //Then the flow area, perimeter, and hydraulic radius for each subsection and the entire channel become // Subsection 1: A_c1=21;// m^2 p_1=10.486; // m R_h1=A_c1/p_1;// m // Subsection 2: A_c2=16;// m^2 p_2=10;// m R_h2=A_c2/p_2;// m // Entire channel A_c=A_c1+A_c2;// m^2 p=p_1+p_2;// m R_h=A_c/p;// m //Using the Manning equation for each subsection, a=1;//m^(1/3)/s v_1=(a/n_1)*(A_c1*R_h1^(2/3))*(S_0)^(1/2);// m^3/s v_2=(a/n_2)*(A_c2*R_h2^(2/3))*(S_0)^(1/2);// m^3/s v=v_1+v_2;// m^3/s printf('The total flow rate through the channel,V=%0.0f m^3/s\n',v); n_eff=(a*A_c*R_h^(2/3)*S_0^(1/2))/v; printf('The effective Manning coefficient for the entire channel ,n_eff=%0.3f \n',n_eff);
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function [out]=grayconnected(input1,input2,input3,varargin) inputn=mattolist(input1); [lhs rhs] = argn(0) if rhs>4 then error(msprintf("Too many input arguments")) elseif rhs==4 then a=opencv_grayconnected(inputn,input2,input3,varargin(1)); dimension=size(a) for i = 1:dimension out(:,:,i)=a(i); end else a=opencv_grayconnected(inputn,input2,input3); dimension=size(a) for i = 1:dimension out(:,:,i)=a(i); end end, endfunction;
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//i/p arg x is a vector x=[1 2 3 4 5 7 89 8]; fc=100; fs=500; y = modulate(x,fc,fs,'pwm'); disp(y); //output //!--error 10000 //x must lie between 0 and 1 //at line 115 of function modulate called by : //y = modulate(x,fc,fs,'pwm');
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clc; //e.g 27.15 hfe=100; hie=2*10**3; Rc=470; Re1=100; Re2=100; R1=15000; R2=5600; AV=(hfe*Rc)/hie; disp(AV); a=((R1*R2)/(R1+R2)); Ri=(a*hie)/(a+hie); disp('ohm',Ri*1,"Ri="); b=Re1/Rc; AV1=AV/(1+b*AV); disp(AV1); Ri1=Ri*(1+b*AV); disp('OHM',Ri1*1,"Ri1=");
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//Calculating additional resistance required //Chapter 4 //Example 4.23 //page 320 clear; clc; disp("Example 4.23") // we know (Ts/Tm)=((2*a)/(1+a^2)) //where a=(R2/X20) //at starting contion since Tm=Ts disp("At starting contion since Tm=Ts") a=1 //we obtain from the relations R2=0.05; //circuit resistance in ohms X2=0.4; //standstill reactance in ohms r=(a*X2)-R2; //r is the extra that is added to the rotor circuit printf("extra resistance added,r=%fohms",r)
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syms m11 m12 m13 m21 m22 m23 m31 m32 m33 ^ s=%s; poly(0,"l"); A=[0 1 0;3 0 2;-12 -7 -6] [r c]=size(A) I=eye(r,c); p=l*I-A; q=det(p); // determinant of li-p // roots of q are l1=-1; l2=-2; l3=-3; x1=[m11;m21;m31]; q1=(l1*I-A)*1 // on solving we find m11=1 m21=-1 31=-1 m11=1;m21=-1;m31=-1; x2=[m12;m22;m32]; q2=(l2*I-A)*1 // on solving we find m12=2 m22=-4 m32=1 m12=2;m22=-4;m32=1; x3=[m13;m23;m33]; q3=(l3*I-A)*1 // on solving we get m13=1 m23=-3 m33=3 m13=1;m23=-3;m33=3; // modal matrix is M=[m11 m12 m13;m21 m22 23;m31 m32 m33]
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function [m,n,nx]=g_size(x,flag) // only to be called by size function for dynamical systems //! [lhs,rhs]=argn(0) x1=x(1); if x1(1)=='r' then if lhs==1 then if rhs==1 then m=size(x(2)); else m=size(x(2),flag); end elseif lhs==2 then if rhs<>1 then error(41),end [m,n]=size(x(2)); elseif lhs>2 then error('bad call to size function (not state-space!)'); end else [a,b,c,d]=x(2:5);[m,w]=size([c,d]),[w,n]=size([b;d]); if lhs==1 then if rhs==1 then m=[m,n] elseif flag==1|part(flag,1)=='r' then m=m elseif flag==2|part(flag,1)=='2' then m=n elseif flag=='*' then m=m*n end elseif lhs==2 then elseif lhs==3 then [nx,nx]=size(a); end; end
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//example 7 //Second-Law Analysis of an Ideal Rankine Cycle clear clc xdest12=0 //irreversibility during the process 1 to 2 in kJ/kg xdest34=0 //irreversibility during the process 3 to 4 in kJ/kg s2=1.2132 //specific entropy for state 2 in kJ/kg-K s4=6.7450 //specific entropy for state 4 in kJ/kg-K s1=s2 //specific entropy for state 1 in kJ/kg-K s3=s4 //specific entropy for state 3 in kJ/kg-K qin23=2728.6 //heat input for the process 2 to 3 in kJ/kg Tsource=1600 //temperature of furnaace in K To=290 //temp. of cooling medium in K xdest23=To*(s3-s2-qin23/Tsource) //irreversibility during the process 2 to 3 in kJ/kg Tsink=To //temperature of sink qout41=2018.6 //in kJ/kg xdest41=To*(s1-s4+qout41/Tsink) //irreversibility during the process 4 to 1 in kJ/kg xdestcycle=xdest12+xdest23+xdest34+xdest41 //irreversibility of cycle ho=71.355 //in kJ/kg so=0.2533 //in kJ/kg-K h4=2403.0 //in kJ/kg e4=(h4-ho)-To*(s4-so)//exergy of steam leaving the turbine in kJ/kg printf("\n Hence, the exergy destruction associated with the rankine cycle is = %.0f kJ/kg. \n",xdestcycle); printf("\n and exergy of steam leaving the turbine is = %.0f. \n",e4);
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// chapter 10 , Example10 2 , pg 290 Er=1.0024 //Dielectric constant N=2.7*10^25 //(in atoms/m^3) E0=8.85*10^-12 //permittivity of free space (in F/m) Alpha_e=(E0*(Er-1))/N //electronic polarization printf("Electronic polarization (in F*m^2)\n") disp(Alpha_e)
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//Example 2_7 clc(); clear; //To Calculate highest power of spectrum seen with mono chromaic light lamda=6000 //units in armstrongs lamda=lamda*10^-8 //units in cm n=5000 e=1/n //units in cm k=e/lamda printf("The highest order spectrum Seen with monochromatic light is %.2f",k)
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clear;lines(0); plot2d([0;1],[0;1],0) xstring(0.5,0.5,["Scilab" "is"; "not" "esilaB"]) //Other example alphabet=["a" "b" "c" "d" "e" "f" "g" .. "h" "i" "j" "k" "l" "m" "n" .. "o" "p" "q" "r" "s" "t" "u" .. "v" "w" "x" "y" "z"]; xbasc() plot2d([0;1],[0;2],0) xstring(0.1,1.8,alphabet) // alphabet xstring(0.1,1.6,alphabet,0,1) // alphabet in a box xstring(0.1,1.4,alphabet,20) // angle xset("font",1,1) // use symbol fonts xstring(0.1,0.1,alphabet) xset("font",1,3) // change size font xstring(0.1,0.3,alphabet) xset("font",1,24); xstring(0.1,0.6,"a") //big alpha xset("default")
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//Determine the moment //Refer fig. 3.5 //Take clockwise moment as positive //Apply Varignon's Theorem MA=100*300*cosd(60)-100*500*sind(60) //N-mm printf("MA=%f N-mm,Anticlockwise",-MA)
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clc;funcprot(0);//Example 2.1 //Initilisation of Variables T1=1300;.........//outermost tempatarure of composite wall in degrees celcius T3=115;.........//outermost tempatarure of composite wall in degrees celcius L1=500;.........//thickness of first slab in mm L2=161;.........//thickness of second slab in mm K1=1.4;.........//thermal conductivity of first slab in W/(m*K) K2=0.35;.......//thermal conductivity of second slab in W/(m*K) A=1;.....//area of slab in m^2 //Calculations R1=L1/(A*K1);.........//resistance of first slab in K/W R2=L2/(A*K2);.........//resistance of second slab in K/W R=R1+R2;..........//total resistace in K/W Q=(T1-T3)/R;.........//heat transfer in W T2=T1-(Q*R1);.......//temparatures of surface in contact disp(Q,"conduction heat transfer in W:") disp(T2,"temparature of surface in contact:")
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clc,clear printf('Example 5.10\n\n') VA=125*10^3 V_L=400,V_ph=V_L/sqrt(3) I_L=VA/(sqrt(3)*V_L) I_aph=I_L I_f=4,I_asc=I_aph/2 //for half load.. refer to graph V_OC_line=140 V_OC_ph=V_OC_line/sqrt(3) I_asc_ph=I_asc Z_s= V_OC_ph/I_asc_ph R_a=0.1,X_s=sqrt(Z_s^2-R_a^2) //armature resistance and synchronous reactance phi=acos(0.8) E_ph = sqrt((V_ph*cos(phi)+I_asc*R_a)^2 +(V_ph*sin(phi)- I_asc*X_s)^2) regulation=100*(E_ph-V_ph)/V_ph printf('Voltage regulation at 0.8 pf leading for half load is %.2f percent\n',regulation)
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function XcosDesSet() global bOK; bOK = %f; screen_area = get(0, "screensize_px") XcosDesUI_wight = 540; XcosDesUI_high = 465; XcosDesUI_x = (screen_area(3)-XcosDesUI_wight)/2; XcosDesUI_y = (screen_area(4)-XcosDesUI_high)/2; //R = 255;G = 233; B = 220; R = 28;G = 120; B = 135; XcosDesUI = figure("figure_name", "Xcos模块帮助文档生成向导",... "infobar_visible", "off",... "toolbar_visible", "off",... "dockable", "off",... "menubar", "none",... "default_axes", "off", ... "Position",[XcosDesUI_x XcosDesUI_y XcosDesUI_wight XcosDesUI_high],... "resize", "off",... "BackgroundColor", [R/255 G/255 B/255],... "Icon",AutoGenHelpToolbox_root+"images"+filesep()+"Example_images.png",... "immediate_drawing","on",... "Tag", "XcosDesGuider",... "visible", "off"); //基本信息设置标题 Baseinfo = uicontrol(XcosDesUI,"Position", [10 435 160 25], ...//2 "Style", "text",... "FontSize", 20,... "String", "--基本信息设置--",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //模块名称标题 BlockName_title = uicontrol(XcosDesUI,"Position", [30 405 80 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "模块名称",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //模块名称文本框 BlockName_Context = uicontrol(XcosDesUI, "Position", [120 405 150 25],...//3 "Border",[],... "Style", "edit",... "String", "",... "Callback_Type",10,... "Verticalalignment","top",... "Tag", "BlockNameEdit_Tag"); //概述标题 Overview_title = uicontrol(XcosDesUI,"Position", [30 375 80 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "概 述",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //概述文本框 Overview_Context = uicontrol(XcosDesUI, "Position", [120 350 150 50],...//3 "Border",[],... "Style", "edit",... "String", "",... "Max",2,... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "OverviewEdit_Tag"); //详述标题 Detailed_title = uicontrol(XcosDesUI,"Position", [30 320 80 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "详细描述",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //详述文本框 Detailed_Context = uicontrol(XcosDesUI, "Position", [120 245 150 100],...//3 "Border",[],... "Style", "edit",... "String", "",... "Max",2,... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "DetailedEdit_Tag"); //引脚及参数信息设置 Paraminfo = uicontrol(XcosDesUI,"Position", [10 210 220 25], ...//2 "Style", "text",... "FontSize", 20,... "String", "--引脚及参数信息设置--",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //输入复选框 Detailed_title = uicontrol(XcosDesUI,"Position", [30 170 25 25], ...//2 "Style", "checkbox",... "Callback", "InputCheckbox_callback()",... "Tag","InputCheckbox",... "Verticalalignment","middle",... "Callback_Type",10,... "BackgroundColor", [R/255 G/255 B/255]); //输入标题1 Detailed_title = uicontrol(XcosDesUI,"Position", [55 170 40 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "输入",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //输入标题2 Detailed_title = uicontrol(XcosDesUI,"Position", [105 170 100 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "有 个",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255],... "Tag","Input_title",... "Visible","off"); //输入文本框 Detailed_Context = uicontrol(XcosDesUI, "Position", [130 170 40 25],...//3 "Border",[],... "Style", "edit",... "String", "",... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "InputEdit_Tag",... "Visible","off"); //输出复选框 Detailed_title = uicontrol(XcosDesUI,"Position", [30 130 25 25], ...//2 "Style", "checkbox",... "Callback", "OutputCheckbox_callback()",... "Verticalalignment","middle",... "Tag","OutputCheckbox",... "Callback_Type",10,... "BackgroundColor", [R/255 G/255 B/255]); //输出标题1 Detailed_title = uicontrol(XcosDesUI,"Position", [55 130 40 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "输出",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //输出标题2 Detailed_title = uicontrol(XcosDesUI,"Position", [105 130 100 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "有 个",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255],... "Tag","Output_title",... "Visible","off"); //输出文本框 Detailed_Context = uicontrol(XcosDesUI, "Position", [130 130 40 25],...//3 "Border",[],... "Style", "edit",... "String", "",... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "OutputEdit_Tag",... "Visible","off"); //参数复选框 Detailed_title = uicontrol(XcosDesUI,"Position", [30 90 25 25], ...//2 "Style", "checkbox",... "Callback", "ParamCheckbox_callback()",... "Verticalalignment","middle",... "Tag","ParamCheckbox",... "Callback_Type",10,... "BackgroundColor", [R/255 G/255 B/255]); //参数标题1 Detailed_title = uicontrol(XcosDesUI,"Position", [55 90 40 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "参数",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //参数标题2 Detailed_title = uicontrol(XcosDesUI,"Position", [105 90 100 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "有 个",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255],... "Tag","Param_title",... "Visible","off"); //参数文本框 Detailed_Context = uicontrol(XcosDesUI, "Position", [130 90 40 25],...//3 "Border",[],... "Style", "edit",... "String", "",... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "ParamEdit_Tag",... "Visible","off"); //其他信息设置 Paraminfo = uicontrol(XcosDesUI,"Position", [260 210 160 25], ...//2 "Style", "text",... "FontSize", 20,... "String", "--其他信息设置--",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //接口函数标题 InterName_title = uicontrol(XcosDesUI,"Position", [280 180 120 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "接口函数名称",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //接口函数文本框 InterName_Context = uicontrol(XcosDesUI, "Position", [400 180 120 25],...//3 "Border",[],... "Style", "edit",... "String", "",... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "InterNameEdit_Tag"); //计算函数标题 CalcuName_title = uicontrol(XcosDesUI,"Position", [280 150 120 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "计算函数名称",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //计算函数文本框 CalcuName_Context = uicontrol(XcosDesUI, "Position", [400 150 120 25],...//3 "Border",[],... "Style", "edit",... "String", "",... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "CalcuNameEdit_Tag"); //参见标题 SeeAlso_title = uicontrol(XcosDesUI,"Position", [280 120 120 25], ...//2 "Style", "text",... "FontSize", 18,... "String", " 参见",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //参见文本框 SeeAlso_Context = uicontrol(XcosDesUI, "Position", [400 70 120 75],...//3 "Border",[],... "Style", "edit",... "String", "",... "Max",2,... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "SeeAlsoEdit_Tag"); //作者标题 Author_title = uicontrol(XcosDesUI,"Position", [280 40 120 25], ...//2 "Style", "text",... "FontSize", 18,... "String", " 作者",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //作者文本框 Author_Context = uicontrol(XcosDesUI, "Position", [400 40 120 25],...//3 "Border",[],... "Style", "edit",... "String", "SiROS研发团队",... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "AuthorEdit_Tag"); //模块图片标题 Picture_title = uicontrol(XcosDesUI,"Position", [280 435 120 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "模块图标预览",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //模块图片预览 Picture_preview = uicontrol(XcosDesUI,"Position", [330 350 80 80], ...//2 "Style", "pushbutton",... "FontSize", 18,... "Icon",AutoGenHelpToolbox_root+"images"+filesep()+"Example_images.png",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [255/255 255/255 255/255],... "Tag","Picture_preview"); //模块图片选择 Picture_button = uicontrol(XcosDesUI,"Position", [430 380 100 25], ...//2 "Style", "pushbutton",... "FontSize", 10,... "String","从文件中选择",... "Verticalalignment","middle",... "Callback_Type",10,... "callback", "ChoosePicture_action()"); //示例复选框 Demos_checkbox = uicontrol(XcosDesUI,"Position", [280 325 25 25], ...//2 "Style", "checkbox",... "Callback", "DemosCheckbox_callback()",... "Tag","DemosCheckbox",... "Verticalalignment","middle",... "Callback_Type",10,... "BackgroundColor", [R/255 G/255 B/255]); //示例标题 Demos_title = uicontrol(XcosDesUI,"Position", [310 325 140 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "是否有示例文件",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //示例地址文本框 Demos_Context = uicontrol(XcosDesUI, "Position", [290 300 180 25],...//3 "Border",[],... "Style", "edit",... "String", "",... "Enable","off",... "Verticalalignment","top",... "Callback_Type",10,... "visible","off",... "Tag", "DemosfileEdit_Tag"); //示例地址选择按钮 Demos_button = uicontrol(XcosDesUI,"Position", [490 300 40 25], ...//2 "Style", "pushbutton",... "FontSize", 10,... "String","...",... "visible","off",... "Tag","Demosfilebutton_Tag",... "Verticalalignment","middle",... "Callback_Type",10,... "callback", "ChooseDemosfile_action()"); // //帮助文档生成目标路径标题 Destdir_title = uicontrol(XcosDesUI,"Position", [280 270 160 25], ...//2 "Style", "text",... "FontSize", 18,... "String", "帮助文档存放路径",... "Verticalalignment","middle",... "ForegroundColor", [255/255 255/255 255/255],... "BackgroundColor", [R/255 G/255 B/255]); //帮助文档生成目标路径文本框 Destdir_Context = uicontrol(XcosDesUI, "Position", [290 240 180 25],...//3 "Border",[],... "Style", "edit",... "String", "",... "Enable","off",... "Verticalalignment","top",... "Callback_Type",10,... "Tag", "DestdirEdit_Tag"); //帮助文档生成目标路径选择 Destdir_button = uicontrol(XcosDesUI,"Position", [490 240 40 25], ...//2 "Style", "pushbutton",... "FontSize", 10,... "String","...",... "Verticalalignment","middle",... "Callback_Type",10,... "callback", "ChooseDestdir_action()"); //确定按钮 ok_button = uicontrol(XcosDesUI, "Position", [135 25 80 30], ...//10 "Style", "pushbutton",... "FontSize", 16,... "String", "下一步", ... "Callback_Type",10,... "callback", "XcosDesUIok_action()"); //取消按钮 cancel_button = uicontrol(XcosDesUI, "Position", [30 25 80 30], ...//11 "Style", "pushbutton",... "FontSize", 16,... "String", "取消", ... "Callback_Type",10,... "callback", "XcosDesUIcancel_action()"); //显示界面 XcosDesUI.visible = "on"; global Stop; Stop = %f; //卡循环等待选择结束 while %t, if XcosDesUI_quit() && Stop then break; end end clearglobal Stop; endfunction //关闭按钮的执行函数 function [re] = XcosDesUI_quit() re = %f; if (findobj("Tag","XcosDesGuider") == []) re = %t; global Stop; Stop = %t; end endfunction //输入复选框的回调函数 function InputCheckbox_callback() handle1 = findobj("Tag","InputCheckbox"); handle2 = findobj("Tag","Input_title"); handle3 = findobj("Tag","InputEdit_Tag"); choose = get(handle1,"Value") if(choose == 1) then handle2.visible = "on"; handle3.visible = "on"; else handle2.visible = "off" handle3.visible = "off";; end endfunction //输出复选框的回调函数 function OutputCheckbox_callback() handle1 = findobj("Tag","OutputCheckbox"); handle2 = findobj("Tag","Output_title"); handle3 = findobj("Tag","OutputEdit_Tag"); choose = get(handle1,"Value") if(choose == 1) then handle2.visible = "on"; handle3.visible = "on"; else handle2.visible = "off" handle3.visible = "off";; end endfunction //参数复选框的回调函数 function ParamCheckbox_callback() handle1 = findobj("Tag","ParamCheckbox"); handle2 = findobj("Tag","Param_title"); handle3 = findobj("Tag","ParamEdit_Tag"); choose = get(handle1,"Value"); if(choose == 1) then handle2.visible = "on"; handle3.visible = "on"; else handle2.visible = "off" handle3.visible = "off";; end endfunction //示例复选框的回调函数 //DemosfileEdit_Tag Demosfilebutton_Tag DemosCheckbox function DemosCheckbox_callback() handle1 = findobj("Tag","DemosCheckbox"); handle2 = findobj("Tag","DemosfileEdit_Tag"); handle3 = findobj("Tag","Demosfilebutton_Tag"); choose = get(handle1,"Value"); if(choose == 1) then handle2.visible = "on"; handle3.visible = "on"; else handle2.visible = "off" handle3.visible = "off";; end endfunction //检查参数函数 function [res] = checkParams() res = %f; HandleName = ["BlockNameEdit_Tag","OverviewEdit_Tag","DetailedEdit_Tag","InterNameEdit_Tag","CalcuNameEdit_Tag","DestdirEdit_Tag"]; WarningMessage = ["模块名称","模块概述","模块详细信息","接口函数名称","计算函数名称","帮助文档存储路径"]; for i = 1:size(HandleName,2) execstr("handle = findobj(""Tag"","""+HandleName(i)+""");"); if handle.String == "" then messagebox(WarningMessage(i)+"不能为空!", "警告!", "warning"); return; end end HandleCheckbox = ["InputCheckbox","OutputCheckbox","ParamCheckbox","DemosCheckbox"]; HandleCheckbox_Context = ["InputEdit_Tag","OutputEdit_Tag","ParamEdit_Tag","DemosfileEdit_Tag"]; CheckboxWarningMessage = ["已选择输入,输入个数","已选择输出,输出个数","已选择参数,参数个数","已选择示例,示例文件路径"]; for i = 1:size(HandleCheckbox,2) execstr("handle1 = findobj(""Tag"","""+HandleCheckbox(i)+""");"); execstr("handle2 = findobj(""Tag"","""+HandleCheckbox_Context(i)+""");"); if((handle1.Value == 1) && (handle2.String == "")) then messagebox(CheckboxWarningMessage(i)+"不能为空!", "警告!", "warning"); return; end end res = %t; endfunction //下一步按钮回调函数 function XcosDesUIok_action() res = checkParams(); if (res) then GetValueFromXcosUI(); global bOK; bOK = %t; handle = findobj("Tag","XcosDesGuider"); close(handle); end endfunction //取消按钮回调函数 function XcosDesUIcancel_action() global bOK; global xcosobj; xcosobj = []; bOK = %f; handle = findobj("Tag","XcosDesGuider"); close(handle); endfunction //选择预览图按钮回调函数 function ChoosePicture_action() [PathFileName, Path, FilterIndex] = uigetfile(["*.gif";"*.png"],"","选择模块图片(png格式或者gif格式)",%f); if(PathFileName == "") return; else handle = findobj("Tag","Picture_preview"); handle.Icon = Path + filesep() + PathFileName; end endfunction //选择示例按钮回调函数 function ChooseDemosfile_action() [PathFileName, Path, FilterIndex] = uigetfile(["*.cos";"*.zcos"],"","选择示例文件(zcos格式或者cos格式)",%f); if(PathFileName == "") return; else handle = findobj("Tag","DemosfileEdit_Tag"); handle.String = Path + filesep() + PathFileName; end endfunction //从UI控件中获取对应的值 function GetValueFromXcosUI() global xcosobj; xcosobj = struct(); //获取基础信息 InfoTag = ["BlockNameEdit_Tag","OverviewEdit_Tag","DetailedEdit_Tag","InterNameEdit_Tag","CalcuNameEdit_Tag","SeeAlsoEdit_Tag","AuthorEdit_Tag","DestdirEdit_Tag"]; InfoStructName = ["XcosBlockName","Overview","Detailed","InterName","CalcuName","SeeAlso","Author","Destdir"]; for i = 1:size(InfoTag,2) execstr("handle = findobj(""Tag"","""+InfoTag(i)+""");"); execstr("xcosobj." + InfoStructName(i) + "=handle.String"); end //获取端口信息 PinTag = ["InputCheckbox","OutputCheckbox","ParamCheckbox","DemosCheckbox";"InputEdit_Tag","OutputEdit_Tag","ParamEdit_Tag","DemosfileEdit_Tag"]; PinStruct = ["Input","Output","Params","DemofilePath"]; for i = 1:size(PinTag,2) execstr("handle1 = findobj(""Tag"","""+PinTag(1,i)+""");"); execstr("handle2 = findobj(""Tag"","""+PinTag(2,i)+""");"); if (handle1.Value == 1) then execstr("xcosobj." + PinStruct(i) + "=handle2.String"); else execstr("xcosobj." + PinStruct(i) + "=""0"""); end end //获取图标信息"Icon","Picture_preview", handle = findobj("Tag","Picture_preview"); xcosobj.Icon = handle.Icon; //参数部分的所有变量初始化 xcosobj.ParamsData = struct();//"Name","Dim1","Dim2","Details","Type" xcosobj.ParamsData.Name = []; xcosobj.ParamsData.Dim1 = []; xcosobj.ParamsData.Dim2 = []; xcosobj.ParamsData.Details = []; xcosobj.ParamsData.Type = []; endfunction //帮助文档目标文件夹选择回调函数 function ChooseDestdir_action() handle = findobj("Tag","DestdirEdit_Tag"); filedir = uigetdir(SCI , "选择帮助文档存放路径"); if filedir<>[] then handle.String = filedir; else return; end endfunction
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function [txt,ilst,vnms,vtps,lcount]=cod2sci(lst,ilst,vnms,vtps) // //! // Copyright INRIA nlst=size(lst) txt=[] ilst=ilst-1 while ilst<nlst then ilst=ilst+1 op=lst(ilst) if type(op)==15 then return,end select op(1) case '1' then //stackp // write(6,'stackp '+op(2)); prev=lst(ilst-1) if size(prev,'*')==1 then prev=[prev ' '],end if prev(1:2)==['5','25']|prev(1)=='20' then lhs=evstr(prev(4)) else lhs=1 end if lhs==1 then expk=stk(1); opk=lst(ilst);ilst=ilst+1 opk2=opk(2) if expk(2)<>'-1'& expk(2)<>'-2' then if opk(2)=='ans' then txt=[txt;expk(1)+';'] else if funptr(opk2)<>0 then opk2='%'+opk(2),end txt=[txt;opk2+' = '+expk(1)+';'] end nv=find(opk(2)==vnms(:,2)) if nv==[] then nv=size(vnms,1)+1, // if funptr(opk2)<>0 then opk2='%'+opk(2),end end nv=nv($) vnms(nv,:)=[opk2,opk(2)] vtps(nv)=list(expk(5),expk(3),expk(4),0) end else //if size(stk)==1 then LHS=[] for k=1:lhs expk=stk(k); opk=lst(ilst);ilst=ilst+1 opk2=opk(2) if funptr(opk2)<>0 then opk2='%'+opk(2),end LHS=[opk2,LHS] nv=find(opk(2)==vnms(:,2)) if nv==[] then nv=size(vnms,1)+1, end nv=nv($) vnms(nv,:)=[opk2,opk(2)] if size(expk)<5 then pause,end vtps(nv)=list(expk(5),expk(3),expk(4),0) end if stk(1)(2)=='-1' then // variable has not been previously stored txt=[txt;'['+makeargs(LHS)+'] = '+stk(1)(1)+';'] end end if ilst<=nlst then if lst(ilst)(1)<>'15' then ilst=ilst-1, else lcount=lcount+1 end end case '12' then //pause txt=[txt;'pause'] case '13' then //break txt=[txt;'break'] case '14' then //abort txt=[txt;'abort'] case '15' then ,//eol txt=[txt;' '] lcount=lcount+1 case '18' then case '99' then //return txt=[txt;'return'] else [stk,t1,ilst,vnms,vtps]=exp2sci(lst,ilst,vnms,vtps); txt=[txt;t1];t1=[] ilst=ilst-1 end end ilst=ilst+1
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function [stk,txt,top]=sci_islogical() // Copyright INRIA txt=[] stk=list('or(type('+stk(top)(1)+'==[4,6])','0','1','1','4')
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function s=%s_s_sp(a,b) // %s_s_sp - substract a sparse matrix b to a scalar matrix a //! // Copyright INRIA if size(a)==[-1,-1] then //eye+b [m,n]=size(b) s=(0+a)*speye(m,n)-b else s=a-full(b) end
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% Entering a vector and displaying it x = [1 2 3 4]; y = 10 + x;
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function [s_alp,s_cux,s_cuy,s_cuz,... s_uxx,s_uxy,s_uxz,s_uyy,s_uyz,s_uzz,... s_qxx,s_qxy,s_qxz,s_qyy,s_qyz,s_qzz... ]=sources_parts(... nx,ny,nz,... x,y,z,r,psi,... alp,cux,cuy,cuz,rg,... uxx,uxy,uxz,uyy,uyz,uzz,... gxx,gxy,gxz,gyy,gyz,gzz,... qxx,qxy,qxz,qyy,qyz,qzz,... txx, txy, txz, tyy, tyz, tzz,... dxuxx,dxuxy,dxuxz,dxuyy,dxuyz,dxuzz,... dyuxx,dyuxy,dyuxz,dyuyy,dyuyz,dyuzz,... dzuxx,dzuxy,dzuxz,dzuyy,dzuyz,dzuzz ... ) // //function [s_alp,s_cux,s_cuy,s_cuz,... // s_uxx,s_uxy,s_uxz,s_uyy,s_uyz,s_uzz,... // s_qxx,s_qxy,s_qxz,s_qyy,s_qyz,s_qzz... // ]=sources(... // nx,ny,nz,... // x,y,z,r,psi,... // alp,cux,cuy,cuz,rg,... // uxx,uxy,uxz,uyy,uyz,uzz,... // gxx,gxy,gxz,gyy,gyz,gzz,... // qxx,qxy,qxz,qyy,qyz,qzz,... // dxuxx,dxuxy,dxuxz,dxuyy,dxuyz,dxuzz,... // dyuxx,dyuxy,dyuxz,dyuyy,dyuyz,dyuzz,... // dzuxx,dzuxy,dzuxz,dzuyy,dzuyz,dzuzz ... // ) //$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ // // [FILE] equations.cpp // // [VERSION] H3expresso (c) 1995 Joan Masso, NCSA & UIB // // [PURPOSE] The "meat" of the code!!! The Einstein Equations in // the harmonic formulation. // // Check the paper describing the equations: // C. Bona and J. Masso, Physical Review Letters, 68, 1097 (1992) // // or, in my thesis: "Numerical Relativity: The Quest for a 3-D Code", // University of the Balearic Islands, 1992. // // // [ROUTINES] Sources // Fluxes // dummyentry // // [COMMENTS] These routines have been generated using Mathematica+MathTensor // The output may look kinda ugly... // //$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ //============================================================================== // // [ROUTINE NAME] Sources // [AUTHOR] Joan Masso, NCSA & UIB // // [PURPOSE] Compute the sources of the equations // // [ARGUMENTS] // [INPUT] // nx,ny,nz : grid sizes of the 3d cube. // Full list of grid and metric arrays // [OUTPUT] // s_alp,s_cux,...,s_gxx,...s_qxx,... : Sources of the variables // that DO have a source term. // // [VARIABLES] A bunch of 3d arrays (40) is declared to simplify the // computations. Without them, this routine would be MUCH longer! // and the code MUCH slower! Too bad they take so much memory... // // [INCLUDES] metric.h declares all the passed grid and metric arrays. // // [CALLED BY] Method // [CALLS TO] Dummyentry // // [WARNING] A very stupid dummyentry routine has to be called at some // points to force most fortran compilers to generate code up to // that point and avoid trying to optimize the whole thing. // Both the cm5 and the c90 have problems without the calls. // //<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<< // declare sources $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ // real s_alp(nx,ny,nz) // real s_cux(nx,ny,nz),s_cuy(nx,ny,nz),s_cuz(nx,ny,nz) // real s_uxx(nx,ny,nz),s_uxy(nx,ny,nz),s_uxz(nx,ny,nz) // & ,s_uyy(nx,ny,nz),s_uyz(nx,ny,nz),s_uzz(nx,ny,nz) // real s_qxx(nx,ny,nz),s_qxy(nx,ny,nz),s_qxz(nx,ny,nz) // & ,s_qyy(nx,ny,nz),s_qyz(nx,ny,nz),s_qzz(nx,ny,nz) //c ****** declare all auxiliar quantities ****** // real qsum(nx,ny,nz),lx(nx,ny,nz),ly(nx,ny,nz),lz(nx,ny,nz) // real Fxxx(nx,ny,nz),Fxxy(nx,ny,nz),Fxxz(nx,ny,nz) // & ,Fxyy(nx,ny,nz),Fxyz(nx,ny,nz),Fxzz(nx,ny,nz) // real Fyxx(nx,ny,nz),Fyxy(nx,ny,nz),Fyxz(nx,ny,nz) // & ,Fyyy(nx,ny,nz),Fyyz(nx,ny,nz),Fyzz(nx,ny,nz) // real Fzxx(nx,ny,nz),Fzxy(nx,ny,nz),Fzxz(nx,ny,nz) // & ,Fzyy(nx,ny,nz),Fzyz(nx,ny,nz),Fzzz(nx,ny,nz) // real Hxxx(nx,ny,nz),Hxxy(nx,ny,nz),Hxxz(nx,ny,nz) // & ,Hxyy(nx,ny,nz),Hxyz(nx,ny,nz),Hxzz(nx,ny,nz) // real Hyxx(nx,ny,nz),Hyxy(nx,ny,nz),Hyxz(nx,ny,nz) // & ,Hyyy(nx,ny,nz),Hyyz(nx,ny,nz),Hyzz(nx,ny,nz) // real Hzxx(nx,ny,nz),Hzxy(nx,ny,nz),Hzxz(nx,ny,nz) // & ,Hzyy(nx,ny,nz),Hzyz(nx,ny,nz),Hzzz(nx,ny,nz) //c ****** compute first all auxiliar quantities ****** //c q trace qsum = gxx.*qxx + 2*gxy.*qxy + 2*gxz.*qxz + gyy.*qyy + 2*gyz.*qyz + gzz.*qzz; //c L up lx = -cux - dxuxx - dyuxy - dzuxz + dxuxx.*uxx.*gxx./2 + dyuxx.*uxy.*gxx./2 +... dzuxx.*uxz.*gxx./2 + dxuxy.*uxx.*gxy + dyuxy.*uxy.*gxy + dzuxy.*uxz.*gxy + dxuxz.*uxx.*gxz +... dyuxz.*uxy.*gxz + dzuxz.*uxz.*gxz + dxuyy.*uxx.*gyy./2 + dyuyy.*uxy.*gyy./2 + dzuyy.*uxz.*gyy./2 +... dxuyz.*uxx.*gyz + dyuyz.*uxy.*gyz + dzuyz.*uxz.*gyz + dxuzz.*uxx.*gzz./2 + dyuzz.*uxy.*gzz./2 +... dzuzz.*uxz.*gzz./2; ly = -cuy - dxuxy - dyuyy - dzuyz + dxuxx.*uxy.*gxx./2 + dyuxx.*uyy.*gxx./2 ... + dzuxx.*uyz.*gxx./2 + dxuxy.*uxy.*gxy + dyuxy.*uyy.*gxy + dzuxy.*uyz.*gxy + dxuxz.*uxy.*gxz +... dyuxz.*uyy.*gxz + dzuxz.*uyz.*gxz + dxuyy.*uxy.*gyy./2 + dyuyy.*uyy.*gyy./2 + dzuyy.*uyz.*gyy./2 +... dxuyz.*uxy.*gyz + dyuyz.*uyy.*gyz + dzuyz.*uyz.*gyz + dxuzz.*uxy.*gzz./2 + dyuzz.*uyy.*gzz./2 +... dzuzz.*uyz.*gzz./2; lz = -cuz - dxuxz - dyuyz - dzuzz + dxuxx.*uxz.*gxx./2 + dyuxx.*uyz.*gxx./2 +... dzuxx.*uzz.*gxx./2 + dxuxy.*uxz.*gxy + dyuxy.*uyz.*gxy + dzuxy.*uzz.*gxy + dxuxz.*uxz.*gxz +... dyuxz.*uyz.*gxz + dzuxz.*uzz.*gxz + dxuyy.*uxz.*gyy./2 + dyuyy.*uyz.*gyy./2 + dzuyy.*uzz.*gyy./2 +... dxuyz.*uxz.*gyz + dyuyz.*uyz.*gyz + dzuyz.*uzz.*gyz + dxuzz.*uxz.*gzz./2 + dyuzz.*uyz.*gzz./2 +... dzuzz.*uzz.*gzz./2; // call dummyentry(1) //c auxiliar Chistoffel Gam: u u u Fxxx = -(dxuxx.*uxx)./2 - dyuxx.*uxy./2 - dzuxx.*uxz./2; Fxxy = -(dxuxx.*uxy)./2 - dyuxx.*uyy./2 - dzuxx.*uyz./2; Fxyy = dxuyy.*uxx./2 - dxuxy.*uxy + dyuyy.*uxy./2 + dzuyy.*uxz./2 - dyuxy.*uyy - dzuxy.*uyz; Fxxz = -(dxuxx.*uxz)./2 - dyuxx.*uyz./2 - dzuxx.*uzz./2; Fxyz = dxuyz.*uxx./2 - dxuxz.*uxy./2 + dyuyz.*uxy./2 - dxuxy.*uxz./2 + dzuyz.*uxz./2 -... dyuxz.*uyy./2 - dyuxy.*uyz./2 - dzuxz.*uyz./2 - dzuxy.*uzz./2; Fxzz = dxuzz.*uxx./2 + dyuzz.*uxy./2 - dxuxz.*uxz + dzuzz.*uxz./2 - dyuxz.*uyz - dzuxz.*uzz; Fyxx = -(dxuxy.*uxx) + dxuxx.*uxy./2 - dyuxy.*uxy - dzuxy.*uxz + dyuxx.*uyy./2 + dzuxx.*uyz./2; Fyxy = -(dxuyy.*uxx)./2 - dyuyy.*uxy./2 - dzuyy.*uxz./2; Fyyy = -(dxuyy.*uxy)./2 - dyuyy.*uyy./2 - dzuyy.*uyz./2; Fyxz = -(dxuyz.*uxx)./2 + dxuxz.*uxy./2 - dyuyz.*uxy./2 - dxuxy.*uxz./2 -dzuyz.*uxz./2 +... dyuxz.*uyy./2 - dyuxy.*uyz./2 + dzuxz.*uyz./2 - dzuxy.*uzz./2; Fyyz = -(dxuyy.*uxz)./2 - dyuyy.*uyz./2 - dzuyy.*uzz./2; Fyzz = dxuzz.*uxy./2 - dxuyz.*uxz + dyuzz.*uyy./2 - dyuyz.*uyz + dzuzz.*uyz./2 - dzuyz.*uzz; Fzxx = -(dxuxz.*uxx) - dyuxz.*uxy + dxuxx.*uxz./2 - dzuxz.*uxz + dyuxx.*uyz./2 + dzuxx.*uzz./2; Fzxy = -(dxuyz.*uxx)./2 - dxuxz.*uxy./2 - dyuyz.*uxy./2 + dxuxy.*uxz./2 -dzuyz.*uxz./2 -... dyuxz.*uyy./2 + dyuxy.*uyz./2 - dzuxz.*uyz./2 + dzuxy.*uzz./2; Fzyy = -(dxuyz.*uxy) + dxuyy.*uxz./2 - dyuyz.*uyy + dyuyy.*uyz./2 - dzuyz.*uyz + dzuyy.*uzz./2; Fzxz = -(dxuzz.*uxx)./2 - dyuzz.*uxy./2 - dzuzz.*uxz./2; Fzyz = -(dxuzz.*uxy)./2 - dyuzz.*uyy./2 - dzuzz.*uyz./2; Fzzz = -(dxuzz.*uxz)./2 - dyuzz.*uyz./2 - dzuzz.*uzz./2; //call dummyentry(2) //c auxiliar Christoffel Ham: u d d Hxxx = 2*Fxxx.*gxx + 2*Fxxy.*gxx.*gxy + 2*Fxyy.*gxy + 2*Fxxz.*gxx.*gxz +... 2*Fxyz.*gxy.*gxz + 2*Fxzz.*gxz; Hxxy = Fxxx.*gxx.*gxy + 2*Fxxy.*gxy + Fxxz.*gxy.*gxz + Fxxy.*gxx.*gyy +... Fxyy.*gxy.*gyy + Fxyz.*gxz.*gyy + Fxxz.*gxx.*gyz + Fxyz.*gxy.*gyz + Fxzz.*gxz.*gyz; Hxyy = 2*Fxxx.*gxy + 2*Fxxy.*gxy.*gyy + 2*Fxyy.*gyy + 2*Fxxz.*gxy.*gyz +... 2*Fxyz.*gyy.*gyz + 2*Fxzz.*gyz; Hxxz = Fxxx.*gxx.*gxz + Fxxy.*gxy.*gxz + 2*Fxxz.*gxz + Fxxy.*gxx.*gyz +... Fxyy.*gxy.*gyz + Fxyz.*gxz.*gyz + Fxxz.*gxx.*gzz + Fxyz.*gxy.*gzz + Fxzz.*gxz.*gzz; Hxyz = Fxxx.*gxy.*gxz + Fxxy.*gxz.*gyy + Fxxy.*gxy.*gyz + Fxxz.*gxz.*gyz... + Fxyy.*gyy.*gyz + 2*Fxyz.*gyz + Fxxz.*gxy.*gzz + Fxyz.*gyy.*gzz + Fxzz.*gyz.*gzz; Hxzz = 2*Fxxx.*gxz + 2*Fxxy.*gxz.*gyz + 2*Fxyy.*gyz + 2*Fxxz.*gxz.*gzz +... 2*Fxyz.*gyz.*gzz + 2*Fxzz.*gzz; Hyxx = 2*Fyxx.*gxx + 2*Fyxy.*gxx.*gxy + 2*Fyyy.*gxy + 2*Fyxz.*gxx.*gxz +... 2*Fyyz.*gxy.*gxz + 2*Fyzz.*gxz; Hyxy = Fyxx.*gxx.*gxy + 2*Fyxy.*gxy + Fyxz.*gxy.*gxz + Fyxy.*gxx.*gyy +... Fyyy.*gxy.*gyy + Fyyz.*gxz.*gyy + Fyxz.*gxx.*gyz + Fyyz.*gxy.*gyz + Fyzz.*gxz.*gyz; Hyyy = 2*Fyxx.*gxy + 2*Fyxy.*gxy.*gyy + 2*Fyyy.*gyy + 2*Fyxz.*gxy.*gyz +... 2*Fyyz.*gyy.*gyz + 2*Fyzz.*gyz; Hyxz = Fyxx.*gxx.*gxz + Fyxy.*gxy.*gxz + 2*Fyxz.*gxz + Fyxy.*gxx.*gyz +... Fyyy.*gxy.*gyz + Fyyz.*gxz.*gyz + Fyxz.*gxx.*gzz + Fyyz.*gxy.*gzz + Fyzz.*gxz.*gzz; Hyyz = Fyxx.*gxy.*gxz + Fyxy.*gxz.*gyy + Fyxy.*gxy.*gyz + Fyxz.*gxz.*gyz... + Fyyy.*gyy.*gyz + 2*Fyyz.*gyz + Fyxz.*gxy.*gzz + Fyyz.*gyy.*gzz + Fyzz.*gyz.*gzz; Hyzz = 2*Fyxx.*gxz + 2*Fyxy.*gxz.*gyz + 2*Fyyy.*gyz + 2*Fyxz.*gxz.*gzz +... 2*Fyyz.*gyz.*gzz + 2*Fyzz.*gzz; Hzxx = 2*Fzxx.*gxx + 2*Fzxy.*gxx.*gxy + 2*Fzyy.*gxy + 2*Fzxz.*gxx.*gxz +... 2*Fzyz.*gxy.*gxz + 2*Fzzz.*gxz; Hzxy = Fzxx.*gxx.*gxy + 2*Fzxy.*gxy + Fzxz.*gxy.*gxz + Fzxy.*gxx.*gyy +... Fzyy.*gxy.*gyy + Fzyz.*gxz.*gyy + Fzxz.*gxx.*gyz + Fzyz.*gxy.*gyz + Fzzz.*gxz.*gyz; Hzyy = 2*Fzxx.*gxy + 2*Fzxy.*gxy.*gyy + 2*Fzyy.*gyy + 2*Fzxz.*gxy.*gyz +... 2*Fzyz.*gyy.*gyz + 2*Fzzz.*gyz; Hzxz = Fzxx.*gxx.*gxz + Fzxy.*gxy.*gxz + 2*Fzxz.*gxz + Fzxy.*gxx.*gyz +... Fzyy.*gxy.*gyz + Fzyz.*gxz.*gyz + Fzxz.*gxx.*gzz + Fzyz.*gxy.*gzz + Fzzz.*gxz.*gzz; Hzyz = Fzxx.*gxy.*gxz + Fzxy.*gxz.*gyy + Fzxy.*gxy.*gyz + Fzxz.*gxz.*gyz+... Fzyy.*gyy.*gyz + 2*Fzyz.*gyz + Fzxz.*gxy.*gzz + Fzyz.*gyy.*gzz + Fzzz.*gyz.*gzz; Hzzz = 2*Fzxx.*gxz + 2*Fzxy.*gxz.*gyz + 2*Fzyy.*gyz + 2*Fzxz.*gxz.*gzz +... 2*Fzyz.*gyz.*gzz + 2*Fzzz.*gzz; // call dummyentry(3) //c .*.*.*.*.* now, the sources of the equations .*.*.*.*.* //c source of lapse s_alp = alp./rg .*(-(alp.*qsum)./2); //c source momentum s_cux = alp./rg.*(lx.*qsum + Hxxx.*qxx - 2*gxx.*lx.*qxx - 2*gxy.*ly.*qxx-... 2*gxz.*lz.*qxx + 2*Hxxy.*qxy - 2*gxy.*lx.*qxy - 2*gyy.*ly.*qxy -... 2*gyz.*lz.*qxy + 2*Hxxz.*qxz - 2*gxz.*lx.*qxz - 2*gyz.*ly.*qxz -... 2*gzz.*lz.*qxz+ Hxyy.*qyy + 2*Hxyz.*qyz + Hxzz.*qzz); s_cuy = alp./rg.*(ly.*qsum + Hyxx.*qxx + 2*Hyxy.*qxy - 2*gxx.*lx.*qxy -... 2*gxy.*ly.*qxy - 2*gxz.*lz.*qxy + 2*Hyxz.*qxz + Hyyy.*qyy - 2*gxy.*lx.*qyy -... 2*gyy.*ly.*qyy - 2*gyz.*lz.*qyy + 2*Hyyz.*qyz - 2*gxz.*lx.*qyz -... 2*gyz.*ly.*qyz - 2*gzz.*lz.*qyz + Hyzz.*qzz); s_cuz = alp./rg.*(lz.*qsum + Hzxx.*qxx + 2*Hzxy.*qxy + 2*Hzxz.*qxz -... 2*gxx.*lx.*qxz - 2*gxy.*ly.*qxz - 2*gxz.*lz.*qxz + Hzyy.*qyy +... 2*Hzyz.*qyz- 2*gxy.*lx.*qyz - 2*gyy.*ly.*qyz - 2*gyz.*lz.*qyz +... Hzzz.*qzz - 2*gxz.*lx.*qzz - 2*gyz.*ly.*qzz - 2*gzz.*lz.*qzz); // call dummyentry(4) //c source g s_uxx = (alp./rg).*(qxx); s_uxy = (alp./rg).*(qxy); s_uyy = (alp./rg).*(qyy); s_uxz = (alp./rg).*(qxz); s_uyz = (alp./rg).*(qyz); s_uzz = (alp./rg).*(qzz); //c source of q s_qxx = txx-0.5*gxx.*(txx+tyy+tzz)+alp.*rg.*( 2*cux.^2 - 2*Fxxx.*Hxxx - 4*Fxxy.*Hxxy - 4*Fxxz.*Hxxz - 2*Fxyy.*Hxyy -... 4*Fxyz.*Hxyz - 2*Fxzz.*Hxzz - 2*lx.^2 + gxx.*(qxx.^2)./(rg.^2) +... 2*gxy.*qxx.*qxy./(rg.^2) + gyy.*(qxy.^2)./(rg.^2) + 2*gxz.*qxx.*qxz./(rg.^2) +... 2*gyz.*qxy.*qxz./(rg.^2) + gzz.*(qxz.^2)./(rg.^2)); s_qxy = txy-0.5*gxy.*(txx+tyy+tzz)+alp.*rg.*( 2*cux.*cuy - 2*Fyxx.*Hxxx - 4*Fyxy.*Hxxy - 4*Fyxz.*Hxxz -... 2*Fyyy.*Hxyy - 4*Fyyz.*Hxyz - 2*Fyzz.*Hxzz - 2*lx.*ly + gxx.*qxx.*qxy./(rg.^2) +... gxy.*(qxy.^2)./(rg.^2) + gxz.*qxy.*qxz./(rg.^2) + gxy.*qxx.*qyy./(rg.^2) + gyy.*qxy.*qyy./(rg.^2) +... gyz.*qxz.*qyy./(rg.^2) + gxz.*qxx.*qyz./(rg.^2) + gyz.*qxy.*qyz./(rg.^2) + gzz.*qxz.*qyz./(rg.^2)); s_qyy = tyy-0.5*gyy.*(txx+tyy+tzz)+alp.*rg.*( 2*cuy.^2 - 2*Fyxx.*Hyxx - 4*Fyxy.*Hyxy - 4*Fyxz.*Hyxz -... 2*Fyyy.*Hyyy - 4*Fyyz.*Hyyz - 2*Fyzz.*Hyzz - 2*(ly.^2) + gxx.*(qxy.^2)./(rg.^2) +... 2*gxy.*qxy.*qyy./(rg.^2) + gyy.*(qyy.^2)./(rg.^2) + 2*gxz.*qxy.*qyz./(rg.^2) + 2*gyz.*qyy.*qyz./(rg.^2) +... gzz.*(qyz.^2)./(rg.^2)) s_qxz = txz-0.5*gxz.*(txx+tyy+tzz)+alp.*rg.*( 2*cux.*cuz - 2*Fzxx.*Hxxx - 4*Fzxy.*Hxxy - 4*Fzxz.*Hxxz -... 2*Fzyy.*Hxyy - 4*Fzyz.*Hxyz - 2*Fzzz.*Hxzz - 2*lx.*lz + gxx.*qxx.*qxz./(rg.^2) +... gxy.*qxy.*qxz./(rg.^2) + gxz.*(qxz.^2)./(rg.^2) + gxy.*qxx.*qyz./(rg.^2) + gyy.*qxy.*qyz./(rg.^2) +... gyz.*qxz.*qyz./(rg.^2) + gxz.*qxx.*qzz./(rg.^2)+ gyz.*qxy.*qzz./(rg.^2) + gzz.*qxz.*qzz./(rg.^2)); s_qyz = tyz-0.5*gyz.*(txx+tyy+tzz)+alp.*rg.*( 2*cuy.*cuz - 2*Fzxx.*Hyxx - 4*Fzxy.*Hyxy - 4*Fzxz.*Hyxz -... 2*Fzyy.*Hyyy - 4*Fzyz.*Hyyz - 2*Fzzz.*Hyzz - 2*ly.*lz + gxx.*qxy.*qxz./(rg.^2) +... gxy.*qxz.*qyy./(rg.^2) + gxy.*qxy.*qyz./(rg.^2) + gxz.*qxz.*qyz./(rg.^2) + gyy.*qyy.*qyz./(rg.^2) +... gyz.*(qyz.^2)./(rg.^2) + gxz.*qxy.*qzz./(rg.^2)+ gyz.*qyy.*qzz./(rg.^2) + gzz.*qyz.*qzz./(rg.^2)); s_qzz = tzz-0.5*gzz.*(txx+tyy+tzz)+alp.*rg.*( 2*(cuz.^2) - 2*Fzxx.*Hzxx - 4*Fzxy.*Hzxy - 4*Fzxz.*Hzxz - ... 2*Fzyy.*Hzyy - 4*Fzyz.*Hzyz - 2*Fzzz.*Hzzz - 2*(lz.^2) + gxx.*(qxz.^2)./(rg.^2) + ... 2*gxy.*qxz.*qyz./(rg.^2) + gyy.*(qyz.^2)./(rg.^2) + 2*gxz.*qxz.*qzz./(rg.^2) +... 2*gyz.*qyz.*qzz./(rg.^2) + gzz.*(qzz.^2)./(rg.^2)); endfunction
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example13_3.sce
v1=10; fsd1=0.03; v2=5; i1=50*10^(-6); r1=20*10^3; fsd2=0.02; i2=10*10^(-6); disp("Part a"); r=v2/i2-r1; disp("The resistance (in kΩ) is"); disp(r/1000); disp("Part b"); e1=fsd1*v1*100/v2; e2=fsd2*i1*100/i2; e=e1+e2; disp("The maximum possible error is"); disp(e);
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Ex2_8.sce
clc // // // //Variable declaration n=2 //order of spectral line theta=30 //Angular Width invde=5000 //Inverse of diffraction element //Calculations thetarad=(%pi/180)*(theta) sinetheta=sin(thetarad) lambdaa=((sinetheta)/(n*invde))*10**8 //Result printf("\n The Wavelength is %i Angstrom",lambdaa)
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19_4.sce
clc //initialisation of variables No= 0.979889 v= 2989.74 //cm^-1 rc= 1.2746 //A T= 25 //C E1= 6.8635 //cal deg^-1 mole^-1 E2= 11.4392 //cal deg^-1 mole^-1 E3= 7.2820 //cal deg^-1 mole^-1 E4= 4.5757 //cal deg^-1 mole^-1 E5= 2.7676 //cal deg^-1 mole^-1 r1= 0.265 //A r= 35.99 //A //CALCULATIONS Et= E1*log10(r)+E2*log10(273.15+T)- E3 Ei= E4*log10(r1)+E4*log10(273.15+T)-E5 //RESULTS printf ('Transitional energy = %.1f cal deg^-1 mole^-1',Et) printf ('\n rorational energy = %.1f cal deg^-1 mole^-1',Ei)
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exa_5_12.sce
// Exa 5.12 clc; clear; close; // Given data f=2.5;// in kHz f=f*10^3;// in Hz // Part (i) when t=0.1;// in sec count= f*t; disp(count,"When GATE ENABLE time is 0.1 sec then the counter will count or display") // Part (ii) when t=1;// in sec count= f*t; disp(count,"When GATE ENABLE time is 1 sec then the counter will count or display") // Part (iii) when t=10;// in sec count= f*t; disp(count,"When GATE ENABLE time is 10 sec then the counter will count")
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example1_5.sce
clear; clc; //Example1.5 (The cost of Heat loss through a Roof) //(a) k=0.8;//The thermal conductivity of the roof[W/m.degree.C] A=6*8;//Area of the roof[m^2] t1=15;//temperature of inner surface roof[degree C] t2=4;//temperature of outer surface roof[degree C] L=0.25;//thickness of roof[m] Q_=k*A*(t1-t2)/L;//[W] disp("W",Q_,"The steady rate of heat transfer through the roof is") //(b) dt=10;//time period[h] Q=Q_*dt/1000;//[kWh] u_cost=0.08;//Unit cost of energy[$/kWh] Cost=Q*u_cost;//[$] disp(Cost,"and its cost is $","kWh",Q,"The amount of heat lost through the roof")
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/1511/CH4/EX4.6/ex4_6.sce
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ex4_6.sce
// Example 4.6 page no-207 clear clc vbb=-1 //V Rb=50 //K-Ohm vbe=-0.1 Icbo=(vbe-vbb)/Rb printf("\nIcbo =%.0f micro A",Icbo*1000) t=log(Icbo*1000/2)*10/(log(2)) printf("\nDelta_T = %d°C \nHence, T=%d°C",ceil(t),ceil(t)+25)
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/788/CH3/EX3.12.b/3_12_soln.sce
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3_12_soln.sce
clc; pathname=get_absolute_file_path('3_12_soln.sce') filename=pathname+filesep()+'3_12_data.sci' exec(filename) // Solution: // Acceleration due to gravity, g=32.2; //ft/s^2 // Jet velocity through siphon, v2=sqrt(2*g*(h-Hl)); //ft/s // rounding off the above answer v2=fix(v2)+(fix(floor((v2-fix(v2))*10))/10); //ft/s // Area of the U tube, A=(%pi/4)*((d/12)^2); //ft^2 // flow rate through siphon, Q=A*v2; //ft^3/s Q_gpm=449*Q; //gpm // rounding off the above answer Q_gpm=fix(Q_gpm)+(fix(floor((Q_gpm-fix(Q_gpm))*10))/10); //gpm // Results: printf("\n Results: ") printf("\n The velocity through siphon is %.1f ft/s.",v2) printf("\n The Flow rate through siphon is %.1f gpm.",Q_gpm)
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/NLP_Project/test/blog/bow/bow.14_19.tst
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