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//Optoelectronics and Fiber Optics Communication by C.R. Sarkar and D.C. Sarkar //Example 4.1 //OS = Windows 7 //Scilab version 5.5.2 clc; clear; //given h=6.62*10^-34;//Plank's constant in SI units c=3*10^8;//speed of the light in m/s e=1.9*10^-19;//electric charge in columb I=50*10^-3;//drive current in A lamda=0.85*10^-6;//peak emission wavelength in m taur=50*10^-9;//radiative carrier life time in s taunr=100*10^-9;//nonradiative carrier life time in s Tp=(taur*taunr)/(taur+taunr);///total carrier life time in s etaint=Tp/taur;//equation of internal efficiency c1=(I*h*c)/(e*lamda);//constant value Pint=(etaint)*c1;//internal optical power generated in W mprintf("\n Total carrier life time is =%.2fns ",Tp*1e9);//multiplication by 1e9 for conversion of unit from s to ns mprintf("\n Optical power generated internally is= %.2f mW ",Pint*1e3);//multiplication by 1e3 for conversion of unit from W to mW//the answer vary due to rounding
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/** * Coloca em a os coeficientes do polinomio de GRAU ESPECIFICADO EM P que * melhor se ajuste aos pares x,y. * PARA RETAS -> p=1 * PARA PARABOLAS -> p=2... */ clear p = 1 //q1 Ordem do polinomio a ser gerado p = 1 //q2 Ordem do polinomio a ser gerado p = 2 //q3 Ordem do polinomio a ser gerado p = 2 //q4 Ordem do polinomio a ser gerado p = 3 //q5 Ordem do polinomio a ser gerado // Pares (x,y) //x = [0:0.2:1]' //q1 Coordenada x transposta //x = [0:0.2:1]' //q2 Coordenada x transposta //x = [1:0.5:12]' //q3 Coordenada x transposta //x = [1:0.5:12]' //q4 Coordenada x transposta x = [1:0.5:12]' //q5 Coordenada x transposta //y = sin(x+5) //q1 Coordenada y transposta //y = cos(x+6) //q2 Coordenada y transposta //y = 3*sin(x+10)+x^2 //q3 Coordenada y transposta //y = 10*sin(x)+x^2 //q4 Coordenada y transposta y = sin(8+1./x) //q5 Coordenada y transposta n = size(x,1) //plot(x,y,'ro-'),xgrid // Plota grafico dos pontos // Monta matriz simetrica de minimos quadrados for i=1:p+1 //for (i=1; i<= p+1; i++) for j=1:p+1 M(i,j) = sum(x.^(i+j-2)) // . elemento a elemento end // Monta matriz de resultado b for i=1:p+1 b(i) = sum(y.*x.^(i-1)) end // Pegando os coeficientes do polinomio de ajuste a = inv(M)*b; // Monta polinomio para plotagem XX = 1:0.5:12 // Colocar os mesmos pontos passados por X, ou que pegue todos pontos de X pra deixar o grafico melhor YY = 0 residuo = 0 for i=1:p+1 YY = YY+a(i)*XX.^(i-1); // Polinomio residuo = residuo+a(i)*x.^(i-1); end residuo = residuo - y; //plot(XX,YY,'b-');xgrid t=2; f=(a(1,1)+a(2,1)*t) // ... +a(n,1)*t^n //disp(a(1)); //questão 1 //disp(a(2)); //questão 2 //disp(a(3)); //questão 3 //disp(a(1)+(a(2)*3.14)+(a(3)*3.14^2))//questão 4 // Valor do polinomio de ajuste no ponto, polinomio disp(a(1)+(a(2)*2.1)+(a(3)*2.1^2)+(a(4)*2.1^3))//questão 5 // Valor do polinomio de ajuste no ponto, polinomio // YY = a(1) + a(2)*XX + a(2)*XX^2 ... a(n)*XX^n
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//example 8.13 clc; clear; disp('For SR flip flop Qn+1 = S + R`Qn and for D flip-flop Qn+1 = D .'); disp('Thus with D = S + R`Qn we get circuit which behaves like SR flip-flop.');
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//Example 2_2 clc; clear;close; //Given data: Vo=50;//V R=10;//ohm //Vin=100*sin(omega*t);//V Vm=100;//V //Solution : omega_t=asin(Vo/Vm);//radian Iavg=1/2/%pi*integrate('(Vm*sin(omega_t)-Vo)/R','omega_t',omega_t,omega_t+2*%pi/3);//A disp(Iavg,"Average current in the circuit(A) : ");
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function p=anpath(i,j,g) [lhs,rhs]=argn(0), if rhs==2 then g=the_g, end if ( i<0 | i>g_nodnum(g) | j<0 | j>g_nodnum(g)) then error('bad internal node number') end [l,v]=dfs(i,g) p=prevn2p(i,j,v,g)
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//Given that h = 8.5 //in meter\ g = 9.8 //in m/s^2 //Sample Problem 8-3 printf("**Sample Problem 8-3**\n") //Using conservation of energy //Change in Potential energy = Change in Kinetic energy //m* g* h = .5* m* v^2 v = sqrt(2* g * h) printf("The velocity of child at the bottom will be %fm/s", v)
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## Test msgout --filter option read <sample1.fi =C msgout --filter=/Author:|Committer:|Committer-Date:/
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% options([abox_target(allinonefile), tbox_target(allinonefile)]). options([abox_target(allinonefile), tbox_target(allinonefile), projection(no), ground_optim(no)]). options([abox_target(allinonefile), tbox_target(allinonefile), projection(no), ground_optim(no), unfold(yes)]). concept(d). role(a). role(b). role(c). subrole(arole(b),arole(a)). subrole(arole(c),arole(a)). implies(some(arole(a),top),aconcept(d)). rassertion(arole(b),i1,i2). rassertion(arole(a),d1,d2). cassertion(aconcept(d),d5). % expected result: aconcept(c): i1 %query(instances(aconcept(c)), _).
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clc //initialisation of variables w= 3 //ft h= 15 //ft d= 140 //lbs/ft^3 x= 6 //in W= 62.4 //lbs/ft^3 //CALCULATIONS W1= h*w*d h= (W1*x*6/(W*12))^(1/3) //RESULTS printf (' height of water rise = %.2f ft',h)
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spLitTEr y {} FiLTeR lua { } FILTer t {NOt iU NOt q } j -> C gROupEr j {AgGREgaTE UG.Y } uNGroUPer I { } gROUPfiLTER v {nOt A::2aCB:2:6dFf:fe:7:3/5 = C 96 >> G Or nOT o ( ) oR U << R oR BiTAnD ( 057, ) OR bitand ( ) OR bMnWHe ( 3, ) or m ( ) or 4 = 250.0.251.244 bItaNd ( ) } MERgEr KDhNA { MOdulE O { brAncheS K, DIQjE nOT t ( 237.253.4.253 ) } eXpORT ER }
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clc clear //Input data Mx=1.5 //Mach number P=40 //Static pressure in kPa //Calculation p1=3.413 //Pressure ratio in (Poy/Px) from normal shock gas tables @Mx Poy=p1*P //Pressure acting on front of the body in kPa //Output printf('Pressure acting on front of the body is %3.1f kPa',Poy)
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clc A=0.1*10^-4 disp("A = "+string(A)+" cm^2") //initializing value of area. Dp=7.77*10^-4 disp("Dp= "+string(Dp)+" cm^2/s") //initializing value of diffusion cofficient. Lp=0.233*10^-5 disp("Lp = "+string(Lp)+" cm") //initializing value of diffusion length. x=500*10^-8 disp("x = "+string(x)+" cm") //initializing value of distance P=10^17*10^6 disp("P(O)-po = "+string(P)) //initializing value of P(O)-po e=1.6*10^-19 disp("e = "+string(e)+"column")//initializing value of charge of electron. I=(((e*A*Dp*P)/Lp)*exp(-x/Lp)) disp("Hole current,I=(((e*A*Dp*[P(O)-po])/Lp)*exp(-x/Lp))= "+string(I)+"amphere")//calculation Q=(e*A*Dp*Lp*P) disp("stored excess hole ,Q=(e*A*Dp*Lp*P))= "+string(Q)+"C")//calculation //the value of current(I) given after calculation in the book is wrong, (as the value of Lp used in the formula while finding value of hole current (I)at two places //is used different). //I have used the value Lp=0.233*10^-5 cm
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no_logfile = false; active_buttons = 3; button_codes = 1,2,3; response_matching = simple_matching; write_codes = true; response_port_output=false; default_monitor_sounds = false; default_font = "NSimSun"; default_font_size = 40; default_text_color = 0, 0, 0; default_background_color = 122, 122, 122; default_formatted_text = true; stimulus_properties = letter, string, is_target, string, stim, string, x_pos, number, y_pos, number, x_sel, number, y_sel, number; event_code_delimiter = "/n"; default_path = "C:\Users\Psychology\Desktop\EAPSI_BEIJING\Presentation_Files\Stimuli"; begin; #================================================================================================= #TEXT #================================================================================================= picture { text { caption = "退出程序"; }ExitProgramText; x = 0; y = 0; }ExitProgram; picture { text { caption = "..."; }TriggerWaitText; x = 0; y = 0; }TriggerWait; picture { text { caption = " "; }IntroText1; x = 0; y = 0; }Intro; #affect rating trial { trial_type = fixed; stimulus_event { nothing {}; } AffectRateEvent; }AffectRateTrial; #success rating trial { trial_type = fixed; stimulus_event { nothing {}; } SuccessRateEvent; }SuccessRateTrial; #--------------------------------------- #affect rating scale picture { box { height = 1; width = 1; }; x = -400; y = 200; text { caption = "请用1~9间的一个数字对 你看到每张照片时的感受进行评分"; font_size = 30; }AffectText1; x = -400; y = 0; } scale7; array { LOOP $q 9; text {caption = " "; font_size = 35; # background_color = 100, 100, 100; #debugging code to show label position }; ENDLOOP; } scale_labels7; #--------------------------------------- #success rating scale picture { box { height = 1; width = 1; }; x = -400; y = 200; text { caption = "请用1~9间的一个数字 表示当你看到每一张照片时 你多成功地压抑了自己的面部表情反应"; font_size = 30; }SuccessText1; x = -400; y = 0; } scale8; array { LOOP $q 9; text {caption = " "; font_size = 35; # background_color = 100, 100, 100; #debugging code to show label position }; ENDLOOP; } scale_labels8; #----- Get Version Number -------- trial { trial_duration = forever; trial_type = specific_response; terminator_button = 3; #enter button is pressed picture { text { caption = " "; } Versiontext1; x = 0; y = 0; } Versionpic1; } VersionInfoTrial; picture { text { caption = "请输入版本编号,按回车键继续"; }; x = 0; y = 0; text { caption = " "; } Versiontext2; x = 0; y = -180; } Versionpic2; trial { stimulus_event { nothing {}; } VersionEvent; }VersionTrial; #================================================================================================= #IAPS STIMULUS ARRAYS #================================================================================================= array{ # Look Neutral bitmap { filename = "iaps/5130.jpg"; preload = true; description = "stim_lookneu_5130_"; }; bitmap { filename = "iaps/7020.jpg"; preload = true; description = "stim_lookneu_7020_"; }; bitmap { filename = "iaps/7046.jpg"; preload = true; description = "stim_lookneu_7046_"; }; bitmap { filename = "iaps/2850.jpg"; preload = true; description = "stim_lookneu_2850_"; }; bitmap { filename = "iaps/5920.jpg"; preload = true; description = "stim_lookneu_5920_"; }; bitmap { filename = "iaps/1670.jpg"; preload = true; description = "stim_lookneu_1670_"; }; bitmap { filename = "iaps/1935.jpg"; preload = true; description = "stim_lookneu_1935_"; }; bitmap { filename = "iaps/1945.jpg"; preload = true; description = "stim_lookneu_1945_"; }; bitmap { filename = "iaps/2302.jpg"; preload = true; description = "stim_lookneu_2302_"; }; bitmap { filename = "iaps/5535.jpg"; preload = true; description = "stim_lookneu_5535_"; }; bitmap { filename = "iaps/5120.jpg"; preload = true; description = "stim_lookneu_5120_"; }; bitmap { filename = "iaps/5395.jpg"; preload = true; description = "stim_lookneu_5395_"; }; bitmap { filename = "iaps/2191.jpg"; preload = true; description = "stim_lookneu_2191_"; }; bitmap { filename = "iaps/2122.jpg"; preload = true; description = "stim_lookneu_2122_"; }; bitmap { filename = "iaps/2038.jpg"; preload = true; description = "stim_lookneu_2038_"; }; bitmap { filename = "iaps/2580.jpg"; preload = true; description = "stim_lookneu_2580_"; }; bitmap { filename = "iaps/7234.jpg"; preload = true; description = "stim_lookneu_7234_"; }; bitmap { filename = "iaps/2032.jpg"; preload = true; description = "stim_lookneu_2032_"; }; bitmap { filename = "iaps/6010.jpg"; preload = true; description = "stim_lookneu_6010_"; }; bitmap { filename = "iaps/2440.jpg"; preload = true; description = "stim_lookneu_2440_"; }; bitmap { filename = "iaps/2235.jpg"; preload = true; description = "stim_lookneu_2235_"; }; bitmap { filename = "iaps/2309.jpg"; preload = true; description = "stim_lookneu_2309_"; }; bitmap { filename = "iaps/5471.jpg"; preload = true; description = "stim_lookneu_5471_"; }; bitmap { filename = "iaps/2397.jpg"; preload = true; description = "stim_lookneu_2397_"; }; bitmap { filename = "iaps/8193.jpg"; preload = true; description = "stim_lookneu_8193_"; }; bitmap { filename = "iaps/7002.jpg"; preload = true; description = "stim_lookneu_7002_"; }; bitmap { filename = "iaps/7010.jpg"; preload = true; description = "stim_lookneu_7010_"; }; bitmap { filename = "iaps/7590.jpg"; preload = true; description = "stim_lookneu_7590_"; }; bitmap { filename = "iaps/7011.jpg"; preload = true; description = "stim_lookneu_7011_"; }; bitmap { filename = "iaps/7820.jpg"; preload = true; description = "stim_lookneu_7820_"; }; bitmap { filename = "iaps/9913.jpg"; preload = true; description = "stim_lookneu_9913_"; }; bitmap { filename = "iaps/1903.jpg"; preload = true; description = "stim_lookneu_1903_"; }; bitmap { filename = "iaps/2381.jpg"; preload = true; description = "stim_lookneu_2381_"; }; bitmap { filename = "iaps/2620.jpg"; preload = true; description = "stim_lookneu_2620_"; }; bitmap { filename = "iaps/7560.jpg"; preload = true; description = "stim_lookneu_7560_"; }; bitmap { filename = "iaps/7042.jpg"; preload = true; description = "stim_lookneu_7042_"; }; }IAPS_Look_Neutral; array{ # Look Negative Version 1 bitmap { filename = "iaps/9220.jpg"; preload = true; description = "stim_lookneg_9220_"; }; bitmap { filename = "iaps/1090.jpg"; preload = true; description = "stim_lookneg_1090_"; }; bitmap { filename = "iaps/9410.jpg"; preload = true; description = "stim_lookneg_9410_"; }; bitmap { filename = "iaps/6230.jpg"; preload = true; description = "stim_lookneg_6230_"; }; bitmap { filename = "iaps/2141.jpg"; preload = true; description = "stim_lookneg_2141_"; }; bitmap { filename = "iaps/1220.jpg"; preload = true; description = "stim_lookneg_1220_"; }; bitmap { filename = "iaps/1274.jpg"; preload = true; description = "stim_lookneg_1274_"; }; bitmap { filename = "iaps/3030.jpg"; preload = true; description = "stim_lookneg_3030_"; }; bitmap { filename = "iaps/6020.jpg"; preload = true; description = "stim_lookneg_6020_"; }; bitmap { filename = "iaps/6415.jpg"; preload = true; description = "stim_lookneg_6415_"; }; bitmap { filename = "iaps/1525.jpg"; preload = true; description = "stim_lookneg_1525_"; }; bitmap { filename = "iaps/9322.jpg"; preload = true; description = "stim_lookneg_9322_"; }; bitmap { filename = "iaps/2053.jpg"; preload = true; description = "stim_lookneg_2053_"; }; bitmap { filename = "iaps/2800.jpg"; preload = true; description = "stim_lookneg_2800_"; }; bitmap { filename = "iaps/2375.1.jpg"; preload = true; description = "stim_lookneg_2375.1_"; }; bitmap { filename = "iaps/9927.jpg"; preload = true; description = "stim_lookneg_9927_"; }; bitmap { filename = "iaps/9920.jpg"; preload = true; description = "stim_lookneg_9920_"; }; bitmap { filename = "iaps/9832.jpg"; preload = true; description = "stim_lookneg_9832_"; }; bitmap { filename = "iaps/9635.1.jpg"; preload = true; description = "stim_lookneg_9635.1_"; }; bitmap { filename = "iaps/9620.jpg"; preload = true; description = "stim_lookneg_9620_"; }; bitmap { filename = "iaps/9500.jpg"; preload = true; description = "stim_lookneg_9500_"; }; bitmap { filename = "iaps/9491.jpg"; preload = true; description = "stim_lookneg_9491_"; }; bitmap { filename = "iaps/9423.jpg"; preload = true; description = "stim_lookneg_9423_"; }; bitmap { filename = "iaps/6830.jpg"; preload = true; description = "stim_lookneg_6830_"; }; bitmap { filename = "iaps/9400.jpg"; preload = true; description = "stim_lookneg_9400_"; }; bitmap { filename = "iaps/9340.jpg"; preload = true; description = "stim_lookneg_9340_"; }; bitmap { filename = "iaps/9187.jpg"; preload = true; description = "stim_lookneg_9187_"; }; bitmap { filename = "iaps/9075.jpg"; preload = true; description = "stim_lookneg_9075_"; }; bitmap { filename = "iaps/9440.jpg"; preload = true; description = "stim_lookneg_9440_"; }; bitmap { filename = "iaps/7359.jpg"; preload = true; description = "stim_lookneg_7359_"; }; bitmap { filename = "iaps/6300.jpg"; preload = true; description = "stim_lookneg_6300_"; }; bitmap { filename = "iaps/6570.jpg"; preload = true; description = "stim_lookneg_6570_"; }; bitmap { filename = "iaps/6231.jpg"; preload = true; description = "stim_lookneg_6231_"; }; bitmap { filename = "iaps/3550.jpg"; preload = true; description = "stim_lookneg_3550_"; }; bitmap { filename = "iaps/9254.jpg"; preload = true; description = "stim_lookneg_9254_"; }; bitmap { filename = "iaps/2981.jpg"; preload = true; description = "stim_lookneg_2981_"; }; }IAPS_Look_Negative_1; array{ # Suppress Negative Version 1 bitmap { filename = "iaps/9941.jpg"; preload = true; description = "stim_suppress_9941_"; }; bitmap { filename = "iaps/2456.jpg"; preload = true; description = "stim_suppress_2456_"; }; bitmap { filename = "iaps/9560.jpg"; preload = true; description = "stim_suppress_9560_"; }; bitmap { filename = "iaps/9253.jpg"; preload = true; description = "stim_suppress_9253_"; }; bitmap { filename = "iaps/2683.jpg"; preload = true; description = "stim_suppress_2683_"; }; bitmap { filename = "iaps/2688.jpg"; preload = true; description = "stim_suppress_2688_"; }; bitmap { filename = "iaps/9280.jpg"; preload = true; description = "stim_suppress_9280_"; }; bitmap { filename = "iaps/1275.jpg"; preload = true; description = "stim_suppress_1275_"; }; bitmap { filename = "iaps/9300.jpg"; preload = true; description = "stim_suppress_9300_"; }; bitmap { filename = "iaps/2710.jpg"; preload = true; description = "stim_suppress_2710_"; }; bitmap { filename = "iaps/9181.jpg"; preload = true; description = "stim_suppress_9181_"; }; bitmap { filename = "iaps/6213.jpg"; preload = true; description = "stim_suppress_6213_"; }; bitmap { filename = "iaps/2751.jpg"; preload = true; description = "stim_suppress_2751_"; }; bitmap { filename = "iaps/9342.jpg"; preload = true; description = "stim_suppress_9342_"; }; bitmap { filename = "iaps/1111.jpg"; preload = true; description = "stim_suppress_1111_"; }; bitmap { filename = "iaps/8485.jpg"; preload = true; description = "stim_suppress_8485_"; }; bitmap { filename = "iaps/9911.jpg"; preload = true; description = "stim_suppress_9911_"; }; bitmap { filename = "iaps/9008.jpg"; preload = true; description = "stim_suppress_9008_"; }; bitmap { filename = "iaps/9630.jpg"; preload = true; description = "stim_suppress_9630_"; }; bitmap { filename = "iaps/9610.jpg"; preload = true; description = "stim_suppress_9610_"; }; bitmap { filename = "iaps/9561.jpg"; preload = true; description = "stim_suppress_9561_"; }; bitmap { filename = "iaps/9590.jpg"; preload = true; description = "stim_suppress_9590_"; }; bitmap { filename = "iaps/2811.jpg"; preload = true; description = "stim_suppress_2811_"; }; bitmap { filename = "iaps/9413.jpg"; preload = true; description = "stim_suppress_9413_"; }; bitmap { filename = "iaps/9295.jpg"; preload = true; description = "stim_suppress_9295_"; }; bitmap { filename = "iaps/3062.jpg"; preload = true; description = "stim_suppress_3062_"; }; bitmap { filename = "iaps/9325.jpg"; preload = true; description = "stim_suppress_9325_"; }; bitmap { filename = "iaps/9250.jpg"; preload = true; description = "stim_suppress_9250_"; }; bitmap { filename = "iaps/9007.jpg"; preload = true; description = "stim_suppress_9007_"; }; bitmap { filename = "iaps/3061.jpg"; preload = true; description = "stim_suppress_3061_"; }; bitmap { filename = "iaps/3051.jpg"; preload = true; description = "stim_suppress_3051_"; }; bitmap { filename = "iaps/6563.jpg"; preload = true; description = "stim_suppress_6563_"; }; bitmap { filename = "iaps/6210.jpg"; preload = true; description = "stim_suppress_6210_"; }; bitmap { filename = "iaps/9301.jpg"; preload = true; description = "stim_suppress_9301_"; }; bitmap { filename = "iaps/3160.jpg"; preload = true; description = "stim_suppress_3160_"; }; bitmap { filename = "iaps/3005.1.jpg"; preload = true; description = "stim_suppress_3005.1_"; }; }IAPS_Suppress_Negative_1; array{ # Look Negative Version 2 bitmap { filename = "iaps/9941.jpg"; preload = true; description = "stim_suppress_9941_"; }; bitmap { filename = "iaps/2456.jpg"; preload = true; description = "stim_suppress_2456_"; }; bitmap { filename = "iaps/9560.jpg"; preload = true; description = "stim_suppress_9560_"; }; bitmap { filename = "iaps/9253.jpg"; preload = true; description = "stim_suppress_9253_"; }; bitmap { filename = "iaps/2683.jpg"; preload = true; description = "stim_suppress_2683_"; }; bitmap { filename = "iaps/2688.jpg"; preload = true; description = "stim_suppress_2688_"; }; bitmap { filename = "iaps/9280.jpg"; preload = true; description = "stim_suppress_9280_"; }; bitmap { filename = "iaps/1275.jpg"; preload = true; description = "stim_suppress_1275_"; }; bitmap { filename = "iaps/9300.jpg"; preload = true; description = "stim_suppress_9300_"; }; bitmap { filename = "iaps/2710.jpg"; preload = true; description = "stim_suppress_2710_"; }; bitmap { filename = "iaps/9181.jpg"; preload = true; description = "stim_suppress_9181_"; }; bitmap { filename = "iaps/6213.jpg"; preload = true; description = "stim_suppress_6213_"; }; bitmap { filename = "iaps/2751.jpg"; preload = true; description = "stim_suppress_2751_"; }; bitmap { filename = "iaps/9342.jpg"; preload = true; description = "stim_suppress_9342_"; }; bitmap { filename = "iaps/1111.jpg"; preload = true; description = "stim_suppress_1111_"; }; bitmap { filename = "iaps/8485.jpg"; preload = true; description = "stim_suppress_8485_"; }; bitmap { filename = "iaps/9911.jpg"; preload = true; description = "stim_suppress_9911_"; }; bitmap { filename = "iaps/9008.jpg"; preload = true; description = "stim_suppress_9008_"; }; bitmap { filename = "iaps/9630.jpg"; preload = true; description = "stim_suppress_9630_"; }; bitmap { filename = "iaps/9610.jpg"; preload = true; description = "stim_suppress_9610_"; }; bitmap { filename = "iaps/9561.jpg"; preload = true; description = "stim_suppress_9561_"; }; bitmap { filename = "iaps/9590.jpg"; preload = true; description = "stim_suppress_9590_"; }; bitmap { filename = "iaps/2811.jpg"; preload = true; description = "stim_suppress_2811_"; }; bitmap { filename = "iaps/9413.jpg"; preload = true; description = "stim_suppress_9413_"; }; bitmap { filename = "iaps/9295.jpg"; preload = true; description = "stim_suppress_9295_"; }; bitmap { filename = "iaps/3062.jpg"; preload = true; description = "stim_suppress_3062_"; }; bitmap { filename = "iaps/9325.jpg"; preload = true; description = "stim_suppress_9325_"; }; bitmap { filename = "iaps/9250.jpg"; preload = true; description = "stim_suppress_9250_"; }; bitmap { filename = "iaps/9007.jpg"; preload = true; description = "stim_suppress_9007_"; }; bitmap { filename = "iaps/3061.jpg"; preload = true; description = "stim_suppress_3061_"; }; bitmap { filename = "iaps/3051.jpg"; preload = true; description = "stim_suppress_3051_"; }; bitmap { filename = "iaps/6563.jpg"; preload = true; description = "stim_suppress_6563_"; }; bitmap { filename = "iaps/6210.jpg"; preload = true; description = "stim_suppress_6210_"; }; bitmap { filename = "iaps/9301.jpg"; preload = true; description = "stim_suppress_9301_"; }; bitmap { filename = "iaps/3160.jpg"; preload = true; description = "stim_suppress_3160_"; }; bitmap { filename = "iaps/3005.1.jpg"; preload = true; description = "stim_suppress_3005.1_"; }; }IAPS_Look_Negative_2; array{ # Suppress Negative Version 2 bitmap { filename = "iaps/9220.jpg"; preload = true; description = "stim_lookneg_9220_"; }; bitmap { filename = "iaps/1090.jpg"; preload = true; description = "stim_lookneg_1090_"; }; bitmap { filename = "iaps/9410.jpg"; preload = true; description = "stim_lookneg_9410_"; }; bitmap { filename = "iaps/6230.jpg"; preload = true; description = "stim_lookneg_6230_"; }; bitmap { filename = "iaps/2141.jpg"; preload = true; description = "stim_lookneg_2141_"; }; bitmap { filename = "iaps/1220.jpg"; preload = true; description = "stim_lookneg_1220_"; }; bitmap { filename = "iaps/1274.jpg"; preload = true; description = "stim_lookneg_1274_"; }; bitmap { filename = "iaps/3030.jpg"; preload = true; description = "stim_lookneg_3030_"; }; bitmap { filename = "iaps/6020.jpg"; preload = true; description = "stim_lookneg_6020_"; }; bitmap { filename = "iaps/6415.jpg"; preload = true; description = "stim_lookneg_6415_"; }; bitmap { filename = "iaps/1525.jpg"; preload = true; description = "stim_lookneg_1525_"; }; bitmap { filename = "iaps/9322.jpg"; preload = true; description = "stim_lookneg_9322_"; }; bitmap { filename = "iaps/2053.jpg"; preload = true; description = "stim_lookneg_2053_"; }; bitmap { filename = "iaps/2800.jpg"; preload = true; description = "stim_lookneg_2800_"; }; bitmap { filename = "iaps/2375.1.jpg"; preload = true; description = "stim_lookneg_2375.1_"; }; bitmap { filename = "iaps/9927.jpg"; preload = true; description = "stim_lookneg_9927_"; }; bitmap { filename = "iaps/9920.jpg"; preload = true; description = "stim_lookneg_9920_"; }; bitmap { filename = "iaps/9832.jpg"; preload = true; description = "stim_lookneg_9832_"; }; bitmap { filename = "iaps/9635.1.jpg"; preload = true; description = "stim_lookneg_9635.1_"; }; bitmap { filename = "iaps/9620.jpg"; preload = true; description = "stim_lookneg_9620_"; }; bitmap { filename = "iaps/9500.jpg"; preload = true; description = "stim_lookneg_9500_"; }; bitmap { filename = "iaps/9491.jpg"; preload = true; description = "stim_lookneg_9491_"; }; bitmap { filename = "iaps/9423.jpg"; preload = true; description = "stim_lookneg_9423_"; }; bitmap { filename = "iaps/6830.jpg"; preload = true; description = "stim_lookneg_6830_"; }; bitmap { filename = "iaps/9400.jpg"; preload = true; description = "stim_lookneg_9400_"; }; bitmap { filename = "iaps/9340.jpg"; preload = true; description = "stim_lookneg_9340_"; }; bitmap { filename = "iaps/9187.jpg"; preload = true; description = "stim_lookneg_9187_"; }; bitmap { filename = "iaps/9075.jpg"; preload = true; description = "stim_lookneg_9075_"; }; bitmap { filename = "iaps/9440.jpg"; preload = true; description = "stim_lookneg_9440_"; }; bitmap { filename = "iaps/7359.jpg"; preload = true; description = "stim_lookneg_7359_"; }; bitmap { filename = "iaps/6300.jpg"; preload = true; description = "stim_lookneg_6300_"; }; bitmap { filename = "iaps/6570.jpg"; preload = true; description = "stim_lookneg_6570_"; }; bitmap { filename = "iaps/6231.jpg"; preload = true; description = "stim_lookneg_6231_"; }; bitmap { filename = "iaps/3550.jpg"; preload = true; description = "stim_lookneg_3550_"; }; bitmap { filename = "iaps/9254.jpg"; preload = true; description = "stim_lookneg_9254_"; }; bitmap { filename = "iaps/2981.jpg"; preload = true; description = "stim_lookneg_2981_"; }; }IAPS_Suppress_Negative_2; bitmap { filename = "iaps/1121.jpg"; }IAPSBit; picture { bitmap IAPSBit; x=0; y=0; }IAPSPic; #================================================================================================= #TRIALS #================================================================================================= #----- IAPS Picture Presentation -------- trial{ stimulus_event{ picture IAPSPic; time=0; duration=3000; }IAPSEvent; }IAPSTrial; #----- ITI -------- trial { trial_duration = 500; trial_type = fixed; stimulus_event { picture { text {caption = "+"; font_size = 60;}ITIText; x = 0; y = 0; }ITI1; }ITIEvent; }ITITrial; #----- Exit Program -------- trial { trial_duration = forever; trial_type = specific_response; terminator_button = 3; stimulus_event { picture {text ExitProgramText;x = 0; y = 0;}; } ExitProgramEvent; }ExitProgramTrial; #==================================================================================================== #BEGIN PCL #==================================================================================================== begin_pcl; # set up mouse mouse mouse1 = response_manager.get_mouse(1); mouse1.set_min_max( 2, -300, 300 ); mouse1.set_restricted( 2, true ); mouse1.set_xy( 0, -300 ); #==================================================================================================== #RATING SCALES IN PCL #==================================================================================================== #-----Affect Rating---------- # Subroutine to draw the scale. # Pass an array of double precision numbers for marker positions # and an array of strings for the corresponding labels sub drawscale7( double& min7, double& max7, array<double,1>& markers7 , array<string,1>& labels7 ) begin double ym7 = 600.0 / (max7 - min7); # calculate y multiplier for scale # Build the scale: line_graphic slider7 = new line_graphic; slider7.set_line_width( 12.0 ); slider7.set_line_color( 0, 0, 0, 255 ); slider7.add_line( -25.0, 0.0, 25.0, 0.0 ); slider7.redraw(); scale7.add_part( slider7, 0, 0 ); line_graphic track7 = new line_graphic; track7.set_line_width( 10.0 ); track7.set_line_color( 0, 0, 0, 255 ); track7.add_line( 0.0, -302.0, 0.0, 301.0 ); track7.redraw(); scale7.add_part( track7, 0, 0 ); line_graphic tick7 = new line_graphic; tick7.set_line_width( 5.0 ); tick7.set_line_color( 0, 0, 0, 255 ); tick7.add_line( 0.0, 0.0, 40.0, 0.0 ); tick7.redraw(); loop int j = 1 until j > markers7.count() begin # add a tick mark to the scale: scale7.add_part( tick7, 0, int( (markers7[j]-min7) * ym7 - 300.0 ) ); # define the text of the label: scale_labels7[j].set_caption(labels7[j]); scale_labels7[j].redraw(); # complicated stuff required to left-align the labels: int xx = 50 + int( scale_labels7[j].width() / 2.0 ); # add the label to the scale: scale7.add_part( scale_labels7[j], xx, int( (markers7[j]-min7) * ym7 - 298.0) ); j = j + 1 end; scale7.set_part_on_top( 3, true ); end; #------------------------------------------------------------------- # Subroutine to display a vertical scale and collect a response. # Pass an array of double precision numbers for marker positions # and an array of strings for the corresponding labels sub double runvscale7( double& min7, double& max7, array<double,1>& markers7 , array<string,1>& labels7 ) begin double ym7 = 600.0 / (max7 - min7); # calculate y multiplier for scale int rt_start = clock.time(); # Show scale until button pressed: loop int count = response_manager.total_response_count( 1 ) until response_manager.total_response_count( 1 ) > count begin mouse1.poll(); #read the mouse scale7.set_part_y( 3, mouse1.y() ); #position the slider scale7.present(); end; double rating7a = double((mouse1.y() + 300)) / ym7 + min7; AffectRateEvent.set_event_code( "affect_rating_" + string( rating7a ) ); AffectRateTrial.present(); return rating7a; end; double min7 = -100.0; double max7 = 100.0; array< double > markers7[9] = { -100.0, -75.0, -50.0, -25.0, 0, 25.0, 50.0, 75.0, 100.0}; array< string > labels7[9] = { "1 非常不愉快", "2", "3", "4", "5", "6", "7", "8", "9 非常愉快" }; #-----Success Rating---------- # Subroutine to draw the scale. # Pass an array of double precision numbers for marker positions # and an array of strings for the corresponding labels sub drawscale8( double& min8, double& max8, array<double,1>& markers8 , array<string,1>& labels8 ) begin double ym8 = 600.0 / (max8 - min8); # calculate y multiplier for scale # Build the scale: line_graphic slider8 = new line_graphic; slider8.set_line_width( 12.0 ); slider8.set_line_color( 0, 0, 0, 255 ); slider8.add_line( -25.0, 0.0, 25.0, 0.0 ); slider8.redraw(); scale8.add_part( slider8, 0, 0 ); line_graphic track8 = new line_graphic; track8.set_line_width( 10.0 ); track8.set_line_color( 0, 0, 0, 255 ); track8.add_line( 0.0, -302.0, 0.0, 301.0 ); track8.redraw(); scale8.add_part( track8, 0, 0 ); line_graphic tick8 = new line_graphic; tick8.set_line_width( 5.0 ); tick8.set_line_color( 0, 0, 0, 255 ); tick8.add_line( 0.0, 0.0, 40.0, 0.0 ); tick8.redraw(); loop int j = 1 until j > markers8.count() begin # add a tick mark to the scale: scale8.add_part( tick8, 0, int( (markers8[j]-min8) * ym8 - 300.0 ) ); # define the text of the label: scale_labels8[j].set_caption(labels8[j]); scale_labels8[j].redraw(); # complicated stuff required to left-align the labels: int xx = 50 + int( scale_labels8[j].width() / 2.0 ); # add the label to the scale: scale8.add_part( scale_labels8[j], xx, int( (markers8[j]-min8) * ym8 - 298.0) ); j = j + 1 end; scale8.set_part_on_top( 3, true ); end; #------------------------------------------------------------------- # Subroutine to display a vertical scale and collect a response. # Pass an array of double precision numbers for marker positions # and an array of strings for the corresponding labels sub double runvscale8( double& min8, double& max8, array<double,1>& markers8 , array<string,1>& labels8 ) begin double ym8 = 600.0 / (max8 - min8); # calculate y multiplier for scale int rt_start = clock.time(); # Show scale until button pressed: loop int count = response_manager.total_response_count( 1 ) until response_manager.total_response_count( 1 ) > count begin mouse1.poll(); #read the mouse scale8.set_part_y( 3, mouse1.y() ); #position the slider scale8.present(); end; double rating8a = double((mouse1.y() + 300)) / ym8 + min8; SuccessRateEvent.set_event_code( "success_rating_" + string( rating8a ) ); SuccessRateTrial.present(); return rating8a; end; double min8 = -100.0; double max8 = 100.0; array< double > markers8[9] = { -100.0, -75.0, -50.0, -25.0, 0, 25.0, 50.0, 75.0, 100.0}; array< string > labels8[9] = { "1 完全没成功", "2", "3", "4", "5", "6", "7", "8", "9 非常成功" }; #draw scales drawscale7(min7, max7, markers7, labels7 ); drawscale8(min8, max8, markers8, labels8 ); #==================================================================================================== #2D IMAGE ARRAYS FOR RANDOMIZATION #==================================================================================================== #put IAPS condition arrays into one array for randomizing - Version 1 array<bitmap>IAPS_1[3][36]; IAPS_1[1].assign( IAPS_Look_Neutral ) ; IAPS_1[2].assign ( IAPS_Look_Negative_1 ) ; IAPS_1[3].assign ( IAPS_Suppress_Negative_1 ) ; #put IAPS condition arrays into one array for randomizing - Version 2 array<bitmap>IAPS_2[3][36]; IAPS_2[1].assign( IAPS_Look_Neutral ) ; IAPS_2[2].assign ( IAPS_Look_Negative_2 ) ; IAPS_2[3].assign ( IAPS_Suppress_Negative_2 ) ; #==================================================================================================== #IMAGE RANDOMIZATION #==================================================================================================== #temporary array to hold all possible array numbers array<int> which_array_IAPS_1[IAPS_1.count()]; which_array_IAPS_1.fill( 1, 0, 1, 1 ); which_array_IAPS_1.shuffle(); #temporary array to hold all possible stim numbers array<int>which_stim_IAPS_1[IAPS_1.count()][0]; loop int i = 1 until i > which_stim_IAPS_1.count() begin loop int j = 1 until j > IAPS_1[i].count() begin which_stim_IAPS_1[i].add( j ); j = j + 1; end; which_stim_IAPS_1[i].shuffle(); i = i + 1; end; array<int>stim_order_IAPS_1[0][0]; #now use a loop to make a full stim order array<int>stim_ctrs_IAPS_1[IAPS_1.count()]; stim_ctrs_IAPS_1.fill( 1, 0, 1, 0 ); loop int array_ctr = 1; int i = 1 until i > IAPS_1.count() * IAPS_1[1].count() begin int this_array = which_array_IAPS_1[array_ctr]; int this_stim = which_stim_IAPS_1[this_array][stim_ctrs_IAPS_1[this_array]]; array<int> temp[2]; temp[1] = this_array; temp[2] = this_stim; stim_order_IAPS_1.add( temp ); #recycle the array counter once we've gone through them all array_ctr = array_ctr + 1; if ( array_ctr > IAPS_1.count() ) then array_ctr = 1; which_array_IAPS_1.shuffle(); end; stim_ctrs_IAPS_1[this_array] = stim_ctrs_IAPS_1[this_array] + 1; i = i + 1; end; #==================================================================================================== #MAIN #==================================================================================================== #Baseline Fixation ITITrial.set_duration(1000); ITIEvent.set_event_code("fix"); ITITrial.present(); loop int i = 1; int stim_ctr = 1; until stim_ctr > 108 begin int this_array = stim_order_IAPS_1[i][1]; int this_stim = stim_order_IAPS_1[i][2]; #Picture Presentation IAPSPic.set_part( 1, IAPS_1[this_array][this_stim]); IAPSEvent.set_event_code( IAPS_1[this_array][this_stim].description() + string( stim_ctr ) ); IAPSTrial.present(); #Affect Rating line_graphic slider7 = new line_graphic; scale7.remove_part(3); slider7.set_line_width( 12.0 ); slider7.set_line_color( 255, 0, 0, 255 ); slider7.add_line( -25.0, 0.0, 25.0, 0.0 ); slider7.redraw(); scale7.insert_part(3, slider7, 0, 0); scale7.set_part_on_top( 3, true ); #show scale mouse1.set_min_max(2, -300, 300); mouse1.set_xy( 0, -300 ); runvscale7 (min7, max7, markers7, labels7 ); #ITI int fix = 1000; ITITrial.set_duration(fix); ITITrial.present(); #Success rating line_graphic slider8 = new line_graphic; scale8.remove_part(3); slider8.set_line_width( 12.0 ); slider8.set_line_color( 255, 0, 0, 255 ); slider8.add_line( -25.0, 0.0, 25.0, 0.0 ); slider8.redraw(); scale8.insert_part(3, slider8, 0, 0); scale8.set_part_on_top( 3, true ); #show scale mouse1.set_min_max(2, -300, 300); mouse1.set_xy( 0, -300 ); runvscale8 (min8, max8, markers8, labels8 ); #ITI ITIEvent.set_duration(fix); ITITrial.present(); i = i + 1; stim_ctr = stim_ctr + 1; end; #Close Program ExitProgramEvent.set_event_code("exit_program"); ExitProgramTrial.present();
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clc clear //Input data p1=15//Pressure in bar T1=300+273//Temperature in K p2=10//Pressure in bar nn=95//Nozzle efficiency in percent a=20//Nozzle angle in degrees x=5//The blade exit angle is 5 degrees less than the inlet angle f=0.9//Friction factor m=1350//Steam flow rate in kg/h //Calculations h1=3038.9//Enthalpy in kJ/kg s1=6.9224//Entropy in kJ/kg.K s2=s1//Entropy in kJ/kg.K t2s=250//Temperature in degree C h2s=2943.1//Enthalpy in kJ/kg V1=44.72*sqrt((nn/100)*(h1-h2s))//Velocity in m/s Vb=V1*(cosd(a)/2)//Velocity in m/s b1=atand((V1*sind(a))/((V1*cosd(a))-Vb))//Blade angle in degrees b2=b1-x//Blade angle in degrees Vr1=((V1*sind(a))/sind(b1))//Velocity in m/s Vr2=(f*Vr1)//Velocity in m/s dVw=(Vr1*cosd(b1))+(Vr2*cosd(b2))//Velocity in m/s dVa=(Vr1*sind(b1))-(Vr2*sind(b2))//Velocity in m/s Pa=(m/3600)*dVa//Axial thrust in N Pt=(m/3600)*dVw//Tangential thrust in N WD=(Pt*Vb*10^-3)//Diagram Power in kW dn=((WD*1000)/((1/2)*(m/3600)*V1^2))*100//Diagram efficiency in percent //Output printf('(a) Axial thrust is %3.2f N \n Tangential thrust is %3.2f N \n\n (b) Diagram Power is %3.3f kW \n\n (c) Diagram Efficiency is %3.1f percent',Pa,Pt,WD,dn)
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//Chapter 2, Problem 8, Figure 2.8 clc; V1=20; //Voltage of resistor A I1=20*10^-3; //Current of resistor A V2=16; //Voltage of resistor B I2=5*10^-3; //Current of resistor B R1=V1/I1; //Calculating resistance of resistor A using Ohms law R2=V2/I2; //Calculating resistance of resistor B using Ohms law printf("Resistance of resistor A = %d k.ohms\n\n\n",R1/1000); printf("Resistance of resistor B = %f k.ohms\n\n\n",R2/1000);
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// Scilab code Exa2.2.3 To calculate the energy required to remove a neutron from Kr-81, Kr-82, Kr-83 : Page 68 (2011) // For Kr-80, m_p = 1.007825; // Mass of proton, amu m_n = 1.008665; // Mass of neutron, amu Z = 36; // Number of protons N_80 = 44; // Number of neutrons M_n_80 = 79.91628; // Mass of Kr nucleus BE_Kr_80 = (Z*m_p+N_80*m_n-M_n_80)*931.49; // Binding energy for Kr-80, MeV // For Kr-81, N_81 = 45; // Number of neutrons M_n_81 = 80.91661; // Mass of Kr-81 nucleus BE_Kr_81 = (Z*m_p+N_81*m_n-M_n_81)*931.49; // Binding energy for Kr-81 nucleus // For Kr-82 N_82 = 46; // Number of neutrons M_n_82 = 81.913482; // Mass of Kr nucleus BE_Kr_82 = (Z*m_p+N_82*m_n-M_n_82)*931.49; // Binding energy for Kr-82,MeV // For Kr-83 N_83 = 47; // Number of protons M_n_83 = 82.914134; // Mass of Kr-83 nucleus BE_Kr_83 = (Z*m_p+N_83*m_n-M_n_83)*931.49; // Binding energy for Kr-83, MeV E_sep_81 = BE_Kr_81-BE_Kr_80; // Energy seperation of neutron for Kr-81, MeV E_sep_82 = BE_Kr_82-BE_Kr_81; // Energy seperation of neutron for Kr-82, MeV E_sep_83 = BE_Kr_83-BE_Kr_82; // Energy seperation of neutron for Kr-83, MeV , printf("\nEnergy seperation of neutron for Kr-81 = %4.2f MeV\nEnergy seperation of neutron for Kr-82 = %4.2f MeV\nEnergy seperation of neutron for Kr-83 = %5.2f MeV", E_sep_81, E_sep_82, E_sep_83); // Result // Energy seperation of neutron for Kr-81 = 7.76 MeV // Energy seperation of neutron for Kr-82 = 10.99 MeV // Energy seperation of neutron for Kr-83 = 7.46 MeV
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clc function v=f(t), v=200*sin(377*t), endfunction //Defining functions function i=f1(t), i=8*sin(377*t-%pi/6), endfunction V=200/sqrt(2); //Assigning values to parameters I=8/sqrt(2); P=V*I*cos(%pi/6) disp("Watts",P,"Active Power"); Q=V*I*sin(%pi/6); disp("VAR",Q,"Reactive Power"); S=V*I; disp("VA",S,"Apparent Power");
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clc //initialisation of variables S= 1.6315 //Btu/lb R //CALCULATIONS P= 70 //psia t= 302.92 //F h= 1180.6 //Btu/lb //RESULTS printf ('Pressure= %.2f Psia',P) printf (' \n Temperature = %.2f F',t) printf (' \n Enthalpy= %.1f Btu/lb',h)
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xhat=[1 2 3 4 5]; nd=4; y=icceps(xhat,nd); disp(y); // output // column 1 to 3 // // 653803.49 653803.47 653803.47 // // column 4 to 5 // // 653803.45 653803.5
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clear; clc; // Stoichiometry // Chapter 5 // Energy Balances // Example 5.15 // Page 238 printf("Example 5.15, Page 238 \n \n"); // solution qv1 = 50 // l/s qm = qv1*1.08 // kg/s fi = qm*3.08*(263.15-258.15) // kW lv = 384.19-168.7 // kJ/kg qm2 = fi/lv H = 256.35 // kJ/kg x = poly(0, 'x') p = H*(qm2+x) - 168.7*qm2-x*384.19 a = qm2+roots(p) printf(" Flow of vapor from he chiller = "+string(a)+" kg/s.")
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function y=T(n) S=................. y=................. while ............. tirage = grand(1,1,'uin',1,n) S=S+tirage y=............. end endfunction
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function [Ack] = AutoGenSciHelpSet() global bOK; global sciobj; Ack = %f; SciDesSet(); if(bOK) then setsize = strtod(sciobj.Input); for i = 1 : setsize SciParamSet("Input",i); if ~bOK then disp("在第"+string(i)+"个输入参数时退出."); return; end end else disp("退出帮助文档自动生成流程."); return; end if(bOK) then setsize = strtod(sciobj.Output); for i = 1 : setsize SciParamSet("Output",i); if ~bOK then disp("在第"+string(i)+"个输出参数时退出."); return; end end else disp("退出帮助文档自动生成流程."); return; end GenSciHelpXml(); Ack = %t; endfunction
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errcatch(-1,"stop");mode(2);//Example 1_2 ; ; //Given data dv_dt=190;//V/µs IC=8*10^-3;//A //Solution : C=IC/(dv_dt/10^-6);//F disp(C,"Capacitance of depletion layer in F : "); exit();
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//Part A Chapter 7 Example 4 clc; clear; close; T=110+273.15;//K h=50;//cm p=143.47;//kPa(at 110 degree C) g=9.81;//ravity constant p_dash=p-(1000*g*h/100)/1000;//kPa(pressure at 50 cm depth) Tsat=108.866;//degree C(for pdash=138.365 kPa); disp("Pressure at 50 cm depth is "+string(p_dash)+" kPa. From steam table, Boiling point = "+string(Tsat)+" degree C");
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6_28.sce
clc,clear printf('Example 6.28\n\n') kW=[250,300,150] cosphi=[0.9,0.75,0.8] //all lagging tanphi=tan(acos(cosphi)) kVAR=kW.*tanphi kW_total=kW(1)+kW(2)+kW(3) kVAR_total=kVAR(1)+kVAR(2)+kVAR(3) phi_1=acos(0.8)//pf of machine 1 kW_1=100 //active component of machine 1 kVAR_1=kW_1*tan(phi_1) //reactive component of machine 1 kW_2=kW_total - kW_1 //active component of machine 1 kVAR_2=kVAR_total-kVAR_1 //reactive component of machine 2 phi_2=atan(kVAR_2/kW_2) pf_2=cos(phi_2) //power factor of machine 2 printf('Output of second alternator= %.0f kW',kW_2) printf('\npower factor of machine 2 = %.4f and lagging',pf_2)
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bozhink/Code-Chunks
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laplacian.sce
i=-2.; e=1.; t=0.; A20x20 = [ i e t t t t t t t t t t t t t t t t t t t t; e i e t t t t t t t t t t t t t t t t t t t; t e i e t t t t t t t t t t t t t t t t t t; t t e i e t t t t t t t t t t t t t t t t t; t t t e i e t t t t t t t t t t t t t t t t; t t t t e i e t t t t t t t t t t t t t t t; t t t t t e i e t t t t t t t t t t t t t t; t t t t t t e i e t t t t t t t t t t t t t; t t t t t t t e i e t t t t t t t t t t t t; t t t t t t t t e i e t t t t t t t t t t t; t t t t t t t t t e i e t t t t t t t t t t; t t t t t t t t t t e i e t t t t t t t t t; t t t t t t t t t t t e i e t t t t t t t t; t t t t t t t t t t t t e i e t t t t t t t; t t t t t t t t t t t t t e i e t t t t t t; t t t t t t t t t t t t t t e i e t t t t t; t t t t t t t t t t t t t t t e i e t t t t; t t t t t t t t t t t t t t t t e i e t t t; t t t t t t t t t t t t t t t t t e i e t t; t t t t t t t t t t t t t t t t t t e i e t; t t t t t t t t t t t t t t t t t t t e i e; t t t t t t t t t t t t t t t t t t t t e i; ]*0.5; B20x20 = inv(A20x20); h = 0.1; a = 2.0; b = a+max(size(A20x20))*h; x = (linspace(a,b,max(size(A20x20))))'; k = sqrt(3.0); s=0.1*(rand(1,max(size(x)))-0.5); psi = exp(-%i*k*(x+s'))+s'; function z=border(psi) z=psi; z(1)=0.0; z(max(size(psi)))=0.0; //z=z/max(abs(real(z))); return; endfunction; function z=setA(n) if n<2 then disp("ERROR: n must be at least 2"); z=0; return; end; z=0.0*ones(n,n); z(1,1)=-2.0; z(1,2)=1.0; z(n,n)=-2.0; z(n,n-1)=1.0; for i=2:n-1; z(i,i) = -2.0; z(i,i-1)=1.0; z(i,i+1)=1.0; end; endfunction; A=setA(300); B=inv(A); h = 0.001; a = -0.1; b = a+max(size(A))*h; x = (linspace(a,b,max(size(A))))'; k = sqrt(190.0); s=(rand(1,max(size(x)))-0.5); psi = exp(-%i*k*(x+s'))+s';
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/3871/CH5/EX5.2/Ex5_2.sce
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FOSSEE/Scilab-TBC-Uploads
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refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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37,975,407
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Ex5_2.sce
//=========================================================================== //chapter 5 example 2 clc;clear all; //Variable declaration I = 5; //current in A d = 30; //deflection I2 = 10; //calculations //L = 10+5*theta - 2*(theta^2) //inductancein uH //partial differentiate w.r.t to theta //dL/dtheta = x = 5- 4*theta //dL/dtheta = 2*K*theta/(I^2) //x = 10-4*theta theta = %pi/(6); K = (((5-(4*theta))*10^-6)*(I^2))/(2*theta) //spring constant in Nm/radian x = ((2*K)/(I2^2))*10^6; theta2 = (5)/(x+4); //result mprintf("spring constant = %3.4e Nm/radian",K); mprintf("\ndeflection for 10 A current = %3.3f radian",theta2);
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nickgreenquist/Intro_To_Intelligent_Systems
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refs/heads/master
2021-01-20T13:23:23.931062
2017-05-04T20:08:05
2017-05-04T20:08:05
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result1.tst
@relation led7digit @attribute Led1 real[0.0,1.0] @attribute Led2 real[0.0,1.0] @attribute Led3 real[0.0,1.0] @attribute Led4 real[0.0,1.0] @attribute Led5 real[0.0,1.0] @attribute Led6 real[0.0,1.0] @attribute Led7 real[0.0,1.0] @attribute number{0,1,2,3,4,5,6,7,8,9} @inputs Led1,Led2,Led3,Led4,Led5,Led6,Led7 @outputs number @data 0 0 4 4 0 0 1 1 2 ? 2 ? 2 2 3 1 3 ? 6 ? 8 ? 3 3 4 4 5 5 7 ? 8 6 3 3 7 1 8 8 0 ? 3 2 7 7 8 8 9 4 9 9 0 6 0 0 1 1 8 8 9 9 2 2 3 3 6 5 6 ? 5 5 6 5 6 6 7 1 1 1 4 4 4 9 5 5 6 6 7 7 8 ? 9 3 1 ? 4 4 5 5 8 8
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refs/heads/master
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exec("/home/m/n/mneus/TP_AN/TP2/gauss.sci"); h = 0.01; n = 5; A = 2*eye(n,n) + (-1)*(diag(ones(1, n-1), 1) + diag(ones(1, n-1), -1)) B = (h^2)*ones(n, 1) //thetaG = GaussPivotPartiel(A, B) //thetaG = inv(A)*B X0 = 10*ones(n, 1); eps = 0.001; N = 100; [X, i] = GaussSeidel(A, B, X0, eps, N)
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royceda/Math-finance
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refs/heads/master
2021-01-10T04:22:52.831869
2015-11-25T22:06:16
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//Rappel function [p] = d1(x,t,K,T,r,sigma) a = log(x/K)+(r+sigma**2/2)*(T-t) p = a /(sigma*sqrt(T-t)) endfunction test = d1(10,100,100,30,0.05,0.1) function [p] = d2(x,t,K,T,r,sigma) p = d1(x,t,K,T,r,sigma) - sigma*sqrt(T-t) endfunction test = d2(10,100,100,30,0.05,0.1) function [p] = Call(x, t, T, K, r, sigma) first = x*cdfnor("PQ",d1(x,t,K,T,r,sigma),0,1); second = K*exp(-r*(T-t))*cdfnor("PQ",d2(x,t,K,T,r,sigma),0,1); p = first - second; endfunction function [p] = Put(x, t, T, K, r, sigma) first = x*cdfnor("PQ",-d1(x,t,K,T,r,sigma),0,1); second = K*exp(-r*(T-t))*cdfnor("PQ",-d2(x,t,K,T,r,sigma),0,1); p = -first + second; endfunction //_______________________________________________________ t = 0; x = 1000; T = 100; K = 1000; r = 0.005; sigma = 0.1; n = 1000; X = grand(n,1,'nor',0,1); function [p] = g(X, x, t, T, K, r, sigma) first = K*exp(-r*(T-t)); second = x*exp(sigma*X*sqrt(T-t)) *exp(-((T-t)*sigma**2)/2) p = max(0, first - second); endfunction test = g(X(1), x, t, T, K, r, sigma); //evaluation with Monte Carlo method function [p] = eval_Put(X, x, t, T, K, r, sigma, n) tmp = 0; for i = 1:n tmp = tmp + g(X(i), x, t, T, K, r, sigma)/n; end p = tmp endfunction function [p]= error_Rate(X, x, t, T, K, r, sigma, n) tmp = 0; I = eval_Put(X, x, t, T, K, r, sigma, n); for i = 1:n tmp = tmp + (g(X(i), x, t, T, K, r) - I)**2/(n-1); end p = tmp; endfunction function [p] = boundary(X, x, t, T, K, r, sigma, n) I = eval_Put(X, x, t, T, K, r, sigma, n); A = error_Rate(X, x, t, T, K, r, sigma, n) p = [I - 1.96*sqrt(A/n), I + 1.96*sqrt(A/n)]; endfunction function [p] = test1(X, x, t, T, K, r, sigma, y) for i = 1:length(y) a(i) = eval_Put(X, x, t, T, K, r, sigma, y(i)); end p = [a]; endfunction function [p] = test2(X, x, t, T, K, r, sigma, y) for i = 1:length(y) b(i) = Put(x, t, T, K, r, sigma); end p = [b]; endfunction function [p] = test3(X, x, t, T, K, r, sigma, y,n) b = boundary(X, x, t, T, K, r, sigma, n) for i = 1:length(y) c(i) = b(1); end p = [c]; endfunction function [p] = test4(X, x, t, T, K, r, sigma, y, n) b = boundary(X, x, t, T, K, r, sigma, n) for i = 1:length(y) c(i) = b(2); end p = [c]; endfunction n = 10 y = [1:1:n]; X = grand(n,1,'nor',0,1); //clf(); //plot2d(y, test1(X, x, t, T, K, r, sigma, y), logflag = 'ln', style=5); //plot2d(y, test2(X, x, t, T, K, r, sigma, y), logflag = 'ln', style=4); //plot2d(y, test3(X, x, t, T, K, r, sigma, y, n), logflag = 'ln', style=2); //plot2d(y, test4(X, x, t, T, K, r, sigma, y, n), logflag = 'ln', style=2); //legend(["Put par Monte Carlo";"Put exacte";"inte"])
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meshcheryakovva/DSS-2017
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2021-03-09T19:19:56.332398
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function V_res = fis_V(inVector, inCodes) // аргументы: входной вектор числовых значений и массив строк-имен переменных f_V=newfls("m"); // тип Мамдани f_V.name="fisV"; f_V.TNorm="min"; // and f_V.SNorm="max"; // or f_V.Comp="one"; // not f_V.defuzzMethod="centroide"; // центр тяжести f_V.ImpMethod = 'min' f_V.AggMethod = 'max' // переменные и функции принадлежности for i=1:11 f_V = addvar(f_V, "input", inCodes(i), [-1 1]); f_V = addmf(f_V,"input",i,"low","trimf",[-1.1 -1.0 0.0]); f_V = addmf(f_V,"input",i,"mid","trimf", [-1.0 0.0 1.0]); f_V = addmf(f_V,"input",i,"high","trimf", [0.0 1.0 1.1]); end f_V = addvar(f_V, "output", "V", [-1 1]); f_V = addmf(f_V,"output", 1, "low","trimf",[-1.1 -1.0 0.0]); f_V = addmf(f_V,"output", 1, "mid","trimf", [-1.0 0.0 1.0]); f_V = addmf(f_V,"output", 1, "high","trimf", [0.0 1.0 1.1]); // матрица правил из FisPro rulesFISProV = [ 3 , 3 , 0 , 3 , 0 , 0 , 0 , 0 , 0 , 3 , 0 , 3; 2 , 3 , 0 , 3 , 0 , 0 , 0 , 0 , 0 , 3 , 0 , 3; 3 , 2 , 0 , 3 , 0 , 0 , 0 , 0 , 0 , 3 , 0 , 3; 3 , 3 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 3 , 0 , 3; 3 , 3 , 0 , 3 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 3; 3 , 3 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 3; 2 , 3 , 0 , 3 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 3; 2 , 2 , 0 , 3 , 0 , 0 , 0 , 0 , 0 , 3 , 0 , 3; 3 , 2 , 0 , 3 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 3; 2 , 3 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 3 , 0 , 3; 2 , 2 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 2; 1 , 2 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 2; 2 , 1 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 2; 2 , 2 , 0 , 1 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 2; 2 , 2 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 1 , 0 , 2; 1 , 1 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 1; 2 , 1 , 0 , 1 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 1; 2 , 2 , 0 , 1 , 0 , 0 , 0 , 0 , 0 , 1 , 0 , 1; 1 , 2 , 0 , 1 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 1; 2 , 1 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 1 , 0 , 1; 2 , 1 , 0 , 1 , 0 , 0 , 0 , 0 , 0 , 1 , 0 , 1; 1 , 2 , 0 , 1 , 0 , 0 , 0 , 0 , 0 , 1 , 0 , 1; 1 , 1 , 0 , 2 , 0 , 0 , 0 , 0 , 0 , 1 , 0 , 1; 1 , 1 , 0 , 1 , 0 , 0 , 0 , 0 , 0 , 2 , 0 , 1; 1 , 1 , 0 , 1 , 0 , 0 , 0 , 0 , 0 , 1 , 0 , 1; 0 , 0 , 3 , 0 , 0 , 3 , 0 , 0 , 3 , 0 , 3 , 3; 0 , 0 , 2 , 0 , 0 , 3 , 0 , 0 , 3 , 0 , 3 , 3; 0 , 0 , 3 , 0 , 0 , 2 , 0 , 0 , 3 , 0 , 3 , 3; 0 , 0 , 3 , 0 , 0 , 3 , 0 , 0 , 2 , 0 , 3 , 3; 0 , 0 , 3 , 0 , 0 , 3 , 0 , 0 , 3 , 0 , 2 , 3; 0 , 0 , 3 , 0 , 0 , 3 , 0 , 0 , 2 , 0 , 2 , 3; 0 , 0 , 2 , 0 , 0 , 3 , 0 , 0 , 3 , 0 , 2 , 3; 0 , 0 , 2 , 0 , 0 , 2 , 0 , 0 , 3 , 0 , 3 , 3; 0 , 0 , 3 , 0 , 0 , 2 , 0 , 0 , 3 , 0 , 2 , 3; 0 , 0 , 2 , 0 , 0 , 3 , 0 , 0 , 2 , 0 , 3 , 3; 0 , 0 , 2 , 0 , 0 , 2 , 0 , 0 , 2 , 0 , 2 , 2; 0 , 0 , 1 , 0 , 0 , 2 , 0 , 0 , 2 , 0 , 2 , 2; 0 , 0 , 2 , 0 , 0 , 1 , 0 , 0 , 2 , 0 , 2 , 2; 0 , 0 , 2 , 0 , 0 , 2 , 0 , 0 , 1 , 0 , 2 , 2; 0 , 0 , 2 , 0 , 0 , 2 , 0 , 0 , 2 , 0 , 1 , 2; 0 , 0 , 1 , 0 , 0 , 1 , 0 , 0 , 2 , 0 , 2 , 1; 0 , 0 , 2 , 0 , 0 , 1 , 0 , 0 , 1 , 0 , 2 , 1; 0 , 0 , 2 , 0 , 0 , 2 , 0 , 0 , 1 , 0 , 1 , 1; 0 , 0 , 1 , 0 , 0 , 2 , 0 , 0 , 1 , 0 , 2 , 1; 0 , 0 , 2 , 0 , 0 , 1 , 0 , 0 , 2 , 0 , 1 , 1; 0 , 0 , 2 , 0 , 0 , 1 , 0 , 0 , 1 , 0 , 1 , 1; 0 , 0 , 1 , 0 , 0 , 2 , 0 , 0 , 1 , 0 , 1 , 1; 0 , 0 , 1 , 0 , 0 , 1 , 0 , 0 , 2 , 0 , 1 , 1; 0 , 0 , 1 , 0 , 0 , 1 , 0 , 0 , 1 , 0 , 2 , 1; 0 , 0 , 1 , 0 , 0 , 1 , 0 , 0 , 1 , 0 , 1 , 1; 0 , 3 , 0 , 0 , 3 , 0 , 3 , 3 , 0 , 0 , 0 , 3; 0 , 2 , 0 , 0 , 3 , 0 , 3 , 3 , 0 , 0 , 0 , 3; 0 , 3 , 0 , 0 , 2 , 0 , 3 , 3 , 0 , 0 , 0 , 3; 0 , 3 , 0 , 0 , 3 , 0 , 2 , 3 , 0 , 0 , 0 , 3; 0 , 3 , 0 , 0 , 3 , 0 , 3 , 2 , 0 , 0 , 0 , 3; 0 , 3 , 0 , 0 , 3 , 0 , 2 , 2 , 0 , 0 , 0 , 3; 0 , 2 , 0 , 0 , 3 , 0 , 3 , 2 , 0 , 0 , 0 , 3; 0 , 2 , 0 , 0 , 2 , 0 , 3 , 3 , 0 , 0 , 0 , 3; 0 , 3 , 0 , 0 , 2 , 0 , 3 , 2 , 0 , 0 , 0 , 3; 0 , 2 , 0 , 0 , 3 , 0 , 2 , 3 , 0 , 0 , 0 , 3; 0 , 2 , 0 , 0 , 2 , 0 , 2 , 2 , 0 , 0 , 0 , 2; 0 , 1 , 0 , 0 , 2 , 0 , 2 , 2 , 0 , 0 , 0 , 1, 0 , 2 , 0 , 0 , 1 , 0 , 2 , 2 , 0 , 0 , 0 , 1; 0 , 2 , 0 , 0 , 2 , 0 , 1 , 2 , 0 , 0 , 0 , 2; 0 , 2 , 0 , 0 , 2 , 0 , 2 , 1 , 0 , 0 , 0 , 2; 0 , 1 , 0 , 0 , 1 , 0 , 2 , 2 , 0 , 0 , 0 , 1; 0 , 2 , 0 , 0 , 1 , 0 , 1 , 2 , 0 , 0 , 0 , 1; 0 , 2 , 0 , 0 , 2 , 0 , 1 , 1 , 0 , 0 , 0 , 1; 0 , 1 , 0 , 0 , 2 , 0 , 1 , 2 , 0 , 0 , 0 , 1; 0 , 2 , 0 , 0 , 1 , 0 , 2 , 1 , 0 , 0 , 0 , 1; 0 , 2 , 0 , 0 , 1 , 0 , 1 , 1 , 0 , 0 , 0 , 1; 0 , 1 , 0 , 0 , 2 , 0 , 1 , 1 , 0 , 0 , 0 , 1; 0 , 1 , 0 , 0 , 1 , 0 , 2 , 1 , 0 , 0 , 0 , 1; 0 , 1 , 0 , 0 , 1 , 0 , 1 , 2 , 0 , 0 , 0 , 1; 0 , 1 , 0 , 0 , 1 , 0 , 1 , 1 , 0 , 0 , 0 , 1]; // добавить столбцы для конъюнкции и весов правил len = size(rulesFISProV,1); rulesV = cat(2, rulesFISProV, ones(len,2)); f_V = addrule(f_V, rulesV); // база правил editfls(f_V) V_res = evalfls(inVector, f_V); // вывод endfunction
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.[[NOM_TABLE_SANS_PRE]]-icon { background-image:url(images/grid16x16.gif) !important; } .demo-[[NOM_TABLE_SANS_PRE]]-shortcut img { background-image: url(images/grid48x48.png); filter:progid:DXImageTransform.Microsoft.AlphaImageLoader(src='system/modules/grid-win/images/grid48x48.png', sizingMethod='scale'); } .demo-[[NOM_TABLE_SANS_PRE]]-option { background-image: url(images/plugin.gif) !important; } .demo-[[NOM_TABLE_SANS_PRE]]-add { background-image: url(images/add.gif) !important; } .demo-[[NOM_TABLE_SANS_PRE]]-remove { background-image: url(images/delete.gif) !important; } .demo-[[NOM_TABLE_SANS_PRE]]-loading { background-image: url(images/loading.gif) !important; } .upload-icon { background: url('images/image_add.png') no-repeat 0 0 !important; }
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(unwatch all) (clear) (set-strategy depth) (open "drtest03.rsl" drtest03 "w") (dribble-on "drtest03.out") (batch "drtest03.bat") (dribble-off) (load "compline.clp") (printout drtest03 "drtest03.bat differences are as follows:" crlf) (compare-files drtest03.exp drtest03.out drtest03) ; close result file (close drtest03)
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pathname=get_absolute_file_path('2_5.sce') filename=pathname+filesep()+'2_5_data.sci' exec(filename) //work done Wd=patm*V printf("\n\nRESULTS\n\n") printf("\nWork done:%f\n",Wd)
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// Chip de teste para função ZX load zx.hdl, output-file zx.out, compare-to zx.cmp, output-list in%B3.5.3 out%B3.1.3; set in %B00000, // in=0 eval, output; set in %B00001, // in=1 eval, output;
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clc //initialization of varaibles P1=15 //psia T1=80+460 //R dm=3 //lb T2=75+460 //R P2=25 //psia //calculations mratio=P1*T2/(P2*T1) m2=dm/(1-mratio) V2=m2*55.16*T2/(P2*144) //results printf("Volume of the apparatus = %.1f cu ft",V2)
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f=50E6 w=2*%pi*f theta=5*%pi/180 C=1E-12 R=1/theta/w/C disp(R) C=10E-12 R=1/theta/w/C disp(R) C=100E-12 R=1/theta/w/C disp(R)
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//if then elseif x=1; if x==1 then txt='x is equal to 1'; elseif x==2 then txt='x is equal to 2'; else txt='x is not equal to 1 nor 2'; end //<-- only one "end" disp(txt) //two nested if statements x=2; if x==1 then txt='x is equal to 1'; else if x==2 then txt='x is equal to 2'; else txt='x is not equal to 1 nor 2'; end //<-- "end" of second "if" end //<-- "end" of first "if" disp(txt)
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function slc=contrss(a,tol) [lhs,rhs]=argn(0) // if a(1)<>'lss' then error(91,1), end; if rhs==1 then tol=sqrt(%eps);end if rhs>2 then error('1 or 2 inputs to contrss : sl [,tol]') end; [a,b,c,d,x0,dom]=a(2:7) // [nc,u]=contr(a,b,tol) u=u(:,1:nc) a=u'*a*u;b=u'*b;c=c*u slc=list('lss',a,b,c,d,u'*x0,dom)
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//To find teeth and torque clc //Given: Ts=100 //Torque on the sun wheel, N-m r=5 //Ratio of speeds of gear S to C, NS/NC //Refer Fig. 13.27 and Table 13.22 //Number of teeth on different wheels: //Calculating the values of x and y y=1 x=5-y //Calculating the number of teeth on wheel E TS=16 TE=4*TS //Calculating the number of teeth on wheel P TP=(TE-TS)/2 //Torque necessary to keep the internal gear stationary: Tc=Ts*r //Torque on CN-m //Caluclating the torque necessary to keep the internal gear stationary Ti=Tc-Ts //Torque necessary to keep the internal gear stationary, N-m //Results: printf("\n\n Number of teeth on different wheels, TE = %d.\n\n",TE) printf(" Torque necessary to keep the internal gear stationary = %d N-m.\n\n",Ti)
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// find output voltage of oscillator // Electronic Principles // By Albert Malvino , David Bates // Seventh Edition // The McGraw-Hill Companies // Example 23-2 , page 897 clear;clc; close; // Given data R=10^3;// lamp resistance in ohms V=2;// lamp voltage in volts Rb=2*10^3;// feedback resistance in ohms // Calculations I=V/R;// lamp current in amperes Vout=I*(R+Rb);// output voltage in volts disp("Volts",Vout,"output voltage=") // Result // Output voltage of the oscillator is 6vrms
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//A Textbook of Chemical Engineering Thermodynamics //Chapter 5 //Some Applications of the Laws of Thermodynamics //Example 8 clear; clc; //Given: P1 = 100; //initial pressure of saturated steam (kPa) P2 = 500; //final pressure (kPa) eff = 0.8; //compression efficiency //Referring steam tables //Properties of steam entering the compressor H1 = 2675.5; //enthalpy (kJ/kg) S1 = 7.3594; //entropy (kJ/kg K) //Properties of compressed steam H2 = 3008; //enthalpy (kJ/kg) S2 = S1; //isentropic compression //To calculate work required and temperature Hs = H2-H1; //Using eq. 5.44 (Page no. 128) W_isentropic = -Hs; W_act = W_isentropic/eff; mprintf('The work required for compression is %f kJ/kg',-W_act); H = Hs/eff; //actual change in enthalpy H_act = H1+H; //actual enthalpy of steam leaving the compressor //From steam tables for superheated steam at 500 kPa and enthalpy of H_act T = 586; //temperature (K) mprintf('\nTemperature of exhaust steam is %i K',T); //end
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// Scilab code Ex7.1: Pg.277 (2008) clc; clear; // Part (1) l = 2; // Orbital quantum momentum // For simplicity assume h_cross be unity h_cross = 1; // Reduced plank's constant, J-s printf("\nThe possible values of L_z (in units of h_cross) are "); for i = -2:2 printf(" %1d ",i); end // Part (2) m = 2; // Magnetic quantum number L_z = m*h_cross; // Z-component of angular momentum L = sqrt(l*(l+1))*h_cross; // Angular momentum printf("\nThe magnitude of L (in units of h_cross) = %4.2f", L); // Part (3) theta = (180/%pi)*acos((L_z)/(L)); // Smallest angle between L & z-axis, degrees printf("\nThe smallest angle between L and z-axis = %4.1f degrees", theta); // Result // The possible values of L_z (in units of h_cross) are -2 -1 0 1 2 // The magnitude of L (in units of h_cross) = 2.45 // The smallest angle between L and z-axis = 35.3 degrees
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// Scilab code Ex6.10: Pg:261 (2008) clc;clear; mu_O = 1.55336; // Refractive index for an ordinary beam mu_E = 1.54425; // Refractive index for an extra-ordinary beam lambda = 5.893e-05; // Wavelength of sodium light, cm t = lambda/(4*(mu_O-mu_E)); // Thickness of quarter wave plate, cm printf("\nThe thickness of the quarter wave plate for quartz = %4.2e cm", t); // Result // The thickness of the quarter wave plate for quartz = 1.62e-003 cm
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mode(0) clear // get a file location filename = uigetfile('*.csv', pwd(), 'Choose a file'); separator = ','; // get data from csv-file with using some separator. Ignore the first line data_values = csvRead(filename, separator, [], [], [], [], [], 1); // get the column names based on the first line col_names = strsplit(mgetl(filename, 1), separator); scale = evstr(x_mdialog('Enter scaling factors for each column', col_names(2:$), string(ones(col_names(2:$))))); scaled_values = data_values for i = 1:size(data_values,2)-1, scaled_values(:,i+1) = data_values(:,i+1)*scale(i) end // define colors and descriptions for columns of data colors = {'r-','g-','b-', 'c-', 'm-', 'k-', 'w-'}; descriptions = col_names(2:$); // Create figure and loop through all columns and plot all data agains first column. f = scf(); for i = 1:size(data_values,2)-1, // plot columns, with different colors plot(data_values(:,1), scaled_values(:,i+1), colors(i)); end // title("") xlabel("Time (µs)"); ylabel("Volgage (V)"); h = legend(descriptions, 4); xgrid() xs2pdf(0, fileparts(filename, 'path') + fileparts(filename, 'fname'));
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//Chapter-6,Example 6_3,Page 6-27 clc() //Given Values: u=0.8*10^-23 //Magnetic dipole moment of an atom in paramagnetic gas in J/T B=0.8 //Magnetic field in tesla K=1.38*10^-23 //Boltzmann constant //To find Temperature at which Average thermal energy is equal to Magnetic energy //i.e. uB=3KT/2 T=2*u*B/(3*K) //Required temperature printf('Required temperature is =%.3f Kelvin \n',T)
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clc clear //Input data V=10*1000//Potential difference applied in V I=2*10^-3//Current in A e=(1.6*10^-19)//Charge of the electron in C m=9.1*10^-31//Mass of the electron in kg //Calculations n=(I/e)/10^16//Number of electrons striking the target per second *10^16 v=sqrt((2*e*V)/m)/10^7//Velocity of the electron in m/s*10^7 lmin=12400/V//Wavelength of the X-rays in angstroms //Output printf('Number of electrons striking the target per second is %3.2f*10^16 \n Velocity of the electron is %3.2f*10^7 m/s \n Wavelength of the X-rays is %3.2f angstroms',n,v,lmin)
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Name=Simp Bolt Punish PlayerCharacters=SimpQuaker BotCharacters=Quaker Bot Close.bot IsChallenge=true Timelimit=60.0 PlayerProfile=SimpQuaker AddedBots=Quaker Bot Close.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=2 BotTeams=1 MapName=SimpVert.map MapScale=3.8125 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=1.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=1.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Reflex WeaponHeroTag=Rockets, RL, Lightning Gun, LG, Railgun, RG, Bolt, BR DifficultyTag=2 AuthorsTag=KovaaK BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Target spawns up high, and you have all the main Reflex weapons available to punish him as he falls. Gain score by doing damage, lose score by taking damage. GameVersion=1.0.4 [Aim Profile] Name=Low Skill MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Low Skill At Feet MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=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=Quaker Bot Close DodgeProfileNames=Long Strafes 2 DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;0.0;0.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Low Skill;Low Skill At Feet;Low Skill;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=Quaker SeeThroughWalls=false [Character Profile] Name=SimpQuaker MaxHealth=10000.0 WeaponProfileNames=Railgun;Rocket Launcher;LG;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1300.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=1600.0 Gravity=4.5 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 [Character Profile] Name=Quaker MaxHealth=300.0 WeaponProfileNames=Railgun;Rocket Launcher;LG;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1300.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=1600.0 Gravity=4.5 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 [Dodge Profile] Name=Long Strafes 2 MaxTargetDistance=1750.0 MinTargetDistance=500.0 ToggleLeftRight=true ToggleForwardBack=true MinLRTimeChange=0.5 MaxLRTimeChange=1.5 MinFBTimeChange=0.5 MaxFBTimeChange=1.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 JumpFrequency=0.2 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Railgun Type=Hitscan ShotsPerClick=1 DamagePerShot=80.0 KnockbackFactor=10.0 TimeBetweenShots=1.0 Pierces=true Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=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=false HeadshotMultiplier=2.0 CooldownType=InfiniteUse MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 CooldownTimer=5.0 MaxCharges=3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=Beam ProjectileGraphic=Ball VisualLifetime=0.5 WallParticleEffect=None HitParticleEffect=Blood BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileWorldHitRadius=1.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomFactor=0.7 ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 ShootSound=Shot HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=10.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=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=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=1.0,1.0,-1.0,5.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=1.0,1.0,-1.0,5.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.01 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false [Weapon Profile] Name=Rocket Launcher Type=Projectile ShotsPerClick=1 DamagePerShot=120.0 KnockbackFactor=14.0 TimeBetweenShots=0.8 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=5090.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=5090.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=100.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=0.0 HeadshotCapable=false HeadshotMultiplier=2.0 CooldownType=InfiniteUse MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 CooldownTimer=5.0 MaxCharges=3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Rocket VisualLifetime=0.1 WallParticleEffect=Flare HitParticleEffect=Flare BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileWorldHitRadius=1.0 ProjectileEnemyHitRadius=2.0 CanAimDownSight=false ADSZoomFactor=0.7 ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 ShootSound=Shot HitscanVisualOffset=X=0.000 Y=0.000 Z=0.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=14.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 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=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true Explosive=true Radius=500.0 DamageAtCenter=120.0 DamageAtEdge=0.1 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=true 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=2 AAPreferClosestPlayer=false AAAlpha=0.5 AAMaxSpeed=0.5 AADeadZone=0.0 AAFOV=180.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.001 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false [Weapon Profile] Name=LG Type=Hitscan ShotsPerClick=1 DamagePerShot=6.0 KnockbackFactor=14.0 TimeBetweenShots=0.046 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=false HeadshotMultiplier=2.0 CooldownType=InfiniteUse MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 CooldownTimer=5.0 MaxCharges=3 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=7.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.05 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileWorldHitRadius=1.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomFactor=0.7 ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 ShootSound=Shot HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=14.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=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=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false [Map Data] reflex map version 8 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// (6.1) Water, initially a saturated liquid at 100C, is contained in a piston–cylinder assembly. The water undergoes a process to the corresponding saturated vapor state, during which the piston moves freely in the cylinder. If the change of state is brought about by heating the water as it undergoes an internally reversible process at constant pressure and temperature, determine the work and heat transfer per unit of mass, each in kJ/kg. //solution T = 373.15 //temperature in kelvin //from table A-2 p = 1.014*10^5 //pressure in pascal vg = 1.673 vf = 1.0435e-3 sg = 7.3549 sf = 1.3069 w = p*(vg-vf)*10^(-3) Q = T*(sg-sf) printf('the work per unit mass in kj/kg is\n\t w = %f',w) printf('\nthe heat transfer per unit mass in kj/kg is \n\t Q = %f',Q)
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clc;funcprot(0);//Example 2.11 //Initilisation of Variables L=0.2;....//length of the steel rod in m d=0.02;....//diameter of steel rod in m Ta=30;....//air surrounding temparature of rod in degrees celcius Tb=300;...//surface tempature of the rod in degrees celcius K=45;....//thermal conductivity of rod in W/m*k h=30;....//Convective heat transfer coefficient in W/m^2*K //calculations P=%pi*d;....//circumference of rod in m A=(%pi*d^2)/4;....//area of rod in m^2 m=sqrt((h*P)/(K*A));....// Q=(sqrt(h*P*K*A))*((Tb-Ta)*tanh(m*L));.....//Heat transfer through fluid from the rod in W disp(Q,"Heat transfer through fluid from the rod in W:")
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clc; m=20000; //mass in kg A=60; //area in metre square g=9.8; //gravitational constant in m/sec square F=m*g; //calculating force in Newton p=F/A; //calculating pressure in Pascal disp(p,"Pressure in Pascal = "); //displaying result. disp(p/(1.013*10^5),"Pressure in atm = "); //displaying result.
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//Example 1_2_u2 clc(); clear; //To calculate the wavelength of the radiation emitted h=6.63*10^-34 m=9.1*10^-31 l=10^-9 c=3*10^8 lamda=(8*m*c*l^2)/(27*h) //units in mts lamda=lamda*10^9 //units in nm printf("The wavelength of the radiation is lamda=%.1fnm",lamda)
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// Case Study: Chapter:13 ,Page No.:434 // 1.Insertion in a sorted list funcprot(0); //Create the list function [List]=create(list1) global List; // Create the current node list1.number=input("Input a number(Type -999 to end); "); if list1.number==-999 then list1.next=NULL; list1.add=NULL; else list1.add=list1.add+1; list1.next=NULL; List(i)=list1; if(i==1) then else List(i-1).next=List(i).add end i=i+1; create(list1);// Create the next node end return; endfunction function []=print1(list1) if list1(i)(1).next~=NULL then printf("%d--->",list1(i)(1).number);//Print current item i=i+1; if list1(i)(1).next==NULL then printf("%d",list1(i)(1).number); end print1(list1);//Move to next item end return; endfunction function [List]=insert(list1) global List; x=input("Input number to be inserted: ");//Read the number //find the location so that number could be placed in sorted order while (list1(i)(1).next~=NULL) if(list1(i)(1).number>=x) then break; end i=i+1; end key=i; //Insetion at end if(list1(i)(1).next==NULL & list1(i)(1).number < x) then list1(i+1)(1).number=x; list1(i+1)(1).add=i+1; list1(i+1)(1).next=NULL; list1(i)(1).next=list1(i+1)(1).add; List=list1; return; end i=1; while (list1(i)(1).next~=NULL) i=i+1; end j=i+1; //Key node found and insert new node or item while(list1(i)(1).add~=key) list1(i+1)(1).number=list1(i)(1).number; i=i-1; end list1(i+1)(1).number=list1(i)(1).number list1(i)(1).number=x; list1(j)(1).add=j; list1(j)(1).next=NULL; list1(j-1)(1).next=list1(j)(1).add; List=list1; endfunction global List; NULL=0;i=1; //Create the structure i.e. node node=struct('number',0,'add',0,'next',0); head=node; //Calling the functions printf("Input a sorted(ascending) list"); List=create(head); printf("\nOriginal List: "); print1(List); List=insert(List); printf("\nNew List: "); print1(List);
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//char i/p w=bartlett('a'); disp(w); //output //!--error 144 //Undefined operation for the given operands. //check or define function %c_3_s for overloading. //at line 23 of function bartlett called by : //w=bartlett('a');
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// Position of Fermi level at room temperature // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 1-22 in page 50 clear; clc; close; // Data given C_Ge=4.41*10^22; // Concentration of Ge atom /cm^3 N_D=4.41*10^15; // Number of free donor atoms N_C=8.87*10^18; // Number of conduction electrons assuming full ionization K_BT=0.026; // Measured in eV at room temperature // Calculation E_F=K_BT*log(N_D/N_C); printf("Position of fermi level is %0.4f",E_F); // Result // Position of Fermi level from edge of conduction band is -0.1977 // Thus E_F is below E_C
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clc clear //input np=350;//number of turn in the primary lm=0.8;//mean length of core in meters am=0.006;//magnetic area in square meter i0=0.8;//no load current in amperes v=500;//supply voltage in volts f=50;//frequency of supply in hertz ur=2000;//relative permeability of the core u0=1.257*(10^-6);//absolute permeability //calculations bm=v/(4.44*am*np*f);//maximum flux density in tesla im=(bm*i0)/(u0*ur*np*(2^0.5));//magnetizing current in amperes sinp=im/i0;//sine of no load phase angle p=v*lm*cos(asin(im/i0));//power loss of core in watts //output mprintf('the maximum flux density in the core will be %3.3fT with a magnetizing current of %3.3fA and a core loss of %3.0fW',bm,im,p)
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Na = 10^16; t = 500*10^-8; kT = 26*10^-3; //in eV q = 1.6*10^-19; ni = 1.5*10^10; eps0 = 8.85*10^-14; //in F/m eps = 11.9*eps0; eps1 = 3.9*eps0; Cox = eps1/t; disp(Cox,"The oxide capacitance (in F/cm2) = ") phiF = kT*log(Na/ni); disp(phiF,"φF(in V) = ") Wmax = (4*eps*phiF/(q*Na))^0.5; disp(Wmax,"The maximum depletion width (in cm) = ") Cmin = eps1/(t+(eps1*Wmax/eps)); disp(Cmin,"The minimum capacitance (in F/cm2) = ") Cfb = eps1/(t+(eps1/eps*(kT*eps/q/Na)^0.5)); disp(Cfb,"The capacitance (in F/cm2) under flat band conditions = ") disp("Note that Cfb is ∼ 80% of Cox and Cmin is ∼ 33% of Cox.")
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clc; T01=270+273; // Temperature at state 1 in kelvin T03=T01; p01=1; // Inlet pressure in bar rp=6; // Pressure ratio eff_c=0.85; // Compressor efficiency T05=1150+273; // Temperature at inlet to expansion in kelvin eff_T=0.9; // Turbine efficiency n=1.24; // Polytropic index R=10.05; // in kJ/kg K T_02=T01*rp^((n-1)/n); T02=T01+(T_02-T01)/eff_c; Cv=R/(n-1); Cp=R+Cv; Wc=2*Cp*(T02-T01); T_06=T05/rp^((n-1)/n); T06=T05-eff_T*(T05-T_06); WT=2*Cp*(T05-T06); Q=Cp*(T05-T02)+Cp*(T05-T06); WN=WT-Wc; eff_th=WN/Q; disp ("%",eff_th*100,"The Cycle efficiency = ");
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backend = Backend.sparc Test.asmdir = Test.asmdir or "sparc" Ld.rtend = "" --- don't need the run-time system -- source files live in src directory Test.source = "src" Options.swap = 1 dofile('l32files.lua') local i = 1 while Test.files[i] do if type(Test.files[i]) == 'table' and Test.files[i].source == 'float-003.c--' then Test.files[i].outdir = 'sparc' end i = i + 1 end
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; define-sort with not well-sorted expression (set-logic QF_UF) (define-sort A () B)
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errcatch(-1,"stop");mode(2);//Ex:4.7 ; ; c=1*10^-6; f1=100; f2=10000; X_c1=1/(2*%pi*f1*c); X_c2=1/(2*%pi*f2*c); printf("Reactance at 100Hz = %f mA",X_c1); printf("\n Reactance at 10kHz = %f mA",X_c2); exit();
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//Problem 7.06: A coil of 300 turns is wound uniformly on a ring of non-magnetic material. The ring has a mean circumference of 40 cm and a uniform cross sectional area of 4 cm2. If the current in the coil is 5 A, calculate (a) the magnetic field strength, (b) the flux density and (c) the total magnetic flux in the ring. //initializing the variables: N = 300; // no. of turns l = 0.40; // in m A = 4E-4; // in m2 I = 5; // in Amperes u0 = 4*%pi*1E-7; ur = 1 //calculation: H = N*I/l B = u0*ur*H Phi = B*A printf("\n\nResult\n\n") printf("\n (a)Magnetic field strength H = %.0f A/m\",H) printf("\n (b)Flux Density = %.2E T",B) printf("\n (c)total magnetic flux = %.2E Wb",Phi)
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function []=isoview(xmin,xmax,ymin,ymax) // setting default plotting to be isoview // Copyright INRIA plot2d(0,0,1,"030"," ",[xmin,ymin,xmax,ymax]);
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// @Harness: verifier // @Purpose: "Test for variable resolution" // @Result: "UnresolvedVariable @ 7:11" architecture unr_var_02 { subroutine foo(e: int): void { e = a[0]; } }
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//acids and bases// //example 2.23// OH=0.0025;//OH- concentration// K=1*10^-14//water ionization constant// H=K/OH; H=H/10^-12; printf("The concentration of H+ ions is %f*10^-12M",H); printf("\nThe concentration of OH- ions is %fM",OH); printf("\nAs concentration of H+ is lesser than the concentration of OH- the cleaning solution will be basic in nature");
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function [ok,sk,stint]=gamatest(P12,P21,gama) // Test if gama is ok. If ok, sk=controller. stint is true (%T) if // internal stability is achieved. // Copyright INRIA write(%io(2),gama); ok=%F;sk=[];stint=%F; [A,B2,C1,D12]=P12(2:5); [A,B1,C2,D21]=P21(2:5); [nx,nx]=size(A); [nx,nw]=size(B1);[ny,nx]=size(C2); Q=C1'*C1;R=D12'*D12;S=C1'*D12; V=B1*B1';L=D21*B1';N=D21*D21'; // Two Riccati [K,X,errx]=leqr(P12,V/gama/gama); [H,Y,erry]=leqe(P21,Q/gama/gama); //tests notok0=or([h==[],k==[]]); if notok0 then write(%io(2),'fail');return;end dom=p12(7); // ------------------> Discrete time case: if dom=='d' then ok1=and(abs(spec(A+B2*K)) < ones(nx,1)); ok2=and(abs(spec(A+H*C2)) < ones(nx,1)); ok3=and(real(spec(gama*gama*eye-B1'*X*B1)) > zeros(nw,1)); ok4=and(real(spec(gama*gama*eye-C1*Y*C1')) > zeros(ny,1)); ok5=and(real(spec(inv(X)+B2*inv(R)*B2'-V/gama/gama)) > zeros(nx,1)); ok6=and(real(spec(inv(Y)+C2'*inv(N)*C2-Q/gama/gama)) > zeros(nx,1)); ok7=mini(real(spec(eye-Y*X/gama/gama))) > 100*%eps; ok=and([ok3,ok4,ok7]); if ~ok then write(%io(2),'fail');return;end E=eye-Y*X/gama/gama; W=(A-L'*inv(N)*C2)*inv((inv(X)+B2*inv(R)*B2'-V)); if rcond(E) > 1.d-4 then Z=inv(E); Ak=A+B2*K*Z+W*(S*K*Z+Q)/gama/gama+H*C2;Bk=H;Ck=-K*Z; Sk=syslin('d',Ak,Bk,Ck); stint=and(abs(spec(h_cl(P,size(C2*B2),sk))) < ones(2*nx,1)) //Sk1=lqg(P,size(c2*B2)); else Ak=A*E+B2*K+W*(S*K+Q*E)/gama/gama+H*C2*E;Bk=H;Ck=-K; Sk=des2ss(Ak,Bk,Ck,0*Ck*Bk,E); stint=and(abs(spec(h_cl(P,size(C2*B2),sk))) < ones(2*nx,1)) end end // -----------------> Continuous time case if dom=='c' then ok1=and(real(spec(A+B2*K)) < zeros(nx,1)); ok2=and(real(spec(A+H*C2)) < zeros(nx,1)); ok3=mini(real(spec(eye-Y*X/gama/gama))) > 100*%eps; ok=and([ok1,ok2,ok3]); if ~ok then write(%io(2),'fail');return;end Z=inv(eye-Y*X/gama/gama);; Ak=A+B2*K*Z+Y*(S*K*Z+Q)/gama/gama+H*C2;Bk=H;Ck=-K*Z; Sk=syslin('c',Ak,Bk,Ck); stint=and(real(spec(h_cl(P,size(C2*B2),sk))) < zeros(2*nx,1)) //Sk1=lqg(P,size(c2*B2)); end write(%io(2),'ok')
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clc //initialisation of variables H=1360//ft t=60//f a=(10^3)*5.5*(10^-3)//f q=(1.36*10^3)*5.5*(10^-3)//f s=(4-1.36)*(10^3)*(3.2*10^-3)//f //CALCULATIONS T=t-q-s//F T1=T+3*a//F //RESULTS printf('the temperature at the mountain top=% f F',T) printf('the temperature on the plain beyond the mountain=% f F',T1)
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//(12.6) At steady state, 100 m3/min of dry air at 32C and 1 bar is mixed adiabatically with a stream of oxygen (O2) at 127C and 1 bar to form a mixed stream at 47C and 1 bar. Kinetic and potential energy effects can be ignored. Determine (a) the mass flow rates of the dry air and oxygen, in kg/min, (b) the mole fractions of the dry air and oxygen in the exiting mixture, and (c) the time rate of entropy production, in kJ/K . min //solution //variable initialization T1 = 32 //temperature of dry air in degree celcius p1 = 1 //pressure of dry air in bar AV1 = 100 //volume rate of dry air in m^3/min T2 = 127 //temperature of oxygen stream in degree celcius p2 = 1 //pressure of oxygen stream in bar T3 = 47 //temperature of mixed stream in degree celcius p3 = 1 //pressure of mixed stream in bar //part(a) Rbar = 8314 //universal gas constant Ma = 28.97 //molar mass of air Mo = 32 //molar mass of oxygen va1 = (Rbar/Ma)*(T1+273)/(p1*10^5) //specific volume of air in m^3/kg ma1dot = AV1/va1 //mass flow rate of dry air in kg/min //from table A-22 and A-23 haT3 = 320.29 //in kj/kg haT1 = 305.22 //in kj/kg hnotT2 = 11711 //in kj/kmol hnotT1 = 9325 //in kj/kmol modot = ma1dot*(haT3-haT1)/[(1/Mo)*(hnotT2-hnotT1)] //in kg/min printf('the mass flow rate of dry air in kg/min is: %f',ma1dot) printf('\nthe mass flow rate of oxygen in kg/min is: %f',modot) //part(b) nadot = ma1dot/Ma //molar flow rate of air in kmol/min nodot = modot/Mo //molar flow rate of oxygen in kmol/min ya = nadot/(nadot+nodot) //mole fraction of air yo = nodot/(nadot+nodot) //mole fraction of oxygen printf('\n\nthe mole fraction of dry air in the exiting mixture is: %f',ya) printf('\nthe mole fraction of dry oxygen in the exiting mixture is: %f',yo) //part(c) //with the help of tables A-22 and A-23 sanotT3 = 1.7669 //in kj/kg.K sanotT1 = 1.71865 //in kj/kg.K sbarT3 = 207.112 //in kj/kmol.K sbarT2 = 213.765 //in kj/kmol.K sigmadot = ma1dot*[sanotT3-sanotT1-(8.314/Ma)*log(ya)] + (modot/Mo)*[sbarT3-sbarT2-8.314*log(yo)] printf('\n\nthe time rate of entropy production, in kJ/K . min is: %f',sigmadot)
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// Exa 5.13 clc; clear; close; format('v',6) // Given data R_S = 600;// in ohm r_i = 400;// in ohm Vs = 1;// in mV Vs = Vs * 10^-3;// in V //Input voltage Vi = Vs*(r_i/(R_S+r_i));// in V // Input current Ii =Vs/(R_S+r_i);// in A Vo = 100;// in mV Vo = Vo * 10^-3;// in V R_L = 5;// in k ohm R_L = R_L * 10^3;// in ohm // Output current Io = Vo/R_L;// in A // voltage gain A_V =Vo/Vi ; disp(A_V,"The voltage gain is"); // current gain A_I = Io/Ii; disp(A_I,"The current gain is"); // Power gain P =A_V*A_I; disp(P,"The power gain is");
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// Inverse Continuous Time Fourier Transform // X(jW)= 2*pi, at W=-Wo clear; clc; close; // CTFT A =1; Dw = 0.005; W1 = 4; Wo=2//Assume Wo=2 w = -W1/2:Dw:W1/2; for i = 1:length(w) if w(i)==-Wo then XW(i) = 2*%pi; else XW(i)=0; end end XW = XW'; //Inverse Continuous-time Fourier Transform t = -3*%pi:%pi/length(w):3*%pi; xt =(1/(2*%pi))*XW *exp(sqrt(-1)*w'*t)*Dw; xt = real(1+xt); plot(t,xt); xlabel(' t Sec'); title('Time domain signal x(t)')
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//Example 3_18 clc; clear; close; format('v',6); //given data : //v=100*sin(314*t) //i=10*sin(314*t-%pi/6) Vm=100;//V omega=314;//rad/s V=Vm/sqrt(2);//V f=omega/2/%pi;//Hz Im=10;//A I=Im/sqrt(2);//A fi=%pi/6;//radian pf=cos(fi);//power factor disp(pf,"Power Factor(Lagging)"); P=V*I*cos(fi);//W disp(P,"Powe Consumed(W)"); Z=V/(I*expm(%i*-fi));//ohm R=real(Z);//ohm disp(R,"Value of R(ohm)"); XL=imag(Z);//ohm L=XL/2/%pi/f*1000;//mH disp(L,"Value of L(mH)");
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// A Textbook of Fluid Mecahnics and Hydraulic Machines - By R K Bansal // Chapter 2 - Pressure and its measurements // Problem 2.7 //Given Data Set in the Problem d=3 a=%pi/4*d^2 D=10 A=%pi/4*D^2 f=80 dens=1000 g=9.81 //Calculations //When pistons are at same level F=f/a*A mprintf("The force on the large piston in level with the small piston is %f N\n",F) //When smaller piston is 40 cm above tha large piston p=(dens*g*40/100)/10^4 //pressure due to 40 cm of the liquid F_=(f/a+p)*A mprintf("The force on the large piston 40 cm below small piston is %f N\n",F_)
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// Example 2.1 clear all; clc; // Given data atom_h = 6.6*10^24; // Number of atoms in Hydrogen // Using the data given in Table II.2, Appendix II for isotropic abundance of deuterium isoab_H2 = 0.015; // Isotropic abundance of deuterium // Calculation totatom_d=(isoab_H2*atom_h)/100; // Result printf('\n Number of deuterium atoms = %2.1E \n',totatom_d);
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//Transport Processes and Seperation Process Principles //Chapter 3 //Example 3.2-2 //Principles of Momentum Transfer and Applications //given data delP=9.32e+4;//pressure diff in N/m2 D1=0.1541;//external diameter in m D0=0.0566;//internal diameter in m Dr=D0/D1; Co=0.61; rho=878; //oil density in kg/m3 v0=(Co/(sqrt(1-(Dr^4))))*sqrt((2*delP)/rho);//velocity calculation in m/s A=(%pi/4)*D0*D0;//cross section area V=A*v0;//volumetric flow rate mprintf("the volumetric flow rate is %f m3/s",V); //end
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clc;clear; //Example 2.11 //given values Win=20; mair=0.25; //calculation v=sqrt(Win/2/mair)//Win = 1/2*m*v^2 if(v >= 8) disp('True'); else disp('False')
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function [y] = BarkerCode(len,opsamples) y=[]; // Display mode mode(0); // Display warning for floating point exception ieee(1); //BarkerCode Generate Barker code //Y = BarkerCode(len,opsamples)) outputs a frame of the Barker code in column vector Y //opsamples specify output frame length properties //length specifies length of barker code // //Author - Harshal Shah //check conditions on length if (~isreal(len) | length(len)~=1 | isnan(len)|~or(len ==[1 2 3 4 5 7 11 13])) then error("BarkerCode:improper length"); end //check condition on opsamples if (~isreal(opsamples) | length(opsamples)~=1 | isnan(opsamples)|ceil(opsamples)~=opsamples|opsamples<=0) then error("BarkerCode:improper output samples"); end //create barker code os specified length select len case 1 then baco = [1]; case 2 then baco =[1 -1]; case 3 then baco = [1 1 -1]; case 4 then baco =[1 1 -1 1]; case 5 then baco =[1 1 1 -1 1]; case 7 then baco =[1 1 1 -1 -1 1 -1]; case 11 then baco =[1 1 1 -1 -1 -1 1 -1 -1 1 -1]; case 13 then baco =[1 1 1 1 1 -1 -1 1 1 -1 1 -1 1]; end //create outputsequence for i =0:opsamples-1 y(i+1)=baco(modulo(i,len)+1); end endfunction
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clear; clc; xdel(winsid()); //close all windows s = %s; G = syslin('c',(s^2-4*s+20)/((s+2)*(s+4))); zeroes = roots(numer(G)); disp(zeroes,"zeroes are:"); poles = roots(denom(G)); disp(poles,"poles are:"); evans(G,10); v = [-6 6 -6 6]; mtlb_axis(v) sgrid([0.45,0],[0],32);//displays the zeta = 0,0.45 line curve_handles=datatipGetEntities()//gets the entities required curve_handles.visible='off'; curve_handles.visible='on'; zeta = 0.45;//damping ratio = 0.45 anglezeta = (%pi-acos(0.45))*180/%pi; disp(anglezeta,"angle made by the line with zeta = 0.45 to the root locus:"); printf("from root locus plotwe have for stable system gain K =(0,1.5)");
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clear //given o=0.14 h=0.86 O=120*o H=120*h O2=134.4+275.5 printf("\n \n Total O2 uniting with oil %.2f ",O2)
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clc; clear; U=15;//ft/sec b=96;//ft c=7.5;//ft W=210;//lb CD=0.046; eff=0.8;//power train efficiency d=2.38*(10^(-3));//slugs/(ft^3) //W=L CL=2*W/(d*(U^2)*b*c); D=0.5*d*(U^2)*b*c*CD; P=D*U/(eff*550);//hp disp(CL,"The lift coefficient=") disp("hp",P,"The power required by the pilot=")
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//example-3.8 //page no-85 //given //the ratio of intercepts of orthorombic unit cell is a:b:c=0.429:1:0.379 //to find:- the miller indices of faces of the following intecepts //(I) 0.214:1:0.188 //(II) 0.858:1:0.754 //(III) 0.429:1:0.126 //solution //let x=0.429 y=1 z=0.379 x1=0.214 y1=1 z1=0.188 p1=x1/x q1=y1/y r1=z1/z //intercepts will be 1/2:1:1/2 //reciprocal is 2:1:2 //so miller indices is (212) x2=0.858 y2=1 z2=0.754 p2=x2/x q2=y2/y r2=z2/z //intercepts willbe 2:1:2 //reciprocal is 1/2:1:1/2 //so miller inces is (121) x3=0.429 y3=1 z3=0.126 p3=x3/x q3=y3/y r3=z3/z //th e intercept will be 1:1:1/3 //reciprocal is 1:1:3 //so miller indices is (113) printf ("the miller indices for part (I),(II) and (III) are (212),(121)and (113) resp")
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clc //Example 15.4 //Calculate the time taken by water in a long pipe to reach its steady state velocity //let (new)*t/r0^2 be denoted by y y=0.05//dimentionless r0=0.077//m mew=1//Pa.s rho=1000//Kg/m^3 new=mew/rho//m^2/s t=y*r0^2/new//s printf("the time taken by water in a long pipe to reach its steady state velocity is % f seconds",t);
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//chapter12 //example12.25 //page261 printf("since base voltage is zero, it means that there is no path \nfor current in the base circuit. So the transistor will be off i.e. I_C=0,I_E=0. \nSo V_C=10V and V_E=0.\nSo obvious fault is R1 is open.\n")
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This is the test file for the fm_filerename_stress test Garbage to follow... KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla KHAKJFSHSH SAFKHASKJNJfnkjasf nahjlfsNJl Ffakfnanmalksfkla
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//Example 12_4 clc(); clear; //To describe the Temperature changes of the gas printf("This type of process is termed as throttling process and described by the equation Delta U=- Delta W\n") printf("Where Delta W is the work done")
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errcatch(-1,"stop");mode(2); A=[1 1 3;1 3 -3;-2 -4 -4] disp("inverse of A is ") inv(A) exit();
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// Scilab Code Ex16.2 Diamagnetic susceptibility of copper: Page-512 (2010) e = 1.6e-019; // Charge on an electron, C m = 9.1e-031; // Mass of an electron, kg mu_0 = 4*%pi*1e-07; // Magnetic permeability of free space, henry/metre Z = 1; // Number of electrons contributing to the magnetic moment r = 1e-010; // Radius of copper atom, m a = 3.608e-010; // Lattice parameter of copper, m // For FCC lattice of Cu, there are 4 atoms per unit cell n = 4; // Number of atoms per unit cell N = n/a^3; // Number of electrons per unit volume, per metre cube chi_dia = -mu_0*Z*e^2*N*r^2/(6*m); // Diamagnetic susceptibility of copper printf("\nThe diamagnetic susceptibility of copper = %3.1e", chi_dia); // Result // The diamagnetic susceptibility of copper = -5.0e-006
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//Chapter-10, Example 10.30, Page 462 //============================================================================= clc clear //INPUT DATA A=30;//Total surface area in m^2 V=10;//Volume in m^3 Ts=1000;//Temperature of the furnace in degree C p=2;//Total pressure in atm ph2o=0.1;//Partial pressure of water vapour in atm pco2=0.3;//Partial pressure of CO2 //CALCULATIONS lms=(3.6*V)/A;//Mean beam length in m pco2lms=(pco2*lms);//pco2lms in m.atm eco2=0.16;//From Fig.10.23 on page no. 458 cco2=1.11;//From Fig.10.23 on page no. 458 cco2eco2=(cco2*eco2);//cco2eco2 value ph2olms=(ph2o*lms);//ph2olms in m.atm eh2o=0.12;//From Fig.10.24 on page no. 459 P=(p+ph2o)/2;//P value in atm ch2o=1.43;//From Fig.10.26 on page no. 460 ch2oeh2o=(ch2o*eh2o);//ch2oeh2o value P1=(ph2o/(ph2o+pco2));//Ratio of pressures X=(pco2lms+ph2olms);//X value in m.atm e=0.035;//Error value from Fig. 10.27 on page no.461 et=(cco2eco2+ch2oeh2o-e);//Total emissivity of the gaseous mixture //OUTPUT mprintf('Emissivity of the gaseous mixture is %3.4f',et) //=================================END OF PROGRAM==============================
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steps_per_dec = 6; decades = 6; start_freq = 0.1; // the transfer function function foo=G(w) D = %i*w; foo = ((D+1000)/(D^2+5*D+100)); endfunction // this section writes the values to a datafile that may be graphed in a spreadsheet fd = mopen("data.txt", "w"); for step = 0:(steps_per_dec*decades), f = start_freq*10^(step/steps_per_dec); //calculate the next frequency w = f*2*%pi; //convert the frequency to radians [gain,phase] = polar(G(w)); //find the gain and convert it to mag and angle gaindb = 20*log10(gain); //convert magnitude to dB phasedeg = 180*phase/%pi; //convert to degrees //mfprint(fd, "%f, %f, %f \n", f, gaindb, phasedeg); end mclose(fd); //to graph it directly the following is used D = poly(0, 'D'); h = syslin('c', ((D+1000)/(D^2+5*D+100))); bode(h, 0.1, 1000, 'Sample Transfer Function');
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// Etape 1 // Convertion de l'image en matrice path_name = 'D:\Users\ADRIEN KEGLER\Documents\Visual Studio 2015\Projects\Exolife\Projet-Exolife\images\HD215497.pbm'; img_in = readpbm (path_name); // Etape 2 // Affichage de l'image de base display_gray(img_in); // Etape 3 // Convolution avec filtre de sobel image_out = seuilSegment(img_in,64,128,192); // Etape 4 // Affichage de l'image finale figure; display_gray (image_out); //Etape 5 // Enregistrer la matrice sous forme d'image writepbm (image_out,"D:\Users\ADRIEN KEGLER\Documents\Visual Studio 2015\Projects\Exolife\Projet-Exolife\images\mission_B3.pbm");
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clear; //clc(); // Example 15.8 // Page: 405 printf("Example-15.8 Page no.-405\n\n"); //***Data***// // The species, we are given are CaCO3, CaO and CO2 // First we write the reaction for the formation of the above species from their elemental part. // So, we have // Ca + C + 1.5O2 = CaCO3 // Ca + 0.5O2 = CaO // C + O2 = CO2 // We must eliminate Ca, C and O2 from these equations because they do not appear in the species list. // Now, solving the 3rd equation for C and substituting in the first equation, we have // Ca + CO2 - O2 + 1.5O2 = CaCO3 // Now, this equation to the equation second, we have // CO2 = -CaO + CaCO3 // or // CaCO3 = CO2 + CaO printf(" There is only one balanced chemical reaction between the species on the species list, viz.\n"); printf(" CaCO3 = CO2 + CaO ");
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europepmc-json_003.tst
Test the '--count' option of europepmc-json script with only one result, queried by its ID, fetched from the command line as an argument (using '--search' option), using the default page size. The post-processing just extracts the hitcount from Europe-pmc response (json formated), and outputs it. We assume that the IDs will not change in the future, so we always expect to get the same result for this query.
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//Chapter 6, Problem 13, Figure 6.8 clc; C1=3*10^-6; //Capacitance on each capacitor C2=6*10^-6; C3=12*10^-6; V=350; //Total voltage across capacitors C=(1/C1)+(1/C2)+(1/C3); //Calculating equivalent capacitance C=1/C; Q=C*V; V1=Q/C1; //Calculating voltage across each capacitor V2=Q/C2; V3=Q/C3; disp("(a)"); printf("Equivalent circuit capacitance = %f uF\n\n\n",C*10^6); disp("(b)"); printf("Charge on each capacitor = %f uF\n\n",Q*10^6); disp("(c)"); printf("Voltage across 3uF capacitor = %f V\n",V1); printf("Voltage across 6uF capacitor = %f V\n",V2); printf("Voltage across 12uF capacitor = %f V\n",V3);
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//Book Name:Fundamentals of Electrical Engineering //Author:Rajendra Prasad //Publisher: PHI Learning Private Limited //Edition:Third ,2014 //Ex10_12.sce clc; clear; p=4; f=50; R2=0.25; N1=1425; N2=1275; Ns=(120*f)/p; s1=(Ns-N1)/Ns; s2=(Ns-N2)/Ns; R=(R2*(s2/s1))-R2; printf("\n External resistance per phase=%1.1f ohm per phase",R)
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// Calculating the possion's ratio clc; Gf=4.2; v=(Gf-1)/2; disp(v,'Possion s ratio=')
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organfilename = xgetfile('*.smb', GL_SYS_DIR+'smb',title='open smb file'); [path,organfname,extension]=fileparts(organfilename); disp(organfname) Flag_windows=1; //open the smb file [fid, err] = mopen(organfilename, 'rb',0); if err //disp("File "+filename+" does not exist!"); return else [P,nbfaces,Faces] = Draw_read_organ(fid,Flag_windows); L=20; O=[0,0,0]; //test different rotation matrice w3=3.14159/2; Vz=[cos(w3) -sin(w3) 0;sin(w3) cos(w3) 0; 0 0 1]; ap=3.14159/2; Vy=[cos(ap) 0 sin(ap);0 1 0;-sin(ap) 0 cos(ap)]; //y-axis rotation matrix for axis angle Vx=[1 0 0; 0 cos(ap) sin(ap); 0 -sin(ap) cos(ap)]; V=Vx; V=eye(3,3); //V=[0.866 -0.5 0; 0 0 -1; 0.5 -0.866 0] C=[0;0.6;0]; [X,Y,Z,CP]=Draw_SMB(P,nbfaces,Faces,L,O,V,C); g=gcf(); //g=scf(); //g.figure_name=smb; g.visible='off'; drawlater(); for i=1:length(X) if size(X(i),2)>1 then //a single facet has problem of 'monotonous' plot3d(X(i),Y(i),list(Z(i),CP(i))) h=get("hdl"); h.hiddencolor=-CP(i); end end g.visible='on'; a=get("current_axes"); a.rotation_angles = [90,-90] ; drawnow(); end //close the file mclose(fid);
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a12=437.98*4.186, a21=1238*4.186, v1=76.92, v2=18.07 //calc of BPP clc disp("the soln of eg 3.4-->"); t=100 x1=.5, R=8.314 a1=16.678,b1=3640.2,c1=219.61 a2=16.2887,b2=3816.44,c2=227.02 x2=1-x1 p1sat=exp(a1-b1/(c1+t)) p2sat=exp(a2-b2/(c2+t)) h12=v2*exp(-a12/(R*(t+273.15)))/v1 h21=v1*exp(-a21/(R*(t+273.15)))/v2 m=h12/(x1+x2*h12)-h21/(x2+x1*h21) g1=exp(-log(x1+x2*h12)+x2*m) g2=exp(-log(x2+x1*h21)-x1*m) p=x1*g1*p1sat+x2*g2*p2sat disp(p,"boiling point pressure in kPa is"); //calc of BPT p=101.325,x1=.5, e=1 x2=1-x1 t1sat=b1/(a1-log(p))-c1 t2sat=b2/(a2-log(p))-c2 tnew=x1*t1sat+x2*t2sat while e>10^-4 do told=tnew, p1sat=exp(a1-b1/(c1+told)),p2sat=exp(a2-b2/(c2+told)), p1sat=p/(g1*x1+g2*x2*(p2sat/p1sat)) tnew=b1/(a1-log(p1sat))-c1, e=abs(tnew-told) end disp(tnew,"boiling point temperature in Celsius is"); //calc of dpp e1=1, e2=1, e3=1, pold=1 t=100,y1=.5 y2=1-y1 p1sat=exp(a1-b1/(c1+t)) p2sat=exp(a2-b2/(c2+t)) g1=1, g2=1, g11=1, g22=1 pnew=1/(y1/(g1*p1sat)+y2/(g2*p2sat)) while e1>.0001 do pold=pnew, while e2>.0001& e3>.0001 do g1=g11,g2=g22, x1=y1*pold/(g1*p1sat) x2=y2*pold/(g2*p2sat) x1=x1/(x1+x2) x2=1-x1 h12=v2*exp(-a12/(R*(t+273.15)))/v1 h21=v1*exp(-a21/(R*(t+273.15)))/v2 m=h12/(x1+x2*h12)-h21/(x2+x1*h21) g11=exp(-log(x1+x2*h12)+x2*m) g22=exp(-log(x2+x1*h21)-x1*m) e2=abs(g11-g1), e3=abs(g22-g2) end pnew=1/(y1/(g1*p1sat)+y2/(g2*p2sat)) e1=abs(pnew-pold) end disp(pnew,"dew point pressure in kPa is"); //calc dpt p=101.325,y1=.5, e4=1, e5=1,e6=1 y2=1-y1 t1sat=b1/(a1-log(p))-c1 t2sat=b2/(a2-log(p))-c2 tnew=y1*t1sat+y2*t2sat g11=1, g22=1 while e4>.0001 do told=tnew, p1sat=exp(a1-b1/(c1+told)) p2sat=exp(a2-b2/(c2+told)), while e5>.0001 & e6>.0001 do g1=g11, g2=g22, x1=y1*p/(g1*p1sat) x2=y2*p/(g2*p2sat) x1=x1/(x1+x2) x2=1-x1 h12=v2*exp(-a12/(R*(t+273.15)))/v1 h21=v1*exp(-a21/(R*(t+273.15)))/v2 m=h12/(x1+x2*h12)-h21/(x2+x1*h21) g11=exp(-log(x1+x2*h12)+x2*m) g22=exp(-log(x2+x1*h21)-x1*m) e5=abs(g11-g1), e6=abs(g22-g2) end p1sat=p*(y1/g1+y2*p1sat/(g2*p2sat)) tnew=b1/(a1-log(p1sat))-c1 e4=abs(tnew-told) end disp(tnew,"dew point temperature in Celsius is");
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clc //to calculate velocity c=3*10^8 //light speed (m/s) //K(kinetic energy)=(m-mo(rest mass))c^2 //it can also be written as mc^2=K+m0c^2 //given that K=2m0c^2(rest mass energy) //m=3m0 m=3 //relativistic mass //formula is v=c sqrt(1-(m0/m)^2) v=c*sqrt(1-(1/m)^2) disp("velocity of a body is v="+string(v)+"m/s")