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//******************************************* // This is the Scilab script for Exercise 8. // // Use the help facility for more information // on individual functions used. // // Author: J. Kaempf, 2015 (updated) //******************************************** clf; scf(0); a=gcf(); a.figure_size= [1000,700]; // read input data eta=read("eta.dat",-1,51); eta0=read("eta0.dat",-1,51); x = (1:1:51)'; y = (1:1:51)'; // location vectors ntot = 150; // total number of frames for n = 1:ntot // animation loop // grab respective data block jtop = (n-1)*51+1; jbot = jtop+50; etac = eta(jtop:jbot,1:51); drawlater; clf; plot3d(x,y,1000*(etac-eta0),alpha=50,theta=50,flag = [2,2,3]); b = gca(); b.data_bounds = [1,1,-20;51,51,20]; drawnow(); // save frames as GIF files (optional) //if n < 10 then // xs2gif(0,'ex100'+string(n)+'.gif') //else // if n < 100 then // xs2gif(0,'ex10'+string(n)+'.gif') // else // xs2gif(0,'ex1'+string(n)+'.gif') // end // end end; // end of animation loop
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//Chapter 22, Problem 29 clc; V=300; //supply voltage I=90; //total current Ra=0.1; //armature resistance n1=15; //speed of motor Rse=0.05; //series winding resistance R1=0.2; //diverter E1=V-(I*(Ra+Rse)); //e.m.f R=(R1*Rse)/(R1+Rse); //equivalent resistance I1=(R1/(R1+Rse)); //current Ia=sqrt(I^2/I1); //armature current E2=V-(Ia*(Ra+R)); //e.m.f n2=(E2*I*n1)/(E1*I1*Ia); //speed of motor 2 printf("Speed n2 = %.3f rev/s\n\n",n2); printf("Speed of the motor from %d rev/s to %.3f rev/s by inserting 0.2 ohm diverter resistance in parallel with the series winding.",n1,n2);
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//<z,zd,u,ar>=exar2() //<z,zd,u,ar>=exar2() // // Exemple de processus ARMAX ( K.J. Astrom) // On simule une version bidimensionnelle // de l'exemple exar1(); //! a=[1,-2.851,2.717,-0.865].*.eye(2,2) b=[0,1,1,1].*.[1;1]; d=[1,0.7,0.2].*.eye(2,2); sig=eye(2,2); ar=armac(a,b,d,2,1,sig); write(%io(2),"Simulation of the ARMAX process :"); armap(ar); u=-prbs_a(300,1,int([2.5,5,10,17.5,20,22,27,35]*100/12)); zd=narsimul(a,b,d,sig,u); z=narsimul(a,b,d,0.0*sig,u); write(%io(2),"Least square identification ARX :"); [la,lb,sig,resid]=armax(3,3,zd,u,1,1); //end
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errcatch(-1,"stop");mode(2);//Exam:2.3 ; ; Z_1=1;//atomic number for hydrogen n_1=1;//first orbit r_1=0.529;//radius of first orbit of electron for hydrogen Z_2=2;//atomic number for helium n_2=2;//second orbit k=r_1*Z_1/n_1; r_2=k*((n_2)^2)/Z_2;//radius of first orbit of electron for helium disp(r_2,'radius of the second bohr orbit in a singly ionized helium atom(in A)='); exit();
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// exercício 1 getf fatorial.sci getf f2t.sci getf usd.sci // exercício 2 getf rotaciona.sci getf escalona.sci getf translada.sci // exercício 3 getf slicing.sci getf dec2bin.sci getf histograma.sci getf cum_hist.sci getf average.sci // exercício 4 getf mediana.sci getf homomorphic.sci // exercício 5 getf otsu.sci getf otsu_im2.sci // exercício 6 getf opening.sci getf closing.sci /////////////// getf labelconnection.sci getf neighborhood.sci getf ajeita.sci // fornecido pelo viriato getf coisa3.sci getf aprende.sci getf deleta_bit2.sci getf deleta_bit.sci getf hist3.sci getf median_filter.sci getf otsu_im.sci getf prepro.sci getf projetao.sci getf range256.sci getf sobel.sci getf borda2cadeia.sci getf localvar.sci // //mputl(['labelconnection';'ajeita';'opening';'closing';'otsu';'otsu_im';'mediana';'homomorphic';'average';'cum_hist';'histograma';'dec2bin';'slicing';'translada';'escalona';'rotaciona';'usd';'f2t';'fatorial'],'names'); //exec('C:\Documents and Settings\Daniel\imagem\subsamplematrix.sci'); //exec('C:\Documents and Settings\Daniel\imagem\componentes.sci'); // //exec('C:\Documents and Settings\Daniel\imagem\dip\mix_fase_mag.sce'); //exec('C:\Documents and Settings\Daniel\imagem\dip\contador.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\histeq2.sci '); //exec('C:\Documents and Settings\Daniel\imagem\dip\histeq.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\Descritores_de_Fourier_Issicaba.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\textura.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\borda2cadeia.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\warp.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\expande.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\zoom.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\motiontransform.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\filtermask.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\localvar.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\gradiente.sci'); //getf dip\histcumul.sci //exec('C:\Documents and Settings\Daniel\imagem\dip\labelconnection.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\neighborhood.sci'); //exec('C:\Documents and Settings\Daniel\imagem\dip\subsamplematrix.sci');
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format(12) function dy = f(t,y) dy = y - t^2 + 1 return dy endfunction function yt = y(t) yt = (t+1)^2 -0.5*%e^t return yt endfunction clc disp("> La aproximación a la solución de la ecuación diferencial") disp(" usando el método de Euler es: ") E = UN_ecua_dif_Euler(0,0.5,1,10) disp(E) disp("> La aproximación a la solución de la ecuación diferencial") disp(" usando el método de Runge-Kutta es: ") RK4 = UN_ecua_dif_RK4(0,0.5,1,10) disp(RK4) disp("> El valor de la solución exacta de la ecuación diferencia es: ") disp(y(1))
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function f = flutuante(v,b,e,m,M) f = 0 cont=0 decimal=0 if b ==2 while (v~=0) if (v>1)&(decimal==0) rd=modulo(v,2) f = f+(rd*(10^cont)) v=int(v/2) cont=cont +1 else decimal=1 if v>0 cont=cont-1 v=v*2 if (int(v)==1) f=f+(1*10^(cont)) v=v-1 end end if abs(cont)==e v=0 end end end end endfunction
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// Scilab Code Ex7.3: Page-377 (2008) clc; clear; M = 58.46; // Gram atomic mass of NaCl, g/mole N = 6.023e+023; // Avogadro's number rho = 2.17; // Density of NaCl, g/cc m = M/N; // Mass of each NaCl molecule, g n = rho/m; // Number of NaCl molecules per unit volume, molecules/cc N = 2*n; // Number of atoms per unit volume, atoms/cc a = (1/N)^(1/3); // Distance between two adjacent atoms in the NaCl, cm printf("\nThe distance between two adjacent atoms in the NaCl = %4.2f angstrom", a/1e-008); // Result // The distance between two adjacent atoms in the NaCl = 2.82 angstrom
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// Example 1.4 clc; clear; close; // Given data format('v',7); RC= 2.2;//in kΩ RE= 4.7;// in kΩ RE= RE*10^3;// in Ω Ri1= 50;// in Ω Ri2= 50;// in Ω VCC= 10;//in V VEE= 10;// in V VBE= 0.7;// in V beta_dc= 100; beta_ac= 100; // Part (a) // Formula Used : ICQ= IE= (VEE-VBE)/(2*RE+Ri/beta_dc) ICQ= (VEE-VBE)/(2*RE+Ri1/beta_dc);//quiescent collector current in A ICQ= ICQ*10^3;// in mA IE= ICQ;// in mA disp("Part (a)") disp(ICQ,"The value of ICQ in mA is : "); // Quiescent collector-emitter voltage, VCEQ= VCC+VBE-ICQ*RC;// in V disp(VCEQ,"The value of VCEQ in volts is : "); // Part (b) re_desh= 26/IE;// AC emitter resistance in Ω // Formula Used : Ad= Vout/Vind= RC/re_desh Ad= RC*10^3/re_desh;// voltage gain disp("Part (b)") disp(Ad,"The voltage gain is : "); // Part (c) Rin1= 2*beta_ac*re_desh;// input resistance in Ω Rin1= Rin1*10^-3;//in kΩ Rin2= Rin1;// in kΩ disp("Part (c)"); disp(Rin1,"The input resistance in kΩ is : "); // Part (d) Rout1= RC;// in kΩ disp("Part (d)"); disp(Rout1,"The output resistance in kΩ is : ");
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function [ImgO] = OuvertureC(Img) exec('.\DilatationC.sce',-1) exec('.\OuvertureC.sce',-1) ImgO=DilatationC(ErosionC(Img)) endfunction
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//fiber optic communications by joseph c. palais //example 2.5 //OS=Windows XP sp3 //Scilab version 5.4.1 clc clear all //given n1=1//refractive index of air d=1e-2//daimeter of circular photodetector in m f=10e-2//lense focal length in m //to find theta=asind(d/(2*f))//acceptance angle in degrees mprintf("Acceptance angle=%fdegree",theta) NA=n1*(sind(theta))//numerical aperture mprintf("\nNumerical Aperture=%f",NA) FCA=2*theta//full cone angle mprintf("\nFull cone angle=%fdegree",FCA)
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clc //initialisation of variables clear w= 12 //ft q= 300 //ft^3/sec h= 10 //ft g= 32.2 //ft/sec^2 R= 2.6 //CALCULATIONS hc= ((q/12)^2/g)^(1/3) r= h/hc h1= hc*(((h/hc)+0.5*(hc/h)^2)-0.5*R^2) //RESULTS printf ('hc = %.2f ft',hc) printf ('\n stream depth = %.2f ft',h1)
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//Exam:3.16 clc; clear; close; N_a1=4*(1/4)+1;//Number of atoms contained in (100) plane r=1.75*10^(-7);//radius of lead atom (in mm) a_1=2*2^(1/2)*r;//edge of unit cell in case of (100) plane PD_100=N_a1/(a_1^2);//Planar density of plane (100) N_a2=4*(1/4)+2*(1/2);//Number of atoms contained in (110) plane a_21=4*r;//top edge of the plane (110) a_22=2*2^(1/2)*r;//vertical edge of the plane (110) PD_110=N_a2/(a_21*a_22);//Planar density of plane (110) N_a3=3*(1/6)+3/2;//Number of atom contained in (111) plane Ar_111=4*(3^(1/2))*r^2;//area of (111) plane PD_111=N_a3/Ar_111;//Planar density of plane (111) disp(PD_100,'Planar density of plane 100(in atoms/mm^2)='); disp(PD_110,'Planar density of plane 110(in atoms/mm^2)='); disp(PD_111,'Planar density of plane 111(in atoms/mm^2)=');
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// Example 4.9, Page No-207 clear clc R1=10*10^3 Rf=100*10^3 Cf=10*10^-9 fa=1/(2*%pi*Rf*Cf) printf("fa= %d Hz", fa)
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m = read_csv('GoogleMatrix2.txt') gmatrix = zeros(500, 500) for i=1:500 for j=1:500 gmatrix(i, j) = str2code(m(i, j)) end end
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//Example 7.8 clc clear function [I] = trap (fun,a,b,n) // Integrate the function over the interval using Trapezoidal Formula // trap (fun,a,b,n) // fun - function to be integrated // a - lower limit of integration // b - upper limit of integration // n - No. of times trapezoidal rule needs to be performed N = n + 1; // N - total no. of points h = (b-a) / (N-1); x = linspace(a,b,N); y = fun(x); sum1 = y(1) + 2 * sum(y(2:N-1)) + y(N); I = h * sum1 / 2; // Trapezoidal Integral Value endfunction function [I] = simp13 (fun,a,b,n) // Integrate the function over the interval using Simpson's 1/3rd rule // simp13 (fun,a,b,n) // fun - function to be integrated // a - lower limit of integration // b - upper limit of integration // n - No. of times simpson's 1/3rd rule needs to be performed N = 2 * n + 1; // N - total no. of points h = (b-a) / (N-1); x = linspace(a,b,N); y = fun(x); sum1 = y(1) + 4 * sum(y(2:2:N-1)) + 2 * sum(y(3:2:N-2)) + y(N); I = h* sum1 / 3; // Simpson's 1/3rd Integral Value endfunction function [f] = fun1(x) f = 1 ./(1+x^2); endfunction n = 4; ntrap = n; ns13 = n/2; I = [trap(fun1,0,1,ntrap); simp13(fun1,0,1,ns13)]; I = round(I*10^4)/10^4; true = intg(0,1,fun1); disp(I(1),"y_trap = ") disp(I(2),"y_simp13 = ") disp(I(2)*4,"Approx pi = ")
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#Test function: #- MultivariateResultant #test 350 with(RegularChains): with(FastArithmeticTools): with(modpn): with(TestTools): ## Setting the polynomial ring with a prime characteristic p := 469762049; vars := [a, b]: v := vars[1]: R := PolynomialRing(p, vars): for i from 1 to 3 do dx := i * 10: dy := i * 10: f := randpoly(vars, dense, degree = dx) mod p: g := randpoly(vars, dense, degree = dy) mod p: fm := PolynomialConvertIn(R, f): gm := PolynomialConvertIn(R, g): ## compute resultant using modpn C Try[testnoerror](i*10, MultivariateResultant(R, fm, gm, p), 'assign'='r1'): r2 := PolynomialConvertOut(r1): ## Maple default Try[testnoerror](i*10 + 1, `mod`(Resultant(f, g, v), p) , 'assign'='r3'): ## Comparing the results Try(i * 10 + 2, evalb(`mod`(Expand(r3 - r2), p) = 0), true); end do: p := 469762049; vars := [a, b, c]: v := vars[1]: R := PolynomialRing(p, vars): for i from 1 to 2 do dx := 8 + i: dy := 8 + i: f := randpoly(vars, dense, degree = dx) mod p: g := randpoly(vars, dense, degree = dy) mod p: fm := PolynomialConvertIn(R, f): gm := PolynomialConvertIn(R, g): ## compute resultant using modpn C Try[testnoerror](i*40, MultivariateResultant(R, fm, gm, p), 'assign'='r1'): r2 := PolynomialConvertOut(r1): ## Maple default Try[testnoerror](i*40 + 1, `mod`(Resultant(f, g, v), p), 'assign'='r3'): ## Comparing the results Try(i * 10 + 2, evalb(`mod`(Expand(r3 - r2), p) = 0), true); end do: #end test;
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//CHAPTER 8- DIRECT CURRENT MACHINES //Example 25 disp("CHAPTER 8"); disp("EXAMPLE 25"); //24 slot 2 pole DC machine with 18 turns per coil //VARIABLE INITIALIZATION slot=24; //number of slots P=2; //number of poles N=18; //number of turns per coil B=1; //in Webers l=20/100; //effective length in meters rad=10/100; //radius in meters w=183.2; //angular velocity in rad/s //SOLUTION A=2; // number of parallel paths Z=slot*P*N; //total number of conductors ar1=(2*%pi*rad*l)/P; // actual pole area ar2=ar1*0.8; //since the magnetic poles 80% of the armature periphery phi=B*ar2; //effective flux per pole //solution (a) E_a=(P*Z*phi*w)/(2*%pi*A); disp(sprintf("(a) The induced emf is %.1f V",E_a)); //solution (b) coil=slot/P; //number of coils in each path = slots/path E_coil=E_a/coil; //induced emf per coil disp(sprintf("(b) The induced emf per coil is %.2f V",E_coil)); //solution (c) E_turn=E_coil/N; //emf induced per turn disp(sprintf("(c) The induced emf per turn is %.2f V",E_turn)); //solution (d) E_cond=E_turn/A; // emf induced per conductor disp(sprintf("(d) The induced emf per conductor is %.3f V",E_cond)); //The answers are slightly different due to the precision of floating point numbers //END
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//chapter 4 Ex 21 clc; clear; close; rent=2/5; food=3/10; conveyance=1/8; Amtleft=1400; PartLeft=1-(rent+food+conveyance); salary=Amtleft/PartLeft; eFood=food*salary; eConveyance=conveyance*salary; printf("The expenditure on food is Rs. %3.0f and that on conveyance is Rs. %3.0f",eFood,eConveyance);
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//129,130,131 examples clear; clc; close; clf; x=linspace(-3,4,8); y=(x-1)^2-4; plot2d(x,y,5); xtitle("Graph of y=(x-1)^2-4","x axis","y axis"); legend("y=(x-1)^2-4"); x=poly(0,'x'); y=(x-1)^2-4; //131 concept disp('At these points curve cuts the axis of x') x=roots(y) xgrid();
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printf("\t example 15.1 \n"); printf("\t approximate values are mentioned in the book \n"); ts=250; T1=400; T2=300; w=10000; // lb/hr W=150000; // lb/hr l=945.3; // Btu/(lb) , table 7 Q=((w)*(l)); // Btu/hr printf("\t total heat required for steam is : %.2e Btu/hr \n",Q); C=0.63; // Btu/(lb)*(F) Q=((W)*(C)*(T1-T2)); // Btu/hr printf("\t total heat required for kerosene is : %.2e Btu/hr \n",Q); delt1=T2-ts; //F delt2=T1-ts; // F printf("\t delt1 is : %.0f F \n",delt1); printf("\t delt2 is : %.0f F \n",delt2); LMTD=((delt2-delt1)/((2.3)*(log10(delt2/delt1)))); printf("\t LMTD is :%.0f F \n",LMTD); UD=100; A=(Q/(UD*LMTD)); printf("\t A : %.2e ft^2 \n",A); WC=94500; // Btu/F vl=0.017; // ft^3/lb, from table 7 vv=13.75; // ft^3/lb, from table 7 printf("\t By the law of mixtures \n"); // Assume 80 per cent of the outlet fluid is vapor v2=(0.8*vv)+(.2*vl); printf("\t v2 : %.0f ft^3/lb \n",v2); vav=(WC*(v2-vl)/(UD*A))-((WC*(T2-ts)/(l*w))*(vv-vl))+vl; printf("\t vav : %.2f ft^3/lb \n",vav); printf("\t By the approximate method \n"); vav1=(vl+v2)/(2); printf("\t vav : %.2f ft^3/lb \n",vav1); row=62.5; rowac=(1/vav); s=(rowac/row); printf("\t actual density : %.3f lb/ft^3 \n",rowac); printf("\t s : %.4f \n",s); rowap=(1/vav1); s=(rowap/row); printf("\t approximate density : %.3f lb/ft^3 \n",rowac); printf("\t s : %.4f \n",s); // end
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//clc() l = 10;//cm k1 = 0.49;//cal/(s.cm.C) x = 2;//cm dt = 0.1;//sec T0 = 100;//C T10 = 50;//C C = 0.2174;//cal/(g.C) rho = 2.7;//g/cm^3 k = k1/(C*rho); L = k * dt / x^2; disp(L,"L =") T(1,1) = 100; T(1,2) = 0; T(1,3) = 0; T(1,4) = 0; T(1,5) = 0; T(1,6) = 50; T(2,1) = 100; T(2,6) = 50; for i = 2:3 for j = 2:5 T(i,j) = T(i-1,j) + L * (T(i-1,j+1) - 2* T(i-1,j) + T(i-1,j-1)); end end disp(T(2,2),"T11 = ") disp(T(2,3),"T12 = ") disp(T(2,4),"T13 = ") disp(T(2,5),"T14 = ") disp(T(3,2),"T21 = ") disp(T(3,3),"T22 = ") disp(T(3,4),"T23 = ") disp(T(3,5),"T24 = ")
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//Eg-1.12 //pg-27 clear clc x = input("enter any value ") v = exp(-(x)^2/2); disp(v)
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//Exa 8.12 clc; clear; close; //Given data : A=200*25;//in um^2 A=A*10^-12;//in m^2 ETA=55;//Quantum Efficiency in % lambda=1.3;//in um lambda=lambda*10^-6;//in meter Id=8;//in nA Id=Id*10^-9;//i Ampere h=6.63*10^-34;//Planks constant q=1.6*10^-19;//in coulamb c=3*10^8;//in m/s NEP=h*c*sqrt(2*q*Id)/((ETA/100)*q*lambda);//in Watts disp(NEP,"Noise equivalent power in Watts : "); Dstar=sqrt(A)/NEP;//in m-Hz^2/W^-1 disp(Dstar,"Specific detectivity of Ge p-i-n photodiode in m-Hz^2/W : "); //Note : Answer in the bok is not accurate.
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// A Texbook on POWER SYSTEM ENGINEERING // A.Chakrabarti, M.L.Soni, P.V.Gupta, U.S.Bhatnagar // DHANPAT RAI & Co. // SECOND EDITION // PART II : TRANSMISSION AND DISTRIBUTION // CHAPTER 10: POWER SYSTEM STABILITY // EXAMPLE : 10.8 : // Page number 273-275 clear ; clc ; close ; // Clear the work space and console funcprot(0) // Given data V = 33.0*10**3 // Line voltage(V) R = 6.0 // Resistance per phase(ohm) X = 15.0 // Reactance per phase(ohm) // Calculations V_S = V/3**0.5 // Sending end phase voltage(V) V_R = V/3**0.5 // Receiving end phase voltage(V) beta = atand(X/R) // β(°) Z = (R**2+X**2)**0.5 // Impedance(ohm) delta_0 = 0.0 // δ(°) P_0 = (V_R/Z**2)*(V_S*Z*cosd((delta_0-beta))-V_R*R)/10**6 // Power received(MW/phase) delta_1 = 30.0 // δ(°) P_1 = (V_R/Z**2)*(V_S*Z*cosd((delta_1-beta))-V_R*R)/10**6 // Power received(MW/phase) delta_2 = 60.0 // δ(°) P_2 = (V_R/Z**2)*(V_S*Z*cosd((delta_2-beta))-V_R*R)/10**6 // Power received(MW/phase) delta_3 = beta // δ(°) P_3 = (V_R/Z**2)*(V_S*Z*cosd((delta_3-beta))-V_R*R)/10**6 // Power received(MW/phase) delta_4 = 90.0 // δ(°) P_4 = (V_R/Z**2)*(V_S*Z*cosd((delta_4-beta))-V_R*R)/10**6 // Power received(MW/phase) delta_5 = 120.0 // δ(°) P_5 = (V_R/Z**2)*(V_S*Z*cosd((delta_5-beta))-V_R*R)/10**6 // Power received(MW/phase) delta_6 = (acosd(R/Z))+beta // δ(°) P_6 = (V_R/Z**2)*(V_S*Z*cosd((delta_6-beta))-V_R*R)/10**6 // Power received(MW/phase) delta = [delta_0,delta_1,delta_2,delta_3,delta_4,delta_5,delta_6] P = [P_0,P_1,P_2,P_3,P_4,P_5,P_6] a = gca() ; a.thickness = 2 // sets thickness of plot plot(delta,P,'ro-') a.x_label.text = 'Electrical degree' // labels x-axis a.y_label.text = 'Power in MW/phase' // labels y-axis xtitle("Fig E10.7 . Power angle diagram") xset('thickness',2) // sets thickness of axes xstring(70,14.12,'P_max = 14.12 MW/phase(approximately)') P_max = V_R/Z**2*(V_S*Z-V_R*R)/10**6 // Maximum power transmitted(MW/phase) delta_equal = 0.0 // δ With no phase shift(°) P_no_shift = (V_R/Z**2)*(V_S*Z*cosd((delta_equal-beta))-V_R*R)/10**6 // Power transmitted with no phase shift(MW/phase) // Results disp("PART II - EXAMPLE : 10.8 : SOLUTION :-") printf("\nPower angle diagram is plotted and is shown in the Figure 1") printf("\nMaximum power the line is capable of transmitting, P_max = %.2f MW/phase", P_max) printf("\nWith equal voltage at both ends power transmitted = %.f MW/phase", abs(P_no_shift))
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// find whether transistor remains in saturated region // Electronic Principles // By Albert Malvino , David Bates // Seventh Edition // The McGraw-Hill Companies // Example 7-6, page 235 clear;clc; close; // Given data Vcc=20;// collector supply voltage in volts Vbb=10;// base voltage in volts Rc=10*10^3;// collector resistance in ohms Rb=1*10^6;// base resistance in ohms Bdc=50; // Calculations Ib=Vbb/Rb;// base current in amperes Ic=Bdc*Ib;// collector current in amperes Vce=Vcc-(Ic*Rc);// collector-emitter voltage in volts disp("Volts",Vce,"collector-emitter voltage") // Result // as Vce>0 ,the transistor is not saturated
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//Example_a_4_8 page no:178 clc; Ip=10;//peak current in mA taken from i(t) equation Ipp=2*Ip; Irms=0.707*Ip; Iav=0.637*Ip; disp(Ip,"the peak value of current is (in mA)"); disp(Ipp,"the peak to peak value of current is(in mA)"); disp(Irms,"the rms value of current is (in mA)"); disp(Iav,"the average value of current is (in mA)");
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clc // Given that lambda1 = 5000 // Wavelength of light in angstrom theta1 = 30 // Optical rotation for lambda1 in degree lambda2 = 4000 // Wavelength of light in angstrom theta2 = 50 // Optical rotation for lambda2 in degree t = 1 // Thickness of plate in mm theta_max = 90 // Angle between prisms for maximum trnsition in degree // Sample Problem 18 on page no. 219 printf("\n # PROBLEM 18 # \n") printf("\n Standard formula used \n theta = a + b/(lambda)^2. \n") b = (theta2-theta1)*(lambda1*1e-10*lambda2*1e-10)^2/((lambda1*1e-10)^2-(lambda2*1e-10)^2) // Calculation for constant b a = theta1 -b/(lambda1*1e-10)^2 // Calculation of constant a t_min = t* theta_max/theta1 // calculation of thickness of material for maximum thickness in mm printf("\n Contents are as : \n a = %f deg/mm \n b = %e deg/mm angestrom^2 \n Thickness of plate required is %dmm.",a,b*1e10^2,t_min)
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clc; clear; lambda=6000*10^-8 //wavelength in cm N=5000 //lines per cm k=3 e=1/5000 //in cm sin_theta=1 //angle in radian //calculation k=(e*sin_theta)/lambda printf("The highest order of spectrum that can be seen is %d",k)
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//Example 7.36 The data below show the percentage increases in price of a few selected food items and the weights clc; clear; W=[33 11 8 5 5 3 7 9 9 10]; I=[180 202 115 212 175 517 260 426 332 279]; IW=I.*W; disp(100+ sum(IW)/sum(W),"Average Percentage increase in food price"); Index=[340 310 220 150 300]; Weight=[60 5 8 9 18]; disp(sum(Index.*Weight)/sum(Weight),"Cost of living index");
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// spadek swobodny z oporem powietrza - ODE 2. rzedu // spadek piłeczki tenisowej z Wieży Eiffla // params: rho = 1.2; cx = 0.47; m = 0.056; R = 0.0343; S = %pi * R ^ 2; g = 9.814; t = [0:0.01:25]; H = 356.5; N0 = [H;0]; // model function h = wysokosc(t, N) h = N(1); endfunction function Ndot = spadek(t, N) Ndot = [N(2); (0.5 * cx * rho * S * N(2) ^ 2 - m * g) / m]; endfunction N = ode('root', N0, t(1), t, spadek, 1, wysokosc); n = size(N, 2); subplot(121); plot(t(1:n), N(1, :)); xtitle('Położenie ciała', 't[s]', 'x[m]'); subplot(122); plot(t(1:n), N(2, :)); xtitle('Prędkość ciała', 't[s]', 'Vx[m/s]');
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clc; m=1; //mass in kg delt=80; //change in temperature in celcius c=1; //specific heat in kcal/kg.celcius Q=m*c*delt; //calculating heat disp(Q,"Heat required in kcal = "); //displaying result t=Q/9.4; //calculating time disp(t,"Time required in second = "); //displaying result
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function [xrold, xr, ea] = newtonraphson(funcion, dfuncion, xr, niter) for i = 1:niter xrold = xr fxr = funcion(xr) dfxr = dfuncion(xr) xr = xr - fxr/dfxr; ea = abs((xr - xrold)/xr)*100; end endfunction
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function Xi = genererRandExpo(lambda, iter) // On génère i lignes sur une colonne de v.a suivant la loi expo Xi = grand(iter,1,'exp',1/lambda); endfunction
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; atanh.tst ; ; Copyright (c) 2009-2023, Arm Limited. ; SPDX-License-Identifier: MIT OR Apache-2.0 WITH LLVM-exception func=atanh op1=7ff80000.00000001 result=7ff80000.00000001 errno=0 func=atanh op1=fff80000.00000001 result=7ff80000.00000001 errno=0 func=atanh op1=7ff00000.00000001 result=7ff80000.00000001 errno=0 status=i func=atanh op1=fff00000.00000001 result=7ff80000.00000001 errno=0 status=i func=atanh op1=7ff00000.00000000 result=7ff80000.00000001 errno=EDOM status=i func=atanh op1=fff00000.00000000 result=7ff80000.00000001 errno=EDOM status=i func=atanh op1=3ff00000.00000001 result=7ff80000.00000001 errno=EDOM status=i func=atanh op1=bff00000.00000001 result=7ff80000.00000001 errno=EDOM status=i func=atanh op1=3ff00000.00000000 result=7ff00000.00000000 errno=ERANGE status=z func=atanh op1=bff00000.00000000 result=fff00000.00000000 errno=ERANGE status=z func=atanh op1=00000000.00000000 result=00000000.00000000 errno=0 func=atanh op1=80000000.00000000 result=80000000.00000000 errno=0 ; No exception is raised with certain versions of glibc. Functions ; approximated by x near zero may not generate/implement flops and ; thus may not raise exceptions. func=atanh op1=00000000.00000001 result=00000000.00000001 errno=0 maybestatus=ux func=atanh op1=80000000.00000001 result=80000000.00000001 errno=0 maybestatus=ux
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clc clear xdel(winsid()) stacksize('max') //[y,Fs,bits] = wavread("/opt/work2/1.wav");Fs,bits //[y,Fs,bits] = wavread("/opt/work2/da.wav");Fs,bits [y,Fs,bits] = wavread("/opt/work2/r.wav");Fs,bits //[y,Fs,bits] = wavread("/opt/work2/20130801115515_16000.wav");Fs,bits //[y,Fs,bits] = wavread("/opt/work2/20130801115553_16000.wav");Fs,bits //[y,Fs,bits] = wavread("/opt/work2/20130801115415_16000.wav");Fs,bits //[y,Fs,bits] = wavread("/opt/work2/wavrecorder/20130808152550_16000.wav");Fs,bits // Pattern gut erkennbar //[y,Fs,bits] = wavread("/opt/work2/wavrecorder/20130808152632_16000.wav");Fs,bits // kein Pattern erkennbar //[y,Fs,bits] = wavread("/opt/work2/wavrecorder/20130808152656_16000.wav");Fs,bits // Pattern gut erkennbar //[y,Fs,bits] = wavread("/opt/work2/wavrecorder/20130808152804_16000.wav");Fs,bits // kein Pattern erkennbar //[y,Fs,bits] = wavread("/opt/work2/wavrecorder/20130812163819_16000.wav");Fs,bits PeriodeProBit = 12; lengthOfFrame = 8; tf = 2400; fcutl = 1900; fcuth = 2900; lengthOfSignal = size(y,2) indFcutl = ceil((lengthOfSignal/Fs)*fcutl); indFcuth = ceil((lengthOfSignal/Fs)*fcuth); t = 0:1/Fs:(size(y,2)-1)*1/Fs; subplot(3,1,1) plot(t,y) //mtlb_axis([0,6, -2, 2]); tmuster = mtlb_imp(0,1/mtlb_double(Fs),2/tf); muster = sin(((2*%pi)*tf)*tmuster); subplot(3,1,2) use_svd = 0; fLsignal = fft(y); fFilter = zeros(max(size(fLsignal)),1); fFilter(indFcutl:indFcuth)=1; fFilter(lengthOfSignal-indFcuth:lengthOfSignal-indFcutl)=1; fsignal = fLsignal.* fFilter'; Signal = mtlb_ifft(fsignal); //plot(t,abs(Signal)) b1 = (tf/mtlb_double(Fs))*ones(1,ceil(mtlb_double(Fs)/tf)); Signal2 = filter(b1,1,abs(Signal)); sigma = max(Signal2)/3; threshold = sigma*ones(length(Signal2),1); plot(t,[Signal2' threshold]); //plot(t,threshold); Signal3 = 0.5*sign(Signal2'-threshold)+0.5; subplot(3,1,3) plot(t,abs(Signal3)); FrameOnEdge=sum(Signal3(1:Fs/tf*lengthOfFrame*PeriodeProBit)); if 0~=FrameOnEdge ind=Fs/tf*lengthOfFrame*PeriodeProBit+1+... find(Signal3(Fs/tf*lengthOfFrame*PeriodeProBit+1:),1); else ind=find(Signal3,1); end result=zeros(1,lengthOfFrame); for i=1:lengthOfFrame pos=ind+ceil(PeriodeProBit*Fs/tf/2)+(i-1)*ceil(PeriodeProBit*Fs/tf); result(i)=Signal3(pos); end result
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//Ex_2_4 clc; clear; close; format('v',6); //given data : N1=500;//turns N2=2000;//turns K=50/100;//coefficient for 50% flux linked diBYdt=10;//A/s L1=200;//mH fi1BYI1=L1/N1; M=N2*fi1BYI1;//mH e2=M*10^-3*diBYdt;//V disp(M/1000,"Mutual Inductance of two coil(H)"); disp(e2,"Induced emf in the coil having 1000 turns(V)");
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clc; R1=2; //resistance in Ohm R2=6; //resistance in Ohm R3=3; //resistance in Ohm V=24; //voltage in volts R=8; //resistance in Ohm I=V/R; //Ohm's Law disp(I,"Current in Ampere = "); //displaying result V1=I*R1; //Ohm's Law disp(V1,"Voltage drop across R1 in Volts = "); //displaying result V2=I*R2; //Ohm's Law disp(V2,"Voltage drop across R2 in Volts = "); //displaying result V3=I*R3; //Ohm's Law disp(V3,"Voltage drop across R3 in Volts = "); //displaying result
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// Example 4.1 clc; clear; close; // Given data I_C= 0.9;// in mA I_E=1;// in mA alpha = I_C/I_E; disp(alpha,"Current gain is : ") // Formula I_E= I_B+I_C I_B= I_E-I_C;// in mA disp(I_B,"The base current in mA is : ")
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clc //initialisation of variables h1=179.43 //under -25 degrees temp in kj/kg h2=219.03 //kj/kg h4=74.59 //kj/kg //CALCULATIONS re=h1-h4 w=h2-h1 cop=re/w //RESULTS printf('the refrigeration effect is %2fkj/kg',re) printf('\ncoefficient of performance is %2f',cop)
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Ws=10^6 //N.m/s deltaP= -83*10^3 //N/m^2 g=9.81 //m/s^2 deltaZ= -103 //m D=10^3 //kg/m^3
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# Simple distilation column test units SI $thermo = VirtualMaterials.Peng-Robinson / -> $thermo thermo + PROPANE n-BUTANE ISOBUTANE n-PENTANE col = Tower.Tower() col.Stage_0 + 20 # twenty two stages` /col.MaxOuterLoops = 50 /col.Damping = 0.9 cd col.Stage_10 f = Tower.Feed() f.Port.T = 30 f.Port.P = 720 f.Port.MoleFlow = 10 f.Port.Fraction = .4 .05 .4 .15 f.Port cd ../Stage_0 l = Tower.LiquidDraw() l.Port.P = 700 l.Port.MoleFlow = 5 cond = Tower.EnergyFeed(0) reflux = Tower.StageSpecification('Reflux') reflux.Value = 1 cd ../Stage_21 l = Tower.LiquidDraw() l.Port.P = 720 reb = Tower.EnergyFeed(1) cd .. TryToSolve = 1 # start calculation # since there was little output here, I will put some profile stuff here L_MassFraction.PROPANE V_MoleFraction.ISOBUTANE L_MassFlow L_Viscosity L_StdVolFraction.PROPANE V_StdVolFraction.PROPANE L_VolumeFlow L_StdLiqVolumeFlow V_StdLiqVolumeFlow cd / #Create streams s_feed = Stream.Stream_Material() s_liqdraw_0 = Stream.Stream_Material() s_liqdraw_21 = Stream.Stream_Material() s_vapdraw_0 = Stream.Stream_Material() ene_cond = Stream.Stream_Energy() ene_reb = Stream.Stream_Energy() s_intvap_1 = Stream.Stream_Material() s_intliq_0 = Stream.Stream_Material() #Create clones in streams cd /s_feed clone = Stream.ClonePort(0) cd /s_liqdraw_0 clone = Stream.ClonePort() cd /s_liqdraw_21 clone = Stream.ClonePort() cd /s_vapdraw_0 clone = Stream.ClonePort() cd /ene_cond clone = Stream.ClonePort() cd clone cd /ene_reb clone = Stream.ClonePort(0) cd /s_intvap_1 clone = Stream.ClonePort(0) cd /s_intliq_0 clone = Stream.ClonePort() cd /s_liqdraw_0 clone2 = Stream.ClonePort() cd /ene_cond clone2 = Stream.ClonePort() #Create clones in tower cd /col.Stage_1 vaporclone = Tower.InternalVapourClone() cd /col.Stage_0 liquidclone = Tower.InternalLiquidClone() #Create a balance for the overall tower cd / bal = Balance.BalanceOp() cd bal NumberStreamsInMat = 1 NumberStreamsOutMat = 2 NumberStreamsInEne = 1 NumberStreamsOutEne = 2 BalanceType = 4 #Create a balance for the top stage cd / stagebalance = Balance.BalanceOp() cd stagebalance BalanceType = 4 NumberStreamsInMat = 1 NumberStreamsOutMat = 2 NumberStreamsOutEne = 2 #Connect the streams to the tower and the clones to the balance /s_feed.Out -> /col.Feed_10_f /s_liqdraw_0.In -> /col.LiquidDraw_0_l /s_liqdraw_21.In -> /col.LiquidDraw_21_l /ene_cond.In -> /col.EnergyFeed_0_cond /ene_reb.Out -> /col.EnergyFeed_21_reb /bal.In0 -> /s_feed.clone /bal.Out0 -> /s_liqdraw_0.clone /bal.Out1 -> /s_liqdraw_21.clone /bal.InQ0 -> /ene_reb.clone /bal.OutQ0 -> /ene_cond.clone /stagebalance.In0 -> /s_intvap_1.clone /stagebalance.Out0 -> /s_intliq_0.clone /stagebalance.Out1 -> /s_liqdraw_0.clone2 /stagebalance.OutQ0 -> /ene_cond.clone2 /s_intliq_0.In -> /col.InternalLiquid_0_liquidclone /s_intvap_1.In -> /col.InternalVapour_1_vaporclone cd /col MaxOuterError = 1e-6 MaxInnerError = 1e-6 TryToRestart = 1 /col.LiquidDraw_0_l #Add degrees of subcooling cd /col.Stage_0 degsubcool = Tower.DegSubCooling() /col.DegSubCool_0_degsubcool.DT = 2 /col.LiquidDraw_0_l /bal.OutQ1 /stagebalance.OutQ1 /col.DegSubCool_0_degsubcool.DT = 4 /col.LiquidDraw_0_l /bal.OutQ1 /stagebalance.OutQ1 /col.DegSubCool_0_degsubcool.DT = 0 /col.LiquidDraw_0_l /bal.OutQ1 /stagebalance.OutQ1 /col.DegSubCool_0_degsubcool.DT = /col.LiquidDraw_0_l.T = 18 /col.DegSubCool_0_degsubcool /bal.OutQ1 /stagebalance.OutQ1 /col.LiquidDraw_0_l.MoleFlow = /col.DegSubCool_0_degsubcool.DT = 2 /col.DegSubCool_0_degsubcool /col.LiquidDraw_0_l /bal.OutQ1 /stagebalance.OutQ1 #Now add a vapour draw and make sure it doesnt break anything /col.TryToSolve = 0 /col.TryToRestart = 0 cd /col.Stage_0 vap = Tower.VapourDraw() cd / #Should solve fine even for vap flow > 0.0 /col.DegSubCool_0_degsubcool.DT = 0 /col.TryToSolve = 1 /col.VapourDraw_0_vap.MoleFlow = 1 /bal.OutQ1 /stagebalance.OutQ1 #Solve with an inconcistency /col.LiquidDraw_0_l.T = /col.LiquidDraw_0_l.MoleFlow = 5 /col.DegSubCool_0_degsubcool.DT = 1 /bal.OutQ1 /stagebalance.OutQ1 #Solve fine again /col.DegSubCool_0_degsubcool.DT = 0 #Should attempt to solve for vapour draw even if TryToSolve = 0 /col.DegSubCool_0_degsubcool.DT = /col.TryToSolve = 0 /col.DegSubCool_0_degsubcool.DT = 1 /col.VapourDraw_0_vap.MoleFlow = /col.VapourDraw_0_vap.MoleFlow /col.TryToSolve = 1 #Solve fine. A DegSubcooling > 0.0 puts a zero lfow in the vap flow /col.VapourDraw_0_vap.MoleFlow = /bal.OutQ1 /stagebalance.OutQ1 # Can not solve because the liquid is subcooled and the vap is > 0.0 /col.DegSubCool_0_degsubcool.DT = /col.LiquidDraw_0_l.T = 18 C /col.VapourDraw_0_vap.MoleFlow = 1 /bal.OutQ1 /stagebalance.OutQ1 #Solve fine /col.VapourDraw_0_vap.MoleFlow = 0 /bal.OutQ1 /stagebalance.OutQ1 #Get rid of the vapour draw wich should not have been there at all to begin with delete /col.Stage_0.vap /bal.OutQ1 /stagebalance.OutQ1 copy / paste /
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clc //Variable Initialisation Ea=230//Input Voltage of motor in volts N1=1200//Rated Speed of Motor in rpm N2=1000//Rated Speed of Motor in rpm Ia=15//Armature Current in Ampere Ia2=1.5*Ia Ra=1.2//Armature resistance in ohm Rb=20 d2=0.5 //Solution Eb1=Ea-(Ia*Ra) Eb2=(N2/N1)*Eb1 d1=(1-(((Eb2/Ia2)-Ra)/Rb)) Eb3=Ia*(((1-d2)*Rb)+Ra) N3=(Eb3/Eb1)*N1 printf('\n\n Duty Ratio Of Chopper=%0.1f\n\n',d1) printf('\n\n Motor Speed=%0.1f rpm\n\n',N3)
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Example_5.sce
//Chapter-18,Example 5,Page 406 clc(); close(); H2 =0.24 //composition of H2 CH4 =0.3 //composition of CH4 CO =0.06 //composition of CO C2H6 =0.11 //composition of C2H6 C2H4 =0.045 //composition of C2H4 C4H8 =0.025 //composition of C4H8 N2=0.12 //composition of N2 CO2=0.08 //composition of CO2 O2=0.02 //composition of O2 //for reaction H2 + (1/2)O2 = H2O V1=H2*(1/2) //volume of O2 required //for reaction CH4 + 2O2 = CO2 + 2H2O V2=CH4*2 //volume of O2 required vCO2_1=CH4*1 //volume of CO2 //for reaction C2H6 + (7/2)O2 = 2CO2 +3H2O V3=C2H6*(7/2) //volume of O2 required vCO2_2=C2H6*2 //volume of CO2 //for reaction C2H4 + 3O2 = 2CO2 +2H2O V4=C2H4*3 //volume of O2 required vCO2_3=C2H4*2 //volume of CO2 //for reaction C4H8 + 6O2 = 4CO2 +4H2O V5=C4H8*6 //volume of O2 required vCO2_4=C4H8*4 //volume of CO2 //for reaction CO + (1/2)O2 = CO2 V6=CO*(1/2) //volume of O2 required vCO2_5=CO*1 //volume of CO2 total_O2= V1+V2+V3+V4+V5+V6-O2 //total volume of oxygen //as air contains 21% of O2 by volume //when 40% excess V_air = total_O2*(100/21)*(140/100) //volume of air printf("the air to fuel ratio is %.3f",V_air) total_CO2 = vCO2_1+vCO2_2+vCO2_3+vCO2_4+vCO2_5+CO2 //total volume of CO2 total_dry= total_CO2 +[N2+(79*V_air/100)]+[(V_air*21/100)-total_O2] printf("\n the total volume of dry products is %.4f cubicmeter ",total_dry) CO2_dry =total_CO2*100/total_dry N2_dry =[N2+(79*V_air/100)]*100/total_dry O2_dry =[(V_air*21/100)-total_O2]*100/total_dry printf("\n Composition of products of combustion on dry basis") printf("\n CO2 = %.3f",CO2_dry) printf("\n N2 = %.3f",N2_dry) printf("\n O2 = %.3f",O2_dry) //calculation mistake in textbook
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PrepAtt20_Disc_Fix_Practice_pcl.sce
# == Header == # # Disc Fix Delay scenario = "17_March_2015"; active_buttons=3; #button press button_codes=251,252,253; # == Screen Parameters == # default_font_size = 24 ; default_font = "Arial"; default_text_color = 0, 0, 0; #noir #screen_width = 1024; #screen_height = 768; #screen_bit_depth = 32; default_background_color = 200, 200, 200; begin; TEMPLATE "PrepAtt_stim_trial.tem" {}; begin_pcl; preset string nom_sujet; #subject # == Temporal Parameters == # int duree_instruc_task=1000; # Display task for 2s int duree_instruc=3000; # Instruction 1s before sounds start int duree_mem_sound=300; int max_rep=3300; # increased by 300 int duree_minstruct=50; int rep_plus=0; int delay_plus1=0; int delay_plus2=0; # === Sound Paramaters == # int dur_sTAR=100; #target sound duration int dur_sDIS=300; # distractor duration int dur_cue=194; #cue presentation 192 (to be changed in Template "PrepAtt_stim_trial.tem" to 200 for trials = 12 trames a 60Hz double correc_atttar =-0.20; double correc_attdis =-0.35; array<double> final_att[4]; # Values of attenuation left and right specific ot each subject array<int>side[4]; # Table of four options 1=left Low, 2= Right Low, 3= Left High 4= Right High double final_atta; # Value of left low double final_attb; # Value of left high double final_attc; # Value of right low double final_attd; # Value of right high double att_sTARa; # Target sound attenuation applied after correction "left low" double att_sTARb; # Target sound attenuation applied after correction "left high" double att_sTARc; # Target sound attenuation applied after correction "right low" double att_sTARd; # Target sound attenuation applied after correction "right high" double att_sDISg; # Distracter sound attenuation left double att_sDISd; # Distracter sound attenuation right # == Variables == # string filename; int nbessais = 0; int num; int trialt; string cue; int codCUE; int delay1; int dis; int dis1; int tar; int fa = 0; int codDIS; string DIS; string TARwav; int delay2; string TAR; int codTAR; int bp; int ISIrand; int nbrep; string temp; array<int> meantr[0]; array<int> meantr_val[0]; array<int> meantr_inval[0]; double moytr; double moytr_val; double moytr_inval; double cue_check; string up; string down; int valide; int rep=0; int rec_time; int missrep=0; int multirep=0; int rep_before_tar=0; int cuefic; int counter; int ER; int SR; int correct =0; int incorrect=0; int norep=0; # == Reading Into Attenuation Files ==# # Open input_file inatt = new input_file; filename.append("../log/"); filename.append(nom_sujet); filename.append("_thresholds"); filename.append(".txt"); inatt.open(filename,false); # Skip first line inatt.get_line(); # Read side 1 inatt.set_delimiter('\t'); temp=inatt.get_line(); side[1]=inatt.get_int(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; temp=inatt.get_line(); temp=inatt.get_line(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; inatt.set_delimiter('\n'); final_att[1]=inatt.get_double(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; # Read side 2 inatt.set_delimiter('\t'); temp=inatt.get_line(); side[2]=inatt.get_int(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; temp=inatt.get_line(); temp=inatt.get_line(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; inatt.set_delimiter('\n'); final_att[2]=inatt.get_double(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; # Read side 3 inatt.set_delimiter('\t'); temp=inatt.get_line(); side[3]=inatt.get_int(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; temp=inatt.get_line();# Read volume temp=inatt.get_line(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; inatt.set_delimiter('\n'); final_att[3]=inatt.get_double(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; # Read side 4 inatt.set_delimiter('\t'); temp=inatt.get_line(); side[4]=inatt.get_int(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; temp=inatt.get_line();# Read volume temp=inatt.get_line(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; inatt.set_delimiter('\n'); final_att[4]=inatt.get_double(); if !inatt.last_succeeded() then term.print( "Error reading file!\n" ); exit(); else end; inatt.close(); # Attenuation Calculation final_atta= final_att[1]; # left low final_attb= final_att[3]; # right low final_attc= final_att[2]; # left high final_attd= final_att[4]; #right high att_sDISg=final_atta+correc_attdis; #for dist left att_sDISd=final_attb+correc_attdis; #for dist right att_sTARa=final_atta + correc_atttar; #tar att_sTARb=final_attb + correc_atttar; #tar att_sTARc=final_attc + correc_atttar; #tar att_sTARd=final_attd + correc_atttar; #tar # == Attenuation Display == # text1.set_caption("Attenuation Gauche: " +string(final_atta)+ " Attenuation Droite: "+string(final_attb)+"\n Press Enter To Continue."); text1.redraw(); info_trial2.present(); # -- Memory -- # # Display trial_instruc2.set_duration(duree_instruc_task); trial_instruc2.present(); trial_no.set_duration(duree_instruc); trial_no.present(); # Play #low Sound_tar_1_low.set_attenuation(att_sTARb); Sound_tar_1_low.set_pan(0.0);# Max left attenuation mem_tar1_low.set_duration(dur_sTAR); mem_tar1_low.present(); trial_no.set_duration(duree_instruc); trial_no.present(); #high Sound_tar_1_high.set_attenuation(att_sTARd); Sound_tar_1_high.set_pan(0.0);# Max left attenuation mem_tar1_high.set_duration(dur_sTAR); mem_tar1_high.present(); trial_no.set_duration(duree_instruc); trial_no.present(); #disc_instruc.present(); #trial_no.set_duration(duree_instruc); #trial_no.present(); # == Display Instructions == # disc_instruc.present(); event_instruc.set_port_code(90); trial_no.set_duration(duree_instruc); trial_no.present(); # == First Reading Into Settings file to find the number of lines == # input_file in = new input_file; filename=""; filename=("Practice_Disc"); filename.append(".txt"); in.open(filename); loop until in.end_of_file() begin in.get_line(); if in.last_succeeded() then nbessais = nbessais+1; else break; end; end; in.close(); # === Creating Results File == # filename=""; filename.append(nom_sujet); filename.append("_"); filename.append("Practice_Disc"); #discrimination filename.append(".txt"); output_file out = new output_file; out.open(filename); out.print("Subject: "+nom_sujet); out.print("\n"); out.print("\n"); out.print("N Cue D1 Dis D2 Tar ER SR FA MR RT"); out.print("\n"); # == Second reading Into Parameters File to Initialize variables in the loop presentation of trials == # filename=""; filename=("Practice_Disc.txt"); in.open(filename); in.get_line(); # Skip First Line int i=1; #Start Loop loop until in.end_of_file() || !in.last_succeeded() || (i > nbessais+1) begin in.set_delimiter('\n'); num=in.get_int(); if !in.last_succeeded() then break; end; valide=in.get_int(); if !in.last_succeeded() then break; end; in.set_delimiter('\"'); cue=in.get_line(); cue=in.get_line(); if !in.last_succeeded() then break; end; in.set_delimiter('\n'); codCUE=in.get_int(); if !in.last_succeeded() then break; end; delay1=in.get_int(); if !in.last_succeeded() then break; end; dis1=in.get_int(); if !in.last_succeeded() then break; end; codDIS=in.get_int(); if !in.last_succeeded() then break; end; in.set_delimiter('\"'); DIS=in.get_line(); DIS=in.get_line(); if !in.last_succeeded() then break; end; in.set_delimiter('\n'); delay2=in.get_int(); if !in.last_succeeded() then break; end; in.set_delimiter('\"'); TAR=in.get_line(); TAR=in.get_line(); if !in.last_succeeded() then break; end; in.set_delimiter('\n'); codTAR=in.get_int(); if !in.last_succeeded() then break; end; bp=in.get_int(); if !in.last_succeeded() then break; end; ISIrand=in.get_int(); if !in.last_succeeded() then break; end; in.get_line(); # == Attribution of Events and Trials Names == # # Output for the matlab code: low_L(A) high_L (B) high_R (C) low_R (D) Blank (E) TAR=TAR+(".wav"); if dis1==0 then dis=1; else dis=2; end; DIS=DIS+(".wav"); Sound_tar_1_low_wav.set_filename(DIS); Sound_tar_1_high_wav.set_filename(DIS); Sound_dis_wav.set_filename(DIS); # Cue + Dis if (cue=="Larrow") then event_cue.set_stimulus(Larrow); event_cue_dis.set_stimulus(Larrow); cuefic=1; end; if (cue=="Rarrow") then event_cue.set_stimulus(Rarrow); event_cue_dis.set_stimulus(Rarrow); cuefic=2; end; if (cue=="Barrow") then event_cue.set_stimulus(Barrow); event_cue_dis.set_stimulus(Barrow); cuefic=0; end; if (DIS!="nul.wav") then Sound_dis.get_wavefile().load(); event_cue_dis.set_event_code(string(codCUE)); event_cue_dis.set_port_code(codCUE); event_dis.set_event_code(string(codDIS)); event_dis.set_port_code(codDIS); if(final_attc>=final_atta) then Sound_dis.set_pan(-att_sDISd+att_sDISg); Sound_dis.set_attenuation(att_sDISg); # Commented to avoid a bug else Sound_dis.set_pan(att_sDISd-att_sDISg); Sound_dis.set_attenuation(att_sDISd); end; else event_cue.set_event_code(string(codCUE)); event_cue.set_port_code(codCUE); end; trial_cue.set_duration(dur_cue+delay1+delay_plus1+dur_sDIS+delay2+delay_plus2); trial_cuedis.set_duration(dur_cue+delay1+delay_plus1+dur_sDIS+delay2+delay_plus2); event_dis.set_delta_time(dur_cue+delay1+delay_plus1); random_trial[dis].present(); if (bool( response_manager.response_count() )) then fa=fa+1; # false alarms rep_before_tar=response_manager.response_count();; rec_time=0; end; # Target if (TAR=="S_tarson_A.wav") then Sound_tar_1_low.set_pan(-1.0);# Max left attenuation Sound_tar_1_low.set_attenuation(att_sTARa); #Sound_tar_1_low.set_attenuation(att_sTARb); tar=1; trial_tar1_low.set_duration(dur_sTAR+max_rep+rep_plus+ISIrand); event_target1_low.set_target_button(bp); #determine la reponse attendue event_target1_low.set_event_code(string(codTAR)); event_target1_low.set_port_code(codTAR); trial_tar1_low.present(); end; if (TAR=="S_tarson_B.wav") then Sound_tar_1_low.set_pan(1.0);# Max right attenuation Sound_tar_1_low.set_attenuation(att_sTARb); tar=2; trial_tar1_low.set_duration(dur_sTAR+max_rep+rep_plus+ISIrand); event_target1_low.set_target_button(bp);#determine la reponse attendue event_target1_low.set_event_code(string(codTAR)); event_target1_low.set_port_code(codTAR); trial_tar1_low.present(); end; if (TAR=="S_tarson_C.wav") then Sound_tar_1_high.set_pan(-1.0);# Max left attenuation Sound_tar_1_high.set_attenuation(att_sTARc); #Sound_tar_1_high.set_attenuation(att_sTARd); tar=3; trial_tar1_high.set_duration(dur_sTAR+max_rep+rep_plus+ISIrand); event_target1_high.set_target_button(bp); #determine la reponse attendue event_target1_high.set_event_code(string(codTAR)); event_target1_high.set_port_code(codTAR); trial_tar1_high.present(); end; if (TAR=="S_tarson_D.wav") then Sound_tar_1_high.set_pan(1.0);# Max right attenuation Sound_tar_1_high.set_attenuation(att_sTARd); tar=4; trial_tar1_high.set_duration(dur_sTAR+max_rep+rep_plus+ISIrand); event_target1_high.set_target_button(bp);#determine la reponse attendue event_target1_high.set_event_code(string(codTAR)); event_target1_high.set_port_code(codTAR); trial_tar1_high.present(); end; if (bool( response_manager.response_count() )) then response_data last = response_manager.last_response_data(); rep=last.button(); stimulus_data last1 = stimulus_manager.last_stimulus_data(); rec_time=last1.reaction_time(); nbrep=response_manager.response_count(); else missrep=missrep+1; rec_time=0; end; if (nbrep>0) then if(nbrep)>1 then multirep=multirep+1; meantr.add(rec_time); rec_time=0; else meantr.add(rec_time); end; end; if rep == bp then correct=correct+1; else incorrect=incorrect+1; end; if cuefic != 0 then if dis1==0 then meantr_val.add(rec_time); else meantr_inval.add(rec_time); end; end; # Write Trial out.print(i); out.print(" "); out.print(cuefic); out.print(" "); out.print(delay1); out.print(" "); out.print(dis1); out.print(" "); out.print(delay2); out.print(" "); out.print(tar); out.print(" "); out.print(bp); out.print(" "); out.print(rep); out.print(" "); out.print(rep_before_tar); out.print(" "); out.print(nbrep); out.print(" "); out.print(rec_time); out.print("\n"); if(DIS!="nul.wav") then Sound_dis.get_wavefile().unload(); end; i=i+1; end; moytr=floor(arithmetic_mean(meantr)); moytr_val=floor(arithmetic_mean(meantr_val)); moytr_inval=floor(arithmetic_mean(meantr_inval)); cue_check= moytr_inval - moytr_val; # == Write Block Results == # out.print("\n"); out.print("nb trial with correct rep:"); out.print(correct); out.print("\n"); out.print("nb trial with incorrect rep:"); out.print(incorrect); out.print("\n"); out.print("nb trial with no rep:"); out.print(missrep); out.print("\n"); out.print("Average RT:"); out.print(moytr); out.print("\n"); out.close(); in.close(); #== Average Reaction Time ==# if cue_check > 19.0 then text1.set_caption("temps de reaction "+string(moytr)+" + \n correct trials = "+string(correct)+" / 9 \n Press Enter To Continue."); text1.redraw(); info_trial2.present(); else text1.set_caption("temps de reaction "+string(moytr)+" - \n correct trials = "+string(correct)+" / 9 \n Press Enter To Continue."); text1.redraw(); info_trial2.present(); end;
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//METODO DE GAUSS COM PIVOTAMENTO PARCIAL a = [10 2 1; 1 5 1; 2 3 10]; b = [7; -8; 6]; //f = [1.00 1 1; 2.00 1 1; 1 1 1]; function u = gauss(a, b) [l,c] = size(a);//sabe as linhas e colunas de a //concatena u = [a b]; //percorrer o pivo for j=1:c//coluna pivo = u(j, j); //pivotamento parcial for k = j+1:l if abs(pivo)<abs(u(k, j)) then aux2 = u(j, :); pivo = u(k,j); u(j,:)=u(k, :); u(k,:)=aux2; end end for i=j+1:l//percorre a linha abaixo do pivo fator=u(i,j)/pivo; //calculo u(i, :) = u(i, :) - fator*u(j, :); end end endfunction [r] = gauss( a, b) //subida TRIANGULAR [l,c] = size(a); for i =l:-1:1 x(i) = b(i)/a(i,i); for j=i+1:c x(i) = x(i) -(a(i,j)/a(i,i)) *x(j); end end x
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ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 0.518687D+00 2 -0.728827D-02 0.418126D-02 3 0.321547D-01 0.163043D-02 0.316275D+00 4 0.145900D-02 0.173612D-03 -0.221307D-02 0.289313D-02 5 0.527835D-03 0.136442D-03 -0.577076D-03 -0.809237D-04 0.391936D-02 6 0.234629D-03 -0.137281D-03 -0.310176D-03 0.610317D-04 -0.730508D-04 7 -0.123416D-03 -0.180246D-03 0.613858D-03 0.701569D-04 -0.104539D-03 8 0.641101D-03 0.241279D-04 -0.631947D-04 -0.351725D-04 0.649292D-04 9 -0.126735D+00 0.201715D-01 0.817361D-01 -0.320260D-01 0.933586D-01 10 0.612479D-01 0.137470D-01 -0.234082D-01 -0.121815D-01 0.171035D+00 11 0.752756D-01 -0.260000D-01 -0.110071D+00 -0.700770D-03 0.377885D-01 12 0.558571D+00 -0.445532D-01 0.591238D+00 -0.250759D-01 0.386974D-01 13 0.577022D-01 -0.130635D-01 0.861011D-01 0.885798D-02 -0.690482D-02 14 0.254904D+00 0.604327D-02 0.481031D+00 0.263991D-01 0.982750D-03 15 -0.773334D+00 -0.666058D-01 -0.833796D+00 0.180361D-01 -0.128218D+00 16 -0.432509D-01 -0.432805D-02 0.135330D-01 -0.267942D-02 -0.272135D-02 17 -0.983672D-03 -0.554665D-03 -0.287712D-03 0.780872D-04 -0.833381D-03 18 -0.115610D+01 0.592494D-01 -0.129246D+00 -0.292457D-01 0.285218D-01 19 0.670108D-01 -0.734621D-03 0.173471D+00 -0.201261D-01 0.339579D-02 20 -0.968025D+00 0.257485D-01 -0.208926D+00 0.295879D-01 -0.296309D-01 21 -0.547430D-01 -0.317787D-02 -0.220364D+00 0.211495D-01 -0.692192D-02 22 0.209257D-02 -0.168608D-03 0.853479D-04 -0.321545D-03 -0.881245D-04 23 -0.236714D-01 -0.116029D-02 0.171870D-01 0.366137D-02 0.150949D-02 24 0.469675D-02 -0.290616D-03 0.227573D-02 0.324765D-03 -0.203963D-03 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 0.714832D-03 7 0.709118D-03 0.329206D-02 8 0.108052D-03 0.281699D-04 0.212915D-02 9 0.664819D-02 0.487421D-01 0.437621D-02 0.578180D+02 10 0.671476D-02 -0.268371D-02 0.326262D-02 0.296703D+01 0.244899D+02 11 0.373203D-01 0.806756D-01 0.159340D-01 0.106059D+02 0.389397D+01 12 0.441981D-01 0.512260D-01 0.181320D+00 0.856449D+01 -0.662457D-01 13 0.479056D-01 0.100432D+00 0.604714D-02 0.889557D+00 -0.123483D+00 14 0.589039D-02 -0.119947D-01 0.168085D+00 0.624816D+00 0.158810D+01 15 0.654600D-02 0.109644D-01 -0.271012D-02 -0.174253D+02 -0.153258D+02 16 0.195334D-02 0.181210D-02 -0.974579D-03 0.156859D+01 -0.490441D+00 17 -0.620799D-04 0.341260D-04 -0.194139D-03 -0.207112D+00 -0.309393D-01 18 -0.176992D-01 -0.915364D-01 0.239307D-01 -0.163497D+01 -0.513266D+01 19 -0.721800D-02 0.735400D-02 -0.211399D-02 0.102954D+01 0.951320D+00 20 -0.705052D-02 0.206270D-01 -0.211726D+00 -0.653019D+01 0.436877D+01 21 0.626102D-02 -0.768039D-02 0.315239D-02 -0.109157D+01 -0.898954D+00 22 -0.296133D-03 -0.545792D-03 -0.184648D-03 -0.732204D-02 0.395505D-02 23 0.915336D-03 0.939770D-03 -0.663082D-03 -0.590298D-01 0.535807D-01 24 -0.164768D-03 -0.280244D-03 -0.239197D-03 -0.111269D-01 -0.259471D-01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 0.502190D+02 12 0.287911D+00 0.165292D+03 13 -0.111004D+00 0.425900D+01 0.132662D+02 14 -0.737189D+00 0.134766D+02 0.536739D+00 0.628002D+02 15 -0.117323D+02 -0.715934D+00 0.511782D+01 0.406004D+00 0.599827D+03 16 -0.197844D-01 0.284029D+00 0.162620D+00 -0.365016D+00 0.192326D+01 17 0.477796D-01 -0.909437D-01 -0.484772D-01 -0.693039D-02 -0.245135D+01 18 -0.136604D+02 0.252171D+01 -0.862083D+00 0.655532D+01 0.650544D+02 19 0.274346D+01 -0.265833D+00 -0.102116D+01 -0.610762D+00 0.305812D+01 20 -0.280676D+01 -0.729210D+02 -0.102696D+01 -0.341395D+02 0.285653D+02 21 -0.161861D+01 0.293005D+00 0.998396D+00 0.663304D+00 -0.268371D+01 22 -0.775191D-01 -0.175651D-01 -0.373940D-01 -0.289598D-01 -0.131394D+00 23 0.161738D+00 0.110617D+00 -0.111564D-01 -0.110116D+00 -0.841569D+00 24 -0.643700D-02 0.216029D-01 -0.797628D-02 0.188750D-02 -0.108120D+00 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 0.851501D+00 17 -0.573768D-01 0.257993D-01 18 0.979719D+00 -0.284836D+00 0.271049D+03 19 -0.824965D-02 -0.143728D-01 0.345429D+00 0.553264D+01 20 0.567896D-02 -0.111012D+00 0.181121D+02 0.631065D+01 0.314043D+03 21 0.181512D+00 0.108247D-01 0.214407D+01 -0.518956D+01 -0.682862D+01 22 -0.496643D-02 0.156447D-02 -0.123664D+01 0.116805D-02 -0.896397D-01 23 -0.168378D-02 0.561123D-02 -0.551526D+00 -0.191446D+00 0.276883D+01 24 0.166775D-02 0.116335D-02 0.185196D-02 -0.318517D-01 -0.140306D+01 ESTIMATED COVARIANCE MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 0.642643D+01 22 -0.540209D-01 0.135947D-01 23 0.248607D+00 -0.254735D-02 0.374433D+00 24 0.294869D-01 0.285020D-03 -0.332177D-01 0.138175D-01 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 1 2 3 4 5 ________ ________ ________ ________ ________ 1 1.000 2 -0.157 1.000 3 0.079 0.045 1.000 4 0.038 0.050 -0.073 1.000 5 0.012 0.034 -0.016 -0.024 1.000 6 0.012 -0.079 -0.021 0.042 -0.044 7 -0.003 -0.049 0.019 0.023 -0.029 8 0.019 0.008 -0.002 -0.014 0.022 9 -0.023 0.041 0.019 -0.078 0.196 10 0.017 0.043 -0.008 -0.046 0.552 11 0.015 -0.057 -0.028 -0.002 0.085 12 0.060 -0.054 0.082 -0.036 0.048 13 0.022 -0.055 0.042 0.045 -0.030 14 0.045 0.012 0.108 0.062 0.002 15 -0.044 -0.042 -0.061 0.014 -0.084 16 -0.065 -0.073 0.026 -0.054 -0.047 17 -0.009 -0.053 -0.003 0.009 -0.083 18 -0.098 0.056 -0.014 -0.033 0.028 19 0.040 -0.005 0.131 -0.159 0.023 20 -0.076 0.022 -0.021 0.031 -0.027 21 -0.030 -0.019 -0.155 0.155 -0.044 22 0.025 -0.022 0.001 -0.051 -0.012 23 -0.054 -0.029 0.050 0.111 0.039 24 0.055 -0.038 0.034 0.051 -0.028 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 6 7 8 9 10 ________ ________ ________ ________ ________ 6 1.000 7 0.462 1.000 8 0.088 0.011 1.000 9 0.033 0.112 0.012 1.000 10 0.051 -0.009 0.014 0.079 1.000 11 0.197 0.198 0.049 0.197 0.111 12 0.129 0.069 0.306 0.088 -0.001 13 0.492 0.481 0.036 0.032 -0.007 14 0.028 -0.026 0.460 0.010 0.040 15 0.010 0.008 -0.002 -0.094 -0.126 16 0.079 0.034 -0.023 0.224 -0.107 17 -0.014 0.004 -0.026 -0.170 -0.039 18 -0.040 -0.097 0.032 -0.013 -0.063 19 -0.115 0.054 -0.019 0.058 0.082 20 -0.015 0.020 -0.259 -0.048 0.050 21 0.092 -0.053 0.027 -0.057 -0.072 22 -0.095 -0.082 -0.034 -0.008 0.007 23 0.056 0.027 -0.023 -0.013 0.018 24 -0.052 -0.042 -0.044 -0.012 -0.045 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 11 12 13 14 15 ________ ________ ________ ________ ________ 11 1.000 12 0.003 1.000 13 -0.004 0.091 1.000 14 -0.013 0.132 0.019 1.000 15 -0.068 -0.002 0.057 0.002 1.000 16 -0.003 0.024 0.048 -0.050 0.085 17 0.042 -0.044 -0.083 -0.005 -0.623 18 -0.117 0.012 -0.014 0.050 0.161 19 0.165 -0.009 -0.119 -0.033 0.053 20 -0.022 -0.320 -0.016 -0.243 0.066 21 -0.090 0.009 0.108 0.033 -0.043 22 -0.094 -0.012 -0.088 -0.031 -0.046 23 0.037 0.014 -0.005 -0.023 -0.056 24 -0.008 0.014 -0.019 0.002 -0.038 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 16 17 18 19 20 ________ ________ ________ ________ ________ 16 1.000 17 -0.387 1.000 18 0.064 -0.108 1.000 19 -0.004 -0.038 0.009 1.000 20 0.000 -0.039 0.062 0.151 1.000 21 0.078 0.027 0.051 -0.870 -0.152 22 -0.046 0.084 -0.644 0.004 -0.043 23 -0.003 0.057 -0.055 -0.133 0.255 24 0.015 0.062 0.001 -0.115 -0.674 ESTIMATED CORRELATION MATRIX FOR PARAMETER ESTIMATES 21 22 23 24 ________ ________ ________ ________ 21 1.000 22 -0.183 1.000 23 0.160 -0.036 1.000 24 0.099 0.021 -0.462 1.000
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j i r o 文 治 郎 b u n p e i 文 平 c h i a k i 千 亜 季 c h i a k i 千 亜 希 c h i a k i 千 亜 紀 c h i a k i 千 亜 貴 c h i a k i 千 昌 c h i a k i 千 明 c h i a k i 千 昭 c h i a k i 千 晃 c h i a k i 千 晶 c h i a k i 千 秋 c h i a k i 智 亜 紀 c h i a k i 智 亜 輝 c h i a k i 智 明 c h i a k i 智 秋 c h i d a 千 田 c h i h a r a 千 原 c h i k a r a 力 c h i k a r a 税 c h i k a s h i 睦 c h i k a s h i 親 志 c h i k a s h i 近 c h i k a s h i 迩 c h i k a s h i 邇 c h i k a t a k e 親 武 c h i w a k i 千 脇 c h i z u r u 千 尋 c h i z u r u 千 津 留 c h i z u r u 千 鶴 c h i z u r u 智 鶴 c h i z u r u 知 鶴 c h o n a n 長 南 c h u j i r o 忠 次 郎 c h u t a 忠 太 d a d e 大 徳 d a i d o j i 大 道 寺 d a i j i 大 路 d a n k a d o m a t s u 旦 門 松 d e i 出 井 d e j i m a 出 島 d e j i m a 出 嶋 d e n k i c h i 伝 吉 d e z h i 得 志 d e z h i 徳 治 d o n g f a n g 東 方 e b a t o 江 波 戸 e b i k o 蛯 子 e b i s u y a 戎 谷 e c h i g o 越 後 e g a m i 江 上 e i i c h i r o 栄 一 郎 e i i c h i r o 栄 市 郎 e i i c h i r o 榮 一 郎 e i i c h i r o 英 一 朗 e i i c h i r o 英 一 郎 e i s u k e 栄 介 e i s u k e 栄 助 e i s u k e 栄 祐 e i s u k e 永 輔 e i s u k e 泳 助 e i s u k e 英 介 e i s u k e 英 助 e i s u k e 英 輔 e i s u k e 詠 介 e i s u k e 詠 助 e n ' y a 円 谷 e n ' y a 塩 谷 e n a r i 江 成 e n o k i 榎 e n o k i 榎 木 e z o e 江 副 e z o e 江 添 f u j i b a y a s h i 藤 林 f u j i i k e 藤 池 f u j i k i 藤 木 f u j i m a 藤 間 f u j i m i 富 士 美 f u j i m i 富 士 見 f u j i n a w a 藤 縄 f u j i s e 藤 瀬 f u j i y a 冨 士 哉 f u j i y a 冨 士 弥 f u j i y a 富 士 哉 f u j i y a 富 士 弥 f u j i y o 不 二 世 f u j i y o 富 士 代 f u k a w a 布 川 f u k a w a 府 川 f u k i t a 吹 田 f u k o 風 子 f u k u e 福 江 f u k u i 福 井 f u k u i 福 居 f u k u m a 福 間 f u k u n i s h i 福 西 f u k u n o 福 野 f u k u s h i g e 福 茂 f u m i k a z u 史 一 f u m i k a z u 史 和 f u m i k a z u 文 一 f u m i k a z u 文 和 f u m i k a z u 文 数 f u m i k o 二 三 子 f u m i k o 典 子 f u m i k o 冨 美 子 f u m i k o 史 子 f u m i k o 婦 美 子 f u m i k o 富 美 子 f u m i k o 扶 美 子 f u m i k o 文 子 f u m i k o 芙 美 子 f u m i y a s u 文 康 f u n a i 船 井 f u r u g o r i 古 郡 f u r u n o 古 野 f u t a i 二 井 f u t t s u 富 津 g e n ' i c h i r o 源 一 郎 g o j o m e 五 城 目 g o m i k a w a 五 味 川 g o s h o g a w a r a 五 所 川 原 g o s h o r a 御 所 浦 g o t e n b a 御 殿 場 g o t o d a 後 藤 田 g u a n g h u i 光 輝 g u a n g y i 光 一 g u n z o 軍 造 h a g i h a r a 萩 原 h a g u r o 羽 黒 h a i k o 羽 衣 子 h a i z h o u 海 舟 h a j i 土 師 h a k o d a 箱 田 h a k o m o r i 箱 守 h a k u s h u 白 州 h a m a d a 浜 田 h a m a n a 浜 名 h a m a o k a 浜 岡 h a n a m u r a 花 村 h a n a n o 花 野 h a n i w a r a 埴 原 h a o p i n g 浩 平 h a r a 原 h a r a k i 原 木 h a r i y a 針 谷 h a r u k a 春 佳 h a r u k a 春 華 h a r u k a 春 香 h a r u k a 晴 佳 h a r u k a 晴 香 h a r u k a 遙 h a r u k a 遙 佳 h a r u k a 遙 香 h a r u k a 遥 h a r u k a 遥 佳 h a r u k a 遥 香 h a r u k a 遼 h a r u m i t s u 春 充 h a r u m i t s u 春 光 h a r u m i t s u 晴 充 h a r u m i t s u 晴 光 h a r u m i t s u 治 光 h a r u m o t o 春 元 h a r u m o t o 春 本 h a r u n o 春 乃 h a r u n o 春 野 h a r u n o r i 治 憲 h a r u n o s u k e 春 之 助 h a r u s h i 治 司 h a r u s u k e 治 助 h a r u t a r o 春 太 郎 h a r u t a r o 治 太 郎 h a r u y o 春 代 h a r u y o 晴 世 h a r u y o 晴 代 h a r u y o 治 代 h a r u y o 陽 代 h a s a k i 波 崎 h a s e 長 谷 h a s e b e 長 谷 部 h a s h i y a 橋 谷 h a s u m i 蓮 実 h a s u m i 蓮 見 h a t a i 畑 井 h a t a n a k a 畑 中 h a t a n a k a 畑 仲 h a t s u i c h i 初 一 h a t s u i c h i 初 市 h a t s u s h i b a 初 芝 h a t s u t a n i 初 谷 h a t s u y o 初 代 h a y a o 速 夫 h a y a o 速 生 h a y a o 速 男 h a y a o 速 郎 h a y a o 速 雄 h a y a o 駿 h e i j i 平 次 h e i j i 平 治 h e i r o k u 平 六 h e i s a k u 平 作 h i d e f u m i 秀 文 h i d e f u m i 英 史 h i d e f u m i 英 文 h i d e n a o 英 直 h i d e t a k e 秀 武 h i d e t o s h i 秀 俊 h i d e t o s h i 秀 利 h i d e t o s h i 秀 寿 h i d e t o s h i 秀 年 h i d e t o s h i 秀 敏 h i d e t o s h i 英 俊 h i d e t o s h i 英 利 h i d e t o s h i 英 年 h i d e t o s h i 英 敏 h i d e t o s h i 豪 紀 h i g a s h i d a 東 田 h i g a s h i k u r u m e 東 久 留 米 h i k i m a 引 間 h i k o h a r u 彦 治 h i k o n e 彦 根 h i r a d e 平 出 h i r a d e 平 手 h i r a g u r i 平 栗 h i r a i s h i 平 石 h i r a i z u m i 平 泉 h i r a k a w a 平 川 h i r a m i 平 見 h i r a n a k a 平 中 h i r a s a k a 平 坂 h i r o h a r u 博 治 h i r o h a r u 寛 治 h i r o h a r u 広 治 h i r o h a r u 弘 春 h i r o h a r u 弘 治 h i r o h a r u 洋 治 h i r o m a s a 博 政 h i r o m a s a 博 昌 h i r o m a s a 博 正 h i r o m a s a 博 雅 h i r o m a s a 宏 政 h i r o m a s a 宏 昌 h i r o m a s a 宏 正 h i r o m a s a 宏 雅 h i r o m a s a 寛 政 h i r o m a s a 寛 昌 h i r o m a s a 寛 正 h i r o m a s a 寛 雅 h i r o m a s a 広 政 h i r o m a s a 広 昌 h i r o m a s a 広 正 h i r o m a s a 広 雅 h i r o m a s a 弘 政 h i r o m a s a 弘 昌 h i r o m a s a 弘 正 h i r o m a s a 弘 雅 h i r o m a s a 洋 政 h i r o m a s a 洋 昌 h i r o m a s a 洋 正 h i r o m a s a 洋 雅 h i r o m a s a 浩 政 h i r o m a s a 浩 昌 h i r o m a s a 浩 正 h i r o m a s a 浩 雅 h i r o m a s a 紘 政 h i r o m a s a 紘 昌 h i r o m a s a 紘 正 h i r o m a s a 紘 雅 h i r o m a s a 裕 政 h i r o m a s a 裕 昌 h i r o m a s a 裕 正 h i r o m a s a 裕 雅 h i r o n a o 寛 直 h i r o s u k e 広 助 h i r o s u k e 洋 右 h i r u m a 昼 間 h i r u m a 比 留 間 h i r u m a 蛭 間 h i s a 久 h i s a 比 佐 h i s a h i k o 久 彦 h i s a k i 久 木 h i s a y o s h i 久 佳 h i s a y o s h i 久 吉 h i s a y o s h i 久 喜 h i s a y o s h i 久 義 h i s a y o s h i 久 芳 h i t s u m e 日 詰 h i w a t a 樋 渡 h o d a k a 保 高 h o n z a w a 本 沢 h o r i y a m a 堀 山 h o s a k a 保 坂 h o s a k a 穂 坂 h o s o b u c h i 細 淵 h o s o e 細 江 h o s o g a y a 細 萱 h o s o n u m a 細 沼 h o t a k a 保 孝 h o t a k a 保 貴 h o t a k a 保 隆 h o t a k a 穂 孝 h o t a k a 穂 隆 h o t a k a 穂 高 h o t o d a 保 土 田 h o t o d a 保 戸 田 h o t o d a 穂 戸 田 h o y a 保 谷 h y o g o 兵 庫 i c h i g e 市 毛 i c h i j i m a 市 島 i c h i j i m a 市 嶋 i c h i k i 一 木 i c h i k i 市 来 i c h i m i y a 一 宮 i c h i n o z a w a 市 野 沢 i c h i s e 市 瀬 i c h i t o 市 東 i c h i t s u k a 市 塚 i c h i y o 一 世 i c h i y o 一 葉 i c h i y o 市 代 i c h i z a w a 市 沢 i d e i 出 井 i e m a s a 家 正 i g i 猪 木 i i z a w a 飯 沢 i k e d a 池 田 i k e d o 池 戸 i k e y a m a 池 山 i k k o 一 行 i k u i n a 生 稲 i k u m a 井 熊 i k u m a 生 馬 i k u m i 幾 実 i k u m i 幾 美 i k u m i 生 実 i k u m i 生 美 i k u m i 育 実 i k u m i 育 巳 i k u m i 育 美 i k u m i 郁 実 i k u m i 郁 巳 i k u m i 郁 美 i k u r o 幾 朗 i k u r o 幾 郎 i k u r o 育 朗 i k u r o 育 郎 i k u r o 郁 朗 i k u r o 郁 郎 i m a b o r i 今 堀 i m a e d a 今 枝 i m a m i y a 今 宮 i n a 伊 奈 i n a 伊 那 i n a h a s h i 稲 橋 i n a i 稲 井 i n a m o t o 稲 元 i n a m o t o 稲 本 i n a s a w a 稲 沢 i n e k i 稲 木 i n n o s h i m a 因 島 i n o k a 猪 岡 i n o k i 猪 木 i n u k a i 犬 飼 i o k a w a 五 百 川 i s a k a 井 坂 i s a k a 伊 坂 i s a k a 伊 阪 i s a m u 偉 i s a m u 力 i s a m u 勇 i s a m u 勲 i s a m u 敢 i s a m u 武 i s a m u 浩 i s a m u 魁 i s e h a r a 伊 勢 原 i s h i j i m a 石 島 i s h i t o b i 石 飛 i s o b e 磯 辺 i s o b e 磯 部 i s o b e 礒 辺 i s o b e 礒 部 i s o d a 磯 田 i s o d a 礒 田 i s s a k u 一 作 i t s u k o 伊 津 子 i t s u k o 伊 都 子 i t s u k o 逸 子 i w a b e 岩 辺 i w a b e 岩 部 i w a h o r i 岩 堀 i w a k a w a 岩 川 i w a m o t o 岩 元 i w a m o t o 岩 本 i w a o k a 岩 岡 i y o k o 伊 代 子 i z u m i m o t o 泉 本 i z u r u 出 j i n b o 神 保 j i n z o 仁 三 j i t s u o 実 男 j i t s u o 実 雄 j o b o j i 浄 法 寺 j u n j i r o 潤 二 郎 j u n n o s u k e 淳 之 助 j u n n o s u k e 潤 之 助 j u n n o s u k e 純 之 介 j u n n o s u k e 純 之 助 j u o 十 王 j u r o 重 郎 k a e d e 楓 k a i 快 k a i 甲 斐 k a i 魁 k a i o n j i 海 音 寺 k a k e g a w a 掛 川 k a k e h i 筧 k a k e i 筧 k a k i u c h i 垣 内 k a k i u c h i 柿 内 k a k u b a r i 角 張 k a m e n o s u k e 亀 之 助 k a m e o k a 亀 岡 k a m e t a r o 亀 太 郎 k a m i k a w a c h i 上 河 内 k a m i k i t a 上 北 k a m i n a k a 上 中 k a m o s h i d a 鴨 志 田 k a n a d a 金 田 k a n a i s h i 金 石 k a n a m e 要 k a n a m o r i 金 森 k a n a m o t o 金 本 k a n e m a t s u 兼 松 k a n e m a t s u 金 松 k a n e m i t s u 兼 光 k a n e m i t s u 金 光 k a n e n o r i 兼 典 k a n e n o r i 兼 則 k a n e n o r i 兼 徳 k a n e n o r i 兼 憲 k a n e s h i g e 金 重 k a n e t o s h i 兼 敏 k a n i 可 児 k a n t a r o 勘 太 郎 k a r a k i d a 唐 木 田 k a r u i z a w a 軽 井 沢 k a s a m a t s u 笠 松 k a s h i m a 加 島 k a s h i m a 嘉 島 k a s h i m a 鹿 島 k a s h i m a 鹿 嶋 k a s h i w a i 柏 井 k a s h i w a m u r a 柏 村 k a t a y a m a 形 山 k a t a y a m a 片 山 k a t s u e 克 恵 k a t s u e 克 枝 k a t s u e 克 江 k a t s u e 克 絵 k a t s u e 克 衛 k a t s u e 勝 恵 k a t s u e 勝 枝 k a t s u e 勝 江 k a t s u e 勝 絵 k a t s u e 勝 衛 k a t s u m a s a 克 昌 k a t s u m a s a 勝 政 k a t s u m a s a 勝 正 k a t s u m a s a 勝 雅 k a t s u m o r i 勝 盛 k a t s u n o b u 勝 伸 k a t s u n o b u 勝 信 k a t s u r a y a m a 葛 山 k a t s u y a m a 勝 山 k a w a h a t a 川 畑 k a w a m i n a m i 河 南 k a w a r a z a k i 河 原 崎 k a w a s h i m a 川 島 k a w a s h i m a 川 嶋 k a w a s h i m a 河 島 k a w a s h i m a 河 嶋 k a w a s o e 川 副 k a w a u c h i 川 内 k a w a u c h i 河 内 k a y o k o 佳 与 子 k a y o k o 佳 世 子 k a y o k o 佳 代 子 k a y o k o 加 世 子 k a y o k o 加 代 子 k a y o k o 嘉 代 子 k a y o k o 嘉 余 子 k a y o k o 夏 代 子 k a y o k o 華 代 子 k a y o k o 賀 世 子 k a y o k o 賀 代 子 k a y o k o 開 代 子 k a y o k o 香 世 子 k a y o k o 香 代 子 k a z u m a 一 真 k a z u m a 一 磨 k a z u m a 一 馬 k a z u m a 和 磨 k a z u m a 和 馬 k a z u m a 数 馬 k a z u m i 一 三 k a z u m i 一 実 k a z u m i 一 己 k a z u m i 一 巳 k a z u m i 一 海 k a z u m i 一 美 k a z u m i 一 身 k a z u m i 和 三 k a z u m i 和 実 k a z u m i 和 己 k a z u m i 和 巳 k a z u m i 和 海 k a z u m i 和 美 k a z u m i 和 臣 k a z u n o b u 一 伸 k a z u n o b u 一 信 k a z u n o b u 和 伸 k a z u n o b u 和 信 k a z u n o b u 和 展 k e b u k a w a 癸 生 川 k e i i c h i 啓 一 k e i i c h i 圭 一 k e i i c h i 圭 市 k e i i c h i 恵 一 k e i i c h i 慶 一 k e i i c h i 敬 一 k e i i c h i 桂 一 k e i i c h i 計 一 k e i i c h i 馨 一 k e i j i r o 啓 二 朗 k e i j i r o 啓 二 郎 k e i j i r o 啓 次 郎 k e i j i r o 圭 二 郎 k e i j i r o 圭 次 郎 k e i j i r o 恵 二 郎 k e i j i r o 慶 次 郎 k e i j i r o 敬 二 郎 k e i j i r o 敬 次 郎 k e i j i r o 桂 次 郎 k e i s a k u 啓 作 k e i s a k u 恵 作 k e i s a k u 敬 作 k e i s a k u 景 作 k e i y a 佳 哉 k e n ' i c h i r o 健 一 朗 k e n ' i c h i r o 健 一 郎 k e n ' i c h i r o 堅 一 郎 k e n ' i c h i r o 建 一 郎 k e n ' i c h i r o 憲 一 郎 k e n ' i c h i r o 研 一 郎 k e n ' i c h i r o 謙 一 郎 k e n ' i c h i r o 賢 一 郎 k e n n o s u k e 健 之 助 k e n n o s u k e 兼 之 助 k e n n o s u k e 謙 之 介 k e s a e 今 朝 恵 k e s a e 今 朝 枝 k e s a e 今 朝 江 k e s a e 今 朝 絵 k i d o 城 戸 k i d o 木 戸 k i d o 木 藤 k i h e i 喜 兵 衛 k i h e i 喜 平 k i h i r a 紀 平 k i i c h i r o 喜 一 郎 k i i c h i r o 暉 一 郎 k i k o 紀 子 k i k u e 喜 久 恵 k i k u e 喜 久 枝 k i k u e 喜 久 栄 k i k u e 喜 久 江 k i k u e 喜 久 絵 k i k u e 希 久 恵 k i k u e 希 久 枝 k i k u e 希 久 江 k i k u e 希 久 絵 k i k u e 紀 久 恵 k i k u e 紀 久 枝 k i k u e 紀 久 江 k i k u e 紀 久 絵 k i k u e 菊 恵 k i k u e 菊 枝 k i k u e 菊 江 k i k u e 菊 絵 k i m a 木 間 k i m o t o 木 元 k i m o t o 木 本 k i m o t o 紀 本 k i n o 木 野 k i n o 紀 k i n z a b u r o 金 三 郎 k i s h i b e 岸 部 k i s h i i 岸 井 k i s h i m o t o 岸 本 k i s h i o 喜 司 夫 k i s h i o 喜 司 生 k i s h i o 喜 司 男 k i s h i o 喜 司 郎 k i s h i o 喜 司 雄 k i s h i o 岸 夫 k i s h i o 岸 男 k i s h i o 岸 雄 k i s h i r o 喜 四 郎 k i s h i r o 木 城 k i s h i r o 輝 志 郎 k i t a k a 橘 高 k i t a k a w a b e 北 川 辺 k i t a k o 喜 多 子 k i t a m o t o 北 本 k i y o h a r a 清 原 k i y o h i k o 喜 代 彦 k i y o h i k o 清 彦 k i y o h i k o 紀 代 彦 k i y o h i k o 聖 彦 k i y o j i 喜 代 二 k i y o j i 喜 代 治 k i y o m i y a 清 宮 k i y o n a r i 清 成 k i y o t o s h i 清 俊 k i y o t o s h i 清 利 k i y o t o s h i 清 敏 k i z a k i 木 崎 k i z u 木 津 k i z u k u r i 木 造 k o a n a 小 穴 k o b a 木 場 k o b a 木 庭 k o f u j i 小 藤 k o h a s e 小 長 谷 k o h a s h i 小 橋 k o i b u c h i 鯉 淵 k o i n o s u k e 鯉 之 助 k o i w a i 小 岩 井 k o i w a i 小 祝 k o j i m a 児 島 k o j i m a 古 島 k o j i m a 小 島 k o j i m a 幸 嶋 k o j u n 孝 順 k o k u r a k i t a 小 倉 北 k o m a m u r a 駒 村 k o m a t s u b a r a 小 松 原 k o m e i 孔 明 k o m e i 幸 明 k o m e i 米 井 k o m e i 高 明 k o m i n a t o 小 湊 k o m i y a 古 宮 k o m i y a 小 宮 k o m i y a m a 小 宮 山 k o m i y a m a 小 見 山 k o m u r a 古 村 k o m u r a 小 村 k o m u r a 幸 村 k o m u r a 香 村 k o n n a i 近 内 k o s a b u r o 幸 三 郎 k o s h i 合 志 k o s h i 孝 司 k o s h i 幸 志 k o s h i 耕 史 k o s h i 耕 司 k o s h i 越 k o s h i d a 越 田 k o s h i k a w a 越 川 k o s h i n u m a 越 沼 k o s h i t s u k a 腰 塚 k o s o n e 小 曽 根 k o s o n e 小 曾 根 k o s o n o 小 園 k o s o n o 小 薗 k o t a k a 小 鷹 k o t a n i 小 谷 k o t o h a r u 士 美 k o w a t a 木 幡 k o y a d a 小 谷 田 k o y u k i 小 雪 k o y u r u 越 k u g o 久 郷 k u i 魁 k u j u k u r i 九 十 九 里 k u k i z a k i 茎 崎 k u m a n o 熊 野 k u m e n o 粂 野 k u n i t a c h i 国 立 k u n i t o m i 国 冨 k u n i y a 国 谷 k u r a g a n e 倉 金 k u r a m i t s u 倉 光 k u r a s a w a 倉 沢 k u r a s h i n a 倉 品 k u r a s h i n a 倉 科 k u r a t a k e 倉 岳 k u r a y o s h i 倉 吉 k u r e m a t s u 榑 松 k u r i k i 栗 城 k u r i k i 栗 木 k u r i s h i m a 栗 島 k u r o h a 黒 羽 k u r o t a n i 黒 谷 k u s a m a 日 馬 k u s a m a 草 間 k u s h i b i k i 櫛 引 k u s u n o s e 楠 瀬 k u s u y a m a 楠 山 k y o i c h i 亨 一 k y o i c h i 協 一 k y o i c h i 強 一 k y o i c h i 強 市 k y o i c h i 恭 一 k y o i c h i 恭 市 k y o i c h i 教 一 k y o i c h i 響 一 k y o k a 京 香 k y o k a 恭 香 k y o k a 杏 香 k y u k i c h i 久 吉 l i j i a 麗 佳 l i p i n g 利 平 l i p i n g 理 平 m a c h i j i m a 町 島 m a c h i j i m a 町 嶋 m a d o n o 真 殿 m a e 前 m a e d a 前 田 m a e h a r a 前 原 m a e h a t a 前 畑 m a e z a w a 前 沢 m a g o s h i 馬 越 m a h o 真 保 m a h o 真 帆 m a h o 真 歩 m a h o 真 秀 m a h o 真 穂 m a h o 麻 帆 m a h o 麻 歩 m a h o 麻 穂 m a i k a 真 衣 香 m a i k a 舞 歌 m a i k a 舞 花 m a i z u r u 舞 鶴 m a k i n o d a 牧 野 田 m a k o 摩 子 m a k o 眞 子 m a k o 真 子 m a k o 磨 香 m a k o 魔 子 m a k o 麻 子 m a k o 麻 湖 m a m i k o 満 美 子 m a m i k o 眞 美 子 m a m i k o 真 実 子 m a m i k o 真 宮 子 m a m i k o 真 美 子 m a m i k o 麻 実 子 m a m i k o 麻 巳 子 m a m i k o 麻 美 子 m a n a k a 真 中 m a n a k a 間 中 m a r u m o 丸 茂 m a r u o k a 丸 岡 m a s a h i s a 昌 久 m a s a h i s a 正 久 m a s a h i s a 雅 久 m a s a k i 将 喜 m a s a k i 将 樹 m a s a k i 将 生 m a s a k i 将 紀 m a s a k i 将 輝 m a s a k i 政 喜 m a s a k i 政 樹 m a s a k i 政 生 m a s a k i 政 紀 m a s a k i 政 貴 m a s a k i 政 輝 m a s a k i 昌 喜 m a s a k i 昌 樹 m a s a k i 昌 毅 m a s a k i 昌 生 m a s a k i 昌 紀 m a s a k i 昌 貴 m a s a k i 昌 輝 m a s a k i 柾 m a s a k i 正 喜 m a s a k i 正 基 m a s a k i 正 木 m a s a k i 正 樹 m a s a k i 正 生 m a s a k i 正 紀 m a s a k i 正 規 m a s a k i 正 貴 m a s a k i 正 起 m a s a k i 正 輝 m a s a k i 眞 崎 m a s a k i 真 崎 m a s a k i 真 樹 m a s a k i 聖 樹 m a s a k i 雅 喜 m a s a k i 雅 基 m a s a k i 雅 己 m a s a k i 雅 樹 m a s a k i 雅 生 m a s a k i 雅 紀 m a s a k i 雅 貴 m a s a k i 雅 輝 m a s a k o 匡 子 m a s a k o 将 子 m a s a k o 政 子 m a s a k o 昌 子 m a s a k o 晶 子 m a s a k o 正 子 m a s a k o 正 沙 子 m a s a k o 眞 佐 子 m a s a k o 真 佐 子 m a s a k o 真 子 m a s a k o 真 沙 子 m a s a k o 真 砂 子 m a s a k o 真 紗 子 m a s a k o 雅 子 m a s a k o 麻 佐 子 m a s a k o 麻 沙 子 m a s a k o 麻 紗 子 m a s a m i 優 美 m a s a m i 公 美 m a s a m i 匡 巳 m a s a m i 将 実 m a s a m i 将 美 m a s a m i 成 美 m a s a m i 政 実 m a s a m i 政 實 m a s a m i 政 己 m a s a m i 政 巳 m a s a m i 政 美 m a s a m i 政 見 m a s a m i 昌 実 m a s a m i 昌 己 m a s a m i 昌 恵 m a s a m i 昌 未 m a s a m i 昌 美 m a s a m i 正 三 m a s a m i 正 実 m a s a m i 正 己 m a s a m i 正 巳 m a s a m i 正 海 m a s a m i 正 美 m a s a m i 正 見 m a s a m i 眞 美 m a s a m i 真 佐 美 m a s a m i 真 実 m a s a m i 真 沙 美 m a s a m i 真 紗 美 m a s a m i 真 美 m a s a m i 雅 実 m a s a m i 雅 己 m a s a m i 雅 巳 m a s a m i 雅 美 m a s a m i 麻 佐 美 m a s a m i 麻 沙 美 m a s a m i 麻 紗 美 m a s a m o r i 雅 守 m a s a y o 征 代 m a s a y o 政 世 m a s a y o 政 代 m a s a y o 昌 代 m a s a y o 晶 代 m a s a y o 正 代 m a s a y o 泰 代 m a s a y o 真 佐 代 m a s a y o 真 沙 代 m a s a y o 真 紗 代 m a s a y o 聖 代 m a s a y o 雅 世 m a s a y o 雅 代 m a s h i t a 真 下 m a s u m u r a 増 村 m a s u o k a 増 岡 m a s u o k a 益 岡 m a s u o k a 舛 岡 m a t s u b a s h i 松 橋 m a t s u h i s a 松 久 m a t s u i s h i 松 石 m a t s u r a 松 浦 m a t s u s a k i 松 崎 m a t s u s h i t a 松 下 m e n d a 免 田 m e s a k i 目 崎 m i c h i h o 三 千 穂 m i c h i n a m i 三 千 波 m i f u y u 未 布 夕 m i g i h i t o 右 人 m i g i t a 右 田 m i k a w a 三 加 和 m i k a w a 三 川 m i k a w a 美 川 m i k i r o 幹 朗 m i k u r a 三 倉 m i n a m i o g u n i 南 小 国 m i n a m i y a m a 南 山 m i n a t o y a 湊 谷 m i n e 三 根 m i n e 峰 m i n e 美 祢 m i n e 美 禰 m i n e d a 峰 田 m i n e t o s h i 峰 俊 m i n e t o s h i 峰 利 m i n e t o s h i 峰 敏 m i o 三 尾 m i o 実 緒 m i o 実 音 m i o 未 央 m i o 未 緒 m i o 澪 m i o 美 央 m i o 美 生 m i o 美 緒 m i o 美 音 m i s u z u 三 鈴 m i s u z u 実 鈴 m i s u z u 美 鈴 m i t s u f u m i 光 文 m i t s u h i s a 光 久 m i t s u h i s a 満 久 m i t s u k a 三 塚 m i t s u m u r a 光 村 m i y a b a y a s h i 宮 林 m i y a k e 三 宅 m i y a t a 宮 田 m i y a t a k e 宮 武 m i z o e 溝 江 m i z o k a m i 溝 上 m i z u i d e 水 出 m o c h i t s u g u 望 嗣 m o c h i t s u g u 望 次 m o g i 茂 木 m o h e i 茂 平 m o i c h i 茂 一 m o m i y a m a 籾 山 m o n o e 物 江 m o r i a k i 守 昭 m o r i a k i 守 章 m o r i b a y a s h i 森 林 m o r i e 森 江 m o r i h a r u 盛 春 m o r i k a m i 森 上 m o r i m a s a 守 正 m o r i n i s h i 森 西 m o r i s h i r i 森 尻 m o r i z o 盛 蔵 m o r o k a 師 岡 m o r o k a 諸 岡 m o r o z u m i 両 角 m o t o e 本 江 m o t o k a w a 本 川 m o t o n a r i 元 成 m o t o n o 本 野 m o t o y a s u 元 保 m o t o y a s u 元 康 m o t o y a s u 基 安 m o t o z a w a 本 沢 m o t o z u m i 元 澄 m u k a i y a m a 向 山 m u k a w a 武 川 m u r a b a y a s h i 村 林 m u r a t a n i 村 谷 m u t s u k o 睦 子 n a g a n e 長 根 n a g a o s a 永 長 n a g a r e y a m a 流 山 n a g a s h i m a 永 島 n a g a s h i m a 長 島 n a h a 那 覇 n a k a 中 n a k a 仲 n a k a 那 珂 n a k a d a 中 田 n a k a d a 仲 田 n a k a g a w a 中 川 n a k a g a w a 中 河 n a k a g a w a 仲 川 n a k a g a w a 那 珂 川 n a k a g u c h i 中 口 n a k a i 中 井 n a k a i 中 居 n a k a i 仲 井 n a k a i 仲 居 n a k a j o 中 条 n a k a k u c h i 中 口 n a k a m i c h i 中 路 n a k a m i c h i 中 道 n a k a m i y a 中 宮 n a k a n o 中 野 n a k a n o 仲 野 n a k a s a 仲 佐 n a k a s h i t a 中 下 n a k a s h i z u 中 静 n a k a t o m i 中 冨 n a k a y a 中 家 n a k a y a 中 屋 n a k a y a 中 矢 n a k a y a 中 谷 n a k a y a 仲 矢 n a k a y a 仲 谷 n a n a o 七 夫 n a n a o 七 尾 n a n a o 七 生 n a n a o 七 男 n a n a o 七 郎 n a n a o 七 雄 n a n a o 奈 奈 雄 n a n i w a 浪 速 n a o 奈 保 n a o 奈 央 n a o 奈 穂 n a o 奈 緒 n a o 尚 n a o 直 n a o s h i g e 尚 茂 n a o s h i g e 直 重 n a o t a 尚 太 n a o t a 直 太 n a o t o k i 尚 時 n a o t o m o 直 友 n a o y o s h i 直 由 n a o y o s h i 直 義 n a o y o s h i 直 良 n a r i h i s a 成 久 n a r i m i 也 実 n a r i m i 成 実 n a r i m i 成 美 n a r i o 成 夫 n a r i o 成 生 n a r i o 成 男 n a r i o 成 郎 n a r i o 成 雄 n a r i t a 成 田 n a r i y u k i 成 之 n a r i y u k i 成 幸 n a r u d o m i 成 富 n a r u k u n i 愛 邦 n a t s u i 夏 井 n a z u k a 名 塚 n i b e 仁 部 n i i g a t a 新 潟 n i i y a 新 家 n i i z e k i 新 関 n i i z u m a 新 妻 n i s h i 西 n i s h i b a y a s h i 西 林 n i s h i f u j i 西 藤 n i s h i g u c h i 西 口 n i s h i h a r a 西 原 n i s h i s a k a 西 坂 n i s h i z u k a 西 塚 n i t o 仁 藤 n i w a t a 庭 田 n o b e 野 辺 n o b u h a r a 信 原 n o b u h a r a 延 原 n o b u k i 信 樹 n o b u k i 誠 喜 n o b u k o 伸 子 n o b u k o 信 子 n o b u k o 喜 子 n o b u k o 宣 子 n o b u k o 展 子 n o b u k o 延 子 n o b u k o 敦 子 n o b u k o 暢 子 n o b u k o 舒 子 n o b u k o 順 子 n o b u r u 暢 n o b u r u 辰 n o b u s a w a 信 沢 n o b u s u k e 信 介 n o b u t a d a 信 忠 n o c h i 野 内 n o m i z u 野 水 n o n a m i 野 波 n o r i a k i 典 明 n o r i a k i 典 昭 n o r i a k i 典 章 n o r i a k i 則 明 n o r i a k i 則 昭 n o r i a k i 則 秋 n o r i a k i 則 章 n o r i a k i 宣 昭 n o r i a k i 徳 明 n o r i a k i 徳 昭 n o r i a k i 徳 章 n o r i a k i 憲 明 n o r i a k i 憲 昭 n o r i a k i 憲 章 n o r i a k i 智 明 n o r i a k i 範 明 n o r i a k i 範 昭 n o r i a k i 範 章 n o r i a k i 紀 彰 n o r i a k i 紀 明 n o r i a k i 紀 昭 n o r i a k i 紀 章 n o r i a k i 規 明 n o r i h i s a 典 久 n o r i h i s a 典 尚 n o r i h i s a 範 久 n o r i h i s a 紀 久 n o r i h i s a 記 久 n o r i t a k a 典 隆 n o r i t a k a 則 孝 n o r i t a k a 徳 高 n o r i t a k a 憲 孝 n o r i t s u g u 憲 嗣 n o r i t s u g u 智 嗣 n o r i y o s h i 典 義 n o r i y o s h i 典 良 n o r i y o s h i 則 良 n o r i y o s h i 展 義 n o r i y o s h i 範 義 n o r i y o s h i 紀 吉 n o s h i 熨 斗 n o t s u 野 津 n o y o r i 野 依 n o z a w a 能 沢 n o z a w a 野 沢 n o z a w a 野 澤 n u m a b e 沼 部 n u n o m u r a 布 村 o b a n a 小 花 o b a n a 尾 花 o c h i a i 落 合 o d a 大 田 o d a 小 田 o d a 尾 田 o d a 織 田 o d a g a k i 小 田 垣 o d a g i 小 田 木 o d a t e 大 舘 o d a t e 大 館 o g o r i 小 郡 o g u c h i 大 口 o g u c h i 小 口 o i 大 井 o i 浩 o i s h i d a 大 石 田 o i w a k e 追 分 o k a h a r a 岡 原 o k a k u r a 岡 倉 o k a n e 大 金 o k a n e 岡 根 o k a n i w a 岡 庭 o k a w a u c h i 大 川 内 o k e d a 桶 田 o k o s h i 大 越 o k u b a y a s h i 奥 林 o k u d a 奥 田 o k u n a k a 奥 中 o k u y a m a 奥 山 o k u z u m i 奥 住 o m i g a w a 小 見 川 o m i n a m i 大 南 o m i n o 小 美 濃 o m i n o 小 美 野 o m o k a w a 面 川 o n o d e r a 小 野 寺 o n o j o 大 野 城 o n o s e 小 野 瀬 o o e 大 上 o o e 大 植 o s a k a s a y a m a 大 阪 狭 山 o s a k i 大 崎 o s a m u r a 長 村 o t a h a r a 大 田 原 o t a h a r a 太 田 原 o t a k i 大 多 喜 o t a k i 大 滝 o t a k i 小 滝 o t o k i c h i 音 吉 o y o s h i 大 吉 r a i t a 雷 太 r a i t a 頼 太 r a k u o 楽 雄 r a n k o 蘭 子 r e n t a r o 廉 太 郎 r e n t a r o 連 太 郎 r i e 利 恵 r i e 利 枝 r i e 利 栄 r i e 利 江 r i e 利 絵 r i e 梨 恵 r i e 梨 枝 r i e 梨 江 r i e 梨 絵 r i e 理 恵 r i e 理 枝 r i e 理 江 r i e 理 絵 r i e 理 英 r i e 莉 恵 r i e 莉 枝 r i e 莉 江 r i e 莉 絵 r i e 莉 英 r i e 里 恵 r i e 里 枝 r i e 里 江 r i e 里 絵 r i i c h i r o 理 一 郎 r i k i 力 r i o 梨 生 r i o 梨 穂 r i o 理 央 r i o 理 緒 r i o 理 音 r i o 里 緒 r i t s u j i 律 次 r u r i 留 里 r u r u k o 瑠 縷 子 r y o k a 涼 香 r y u i c h i 柳 一 r y u i c h i 竜 一 r y u i c h i 隆 一 r y u i c h i 隆 市 r y u i c h i 龍 一 r y u s u k e 竜 介 r y u s u k e 竜 佑 r y u s u k e 竜 祐 r y u s u k e 竜 輔 r y u s u k e 隆 介 r y u s u k e 龍 介 r y u s u k e 龍 祐 s a c h i o 佐 千 夫 s a c h i o 佐 千 雄 s a c h i o 佐 知 夫 s a c h i o 幸 夫 s a c h i o 幸 生 s a c h i o 幸 男 s a c h i o 幸 郎 s a c h i o 幸 雄 s a c h i o 祐 夫 s a c h i y o 佐 千 世 s a c h i y o 佐 千 代 s a c h i y o 佐 智 代 s a c h i y o 咲 千 代 s a c h i y o 幸 世 s a c h i y o 幸 代 s a c h i y o 祥 代 s a d a e 定 枝 s a d a e 定 江 s a d a e 貞 枝 s a d a e 貞 江 s a d a k o 定 子 s a d a k o 節 子 s a d a k o 貞 子 s a d a o m i 定 臣 s a d a o m i 貞 臣 s a d a s h i 貞 司 s a d a s h i 貞 志 s a e k o 佐 恵 子 s a e k o 佐 枝 子 s a e k o 佐 江 子 s a e k o 佐 絵 子 s a e k o 冴 子 s a e k o 小 枝 子 s a e k o 沙 恵 子 s a e k o 沙 枝 子 s a e k o 沙 江 子 s a e k o 沙 絵 子 s a e k o 紗 恵 子 s a e k o 紗 枝 子 s a e k o 紗 江 子 s a e k o 紗 絵 子 s a h o d a 佐 保 田 s a i g a w a 犀 川 s a i j o 西 条 s a i t a m a 埼 玉 s a i w a i 幸 s a k a e 富 s a k a e 彬 s a k a e 復 s a k a e 昌 s a k a e 栄 s a k a e 栄 恵 s a k a e 栄 枝 s a k a e 榮 s a k a e 潤 s a k a e 秀 s a k a g a m i 坂 上 s a k a g a m i 阪 上 s a k a h a r a 坂 原 s a k i 佐 季 s a k i 佐 希 s a k i 佐 紀 s a k i 佐 貴 s a k i 咲 s a k i 早 希 s a k i 早 紀 s a k i 早 記 s a k i 沙 季 s a k i 沙 希 s a k i 沙 樹 s a k i 沙 紀 s a k i 沙 貴 s a k i 紗 季 s a k i 紗 希 s a k i 紗 紀 s a k i 紗 貴 s a k i e 佐 紀 江 s a k i e 咲 恵 s a k i e 咲 枝 s a k i e 咲 江 s a k i e 沙 希 恵 s a k i e 沙 希 絵 s a k i e 沙 貴 恵 s a k i e 紗 希 恵 s a k i e 紗 希 絵 s a k i e 紗 貴 恵 s a k o 佐 古 s a k o 左 古 s a k o 迫 s a k o 酒 向 s a k o d a 迫 田 s a k u j i 作 次 s a k u j i 作 治 s a k u r a k o 桜 子 s a k u r a s h i n 桜 新 s a k u r a u c h i 桜 内 s a n b o n g i 三 本 木 s a n k a w a 三 川 s a n m i y a 三 宮 s a n t a 三 田 s a n w a 三 和 s a o t o m e 五 月 女 s a o t o m e 早 乙 女 s a t a n i 佐 谷 s a t a r o 佐 太 郎 s a w a c h i 沢 地 s a w a t a r i 猿 渡 s e i d o 清 藤 s e i s h i r o 征 四 郎 s e i s h i r o 晴 四 郎 s e i s h i r o 清 四 郎 s e i s h i r o 精 四 郎 s e i s h i r o 聖 四 郎 s e i s h i r o 誠 史 郎 s e i s h i r o 誠 志 郎 s e i t a 清 太 s e i t a 清 田 s e i t o 清 藤 s e i y u 征 勇 s e k i d o 関 戸 s e k i n e 関 根 s e k i t a 赤 田 s e r i k a w a 芹 川 s e t a g a y a 世 田 谷 s e t o g u c h i 瀬 戸 口 s e t o y a m a 瀬 戸 山 s e t s u 節 s e t s u j i 節 次 s e t s u o 摂 夫 s e t s u o 摂 生 s e t s u o 摂 男 s e t s u o 摂 郎 s e t s u o 摂 雄 s e t s u o 節 夫 s e t s u o 節 生 s e t s u o 節 男 s e t s u o 節 郎 s e t s u o 節 雄 s h i 石 s h i 識 s h i b a c h i 芝 地 s h i b a t a 新 発 田 s h i b a t a 柴 田 s h i b a t a 芝 田 s h i b u i 渋 井 s h i d o 志 藤 s h i d o 紫 藤 s h i g a m a 四 釜 s h i g a m a 志 鎌 s h i g e h a r u 繁 春 s h i g e h a r u 繁 治 s h i g e h a r u 茂 春 s h i g e h a r u 茂 治 s h i g e h a r u 重 春 s h i g e h a r u 重 治 s h i g e h i s a 繁 久 s h i g e h i s a 茂 久 s h i g e h i s a 重 久 s h i g e k o 恵 子 s h i g e k o 慈 子 s h i g e k o 成 子 s h i g e k o 滋 子 s h i g e k o 繁 子 s h i g e k o 茂 子 s h i g e k o 重 子 s h i g e k u n i 茂 国 s h i g e m o t o 重 初 s h i g e m o t o 重 本 s h i g e n a r i 重 成 s h i g e o 成 夫 s h i g e o 成 生 s h i g e o 成 男 s h i g e o 成 郎 s h i g e o 成 雄 s h i g e o 滋 雄 s h i g e o 繁 夫 s h i g e o 繁 生 s h i g e o 繁 男 s h i g e o 繁 郎 s h i g e o 繁 雄 s h i g e o 茂 夫 s h i g e o 茂 生 s h i g e o 茂 男 s h i g e o 茂 郎 s h i g e o 茂 雄 s h i g e o 重 夫 s h i g e o 重 生 s h i g e o 重 男 s h i g e o 重 郎 s h i g e o 重 雄 s h i g e o k i 重 沖 s h i g e o k i 重 興 s h i g e r o 繁 郎 s h i g e s h i 彬 s h i g e s h i 重 司 s h i g e t a k e 重 武 s h i i t a n i 椎 谷 s h i i z u 椎 津 s h i k i d a 式 田 s h i m a k o 島 子 s h i m a k o 志 摩 子 s h i m a k o 志 磨 子 s h i m a k o 志 麻 子 s h i m a m u r a 島 村 s h i m a z a w a 嶋 沢 s h i m e 七 五 三 s h i m e 志 免 s h i m o d a 下 田 s h i m o d a 霜 田 s h i m o d e 下 出 s h i m o m i c h i 下 道 s h i m o n a k a 下 中 s h i m o n i t a 下 仁 田 s h i m o s a w a 下 沢 s h i m o t o r i 下 鳥 s h i m o t o r i 霜 鳥 s h i m o z a t o 下 里 s h i n o m i y a 四 宮 s h i n o m i y a 篠 宮 s h i n t a n i 新 谷 s h i o s a k a 塩 坂 s h i o y a 塩 屋 s h i o y a 塩 谷 s h i o y a m a 塩 山 s h i o z a k i 塩 崎 s h i r a k a t a 白 方 s h i r a s a w a 白 沢 s h i r a t a k a 白 鷹 s h i r o 史 朗 s h i r o 史 郎 s h i r o 司 朗 s h i r o 司 郎 s h i r o 嗣 郎 s h i r o 四 良 s h i r o 四 郎 s h i r o 士 朗 s h i r o 士 郎 s h i r o 志 朗 s h i r o 志 郎 s h i r o 詩 郎 s h i r o 館 s h i r o e 白 江 s h i r o i s h i 白 石 s h i r o z u 白 水 s h i u n j i 紫 雲 寺 s h i z u 志 津 s h i z u y a 静 谷 s h o j i r o 正 次 郎 s h o j i r o 省 次 郎 s h o n o s u k e 庄 之 助 s h o n o s u k e 昌 之 介 s h o n o s u k e 正 之 助 s h o r y u 昇 竜 s h o z o 勝 三 s h o z o 尚 三 s h o z o 捷 三 s h o z o 昇 三 s h o z o 昭 三 s h o z o 昭 蔵 s h o z o 昭 造 s h o z o 祥 三 s h u h e i 修 平 s h u h e i 周 平 s h u h e i 秀 平 s h u i c h i 修 一 s h u i c h i 周 一 s h u i c h i 秀 一 s h u i c h i 秋 一 s h u i c h i 衆 一 s h u n t a 俊 太 s h u n t a 瞬 太 s i j i 四 季 s o g i 曽 木 s o g i 曾 木 s o i c h i 壮 一 s o i c h i 宗 一 s o i c h i 宗 市 s o i c h i 惣 一 s o i c h i 操 一 s o i c h i 総 一 s o i c h i 聡 一 s o i c h i 荘 一 s o i c h i 荘 市 s o n o s u k e 惣 之 助 s o t a n i 曽 谷 s u e h a r u 末 春 s u e h a r u 末 治 s u e o 季 夫 s u e o 季 生 s u e o 季 男 s u e o 季 郎 s u e o 季 雄 s u e o 末 夫 s u e o 末 生 s u e o 末 男 s u e o 末 郎 s u e o 末 雄 s u e t a r o 末 太 郎 s u g a 菅 s u g a 須 加 s u g a 須 賀 s u g i o k a 杉 岡 s u g i t o 杉 戸 s u g i u r a 杉 浦 s u g u r u 俊 s u g u r u 傑 s u g u r u 優 s u g u r u 克 s u g u r u 勝 s u g u r u 卓 s u g u r u 捷 s u g u r u 精 s u g u r u 英 s u k e h a c h i r o 助 八 郎 s u m i 住 s u m i 寿 実 s u m i 寿 美 s u m i 澄 s u m i 角 s u m i 隅 s u m i 須 実 s u m i 須 美 s u m i 須 見 s u m i 鷲 見 s u m i n o 住 野 s u m i n o 角 野 s u m i r e 寿 美 礼 s u m i r e 菫 s u n a o 侃 s u n a o 惇 s u n a o 淳 s u n a o 直 s u n a o 素 直 s u n a o k a 砂 岡 s u s a k i 須 崎 s u z u 珠 洲 s u z u 鈴 s u z u i 鈴 井 s u z u m u r a 鈴 村 t a c h i h a r a 立 原 t a d a k i y o 忠 清 t a d a n a r i 忠 成 t a d a n o 但 野 t a d a n o 只 野 t a d a y a s u 忠 泰 t a e 多 恵 t a e 多 枝 t a e 多 栄 t a e 妙 t a g a j o 多 賀 城 t a h a r a 田 原 t a i c h i 太 一 t a i c h i 太 市 t a i c h i r o 太 一 朗 t a i c h i r o 太 一 郎 t a i e i 大 栄 t a j i r o 多 治 郎 t a k a c h i o 高 知 尾 t a k a d e r a 高 寺 t a k a h a t a 高 畑 t a k a m a t s u 高 松 t a k a m u r a 高 村 t a k a n o s u 鷹 巣 t a k a r a i 宝 井 t a k a s h i t a 高 下 t a k a s u 高 須 t a k a s u 鷹 巣 t a k a t a 高 田 t a k a t o m o 孝 友 t a k a t o m o 貴 智 t a k a t o m o 隆 朝 t a k a t o m o 高 智 t a k e g a w a 竹 川 t a k e i s h i 武 石 t a k e i s h i 竹 石 t a k e m o t o 武 本 t a k e m o t o 竹 元 t a k e m o t o 竹 本 t a k e s a b u r o 竹 三 郎 t a k e s h i t a 武 下 t a k e s h i t a 竹 下 t a k e t a 竹 田 t a k e t a n i 武 谷 t a k e t a n i 竹 谷 t a k e t s u g u 武 次 t a k i g u c h i 滝 口 t a k i m u r a 滝 村 t a k i m u r a 瀧 村 t a k i n a m i 滝 波 t a k i n a m i 滝 浪 t a k i n a m i 瀧 波 t a k i n a m i 瀧 浪 t a k i n o 滝 野 t a k i u e 滝 上 t a k i w a k i 滝 脇 t a k i w a k i 瀧 脇 t a m a e 玉 恵 t a m a e 玉 枝 t a m a e 玉 栄 t a m a e 玉 江 t a m a e 玉 絵 t a m a e 珠 恵 t a m a e 珠 枝 t a m a e 珠 江 t a m a e 珠 絵 t a m a k i 玉 城 t a m a k i 玉 木 t a m a k i 玉 置 t a m a k i 珠 季 t a m a k i 環 t a m a k i 田 巻 t a m a k i 田 牧 t a m a k i c h i 玉 吉 t a m a t e 玉 手 t a m e j i 為 治 t a m e y o s h i 為 義 t a m i a k i 民 明 t a n a a m i 棚 網 t a n a a m i 田 名 網 t a n i g a m i 谷 上 t a n o e 田 上 t a t e m a t s u 立 松 t a t s u h a r u 辰 春 t a t s u k o 多 津 子 t a t s u k o 多 鶴 子 t a t s u k o 竜 子 t a t s u k o 辰 子 t a t s u k o 達 子 t a t s u k o 龍 子 t a t s u n o 立 野 t a t s u n o 竜 野 t a t s u n o 辰 野 t a t s u n o 龍 野 t a t s u r o 竜 郎 t a t s u r o 辰 朗 t a t s u r o 辰 郎 t a t s u r o 達 朗 t a t s u r o 達 郎 t a t s u r o 龍 郎 t a t s u s h i 達 司 t a t s u s h i 達 志 t a t s u z o 辰 三 t a t s u z o 辰 蔵 t a t s u z o 達 三 t a z u k o 多 津 子 t a z u k o 多 都 子 t a z u k o 多 鶴 子 t a z u k o 田 津 子 t a z u k o 田 鶴 子 t e i z a b u r o 貞 三 郎 t e n n o 天 王 t e r a g u c h i 寺 口 t e r a h a r a 寺 原 t e r u e 照 恵 t e r u e 照 枝 t e r u e 照 江 t e r u e 照 絵 t e r u i 照 井 t e r u t o 輝 人 t o d o k o r o 冨 所 t o d o k o r o 富 所 t o d o m e 留 目 t o h o k u 東 北 t o k i 土 岐 t o k i 東 樹 t o k i 東 紀 t o k i j i r o 時 二 郎 t o k i j i r o 時 次 郎 t o k i o k a 時 岡 t o k u i 徳 井 t o k u j i 得 二 t o k u j i 徳 二 t o k u j i 徳 司 t o k u j i 徳 次 t o k u j i 徳 治 t o k u j i 渡 久 地 t o k u j u r o 徳 十 郎 t o k u m a t s u 徳 松 t o k u n o s u k e 徳 之 助 t o k u s h i 得 志 t o k u s h i g e 徳 重 t o k u y a m a 徳 山 t o m a b e c h i 苫 米 地 t o m a r i 泊 t o m i g o r o 富 五 郎 t o m i h a r i 冨 張 t o m i h a r i 富 張 t o m i h i s a 冨 久 t o m i s a w a 富 沢 t o m o n o 伴 野 t o m o n o 友 野 t o n o m u r a 殿 村 t o r a j i 寅 次 t o r a j i 寅 治 t o r a o 寅 夫 t o r a o 寅 生 t o r a o 寅 男 t o r a o 寅 郎 t o r a o 寅 雄 t o r a o 登 良 夫 t o r a o 虎 夫 t o r a o 虎 生 t o r a o 虎 男 t o r a o 虎 郎 t o r a o 虎 雄 t o r i k a i 鳥 飼 t o s h i i c h i 俊 一 t o s h i i c h i 利 一 t o s h i i c h i 寿 一 t o s h i i c h i 敏 一 t o s h i k u r a 利 倉 t o s h i m a s a 俊 政 t o s h i m a s a 俊 昌 t o s h i m a s a 俊 正 t o s h i m a s a 利 政 t o s h i m a s a 利 昌 t o s h i m a s a 利 正 t o s h i m a s a 年 正 t o s h i m a s a 敏 正 t o s h i m a s a 稔 正 t o s h i m a s a 紀 正 t o s h i m i t s u 俊 充 t o s h i m i t s u 俊 光 t o s h i m i t s u 利 光 t o s h i m i t s u 敏 充 t o s h i m i t s u 敏 光 t o s h i m o t o 敏 元 t o s h i s a b u r o 敏 三 郎 t o s h i s h i c h i 俊 七 t o s h i y a s u 俊 保 t o s h i y a s u 俊 康 t o s h i y a s u 利 保 t o s h i y a s u 利 康 t o s h i y a s u 敏 康 t o s h i y a s u 敏 恭 t o w a k o 十 和 子 t o y o d o m e 豊 留 t o y o k a 豊 岡 t o y o n a k a 豊 中 t o y o n o 豊 野 t o y o y a m a 豊 山 t s u b a k i i 椿 井 t s u b o y a m a 坪 山 t s u b u k i 津 吹 t s u c h i d a 土 田 t s u c h i k o 土 子 t s u c h i k u r a 土 倉 t s u c h i s a w a 土 沢 t s u h a r a 津 原 t s u k a g o s h i 塚 越 t s u k a h a r a 塚 原 t s u k a h a r a 束 原 t s u k i i 月 井 t s u k i k o 就 子 t s u k i k o 月 子 t s u k i k o 津 紀 子 t s u m o t o 津 本 t s u n a k a w a 綱 川 t s u n e y a m a 常 山 t s u r u i c h i 鶴 市 t s u r u k i 鶴 喜 t s u r u m a k i 弦 巻 t s u r u m a k i 鶴 巻 t s u r u o k a 鶴 岡 u c h i m o t o 内 本 u c h i m u r a 内 村 u d a g a w a 宇 多 川 u d a g a w a 宇 田 川 u d a k a 宇 高 u e i s h i 上 石 u e j i 植 次 u e j i m a 上 島 u e j i m a 植 島 u e k u s a 植 草 u e m u r a 上 村 u e m u r a 植 村 u e s u g i 上 杉 u h e i 宇 平 u m e d a 梅 田 u m e m i y a 梅 宮 u m e m o t o 梅 本 u m e z u 梅 津 u m i 宇 美 u m i 海 u m i 羽 美 u n a z u k i 宇 奈 月 u n n o 海 野 u r a g u c h i 浦 口 u r a k i 浦 木 u r a o 浦 尾 u r a y a s u 浦 安 u r u s h i b a t a 漆 畑 u r u s h i d o 漆 戸 u r u s h i h a r a 漆 原 u s u i 碓 井 u s u i 笛 吹 u s u i 臼 井 u s u i 薄 井 u s u k u r a 臼 倉 u t a g a w a 歌 川 w a k a s h i m a 若 島 w a k a s h i m a 若 嶋 w a k a t a k e 若 竹 w a k e b e 分 部 w a k u r i 和 栗 w a n i b u c h i 鰐 淵 w a n i b u c h i 鰐 渕 w e n y i 文 一 x i p i n g 喜 平 x i u y i 修 一 y a b u n a k a 籔 中 y a b u n a k a 藪 中 y a c h i m a t a 八 街 y a e d a 八 重 田 y a e k o 八 枝 子 y a e k o 八 栄 子 y a e k o 八 重 子 y a e k o 弥 重 子 y a g i m o t o 柳 本 y a i t a 矢 板 y a k o 八 子 y a k o 弥 子 y a k o 谷 古 宇 y a m a g a m i 山 上 y a m a g a m i 山 神 y a m a g i s h i 山 岸 y a m a h a t a 山 畑 y a m a h a t a 山 端 y a m a h i g a s h i 山 東 y a m a s a w a 山 沢 y a m a s h i r o 山 城 y a m a t a n i 山 谷 y a m a u r a 山 浦 y a n a d a 梁 田 y a n a d a 簗 田 y a s a k a 八 坂 y a s o 八 十 y a s u f u m i 康 允 y a s u f u m i 康 史 y a s u f u m i 康 文 y a s u f u m i 泰 史 y a s u f u m i 泰 文 y a s u f u m i 靖 史 y a s u f u m i 靖 文 y a s u i c h i 保 一 y a s u i c h i 安 一 y a s u i c h i 康 一 y a s u i c h i 泰 一 y a s u i c h i 靖 一 y a s u k a t s u 康 勝 y a s u k u n i 保 邦 y a s u k u n i 康 邦 y a s u k u n i 泰 邦 y a s u n o b u 保 伸 y a s u n o b u 保 信 y a s u n o b u 安 信 y a s u n o b u 康 伸 y a s u n o b u 康 信 y a s u n o b u 泰 延 y a s u r a 安 楽 y a s u r a o k a 安 良 岡 y a s u z a w a 安 沢 y a w a t a h a m a 八 幡 浜 y a x i 亜 希 y a y o e 八 代 枝 y o b e 余 部 y o i c h i r o 与 一 郎 y o i c 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// Example 3.9 clc; clear; close; // Given data format('v',8); Rf= 1*10^6;// in Ω Rin= 1*10^6;// in Ω Vout_by_Vin= -Rf/Rin;// (since Vout= -Rf/Rin*Vin) Av= Vout_by_Vin;// voltage gain disp(Av,"The voltage gain is : "); // I_in= Iout (As it is a unity gain inverter) Ain= 1;//input impedance (since I_in= Iout) disp(Ain,"The input impedance is : "); Ap= abs(Av*Ain);// power gain disp(Ap,"The power gain is : ");
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// ELECTRICAL MACHINES // R.K.Srivastava // First Impression 2011 // CENGAGE LEARNING INDIA PVT. LTD // CHAPTER : 4 : DIRECT CURRENT MACHINES // EXAMPLE : 4.6 clear ; clc ; close ; // Clear the work space and console // GIVEN DATA p = 6; // Number of the pole in DC Motor Ia = 20; // Armature Current in Amphere Z = 1000; // Number of the Conductors a = 6; // Number of the Parallel paths phi = 25 * 10 ^ -3; // Flux per pole in Weber // CALCULATIONS T = (p/a)*((Z*Ia*phi)/(2*%pi)); // Deleloped Torque in Newton-Meter // DISPLAY RESULTS disp("EXAMPLE : 4.6 : SOLUTION :-") ; printf("\n (a) Developed Torque in an Six-pole DC Motor , T = %.1f N-m \n ",T);
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errcatch(-1,"stop");mode(2);//caption:Find total number of pulses and display reading //Ex6.9 V=10//input voltage(in V) S=0.001//ramp slope(in V/second) F=1000000//clock frequency(in Hz) T=1/F t=V*S P=t/T disp(P,'total number of pulses=') disp(P,'display reading=') exit();
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clc; d_r = 13600; // Density of manometric fluid (mercury) in kg/m^3 g = 8.92; // Gravitational acceleration in m/s^2 z1=0.589*sind(60); // vertical height of fluid at section 1 z2=2*sind(30); // vertical height of fluid at section 2 z=z2-z1; // Difference in vertical heights of fluid patm = 14.7; // Atmospheric pressure in lbf/in^2 patm=(patm*4.44822*144/0.3048^2); // conversion of lbf/in^2 unit to N/m^2 unit p=patm + (d_r*g*(z2-z1)); // Balance of force at A disp ("m",z,"Difference in vertical heights of fluid"); disp ("kPa",p/1000,"The pressure of fluid in the vessel");
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//Example 4.14 clc disp("V_ph = 200 V, 60 kVA, R_a = 0.016 ohm, X_s = 0.07 ohm") disp("VA = V_ph*I_ph i.e. 60*10^3 = 200*I_ph ...Single phase") disp("Therefore, I_ph = 300 A = I_a ...Full load current") disp("(a) cos(phi) = 1, sin(phi) = 0") eph=sqrt((((200+((300*0.016)))^2)+((300*0.07)^2))) disp("Therefore, E_ph^2 = (V_ph*cos(phi)+I_a*R_a)^2 + (I_a*X_a)^2") format(9) disp(eph,"E_ph(in V) =") disp("(b) cos(phi) = 0.7 lagging, sin(phi) = 0.714") ephi=sqrt(((((200*0.7)+(300*0.016))^2)+(((200*0.7141)+(300*0.07))^2))) disp("Therefore, E_ph^2 = (V_ph*cos(phi)+I_a*R_a)^2 + (V_ph*sin(phi)+I_a*R_a)^2") format(9) disp(ephi,"E_ph(in V) =")
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//Plot of transfer functions defined in PCI Express jitter modeling paper s=poly(0, 's'); v=10^5:10^4:50*10^6; //Generate frequency matrix frequencies=%i*v*2*%pi; //******************** H1 ****************************** zeta = 0.707; f_3db = 7*10^6; //H1 Cutoff frequency ohmega_n = f_3db * 2*%pi / (sqrt(1+2*zeta^2 + sqrt((1+2*zeta^2)^2 + 1))); H = (2*s*zeta*ohmega_n + ohmega_n^2) / (s^2 + 2*s*zeta*ohmega_n + ohmega_n^2); H_Response = freq(H.num, H.den, frequencies); gainplot(v, [H_Response]); xtitle(" ", "Frequency (Hz)", "Magnitude");
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// This file is part of www.nand2tetris.org // and the book "The Elements of Computing Systems" // by Nisan and Schocken, MIT Press. // File name: projects/07/MemoryAccess/BasicTest/BasicTest.tst load question06.asm, output-file question06.out, compare-to question06.cmp, output-list RAM[16]%D1.6.1 RAM[17]%D1.6.1 RAM[18]%D1.6.1 RAM[19]%D1.6.1 RAM[20]%D1.6.1 ; set RAM[16] 8384, // x set RAM[17] 7, // y set RAM[18] 9925, // sum set RAM[19] 9922, // ptr set RAM[20] 9925, // numbers set RAM[21] 9929, // arr set RAM[9920] 98, set RAM[9921] 34, set RAM[9922] 230, set RAM[9923] 17, set RAM[9924] 83, set RAM[9925] 1, set RAM[9926] 5, set RAM[9927] 3, set RAM[9928] 46, set RAM[9929] 999, set RAM[9930] 11, set RAM[9931] 34, set RAM[9932] 230, set RAM[9933] 17, set RAM[9934] 83, set RAM[9935] 1, set RAM[9936] 5, set RAM[9937] 3, set RAM[9938] 46, set RAM[9939] 999, set RAM[9940] 11, output; repeat 600 { ticktock; } output;
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// Ex12_5 Page:247 (2014) clc; clear; e = 1.6e-019; // Charge on an electron, C m = 9.1e-031; // Mass of an electron, kg K = 327; // Thermal conductivity of Zn, W/m/K N_A = 6.023e+026; // Avogadro's number/k-mol T = 300; // Room temperature, K tau = 2.5e-014; // Relaxation time of electrons in divalent Zn, s d = 7.13e+03; // Density of Zn, kg/metre-cube A = 65.38; // Atomic weight of Zn, g/mol N = 2*d*N_A/A; // Number of electrons per unit volume, per metre-cube sigma = N*e^2*tau/m; // Electrical conductivity of Zn, mho/m L = K/(sigma*T); // Lorentz number for Zn, W-ohm/Sq.K printf("\nLorentz number for Zn = %5.3e W-ohm/Sq.K", L); // Result // Lorentz number for Zn = 1.180e-08 W-ohm/Sq.K
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loadbix Main.vm; repeat { vmstep ; }
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//Determine the minimum signal power required K = 1.38e-20; T = 290; Nf = 5; EbNt = 13.5; Rb = 271; Bc = 200; Tg = 0; Rg = 12; Rl = 2.5; Fm = 10; Nt = 10*log10(K*T) + Nf; SNr = EbNt + 10*log10(Rb/Bc); Smin = EbNt + 10*log10(Rb*1000) + Nt; Lpmax = 30 - Smin + (Tg+Rg) - (Rl+Fm ); disp(Smin, 'Min. Signal Power Required (in dBm)') disp(Lpmax, 'Max. allowable path loss (in dB)')
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clear// //Variables nc = 0.5 //Efficiency VCC = 24.0 //Source voltage (in volts) Poac = 3.5 //a.c. power output (in watt) //Calculation Ptrdc = Poac / nc //dc power (in watt) Pcdc = Ptrdc - Poac //Power dissipated as heat (in watt) //Result printf("\n Total power within the circuit is %0.3f W.\nThe power Pcdc = %0.3f W is dissipated in the form of heat within the transistor collector region.",Ptrdc,Pcdc)
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// ELECTRICAL MACHINES // R.K.Srivastava // First Impression 2011 // CENGAGE LEARNING INDIA PVT. LTD // CHAPTER : 4 : DIRECT CURRENT MACHINES // EXAMPLE : 4.7 clear ; clc ; close ; // Clear the work space and console // GIVEN DATA p = 2; // Number of the Pole N = 1000; // Rotation speed of the Armature in RPM Ia = 20; // Armature Current in Amphere CS = 36; // Commutator Segments BW = 1.4; // Brush width is 1.4 times of the Commutator Segments L = 0.09 * 10 ^ -3; // Inducatnce of the each Armature Coil // CALULATIONS a = p; // Number of the Parallel paths (Equal to number of poles because Lap Connected Armature) n = N/60; // Revoultion per second I = Ia/2; // Current Through the each Conductor in Amphere v = n * CS; // Peripheral Velocity of Commutator in Commutator segments per Seconds Tc = BW/v; // Time of the Commutation in Seconds Er = (L*2*I)/Tc; // Reactance voltage in Volts // DISPLAY RESULTS disp("EXAMPLE : 4.7 : SOLUTION :-") ; printf("\n (a) Reactance voltage assuming Linear Commutation , Er = %.4f V \n",Er); printf("\n\n [ TEXT BOOK SOLUTION IS PRINTED WRONGLY ( I verified by manual calculation )]\n" ); printf("\n WRONGLY PRINTED ANSWERS ARE :- (a) Tc = 0.014 s instead of %.4f s \n",Tc); printf("\n (b) Er = 1.2857 V instead of %.4f V\n",Er); printf("\n From Calculation of the Time of commutation (Tc), rest all the Calculated values in the TEXT BOOK is WRONG because of the Time of commutation (Tc) value is WRONGLY calculated and the same used for the further Calculation part \n")
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//Chapter 8 //Page 210 //Example 8.2 //Thevnin clear;clc; //Given Zth = %i * 0.2;Xg = %i * 1; Vt = 0.97; I = 0.8 - %i* 0.2; Vt_b =1; //Calculations //a S = Vt * I'; Eg = Vt + Xg * I; printf("\n P = %.3f per unit \n Q = %.3f per unit\n",real(S),imag(S)) printf("\n Eg = %.2f /_%.2f per unit \n",abs(Eg),atan(imag(Eg),real(Eg))*180/%pi) //b Eth = Vt - Zth * I; delta = asin(real(S) * abs(Zth) / (abs(Eth) * Vt_b)); printf("\n Eth = %.2f /_%.2f per unit \n",abs(Eth),atan(imag(Eth),real(Eth))*180/%pi) printf("\n Phase angle of Vt = %.2f \n",delta*180/%pi) ang = (atan(imag(Eth),real(Eth)) + delta)*180/%pi; Vt_b1 = Vt_b * (cos(ang * %pi / 180)+ %i * sin(ang * %pi / 180)); I_b = (Vt_b1 - Eth) / Zth; printf("\n I_b = %.2f /_%.2f per unit \n",abs(I_b),atan(imag(I_b),real(I_b))*180/%pi) Eg_b = Vt_b1 + Xg * I_b; S_b = Vt_b1 * I_b'; printf("\n P = %.3f per unit \n Q = %.3f per unit\n",real(S_b),imag(S_b)) printf("\n Eg = %.2f /_%.2f per unit \n",abs(Eg_b),atan(imag(Eg_b),real(Eg_b))*180/%pi)
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// // This file is released under the 3-clause BSD license. See COPYING-BSD. function subdemolist = demo_gateway() demopath = get_absolute_file_path("toolbox_skeleton.dem.gateway.sce"); subdemolist = ["1 hot encoding demo" ; "1 hot encode_Demo"; ... "Affinity propagation" ; "Affinity propagation_Demo1.sce"; ... "Affinity propagation 2"; "Affinity propagation_Demo2.sce"; ... "Binarization" ; "Binarization_Demo.sce"; ... "Class rebalancing" ; "Class rebalancing_Demo.sce"; ... "Decision tree demo 1" ; "Decision Tree_Demo1.sce"; ... "Decision tree demo 2" ; "Devision Tree_Demo2.sce"; ... "Elastic net demo 1" ; "Elastic net regression_Demo1.sce"; ... "Elastic net demo 2" ; "Elastic net regression_Demo2.sce"; ... "Ensemble learning demo"; "Ensemble_Demo.sce"; ... "Kmeans cluster demo 1" ; "Kmeans_Demo1.sce"; ... "Kmeans cluster demo 2" ; "Kmeans_Demo2.sce"; ... "Kmediods cluster 1" ; "Kmediods_Demo1.sce"; ... "Kmediods cluster 2" ; "Kmediods_Demo2.sce"; ... "KNN classification 1" ; "Knn classification_Demo1.sce"; ... "KNN classification 2" ; "Knn classification_Demo2.sce"; ... "Least angle regression"; "LARS_Demo.sce"; ... "Lasso regression 1" ; "Lasso regression_Demo1.sce"; ... "Lasso regression 2" ; "Lasso regression_Demo2.sce"; ... "Linear regression" ; "Linear Regression_Demo.sce"; ... "Logistic regression" ; "Logistic Regression_Demo.sce"; ... "Missing value replace" ; "Missing values_Demo.sce"; ... "Naive Bayes" ; "Naive Bayes_Demo.sce"; ... "Naive Bayes Multinom." ; "Naive Bayes Multinomial_Demo.sce"; ... "Neural network" ; "Neural Network_Demo.sce"; ... "Normalization" ; "Normalize_Demo.sce"; ... "Principal components" ; "PCA_Demo.sce"; ... "Single Perceptron" ; "Perceptron_Demo.sce"; ... "Polynomial regression" ; "Polynomial Regression_Demo.sce"; ... "Random forest" ; "Random Forest_Demo.sce"; ... "Regression Tree" ; "Regression Tree_Demo1.sce"; ... "Ridge regression" ; "Ridge regression_Demo.sce"; ... "Scaling 0/1" ; "Scale_Demo.sce"; ... "Spectral clustering 1" ; "Spectral clustering_Demo1.sce"; ... "Spectral clustering 2" ; "Spectral clustering_Demo2.sce"; ... "Support vector class." ; "SVC_Demo.sce"; ... "Support vector reg." ; "SVR_Demo.sce"; ... "Train test split" ; "Train Test split_Demo.sce"; ]; subdemolist(:,2) = demopath + subdemolist(:,2); endfunction subdemolist = demo_gateway(); clear demo_gateway; // remove demo_gateway on stack
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errcatch(-1,"stop");mode(2);//Chapter 6,Example 6.4 Page 200 t = 60 C = 600*10^-12 V = 250 v = 92 R = t/(C*log(V/v)) printf (" R = %e ohm \n ",R) exit();
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printf('From the linear plot of the langmuir isotherm the intercept Xm=1/0.19=5.26milligrams'); Xm=5.26*10^-3; printf('\nThis is the weight of N2 that forms a unimolecular layer of 2g charcoal.'); MW=28;//molecular weight of N2// N=Xm*6.023*10^23/MW;//No. of molecules of N2// TA=N*16*10^-16;//Total area in cm^2// A=TA/2;//Area per gram in cm^2// printf('\nArea of N2 per gram=%fcm^2',A);
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//Example 15.10. clc format(6) disp("(i) To find capacitance, C:") disp(" Frequency of oscillation is") disp(" fo = 1 / 2*pi*fo*R*C*sqrt(6+4K)") disp(" C = 1 / 2*pi*fo*R*C*sqrt(6+4(Rc/R))") fo=1/(2*%pi*(10*10^3)*(7.1*10^3)*sqrt(6+((4*40*10^3)/(7.1*10^3)))) // in Farady x1=fo*10^9 // in nF disp(x1," C(nF) =") disp("(ii) To find hfe:") disp(" We know that hfe >= 23 + 29(R/Rc) + 4(Rc/R)") h=23+(29*(7.1/40))+(4*(40/7.1)) disp(h," hfe >=")
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clear;lines(0); besselk(0.5:3,1:4) besselk(0.5:3,1:4,2)
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//write down systems of equations and find F(s)/X2(s) printf(" the differential equatios are \n F(s)=s^2*M1**X1(s)+(K1+K2)*X2(s)-K2*X2(s)") printf("\n X1(s)=X2(s)*(s^2*M2+K3+K2)/K2\n f=((s^2*M1+K1+K2)*(s^2*M2+K2+K3)-K2^2)/K2\n Transfer function F(s)/X2(s)=f")
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//Chemical Engineering Thermodynamics //Chapter 14 //Thermodynamics of Chemical Reactions //Example 14.9 clear; clc; //Given //2A(g) - B(g)+C(g) T = 400;//Temperature in Kelvin P = 1;//Pressure in atm R = 1.98;//gas constant in Kcal/Kgmole K del_Fo = 3000;//Standard free energy of the reaction in Kcal/Kgmole n_A = 1;//Kgmoles of A n_B = 0.1;//Kgmoles of B n_C = 0.1;//Kgmoles of C //To find out the equilibrium has been attained or not. If not then calculate the equilibrium composition and also find out whether the equilibrium composition will change or not if pressure were increased to 3 atm. //(1)To find out the equilibrium has been attained or not. If not then calculate the equilibrium composition //P_B/P_C = 1 (Given) n_T = n_A+n_B+n_C;//Total Kgmoles of the component p_A = (n_A/n_T)*P;//Partial pressure of A p_B = (n_B/n_T)*P;//Partial pressure of B p_C = (n_C/n_T)*P;//Partial pressure of C //Using the relation 14.36 (page no 312) del_F = del_Fo + (R*T)*log((p_B*p_C)/(p_A^2)); if del_F == 0; then mprintf('1.Equilibrium has been attained.'); else mprintf('1.Equilibrium has not been attained.'); end //Equilibrium composition //At equilibrium del_F = 0 //From equations 14.35(page no 312) and 14.49(page no 320), we got the relations (a),(b)(page no 331) &(c)(page no 332) and //ln(p_C^2/(P-(2*p_C^2)))= -del_Fo/(R*T); Kp = %e^(-del_Fo/(R*T))//equilibrium constant in terms of pressure p_C = (Kp^(1/2))/(1+2*(Kp^(1/2)));//Partial pressure of C at equilibrium in atm p_B = p_C;//as p_B/p_C = 1 p_A = P-(2*p_C);//Partial pressure of A at equilibrium in atm N_A = p_A*P*100; N_B = p_B*P*100; N_C = p_C*P*100; mprintf('\n Equilibrium composition of A,B and C are %f,%f and %f mole percent respectively.',N_A,N_B,N_C); //2.Calculation of composition at 400 K and 3 atm and vapour pressure of C at 400 K is 0.3 atm P = 3;//Pressure in atm P_C = 0.3;//Vapour pressure of C in atm //Since m=0,pressure will not have an effect on equilibrium compositions. mprintf('\n\n 2.The compositions will be the same as above on increasing the pressure.'); p_B1 = p_B*P;//Partial pressure of B in atm p_C1 = p_B1;//Partial pressure of C in atm p_A1 = p_A*P;//Partial pressure of A in atm if P_C < p_C1 p_A2 = ((p_B1*P_C)/Kp)^(1/2);//decreased partial pressure of A in atm mprintf('\n The partial pressure of A drops from %f to %f to compensate for the amount of C condensed.',p_A1,p_A2); //end
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//fiber optic communications by joseph c. palais //example 8.2 //OS=Windows XP sp3 //Scilab version 5.4.1 clc clear all //given n1=1.465//core refractive index n2=1.46//cladding refractive index lambda1=1.3//wavelength in um lambda2=1.55//wavelength in um a=3.96//core radius in um d=0:0.1:5//offset in um //to find V1=2*%pi*a/lambda1*(sqrt(n1^2-n2^2))//V number for lambda1 V2=2*%pi*a/lambda2*(sqrt(n1^2-n2^2))//V number for lambda2 wbya1=0.65+1.69*V1^(-1.5)+2.879*V1^(-6)//mode field radiusto core radius for lambda1 wbya2=0.65+1.69*V2^(-1.5)+2.879*V2^(-6)//mode field radiusto core radius for lambda2 w1=wbya1*a//mode field radius in um for lambda1 w2=wbya2*a//mode field radius in um for lambda2 dbyw1=d./w1//d/w ratio for lambda1 dbyw2=d./w2//d/w ratio for lambda2 L1=-10*log(exp(-(dbyw1)^2))//Coupling Loss for lambda1 L2=-10*log(exp(-(dbyw2)^2))//Coupling Loss for lambda2 xtitle( 'Coupling Loss Vs Lateral misalignment', 'Lateral misalignment in um', 'Coupling Loss in dB') ; plot(d,L1,'d') plot(d,L2,'*cya--') hl=legend(['Loss at Lambda1=1.3um';'Loss at Lambda2=1.55um']);
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//check o/p when i/p is a vector k = [-0.3090 -0.9801 -0.0031 -0.0082 -0.0082]; g = rc2lar(k); disp(g); //output // column 1 to 4 // // - 0.6388789 - 4.6001829 - 0.0062000 - 0.0164004 // // column 5 // // - 0.0164004
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//Calculations on Petrol engine clc,clear //Given: pC=84,pH2=16 //Percentage of Carbon, Hydrogen in fuel p_v=20.9 //Percentage of Oxygen in air by volume //Solution: C=12 //Atomic mass of Carbon(C) H=1 //Atomic mass of Hydrogen(H) O=16 //Atomic mass of Oxygen(O) N=14 //Atomic mass of Nitrogen(N) m_f=100 //Mass of fuel (assume) in kg //Combustion equation //pC/C[C] + pH2/2[H2] + [a[O2] + (100-p_v)/p_v*a[N2]] = b[CO2] + d[O2] + e[N2] + f[H2O] //Equating coefficients b=pC/C,f=pH2/2,d=b/6,a=b+d+f/2 //Coefficients of combustion equation m_a=a*2*O + (100-p_v)/p_v*a*2*N //Mass of air supplied in kg A_F=m_a/m_f //Air fuel ratio P_e=d/(a-d)*100 //Percentage excess air //Results: printf("\n (a)The air fuel ratio by mass, A_F = %.1f/1",A_F) printf("\n (b)The percentage excess air supplied = %.1f percent\n\n",P_e)
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//chapter 12 //example 12.16 //page 508 printf("\n") printf("given") R1=2.7*10^6;R2=560*10^3;f1=150;Yfs=8000*10^-6;Ie=1.2*10^-3;Rl=80*10^3;R6=8.2*10^3; Zi=(R1*R2)/(R1+R2) Xc1=Zi/10 C1=1/(2*3.14*f1*Xc1) Xc2=.65/Yfs C2=1/(2*3.14*f1*Xc2)//use 15pF as standard value re=26*10^-3/Ie Xc3=.65*re C3=1/(2*3.14*f1*Xc3) Xc4=(R6+Rl)/10 C4=1/(2*3.14*f1*Xc4)
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clc b=0.0375; // m t=0.0625; // m U=5; // m/s m=2*%pi*U*t/atan(2*b*t/(t^2-b^2)); L=2*b*(1+m/(%pi*U*b))^(1/2); disp("L =") disp(L) disp("m")
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//Example 1.24 // refractive index clc; clear; //given data : d1=.3;// diameter of ring in cm d2=.25;//diameter of ring(in cm) after placing in medium u=(d1/d2)^2;// refractive index of medium disp(u,"refractive index of medium")
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//Ex_8_5 clc; clear; close; format('v',6); //given data : VCC=20;//V Rc=1.5;//kohm VCE=8;//V IC=4;//mA Beta=50;//unitless\ VBE=0.2;//V disp("Part (a)"); S=12;//Stability factor IB=IC/Beta;//mA Re=(VCC-VCE-IC*Rc)/(IB+IC);//kohm RbBYRe=(S-1)/(1-S/(1+Beta)) Rb=RbBYRe*Re;//kohm IE=IB+IC;//mA VBN=VBE+IE*Re;//V V=VBN+IB*Rb;//V R1=Rb*VCC/V;//kohm IR1=(VCC-VBN)/R1;//mA IR2=IR1-IB;//mA R2=VBN/IR2;//kohm disp(R1,"Value of R1(kohm)"); disp(R2,"Value of R2(kohm)"); disp(Re,"Value of Re(kohm)"); disp("Part (b)"); S=3;//Stability factor IB=IC/Beta;//mA Re=(VCC-VCE-IC*Rc)/(IB+IC);//kohm RbBYRe=(S-1)/(1-S/(1+Beta)) Rb=RbBYRe*Re;//kohm IE=IB+IC;//mA VBN=VBE+IE*Re;//V V=VBN+IB*Rb;//V R1=Rb*VCC/V;//kohm IR1=(VCC-VBN)/R1;//mA IR2=IR1-IB;//mA R2=VBN/IR2;//kohm disp(R1,"Value of R1(kohm)"); disp(R2,"Value of R2(kohm)"); format('v',5); disp(Re,"Value of Re(kohm)"); disp(Rb,"Value of Rb(kohm)"); //Answer in the book is wrong.
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//Example 5.8 //To find the amplitude and period of given function clear,clc; //Period printf('PERIOD:\n') printf('This isnt a periodic function as x^2 is linearly related to x \n') printf('and hence period doesnt exist\n') //Amplitude x = linspace(0,2*%pi,200); y = 2*sin(x^2); amplitude= y/sin(x^2); printf('AMPLITUDE:\n') printf('Amplitude exists unlike period\n') printf('Because sine component of the given function never exceeds 1\n') printf('Function value is always ;ess than constant factor adjacent to sine\n') printf('Hence amplitude is the constant factor multiplied with sine component\n\n') printf('Amplitude = %f as calculated\n',amplitude) x = linspace(0,2*%pi,200); y = 2*sin(x^2) ; set(gca(),"grid",[5 5]); plot(x,y,'b'); xlabel("$0\le x\le 2*pi$","fontsize",4,"color","red"); ylabel("$y(x)= 2*sin(x^2)$","fontsize",4,"color","red"); title("Example 5.8","color","red","fontsize",9);
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%%-*- mode: erlang -*- %%-*- coding: utf-8 -*- % Test control options [{tests, []}]. %% ============================================================================= %% TESTS: CURSOR %% ----------------------------------------------------------------------------- % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % cursor_def % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% "cursor cursor_1 is (select * from dual)|:b.f[f(p.r:q)]|". "cursor cursor_1 is (select * from table_1 intersect select * from table_2) union (select * from table_3 minus select * from table_4)". "cursor cursor_1 is (select * from table_1 intersect select * from table_2) union select * from table_3". "cursor cursor_1 is (select * from table_1 order by (select * from table_2) asc)". "cursor cursor_1 is (select * from table_1 order by (select * from table_2) asc,(select * from table_3) desc)". "cursor cursor_1 is (select * from table_1 order by (select * from table_2))". "cursor cursor_1 is (select * from table_1 order by column_1 asc)". "cursor cursor_1 is (select * from table_1 order by column_1 asc,column_2 desc)". "CURSOR cursor_1 IS (SELECT * FROM table_1 Order By column_1)". "CURSOR cursor_1 IS (SELECT * FROM table_1)". "cursor cursor_1 is (select * from dual)|:b.f[f(p.r:q)]|". "cursor cursor_1 is select * from dual". "cursor cursor_1 is select * from table_1 intersect select * from table_2". "cursor cursor_1 is select * from table_1 minus select * from table_2". "CURSOR cursor_1 IS SELECT * FROM table_1 Order By column_1". "cursor cursor_1 is select * from table_1 union (select * from table_2 minus select * from table_3)". "cursor cursor_1 is select * from table_1 union select * from table_2". "CURSOR cursor_1 IS SELECT * FROM table_1". %% ----------------------------------------------------------------------------- %% TESTS: CURSOR %% =============================================================================
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clc //soltuion //given P=2.5//N/mm^2 D=1600//mm ft=75//N/mm^2 T=60//N/mm^2 fc=125//N/mm^2 //design of longitudinal joint t=(P*D)/(2*ft)+1//mm d=6*sqrt(t)//m pi=3.14 //choose standard avlue fromtable 9.3 //let p be pitch //Pt=(p-d)*t*ft//N//tearing resistance of plate //Pt=(p-34.5)*2100//N Ps=4*1.875*(pi/4)*d^2*T+(pi/4)*d^2*T//N//shearing resistance of rivet//N//shearing resistance of rivet //Ps=Pt //2100*(p-34.5)=Ps //p=Ps/(2100)+34.5//mm //pmax=C*t+41.28=220//mm //since p&gt;pmax,therefore p=220//mm p'=220/2//mm d1=0.2*p + 1.15*d//mm/diatnce between outtr and row and next row d2=0.165*p+0.67*d//mm//distance ebtween inner row for zigzag riveting t1=0.75*t//mm//thickness of wide strap t2=0.625*t//mm//thickness of narrow strap m=1.5*d//mm//margin Pt=(p-d)*t*ft//N Pc=5*d*t*fc//N//crushing resistance of rivet P=p*t*ft//N//strength of the unriveted //joint may also fail due to combine teARING AND shearing reistance Pts=(p-2*d)*t*ft+(pi/4)*d^2*T//N //eff=(least of Pt,Ps,Pts)/P eff=Pts/P//least is Ps //desing for circumferential joint //let n be number of rivets //shearign resistance of revets=total shearing load acting on circumferential joint //n*pi*d^2*T/4=pi*D^2*P/4 //n=D^2*P/(d^2*T)//89.6 say 90 n=90 n1=90/2//number of rivets per row //p1=pi(D+t)/n'// //p1=113.7,say 140mm standard value' p1=140//mm effj=(p1-d)/(p1) d3=0.33*p1+0.67*d//dis btw rows of rivets for zigzag m1=1.5*d printf("calcultion for longitudinal joint") printf("the eff is,%f\n",eff) printf("the pitch is,%f mm\n",p) printf("the thickness of wide strap is,%f mm\n",t1) printf("the thickness of narrow strap is,%f mm\n",t2) printf("the diameter of rivets is,%f mm",d) printf("the margine s,%f mm\n",m) printf("the distance btw outer and next row is,%f mm\n",d1) printf("the distance btw inner rows is,%f mm\n",d2) printf("calculation for circumferencial joint\n") printf("the num of rivets is,%f\n",n) printf("the number of rivets per rwo for cercumferencial joint is,%f\n",n1) printf("the distance btw rows of rivets for zigzag riveting is,%f mm\n",d3) printf("the margin is,%f mm",m1)
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//Chapter-13, Example 13.10, Page 391 //============================================================================= clc clear //INPUT DATA Ie=12;//emitter current in mA b=100;//common-emitter DC current gain //CALCULATIONS Ib=Ie/(1+b);//base current in mA Ic=Ie-Ib;//collector current in mA mprintf("Thus base and collector currents are %1.4f mA and %2.4f mA respectively",Ib,Ic); //=================================END OF PROGRAM=======================================================================================================
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function erro = eqm(y,d) [Input_Size,p]=size(y); erro=0; for k=1:p erro=erro+(d(k)-y(k)).^2; end erro=erro/p; endfunction
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clear // // // //Variable declaration ni1=2.5*10**19 //number of electron hole pairs T1=300 //temperature(K) Eg1=0.72*1.6*10**-19 //energy gap(J) k=1.38*10**-23 //boltzmann constant T2=310 //temperature(K) Eg2=1.12*1.6*10**-19 //energy gap(J) //Calculation x1=-Eg1/(2*k*T1) y1=(T1**(3/2))*exp(x1) x2=-Eg2/(2*k*T2) y2=(T2**(3/2))*exp(x2) ni=ni1*(y2/y1) //number of electron hole pairs //Result printf("\n number of electron hole pairs is %0.2f *10**16 per cubic metre",ni/10**16) printf("\n answer varies due to rounding off errors")
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clc clear //Input data W=3.6//Work function of zinc in eV l=2000*10^-10//Wavelength of light used in m h=6.625*10^-34//Plancks constant in J.s c=3*10^8//Velocity of light in m/s e=1.6*10^-19//Charge of electron in Columbs m=9.1*10^-31//Mass of the electron in kg //Calculations lo=((h*c)/(W*e))//Threshold wavelength of zinc in m KE=((h*c*(lo-l))/(lo*l*e))//Kinetic energy of the photoelectrons in eV v=(sqrt((2*KE*e)/m))/10^5//Velocity of photoelectrons in m/s*10^5 //Output printf('The kinetic energy of the photoelectrons emitted is %3.2f eV \n The velocity of the ejected photoelectrons is %3.2f*10^5 m/s',KE,v)
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//chapter 12 //page no 540 //exa 12_48 //given clear; clc; D=0.5; //ps/nm-km Tb=80; //bit period in ps l=1.5; //in nm Zr=Tb/(D*l); //Modulator spacing in km printf("\n Maximum modulator spacing Zr = %0.2f km",Zr);
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function [stk,txt,top]=sci_find() // Copyright INRIA if lhs==1 then if stk(top)(3)=='1' then //row vector stk=list('find('+stk(top)(1)+')','0','1','?','1') elseif stk(top)(4)=='1' then //column vector stk=list('find('+stk(top)(1)+')''','0','1','?','1') else txt=['/'+'/ mtlb_find('+stk(top)(1)+') may be replaced by' '/'+'/ find('+stk(top)(1)+')'' if '+stk(top)(1)+' is not a row vector'] stk=list('mtlb_find('+stk(top)(1)+')','0','1','?','1') end elseif lhs==2 then i=lst(ilst+1)(2) j=lst(ilst+2)(2) txt='['+j+','+i+'] = find('+stk(top)(1)+');'+i+' = '+i+'(:);'+j+' = '+j+'(:);' stk=list(list('?','-2','1','?','1'),list('?','-2','1','?','1')) else i=lst(ilst+1)(2) j=lst(ilst+2)(2) v=lst(ilst+3)(2) temp=gettempvar() txt=[temp+' = '+stk(top)(1)+';' '['+j+','+i+'] = find('+temp+');'+i+'='+i+'(:);'+j+'='+j+'(:);' temp+' = '+temp+'(:)' 'if '+i+'<>[] then '+v+' = '+temp+'('+i+'+size('+temp+',1)*('+j+'-1)) ;else '+v+' = [],end'] r=list('?','-2','1','?','1'), stk=list(r,r,r) end
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errcatch(-1,"stop");mode(2);//Example 2.2://self inductance ; ; c=20;//pF rs=10000;//ohms l=(c*10^-12)*rs^2;//henry disp(l*10^3,"self inductance in mH") exit();
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clc // Part (a) vg1_ = 0.8919 T1 = 120 vg2_ = 0.77076 T2 = 125 vg_ = [vg1_ vg2_] T_ = [T1 T2] v1 = 0.7964 h1 = 2967.6 P1 = 0.3e03 // in Kpa printf("\n Example 9.6\n\n") T1 = interpln([vg_;T_],v1) printf("Steam will become saturated vapour at %f degree centigrade",T1) // Part (b) vf = 0.001029 vg = 3.407 hf = 334.91 hfg = 2308.8 Psat = 47.39 // In kPa v2 = v1 x2 = (v1-vf)/(vg-vf) h2 = hf+x2*hfg P2 = Psat Q12 = (h2-h1)+v1*(P1-P2) disp(x2,"The quality factor at t=80 degree is") disp("kJ/kg",Q12,"The heat transfered per kg of steam in cooling from 250 degree to 80 degree")
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syms G1 G2 G3 G4 H1 H2 a= G1*G2 //shifting the take off point b= a/(1+(a*H2)) c=(1+(G3/G2)) Y= b*c*(G4/(1+G4*H1)) disp(Y,"C/R = ")
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clc //initialisation of variables g=32.2//ft/sec^2 J=778 cp=0.24 T1=2175//R Q=300//b th u v1=526//ft/sec A=0.342//ft^2 p1=98.8//lb/in^2 W1=22.06//lb/sec r=1.65 //CALCULATIONS b=2*g*J*cp a=T1+(Q/cp)+(v1*v1/b) c=T1*(1+(W1*v1/(144*A*g*p1))) d=(v1*v1/b)-(W1*v1/(144*A*g*p1)) v2=r*v1 T2=T1+(Q/cp)+(v1*v1*(1-r*r)/b) p2=(p1*T2)/(T1*r) np2=p2*(22.061+0.361)/22.061 //RESULTS printf ('Temperature = %.f R',T2+15) printf ('\n pressure = %.1f Lb/in^2',np2+0.9)
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%Background cenario_deserto.bg %Music desert-loop.ogg % OBJECT-NAME X-RELATIVE Y-RELATIVE X-SCALE Y-SCALE H-FLIP V-FLIP river1 0.4237 0.0418 1.0000 1.0000 0 0 river1 0.4237 0.1252 1.0000 1.0000 0 0 river1 0.4237 0.2085 1.0000 1.0000 0 0 river1 0.4237 0.2918 1.0000 1.0000 0 0 river1 0.4246 0.3752 1.0000 1.0000 0 0 river1 0.4246 0.4585 1.0000 1.0000 0 0 river1 0.4237 0.6181 1.0000 1.0000 0 0 river1 0.4237 0.6996 1.0000 1.0000 0 0 river1 0.4237 0.7830 1.0000 1.0000 0 0 river1 0.4237 0.8645 1.0000 1.0000 0 0 river1 0.4237 0.9461 1.0000 1.0000 0 0 river1 0.4237 1.0294 1.0000 1.0000 0 0 river2 0.5683 0.2847 1.0000 1.0000 0 0 river2 0.5683 0.3663 1.0000 1.0000 0 0 river2 0.5683 0.4479 1.0000 1.0000 0 0 river2 0.5628 0.4975 1.0000 1.0000 0 0 river2 0.5674 0.6128 1.0000 1.0000 0 0 river2 0.5674 0.6961 1.0000 1.0000 0 0 river2 0.5674 0.7776 1.0000 1.0000 0 0 river2 0.5665 0.8574 1.0000 1.0000 0 0 river2 0.5665 0.9408 1.0000 1.0000 0 0 river2 0.5674 1.0223 1.0000 1.0000 0 0 merchant 0.8364 0.9603 1.0000 1.0000 0 0 merchant 0.0174 0.7315 1.0000 1.0000 0 0 charmer 0.8374 0.1659 1.0000 1.0000 0 0 charmer 0.3267 0.1571 1.0000 1.0000 0 0 house-02 0.9179 0.1589 1.0000 1.0000 0 0 house-02 0.9572 0.8255 1.0000 1.0000 0 0 bridge 0.4960 0.4762 1.0000 1.0000 0 0 river2 0.5701 0.0418 1.0000 1.0000 0 0 river2 0.5701 0.1234 1.0000 1.0000 0 0 river2 0.5701 0.2049 1.0000 1.0000 0 0 river1 0.4246 0.5401 1.0000 1.0000 0 0 house2 0.1044 0.8840 1.0000 1.0000 0 0 river2 0.5692 0.5383 1.0000 1.0000 0 0
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clc; clear; format('v',11); epsilone_0=8.85*10^-12; m_0=4*%pi*10^-7; //The permeability of air. Z=300; a=1*10^-3; b=2*a*cosh(Z*%pi*sqrt(epsilone_0/m_0)); disp(b,"b(in meter)=");
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//CAPTION:Crossed-Field_Amplifier //chapter_no.-10, page_no.-473 //Example_no.10-2-1 clc; //(a) Calculate_the_induced_RF_power Vao=2*(10^3);//Anode_dc_voltage Iao=1.5;//Anode_dc_current ne=.20;//Electronic_efficiency Pgen=Vao*Iao*ne; disp(Pgen,'the_induced_RF_power(in W)is ='); //(b) Calculate_the_total_RF_output_power Pin=80;//RF_input_power Pout=Pin+(Pgen); disp(Pout,'the_total_RF_output_power(in W)is ='); //(c) Calculate_the_power_gain g=Pout/Pin; g=10*log10(g);//in_decibels disp(g,'the_power_gain(in dB)is =');
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// Scilab code Ex3.16: Pg 99 (2008) clc; clear; C_1 = 3e-06; // Capacitance, F C_2 = 6e-06; // Capacitance, F V_1 = 250; // Voltage across capacitor C_1, V // Since each capacitor will take charge according to its capacitance, so we have Q = C_1*V_1; // Charge on first capacitor C_1, C W_1 = 0.5*C_1*(V_1^2); // Energy stored, J // When the two capacitors are connected in parallel the 3 micro-farad will share its charge with 6 micro-farad capacitor. Thus the total charge in the system will remain unchanged, but the total capacitance will now be different C = C_1 + C_2; // Total capacitance, F // Since Q = C*V, solving for V V = Q/C; // Voltage across capacitor C_2, V W = 0.5*C*(V^2); // Total energy stored by the combination, J printf("\nThe charge and energy stored by %1d micro-F capcitor are %3.2f mC and %5.2f mJ respectively ", C_1/1e-06, Q/1e-03 , W_1/1e-03); printf("\nThe p.d. between the plates = %5.2f V", V); printf("\nThe energy stored by the combination of %1d micro-F and %1d micro-F capacitors = %5.2f mJ", C_1/1e-06, C_2/1e-06, W/1e-03); // Result // The charge and energy stored by 3 micro-F capcitor are 0.75 mC and 93.75 mJ respectively // The p.d. between the plates = 83.33 V // The energy stored by the combination of 3 micro-F and 6 micro-F capacitors = 31.25 mJ
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clear; close; clc; T0=2; t=-6:0.01:6; x=[]; for i=1:length(t) if modulo(t(i),T0)==0 then x(i)=1; else x(i)=0; end end plot(t,x,'r') //by sifting property ck=1/T0; //trigmometeric form a0=2*ck; a=2*real(ck); b=2*imag(ck);
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function[L]=Choleski(A) [n,n]=size(A) for i=1:n s(i)=0 for k=1:i-1 s(i)=s(i)+A(i,k) end L(i,i)=sqrt(A(i,i)-s(i)) for j=i+1:n s=0 for k=1:i-1 s=s+A(i,k)*A(j,k) end L(i,j)=(A(i,j)-s)/L(i,i) end end endfunction
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Name=eneways bots PlayerCharacters=EGODEATH BotCharacters=soar.bot IsChallenge=true Timelimit=60.0 PlayerProfile=EGODEATH AddedBots=soar.bot PlayerMaxLives=0 BotMaxLives=1 PlayerTeam=1 BotTeams=2 MapName=kovdmm4b.map MapScale=3.8125 BlockProjectilePredictors=false BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=1.0 ScorePerKill=10.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=overwatch WeaponHeroTag=tracking DifficultyTag=1 AuthorsTag=gli BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=kind of like a winston jumping over you, vertical/horizontal crossup practice GameVersion=0.99.5 [Aim Profile] Name=At Feet MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Medium Skill At Feet MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Medium Skill 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 [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=soar DodgeProfileNames=ADAD DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;0.5;2.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=At Feet;Medium Skill At Feet;Medium Skill;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=soaring bot SeeThroughWalls=true [Character Profile] Name=EGODEATH MaxHealth=100.0 WeaponProfileNames=Track_fullsound;track_earlove;track_earlove2;pistol;QWRL;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=1300.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=true MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=true JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 [Character Profile] Name=soaring bot MaxHealth=1000.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=1.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1500.0 MaxCrouchSpeed=500.0 Acceleration=10000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=0.0 Gravity=4.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=0.212 Z=0.020 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=300.0 MainBBRadius=50.0 MainBBHasHead=false MainBBHeadRadius=20.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=300.0 ProjBBRadius=50.0 ProjBBHasHead=false ProjBBHeadRadius=20.0 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=soaring.abilmov;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 [Dodge Profile] Name=ADAD MaxTargetDistance=5500.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.05 MaxLRTimeChange=0.3 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.9 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=2.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.3 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.16 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.1 MaxCrouchTime=0.1 MinJumpTime=0.0 MaxJumpTime=0.0 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=Track_fullsound Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=1.0 TimeBetweenShots=0.01 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=1000000.0 GravityScale=1.0 HeadshotCapable=true 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=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 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=0.001 HitSoundCooldown=0.001 ShootSound=Shot HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=1.0 RecoilNegatable=false DecalType=0 DecalSize=15.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=0.1 TaggingDuration=0.01 TaggingMaxFactor=0.5 TaggingHitFactor=0.001 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 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=track_earlove Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.01 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=1000000.0 GravityScale=1.0 HeadshotCapable=true 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=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 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=0.05 HitSoundCooldown=0.05 ShootSound=Shot HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=0.1 TaggingDuration=0.0 TaggingMaxFactor=0.0 TaggingHitFactor=0.0 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 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=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=1.0 AAMaxSpeed=1000.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=track_earlove2 Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.01 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=1000000.0 GravityScale=1.0 HeadshotCapable=true 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=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.5 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=0.1 HitSoundCooldown=0.1 ShootSound=Shot HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=true AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=0.1 TaggingDuration=0.0 TaggingMaxFactor=0.0 TaggingHitFactor=0.0 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 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=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=1.0 AAMaxSpeed=1000.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=pistol Type=Hitscan ShotsPerClick=1 DamagePerShot=100.0 KnockbackFactor=4.0 TimeBetweenShots=0.1 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=4.0 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=None ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=Gunshot HitParticleEffect=Flare BounceOffWorld=false BounceFactor=0.5 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=4.0 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=false AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.1 MinRecoilUp=0.1 MinRecoilHoriz=0.1 MaxRecoilHoriz=0.1 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.05 AAMode=0 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=360.0 AADeadZone=0.0 AAFOV=360.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 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refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
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clc clear //Input data C=300 //Velocity of air in m/s P=1 //Static pressure in kPa T=290 //Static temperature in K k=1.4 //Adiabatic constant R=287 //Specific gas constant in J/kg-k Cp=1005 //Specific heat capacity at constant pressure in J/kg-K //Calculation To=T+(C^2/(2*Cp)) //Stagnation temperature in K Po=P*(To/T)^(k/(k-1)) //Stagnation pressure in kPa a=sqrt(k*R*T) //Sound velocity in m/s Co=sqrt(k*R*To) //Sound velocity at Stagnation condition in m/s //Output printf('(A)Stagnation pressure and temperature are %3.4f bar and %3.2f K\n (B)Velocity of sound in the dynamic and stagnation conditions are %3.2f m/s and %3.2f m/s',Po,To,a,Co)