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example2_14.sce
clear; clc; // Stoichiometry // Chapter 2 // Basic Chemical Calculations // Example 2.14 // Page 24 printf("Example 2.14, Page 24 \n \n"); // solution m = 100 //[kg] Lye (basis) m1 = 73 //[kg] NaOH M1 = 40 // NaOH M2 = 62 // Na2O p = (M2*m1)/(2*M1) printf("percentage of Na2O in the solution is "+string(p)+".")
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Ex1_4.sce
//Calculations on four stroke petrol engine clc,clear //Given: bp=35 //Brake power in kW eta_m=80 //Mechanical efficiency in percent bsfc=0.4 //Brake specific fuel consumption in kg/kWh A_F=14/1 //Air-fuel ratio CV=43000 //Calorific value in kJ/kg //Solution: //(a) ip=bp*100/eta_m //Indicated power in kW //(b) fp=ip-bp //Frictional power in kW //(c) //Since, 1 kWh = 3600 kJ eta_bt=1/(bsfc*CV/3600) //Brake thermal efficiency //(d) eta_it=eta_bt/eta_m*100 //Indicated thermal efficiency //(e) m_f=bsfc*bp //Fuel consumption in kg/hr //(f) m_a=A_F*m_f //Air consumption in kg/hr //Results: printf("\n (a)The indicated power, ip = %.2f kW\n (b)The friction power, fp = %.2f kW",ip,fp) printf("\n (c)The brake thermal efficiency, eta_bt = %.1f percent\n (d)The indicated thermal efficiency, eta_it = %.1f percent",eta_bt*100,eta_it*100) printf("\n (e)The fuel consumption per hour, m_f = %.1f kg/hr\n (f)The air consumption per hour, m_a = %d kg/hr\n\n",m_f,m_a)
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sebherv/master2
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2018-02-09T15:09:24
2018-02-09T15:09:24
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exo4.sci
// Exo 4: plotting and projecting confidence regions // Gen data et gen modèle // Our model is m2 (with 3 parameters), our Cm is inv(G2'*G2) exec('/Users/sebh/Desktop/MasterII/repos_master2/ProbInverses/TP1/01genTestDistribs.sce',-1); exec('/Users/sebh/Desktop/MasterII/repos_master2/ProbInverses/TP1/02leastsquares.sce',-1); Cm = inv(G2'*Ct*G2); covmls=correlationMatrix(Cm) ins1D=sqrt(4)*sqrt(diag(Cm)) // Calcul des ellipses à 95% pour 3 paramètres
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/3769/CH8/EX8.20/Ex8_20.sce
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FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
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Ex8_20.sce
clear //Given e=1.6*10**-19 f=6.8*10**15 r=0.51*10**-10 u=4*3.14*10**-7 //T/A m //Calculation // I=e*f B=(u*I)/(2*r) M=1*I*%pi*r**2 //Result printf("\n The effective dipole moment is %0.0f *10**-24 Am**2",M*10**24)
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Exa2_11.sce
//Exa 2.11 clc; clear; close; //Given data IES=10^-14;//in A alfaF=1;//unitless alfaR=0.1;//unitless //Formula : alfaF*IES=alfaR*ICS ICS=(alfaF/alfaR)*IES;//in Ampere disp(ICS,"Collector base junction saturation current in Ampere : "); RelativeSize=ICS/IES;//unitless disp("Collector is "+string(RelativeSize)+" times larger in size than emitter."); BetaR=alfaR/(1-alfaR);//unitless disp(BetaR,"Value of BetaR : ");
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Ex9_13.sce
// Given:- Wnetdot = 45.00 // in MW T1 = 300.00 // in kelvin p1 = 100.00 // in kpa etac = 0.84 // The isentropic efficiency of the compressor T3 = 1400.00 // in kelvin p2 = 1200.00 // in kpa p3 = p2 etat = 0.88 // isentropic efficiency of the turbine T5 = 400.00 // in kelvin p4 = 100.00 // in kpa p5 = p4 T7 = 400.00 // in degree celcius p7 = 8.00 // in MPa etatw =0.9 // isentropic efficiency of turbine of the vapor cycle p8 = 8.00 // in kpa p9 = p8 etap = 0.8 // isentropic efficiency of pump of the vapor cycle T0 = 300.00 // in kelvin p0 = 100.00 // -in kpa // Analysis // With procedure similar to that used in the examples of chapters 8 and 9,we can determine following property data h1 = 300.19 // in kj/kg h2 = 669.79 // in kj/kg h3 = 1515.42 // in kj/kg h4 = 858.02 // in kj/kg h5 = 400.98 // in kj/kg h6 = 183.96 // in kj/kg h7 = 3138.30 // in kj/kg h8 = 2104.74 // in kj/kg h9 = 173.88 // in kj/kg s1 = 1.7020 // in kj/kg.k s2 = 2.5088 // in kj/kg.k s3 = 3.3620 // in kj/kg.k s4 = 2.7620 // in kj/kg.k s5 = 1.9919 // in kj/kg.k s6 = 0.5975 // in kj/kg.k s7 = 6.3634 // in kj/kg.k s8 = 6.7282 // in kj/kg.k s9 = 0.5926 // in kj/kg.k // Part(a) // By applying mass and energy rate balances // Calculations mvdotbymgdot = (h4-h5)/(h7-h6) // ratio of mass flow rates of vapor and air mgdot = (Wnetdot*10**3)/(((h3-h4)-(h2-h1)) + mvdotbymgdot*((h7-h8)-(h6-h9))) // mass flow rate of air in kg/s mvdot = mvdotbymgdot*mgdot // mass flow rate of vapor in kg/s Wgasdot = mgdot*((h3-h4)-(h2-h1))*10**-3 // net power developed by gas turbine in MW Wvapdot = mvdot*((h7-h8)-(h6-h9))*10**-3 // net power developed by vapor cycle in MW // Results printf( ' Mass flow rate of air is: %.2f kg/s.',mgdot) printf( ' Mass flow rate of vapor is: %.2f kg/s.',mvdot) printf( ' Net power developed by gas turbine is: %.2f MW.',Wgasdot) printf( ' Net power developed by vapor cycle is: %.2f MW.',Wvapdot) // Part(b) // The net rate of exergy increase of the air passing through the combustor is Edotf32 = mgdot*(h3-h2-T0*(s3-s2))*10**-3 // in MW // The net rate exergy is carried out by the exhaust air stream at 5 is Edotf51 = mgdot*(h5-h1-T0*(s5-s1))/10**3 // in MW // The net rate exergy is carried out as the water passes through the condenser is Edotf89 = mvdot*(h8-h9-T0*(s8-s9))*10**-3 // in MW R = 8.314 // universal gas constant, in SI units M = 28.97 // molar mass of air in grams // The rate of exergy destruction for air turbine is Eddott = mgdot*T0*(s4-s3-(R/M)*log(p4/p3))/10**3 // in MW // The rate of exergy destruction for compressor is Eddotc = mgdot*T0*(s2-s1-(R/M)*log(p2/p1))/10**3 // in MW // The rate of exergy destruction for steam turbine is Eddotst = mvdot*T0*(s8-s7)/10**3 // in MW // The rate of exergy destruction for pump is Eddotp = mvdot*T0*(s6-s9)/10**3 // in MW // For heat exchanger EddotHE = T0*(mgdot*(s5-s4)+mvdot*(s7-s6))/10**3 // in MW // Results printf( ' Balance sheet') printf( 'Net exergy increase of the gas passing') printf( ' Through the combustor: %.2f MW',Edotf32) printf( 'Disposition of the exergy:') printf( '• Net power developed') printf( 'gas turbine cycle %.2f MW',Wgasdot) printf( 'vapor cycle %.2f MW',Wvapdot) printf( '• Net exergy lost') printf( 'with exhaust gas at state 5 %.2f MW',Edotf51) printf( 'from water passing through condenser %.2f MW',Edotf89) printf( '• Exergy destruction') printf( 'air turbine %.2f MW',Eddott) printf( 'compressor %.2f MW',Eddotc) printf( 'steam turbine %.2f MW',Eddotst) printf( 'pump %.2f MW',Eddotp) printf( 'heat exchanger %.2f MW',EddotHE)
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/SCAN_16010-4002-001_NEW.sce
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2-BiAs/UCASI_ALIGNMENT_SCAN
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2020-06-21T10:26:29.419281
2017-05-19T02:01:27
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SCAN_16010-4002-001_NEW.sce
clear clc clf(1); clf(2); clf(3); clf(4) format('v', 10) csvDefault("eol", "windows") csvDefault("blank", "on") [ok, sPartNumber] = getvalue("Input Part Number", "PN", list("str", 1), ["16010-4002-001"]); if ~ok then abort end [ok, sSerialNumber] = getvalue("Input Serial Number", "SN", list("str", 1), ["default"]); if ~ok then abort end directory = uigetdir(pwd(), "Select Working Directoy"); status = chdir(directory) realpath = cd(directory) if ~status then disp('failed to change directory') abort end if ~isdir(directory) then [status, err] = mkdir(sSerialNumber, 'imgs') if status ~= 1 then disp(err) abort end end //exec('WriteMatrixCSV.sci'); //exec('PointMatrixToList.sci'); //Define Surface Parameters fConicConstant = -1.374; fRadiusOfCurvature = 38.448; //(mm) iConcavity = +1; //-1 = concave //+1 = convex //no 0! fOffset = 0.0; // mm fPolynomialCoefficients = [0]; //... // [ 0, 0, 2.8265179e-6, -4.8964451e-7;... // 0, 6.5191331e-5, -1.8966279e-7, 0;... // -5.9920375e-5, -7.0557011e-7, 0, 0;... // -2.6125317e-7, 0, 0, 0]; // fRadiusOfCurvature = abs(fRadiusOfCurvature) * -iConcavity; fPolynomialCoefficients = fPolynomialCoefficients * -iConcavity; /////////////////////////////////////////////////////////////////////////////////// /////////////////////////////////////////////////////////////////////////////////// //Define Scan Parameters fOD = 70; //(mm) fID = 28; iN_R = 24; //20; //Number of radial steps iN_T = 16; //20; //Number of angular steps fXs = 0; fYs = 0; /////////////////////////////////////////////////////////////////////////////////// /////////////////////////////////////////////////////////////////////////////////// //Build Polynomial Terms sPolynomialTerms = ''; iNM = size(fPolynomialCoefficients); iN = iNM(1); iM = iNM(2); for i = 1:iN for j = 1:iM if fPolynomialCoefficients(i, j) ~= 0 then sPolynomialTerms = sPolynomialTerms + '+ ' + string(fPolynomialCoefficients(i,j)) +... ' * (x - fXs * ones(x)).^(' + string(i) + ' - 1) .* (y - fYs * ones(y)).^(' + string(j) + ' - 1)'; end end end //Build Polynomial Normal Terms sPnX = ''; sPnY = ''; iNM = size(fPolynomialCoefficients); iN = iNM(1); iM = iNM(2); for i = 1:iN for j = 1:iM if fPolynomialCoefficients(i, j) ~= 0 then sPnX = sPnX + '- ' + string(fPolynomialCoefficients(i,j)) +... ' * ((x - fXs * ones(x)).^' + string(i-1) +' * ' + string(i-1) + ') .* (y - fYs * ones(y)).^' + string(j-1) + ' .* (x - fXs * ones(x)).^(-1)'; sPnY = sPnY + '- ' + string(fPolynomialCoefficients(i,j)) +... ' * ((x - fXs * ones(x)).^' + string(i-1) + ' * ' + string(j-1) + ') .* (y - fYs * ones(y)).^' + string(j-1) + ' .* (y - fYs * ones(y)).^(-1)'; end end end //Build Conic Equation sConic = 'z = (x.^2 - 2 * x * fXs + fXs^2 * ones(x) + y.^2 - 2 * y * fYs + fYs^2 * ones(y)) .*... (R * (ones(x) + sqrt(ones(x) - (1 + fConicConstant) * (x.^2 - 2 * x * fXs + fXs^2 * ones(x) + y.^2 - 2 * y * fYs + fYs^2 * ones(y)) / R^2))) .^ (-1) '; //Build Conic Normals sCnX = 'nx = -(2 * x - 2 * fXs * ones(x)) .* (R * (ones(x) + sqrt(ones(1)-(x.^2 - 2 * x * fXs + fXs^2 * ones(x) + y.^2 - 2 * y * fYs + fYs^2 * ones(y)) * (1 + fConicConstant) / R^2))).^(-1)-... (1 / 2) * (x.^2 - 2 * x * fXs + fXs^2 * ones(x) + y.^2 - 2 * y * fYs + fYs^2 * ones(y)) .* (1 + fConicConstant) .* (2 * x - 2 * fXs * ones(x)) .*... ((R^3 * (ones(x) + sqrt(ones(x) - (x.^2 - 2 * x * fXs + fXs^2 * ones(x) + y.^2 - 2 * y * fYs + fYs^2 * ones(y)) * (1 + fConicConstant) / R^2)).^2)... .* sqrt(ones(x) - (x.^2 - 2 * x * fXs + fXs^2 * ones(x) + y.^2 - 2 * y * fYs + fYs^2 * ones(y)) * (1 + fConicConstant) / R^2)).^(-1) '; sCnY = 'ny = -(2 * y - 2 * fYs * ones(y)) .* (R * (ones(x) + sqrt(ones(1)-(x.^2 - 2 * x *fXs+fXs^2 * ones(x) + y.^2 - 2 * y * fYs + fYs^2 * ones(y)) * (1 + fConicConstant) / R^2))).^(-1)-... (1 / 2) * (x.^2 - 2 * x *fXs + fXs^2 * ones(x) + y.^2 - 2 * y *fYs+fYs^2 * ones(y)) * (1 + fConicConstant) .* (2 * y - 2 *fYs* ones(y)) .*... ((R^3 * (ones(x) + sqrt(ones(x) - (x.^2 - 2 * x *fXs+fXs^2 * ones(x) + y.^2 - 2 * y *fYs+fYs^2 * ones(y)) * (1 + fConicConstant) / R^2)).^2)... .* sqrt(ones(x) - (x.^2 - 2 * x *fXs+fXs^2 * ones(x) + y.^2 - 2 * y *fYs+fYs^2 * ones(y)) * (1 + fConicConstant) / R^2)).^(-1) '; //Define Surface Funtions deff('z = Z(x, y, R)', sConic + sPolynomialTerms); deff('x = X(r, t)', 'x = r'' * cos(t)'); deff('y = Y(r, t)', 'y = r'' * sin(t)'); //deff('x = X(u, v)', 'x = (u * cos(fTheta))'' * ones(v) - ones(u'') * (v * sin(fTheta))'); //deff('y = Y(u, v)', 'y = (u * sin(fTheta))'' * ones(v) + ones(u'') * (v * cos(fTheta))'); //Define Normal Fuctions deff('nx = nX(x, y, R)', sCnX + sPnX); deff('ny = nY(x, y, R)', sCnY + sPnY); //Define Domain in the Polar Parameters (r, t) r = linspace(fID / 2, fOD / 2, iN_R); t = linspace(0, 2 * %pi, iN_T); x = X(r, t); y = Y(r, t); z = Z(x, y, fRadiusOfCurvature); NX = nX(x, y, fRadiusOfCurvature); NY = nY(x, y, fRadiusOfCurvature); NZ = ones(NX); NX = NX; //Flip normals? or not NY = NY; NZ = NZ; fig_the = scf(1); [xf, yf, zf] = nf3d(x', y', z'); xset('colormap', jetcolormap(128)); plot3d1(xf, yf, zf, theta = 300, alpha = 60, leg = "@@", flag = [-1 6 4]); axes_the = gca(); axes_the.axes_reverse = ["off", "off", "off"]; //facets_the = axes_the.children(1); //facets_the.hiddencolor = -1; //colorbar(min(z), max(z)); INV_NMAG = (NX.^2 + NY.^2 + NZ.^2).^(-1/2); NX = NX .* INV_NMAG; NY = NY .* INV_NMAG; NZ = NZ .* INV_NMAG; [a, b] = size(x); for i = 1:a x_list((i - 1) * b + 1 : i * b) = x(i, :) end [a, b] = size(y); for i = 1:a y_list((i - 1) * b + 1 : i * b) = y(i, :) end [a, b] = size(z); for i = 1:a z_list((i - 1) * b + 1 : i * b) = z(i, :) end [a, b] = size(NX); for i = 1:a NX_list((i - 1) * b + 1 : i * b) = NX(i, :) end [a, b] = size(NY); for i = 1:a NY_list((i - 1) * b + 1 : i * b) = NY(i, :) end [a, b] = size(NZ); for i = 1:a NZ_list((i - 1) * b + 1 : i * b) = NZ(i, :) end xarrows([x_list; x_list + NX_list*10], [y_list; y_list + NY_list*10], [z_list; z_list + NZ_list*10], 25) //xs2pdf(gcf(), pwd() + '\' + string(sSerialNumber) + '\imgs\' + string(sPartNumber) + '_'... // + string(sSerialNumber) + '_SURFACE.pdf'); /////////////////////////////////Apply normal offset to target points x_list = x_list + fOffset * NX_list; y_list = y_list + fOffset * NY_list; z_list = z_list + fOffset * NZ_list; ///////////////////////////////////////////////////////////////// SAVE TARGET POINTS sFileToSave = 'TARGET_POINTS.csv'; sTempFile = TMPDIR + "\" + sFileToSave; fFile = mopen(sTempFile, 'wt'); for i=1:length(x_list) - 1 mfprintf(fFile, "%.6f, %.6f, %.6f, %.6f, %.6f, %.6f\n", x_list(i), y_list(i), z_list(i), NX_list(i), NY_list(i), NZ_list(i)); end mfprintf(fFile, "%.6f, %.6f, %.6f, %.6f, %.6f, %.6f", x_list($), y_list($), z_list($), NX_list($), NY_list($), NZ_list($)); mclose(fFile); dos('move ' + sTempFile + ' ' + pwd() + '\' + sFileToSave); ///////////////////////////////////////////////////////////////// M_Actual = csvRead('ACTUAL_POINTS.csv'); [a b] = size(M_Actual) for i=1:iN_R x_actual(i, 1:iN_T) = M_Actual((i - 1) * iN_T + 1:i * iN_T, 1)'; y_actual(i, 1:iN_T) = M_Actual((i - 1) * iN_T + 1:i * iN_T, 2)'; z_actual(i, 1:iN_T) = M_Actual((i - 1) * iN_T + 1:i * iN_T, 3)'; end [a, b] = size(x_actual); for i = 1:a x_actual_list((i - 1) * b + 1 : i * b) = x_actual(i, :) end [a, b] = size(y_actual); for i = 1:a y_actual_list((i - 1) * b + 1 : i * b) = y_actual(i, :) end [a, b] = size(z_actual); for i = 1:a z_actual_list((i - 1) * b + 1 : i * b) = z_actual(i, :) end z_error = z_actual - Z(x_actual, y_actual, fRadiusOfCurvature); fig_error2 = scf(3); xset('colormap', jetcolormap(128)); [xf, yf, zf] = nf3d(x_actual', y_actual', z_error' * 1000); plot3d1(xf, yf, zf, theta = 300, alpha = 60, leg = "@@", flag = [-1 6 4]); colorbar(min(z_error * 1000), max(z_error * 1000),,fmt="%.3f"); a = gca(); a.view = "2d"; a.axes_reverse = ["off", "off", "off"]; format('v', 10) a.x_label.text = "$\Large X \tt(mm)$"; a.y_label.text = "$\Large Y \tt(mm)$"; a.title.text = "$\text{\begin{gather}\Huge{Surface \ Error}$" + ... "$\\ \LARGE{" + sPartNumber + " \ SN" + sSerialNumber + "}$" + ... "$\\ \small{R_{nom} = " + string(fRadiusOfCurvature) + "mm}$" +... "\end{gather}}$"; mkdir('/' + sSerialNumber); mkdir('/' + sSerialNumber + '/imgs'); xs2pdf(gcf(), pwd() + '\' + string(sSerialNumber) + '\imgs\' + string(sPartNumber) + '_'... + string(sSerialNumber) + '_FIGURE_ERROR_REAL.pdf'); function zt = ZT(x, y, parameters) // zt = Z(x - parameters(1) + parameters(4) * sign(x),... // y - parameters(2) + parameters(5) * sign(y),... // fRadiusOfCurvature) + parameters(3); zt = Z(x - parameters(1) + parameters(4) * cos(atan(y, x)),... y - parameters(2) + parameters(4) * sin(atan(y, x)),... fRadiusOfCurvature) + parameters(3); endfunction function ze = ZE(parameters, x_exp, y_exp, z_exp) ze = ZT(x_exp, y_exp, parameters) - z_exp; endfunction param_noms = [0, 0, 0, 0, 0]; //param_binf = [-%inf, -%inf, -%inf, -.020, -%inf]; //param_bsup = [%inf, %inf, %inf, -.019, %inf]; [f, param_opt] = leastsq(list(ZE, x_actual_list', y_actual_list', z_actual_list'), param_noms); //[f, param_opt] = leastsq(list(ZE, x_actual_list', y_actual_list', z_actual_list'),'b', param_binf, param_bsup, param_noms); //z_error_ls_fit_all = z_actual - (Z(x_actual - param_opt(1), y_actual - param_opt(2), param_opt(4)) + param_opt(3)); //z_error_ls_fit_all = - z_error_ls_fit_all; //This makes the sign correct so that a positive error is in the outward surface normal dirrection z_error_ls = z_actual - (Z(x_actual - param_opt(1), y_actual - param_opt(2), fRadiusOfCurvature)); z_error_ls_xyz = z_actual - (Z(x_actual - param_opt(1), y_actual - param_opt(2), fRadiusOfCurvature) + param_opt(3)); z_error_ls_xyz_tool = z_actual - (Z(x_actual - param_opt(1) + param_opt(4) * cos(atan(y_actual, x_actual)), y_actual - param_opt(2) + param_opt(4) * sin(atan(y_actual, x_actual)), fRadiusOfCurvature) + param_opt(3)); //z_error_ls = -z_error_ls; //This makes the sign correct so that a positive error is in the outward surface normal dirrection fig_error2 = scf(4); xset('colormap', jetcolormap(128)); [xf, yf, zf] = nf3d(x_actual', y_actual', z_error_ls' * 1000); plot3d1(xf, yf, zf, theta = 300, alpha = 60, leg = "@@", flag = [-1 6 4]); colorbar(min(z_error_ls * 1000), max(z_error_ls * 1000),,fmt="%.3f"); e = gce(); e.parent.title.text = "$\Large Z_{err} \tt(\mu m)$"; a = gca(); a.view = "2d"; a.axes_reverse = ["off", "off", "off"]; format('v', 10) a.x_label.text = "$\Large X \tt(mm)$"; a.y_label.text = "$\Large Y \tt(mm)$"; a.title.text = "$\text{\begin{gather}\Huge{Surface \ Error}$" + ... "$\\ \LARGE{" + sPartNumber + " \ SN" + sSerialNumber + "}$" + ... "$\\ \normalsize{R_{nom} = " + string(fRadiusOfCurvature) + "mm}$" +... "$\\ \normalsize{X_{offset} = " + string(round(param_opt(1)*1000)/1000) + "mm}$" +... "$\\ \normalsize{Y_{offset} = " + string(round(param_opt(2)*1000)/1000) + "mm}$" +... "\end{gather}}$"; //facets_a = a.children(1); //facets_a.hiddencolor = -1; mkdir('/' + sSerialNumber); mkdir('/' + sSerialNumber + '/imgs'); xs2pdf(gcf(), pwd() + '\' + string(sSerialNumber) + '\imgs\' + string(sPartNumber) + '_'... + string(sSerialNumber) + '_FIGURE_ERROR_FIT_XY.pdf'); //fig_error2 = scf(5); //xset('colormap', jetcolormap(128)); //[xf, yf, zf] = nf3d(x_actual', y_actual', z_error_ls_fit_all' * 1000); //plot3d1(xf, yf, zf, theta = 300, alpha = 60, leg = "@@", flag = [-1 6 4]); //colorbar(min(z_error_ls_fit_all * 1000), max(z_error_ls_fit_all * 1000),,fmt="%.3f"); // //e = gce(); //e.parent.title.text = "$\Large Z_{err} \tt(\mu m)$"; // //a = gca(); //a.view = "2d"; //a.axes_reverse = ["off", "off", "off"]; // //format('v', 10) //a.x_label.text = "$\Large X \tt(mm)$"; //a.y_label.text = "$\Large Y \tt(mm)$"; //a.title.text = "$\text{\begin{gather}\Huge{Surface \ Error}$" + ... // "$\\ \LARGE{" + sPartNumber + " \ SN" + sSerialNumber + "}$" + ... // "$\\ \small{R_{bf} = " + string(round(param_opt(4)*1000)/1000) + "mm}$" +... // "$\\ \small{X_{offset} = " + string(round(param_opt(1)*1000)/1000) + "mm}$" +... // "$\\ \small{Y_{offset} = " + string(round(param_opt(2)*1000)/1000) + "mm}$" +... // "$\\ \small{Z_{offset} = " + string(round(param_opt(3)*1000)/1000) + "mm}$" +... // "\end{gather}}$"; // ////facets_a = a.children(1); ////facets_a.hiddencolor = -1; // //mkdir('/' + sSerialNumber); //mkdir('/' + sSerialNumber + '/imgs'); //xs2pdf(gcf(), pwd() + '\' + string(sSerialNumber) + '\imgs\' + string(sPartNumber) + '_'... // + string(sSerialNumber) + '_FIGURE_ERROR_FIT_XYZR.pdf'); //////////////////////////////////////////////////////// fig_error2 = scf(7); xset('colormap', jetcolormap(128)); [xf, yf, zf] = nf3d(x_actual', y_actual', z_error_ls_xyz_tool' * 1000); plot3d1(xf, yf, zf, theta = 300, alpha = 60, leg = "@@", flag = [-1 6 4]); colorbar(min(z_error_ls_xyz_tool * 1000), max(z_error_ls_xyz_tool * 1000),,fmt="%.3f"); e = gce(); e.parent.title.text = "$\Large Z_{err} \tt(\mu m)$"; a = gca(); a.view = "2d"; a.axes_reverse = ["off", "off", "off"]; format('v', 10) a.x_label.text = "$\Large X \tt(mm)$"; a.y_label.text = "$\Large Y \tt(mm)$"; a.title.text = "$\text{\begin{gather}\Huge{Surface \ Error}$" + ... "$\\ \LARGE{" + sPartNumber + " \ SN" + sSerialNumber + "}$" + ... "$\\ \normalsize{X_{shift} = " + string(round(param_opt(4)*1000)/1000) + "mm}$" +... "$\\ \normalsize{Y_{shift} = " + string(round(param_opt(5)*1000)/1000) + "mm}$" +... "$\\ \normalsize{X_{offset} = " + string(round(param_opt(1)*1000)/1000) + "mm}$" +... "$\\ \normalsize{Y_{offset} = " + string(round(param_opt(2)*1000)/1000) + "mm}$" +... "$\\ \normalsize{Z_{offset} = " + string(round(param_opt(3)*1000)/1000) + "mm}$" +... "\end{gather}}$"; //facets_a = a.children(1); //facets_a.hiddencolor = -1; mkdir('/' + sSerialNumber); mkdir('/' + sSerialNumber + '/imgs'); xs2pdf(gcf(), pwd() + '\' + string(sSerialNumber) + '\imgs\' + string(sPartNumber) + '_'... + string(sSerialNumber) + '_FIGURE_ERROR_FIT_XYZT.pdf'); ////////////////////////////////////////////////////////////////////////// ////////////////////////////////////////////////////////////////////////// ////////////////////////////////////////////////////////////////////////// ////////////////////////////////////////////////////////////////////////// // // //[M N] = size(x) // //for i = 1 : M - 1 // for j = 1 : N - 1 // grad_zu(i, j) = ((z_error_ls_fit_all(i, j) - z_error_ls_fit_all(i + 1, j)) / sqrt((x_actual(i, j) - x_actual(i + 1, j)) ^ 2 + (y_actual(i, j) - y_actual(i + 1, j)) ^ 2) + (z_error_ls_fit_all(i, j + 1) - z_error_ls_fit_all(i + 1, j + 1)) / sqrt((x_actual(i, j + 1) - x_actual(i + 1, j + 1)) ^ 2 + (y_actual(i, j + 1) - y_actual(i + 1, j + 1)) ^ 2)) / 2; // // grad_zv(i, j) = ((z_error_ls_fit_all(i, j) - z_error_ls_fit_all(i, j + 1)) / sqrt((x_actual(i, j) - x_actual(i, j + 1)) ^ 2 + (y_actual(i, j) - y_actual(i, j + 1)) ^ 2) + (z_error_ls_fit_all(i + 1, j) - z_error_ls_fit_all(i + 1, j + 1)) / sqrt((x_actual(i + 1, j) - x_actual(i + 1, j + 1)) ^ 2 + (y_actual(i + 1, j) - y_actual(i + 1, j + 1)) ^ 2)) / 2; // // // x_grad(i,j) = (x_actual(i, j) + x_actual(i, j + 1) + x_actual(i + 1, j) + x_actual(i + 1, j + 1)) / 4; // y_grad(i,j) = (y_actual(i, j) + y_actual(i, j + 1) + y_actual(i + 1, j) + y_actual(i + 1, j + 1)) / 4; // end //end // //grad_mag = (grad_zu.^2 + grad_zv.^2).^(1/2) * 50 * 10^3; ////grad_mag = grad_zv * (50 * 10^3); //slope_error = scf(6); //xset('colormap', jetcolormap(128)); //[xf, yf, zf] = nf3d(x_grad', y_grad', grad_mag'); //plot3d1(xf, yf, zf, theta = 300, alpha = 60, leg = "@@", flag = [-1 6 4]); //colorbar(min(grad_mag), max(grad_mag),,fmt="%.3f"); // //e = gce(); //e.parent.title.text = "$\Large ||{\nabla Z_{err}}|| \tt\Big(\frac{\mu m}{50 mm}\Big)$"; // //a = gca(); //a.view = "2d"; //a.axes_reverse = ["off", "on", "on"]; // //format('v', 10) //a.x_label.text = "$\Large X \tt(mm)$"; //a.y_label.text = "$\Large Y \tt(mm)$"; //a.title.text = "$\text{\begin{gather}\Huge{Slope \ Error}$" + "$\\ \LARGE{' + sPartNumber +' \ SN" + sSerialNumber + "}$" +... // "$\\ \LARGE{R_{bf} = " + string(param_opt(4)) + " mm}\end{gather}}$"; // //facets_a = a.children(1); //facets_a.hiddencolor = -1; // //mkdir('/' + sSerialNumber); //mkdir('/' + sSerialNumber + '/imgs'); //xs2pdf(gcf(), pwd() + '\' + string(sSerialNumber) + '\imgs\' + string(sPartNumber) + '_'... // + string(sSerialNumber) + '_SLOPE_ERROR_FIT_XYZR.pdf'); ////////////////////////////////////////////////////////////////////////// ////////////////////////////////////////////////////////////////////////// ////////////////////////////////////////////////////////////////////////// vTS = datevec(now()); sTimeStampTemp = string(vTS(1:5)); for i = 1 : size(sTimeStampTemp, "*") sTimeStamp(i) = strcat(tokens(sTimeStampTemp(i), " "), ""); end /////////////////////////////////////////////Write RAW points to output folder sFileToSave = 'Surface_Points_' + [sTimeStamp(1)+sTimeStamp(2)+sTimeStamp(3)+sTimeStamp(4)+sTimeStamp(5)] + '.csv'; sTempFile = TMPDIR + "\" + sFileToSave; fFile = mopen(sTempFile, 'wt'); for i=1:size(M_Actual, 1) - 1 mfprintf(fFile, "%f.6, %f.6, %f.6, %f.6, %f.6, %f.6\n", M_Actual(i, 1), M_Actual(i, 2), M_Actual(i, 3), M_Actual(i, 4), M_Actual(i, 5), M_Actual(i, 6)); end mfprintf(fFile, "%f.6, %f.6, %f.6, %f.6, %f.6, %f.6", M_Actual($, 1), M_Actual($, 2), M_Actual($, 3), M_Actual($, 4), M_Actual($, 5), M_Actual($, 6)); mclose(fFile); dos('move ' + sTempFile + ' ' + pwd() + '\' + string(sSerialNumber) + '\' + sFileToSave);
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//(13.6) A mixture of 1 kmol of gaseous methane and 2 kmol of oxygen initially at 25C and 1 atm burns completely in a closed, rigid container. Heat transfer occurs until the products are cooled to 900 K. If the reactants and products each form ideal gas mixtures, determine (a) the amount of heat transfer, in kJ, and (b) the final pressure, in atm. //solution //variable initialization nCH4 = 1 //moles of methane in kmol nO2 = 2 //moles of oxygen in kmol T1 = 25 //in degree celcius p1 = 1 //in atm T2 = 900 //in kelvin Rbar = 8.314 //universal gas constant //The chemical reaction equation for the complete combustion of methane with oxygen is //CH4 + 2O2 ----> CO2 + 2H2O //part(a) //with enthalpy of formation values from table A-25 hfbarCO2 = -393520 hfbarH2O = -241820 hfbarCH4 = -74850 //with enthalpy values from table A-23 deltahbarCO2 = 37405-9364 deltahbarH2O = 31828-9904 Q = ((hfbarCO2 + deltahbarCO2)+2*(hfbarH2O + deltahbarH2O) - hfbarCH4) + 3*Rbar*(T1+273-T2) printf('the amount of heat transfer in kJ is: %f',Q) //part(b) p2 = p1*(T2/(T1+273)) //in atm printf('\nthe final pressure in atm is: %f',p2)
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//Problem 22.05: A 3-phase, 60 Hz induction motor has 2 poles. If the slip is 2% at a certain load, determine (a) the synchronous speed, (b) the speed of the rotor and (c) the frequency of the induced e.m.f.’s in the rotor. //initializing the variables: p = 2/2; // number of pairs of poles f = 60; // in Hz s = 0.02; // slip //calculation: //ns is the synchronous speed, f is the frequency in hertz of the supply to the stator and p is the number of pairs of poles. ns = f/p //The the rotor runs at nr = ns*(1 - s) //frequency of the e.m.f.’s induced in the rotor bars is fr = ns - nr printf("\n\n Result \n\n") printf("\n(a) synchronous speed is %.0f rev/sec",ns) printf("\n(b) rotor speed is %.1f rev/sec",nr) printf("\n(c) frequency of the e.m.f.’s induced in the rotor bars is is %.1f Hz",fr)
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//All the quantities are expressed in SI units alpha1 = 4; alpha2 = -1.1; alpha3 = -4; cl_1 = 0.55; //cl at alpha1 cl_2 = 0; //cl at alpha2 c_m_qc1 = -0.005; //c_m_qc at alpha1 c_m_qc3 = -0.0125; //c_m_qc at alpha3 //the lift slope is given by a0 = (cl_1 - cl_2)/(alpha1-alpha2); //the slope of moment coefficient curve is given by m0 = (c_m_qc1 - c_m_qc3)/(alpha1-alpha3); //from eq.4.71 x_ac = -m0/a0 + 0.25; printf("\nRESULTS\n--------\nThe location of the aerodynamic center is\n x_ac = %1.3f\n",x_ac)
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MFCLCK_f.sci
function [x,y,typ]=MFCLCK_f(job,arg1,arg2) x=[];y=[];typ=[]; select job case 'plot' then standard_draw(arg1) graphics=arg1(2); [orig,sz]=graphics(1:2) xstringb(orig(1),orig(2),['M. freq';'clock'],sz(1),sz(2),'fill') case 'getinputs' then [x,y,typ]=standard_inputs(arg1) case 'getoutputs' then [x,y,typ]=standard_outputs(arg1) case 'getorigin' then [x,y]=standard_origin(arg1) case 'set' then x=arg1; graphics=arg1(2);label=graphics(4) model=arg1(3);dt=model(8) nn=model(9) [ok,label,dt,nn]=getvalue('Set Multifrequency clock parameters',.. ['Block label';'basic period (1/f)';'multiply by (n)'],.. list('str',1,'vec',1,'vec',1),[label;string(dt);string(nn)]) if ok then model(9)=nn model(8)=dt; hh=model(11);hh(2)=dt<>0;model(11)=hh graphics(4)=label x(2)=graphics;x(3)=model end case 'define' then model=list('mfclck',0,0,1,2,[],0,0,2,'d',[%f %f],[%f %f]) x=standard_define([2 2],model) end
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Ex1_24.sce
// Ex 24 Page 366 clc;clear;close; // Given b=3;//cm a=4.5;//cm f=9*10**9;//Hz v=3*10**10;//cm/s lamda=v/f;//cm printf("\n For TE10 mode:") m=1;// for TE10 mode lamda_c = 2*a/m;//cm rho=sqrt(1-(lamda/lamda_c)**2) lamda_g=lamda/rho;//cm vg=rho*v;//cm/s vp=v/rho;//cm/s ZTE=120*%pi/rho;//ohm printf("\n cutoff wavelength = %.f cm",lamda_c) printf("\n guide wavelength = %.2f cm",lamda_g) printf("\n Group velocity = %.1e m/s",vg/100) printf("\n Phase velocity = %.1e m/s",vp/100) printf("\n Characteristic wave impedence = %.f ohm",ZTE) printf("\n\n For TM11 mode:") m=1;n=1// for TE10 mode lamda_c = 2/sqrt((m/a)**2+(n/b)**2);//cm rho=sqrt(1-(lamda/lamda_c)**2) lamda_g=lamda/rho;//cm vg=rho*v;//cm/s vp=v/rho;//cm/s ZTM=120*%pi*rho;//ohm printf("\n cutoff wavelength = %.f cm",lamda_c) printf("\n guide wavelength = %.2f cm",lamda_g) printf("\n Group velocity = %.1e m/s",vg/100) printf("\n Phase velocity = %.1e m/s",vp/100) printf("\n Characteristic wave impedence = %.f ohm",ZTM)
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FOSSEE/Scilab-TBC-Uploads
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ch2_9.sci
// calculation of hysterisis and eddy current losses clc; P1=1500; f1=50; P2=3000; f2=75; A=[1 50;1 75]; //P/f=A+B*f B=[30;40]; v=A\B; disp('at 50Hz'); P_h=v(1)*f1;disp(P_h,'hysterisis loss(W)'); P_e=v(2)*f1^2;disp(P_e,'eddy current loss(W)'); disp('at 75Hz'); P_h=v(1)*f2;disp(P_h,'hysterisis loss(W)'); P_e=v(2)*f2^2;disp(P_e,'eddy current loss(W)');
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/323/CH4/EX4.17/4_17.sci
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4_17.sci
funcprot(0) function [polar] = rect2polar(x,y) //Function to convert rectangular coordinates to polar coordinates polar=ones(1,2) polar(1)=sqrt((x^2)+(y^2)) polar(2)=atan(y/x) polar(2)=(polar(2)*180)/%pi endfunction clc Po=200*10^3 //Output Power f=50 //frequency in hertz Vl=440 n=91 //efficiency pf=0.86 Vph=Vl //For a delta connected load //Since the efficiency and output power have been given in the question, the input power can be easily calculated Pi=(Po/n)*100 printf("\n Input power=%.2f kW \n",Pi*10^-3) //Since the input power is now known we can calculate the line current Il=Pi/(sqrt(3)*Vl*pf) printf("\n Il=%.1f A \n",Il) Iph=Il/sqrt(3) printf("\n Iph=%.1f A \n",Iph) apc=Iph*pf //Active component of phase current printf("\n Active component of phase current=%.1f A \n",apc) rpc=Iph*sqrt(1-pf^2) printf("\n Reactive component of phase current=%.1f A \n",rpc)
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/1931/CH7/EX7.17/17.sce
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17.sce
clc clear //INPUT DATA x=6.40*10^7//electrical conductivity in mho m^-1 t=300//temperature of copper in k L=2.44*10^-8//Lorentz number in W ohm K^-2 //CALCULATION K=x*t*L//thermal conductivity of copper in W m^-1 K^-1 //OUTPUT printf('The thermal conductivity of copper is %3.2f W.m^-1.K^-1',K)
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Chapter14_example7.sce
clc clear //Input data M=2300//Magnetization in A/m B=0.00314//Flux density in Wb/m^2 uo=(4*3.14)*10^-7//Permeability of free space in H/m //Calculations H=(B/uo)-M//Magnetizing force in A/m ur=(M/H)+1//Relative permeability //Output printf('The magnetizing force is %3.0f A/m \n The relative permeability is %3.1f',H,ur)
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3_9.sce
clc //initialisation of variables g= 32.2 //ft/sec^2 d= 12 //in h= 0.1 //m w= 240 //r.p.m W= 62.4 //lbft/sec^2 //CALCULATIONS P= (%pi*(d/24)^4*W*(2*%pi*4)^2)/(4*g) Pt= P+%pi*(d/24)^2*W*(h/12) //RESULTS printf (' Total pressure on bottom of cylinder = %.3f Lb ',Pt)
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Example2_3.sce
//Chapter-2,Example2_3,pg 2_12 n=4 Vofs=15 Res=Vofs/((2^n)-1) D=bin2dec('0110')//decimal equivalent Vo=Res*D printf("output voltage\n") printf("Vo=%.2f V",Vo)
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/1943/CH4/EX4.5/Ex4_5.sce
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Ex4_5.sce
clc clear //Input data C=83.7;//The amount of carbon present in the fuel oil according to ultimate analysis of a fuel oil in % H=12.7;//The amount of hydrogen present in the fuel oil according to ultimate analysis of a fuel oil in % O=1.2;//The amount of oxygen present in the fuel oil according to ultimate analysis of a fuel oil in % N=1.7;//The amount of nitrogen present in the fuel oil according to ultimate analysis of a fuel oil in % S=0.7;//The amount of sulphur present in the fuel oil according to ultimate analysis of a fuel oil in % td=27;//The dry bulb temperature of combustion air in degree centigrade tw=21;//The wet bulb temperature of combustion air in degree centigrade E=0.3;//Excess air and assuming complete combustion in % t=200;//Temperature to find total volume of combustion products in degree centigrade p=1.013;//Pressure to find total volume of combustion procucts in bar //Calculations Wth=(11.5*(C/100))+[34.5*((H/100)-(O/100)*(1/8))]+(4.3*(S/100));//Theoretical air required per kg of fuel in kg WA=(1+E)*Wth;//Actual air required per kg of fuel in kg/kg fuel sh=0.0132;//Specific humidity at DBT and WBT in kg moisture/kg dry air W=WA*sh;//Water vapour entering with air per kg fuel in kg vap/kg fuel Tw=(9*(H/100))+WA;//Total water vapour formed per kg fuel in kg CO2=(44/12)*(C/100);//mass of carbondioxide gas per kg of fuel O2=0.232*E*Wth;//Mass of oxygen gas per kg of fuel N2=0.768*(1+E)*Wth+(N/100);//Mass of nitrogen gas per kg of fuel SO2=(64/32)*(S/100);//Mass of nitrogen gas per kg of fuel H2O=1.383;//Mass of water per kg of fuel M=(CO2/44)+(O2/32)+(N2/28)+(SO2/64)+(H2O/18);//Moles of combustion gases formed per kg fuel VG=M*22.4*[(273+t)/273]*(1.013/1.013);//Volume of flue gases at 200 degree centigrade and 1.013 bar per kg fuel CO21=((CO2/44)/[(CO2/44)+(O2/32)+(N2/28)])*100;//Composition of dry flue gas CO2 by volume O21=((O2/32)/[(CO2/44)+(O2/32)+(N2/28)])*100;//Composition of dry flue gas O2 by volume N21=((N2/28)/[(CO2/44)+(O2/32)+(N2/28)])*100;//Composition of dry flue gas N2 by volume //Output printf('(a)The total volume of combustion products at 200 degee centigrade and 1.013 bar = %3.2f m^3 \n (b)The dry flue gas analysis based on carbondioxide,oxygen and nitrogen is \n Carbondioxide = %3.2f percent \n Oxygen = %3.2f percent \n Nitrogen = %3.2f percent',VG,CO21,O21,N21)
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ex4_15.sce
//Page Number: 4.17 //Example 4.15 clc; //Given //x(t)=10cos(wct+3sinwmt) //Comparing with standard equation B=3; fm=1D+3; //hz fb=2*(B+1)*fm; //(a)fm is doubled fma=2*fm; fba=2*(B+1)*fma; disp(fba,"fb with 2fm: "); //(b)fm is one halved fmb=fm/2; fbb=2*(B+1)*fmb; disp(fbb,"fb with 0.5fm: ");
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/Run and Gun.sce
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Run and Gun.sce
Name=Run and Gun PlayerCharacters=Player BotCharacters=Counter-Striker Bot PEEKER.bot;Counter-Striker Bot PEEKER.bot IsChallenge=false Timelimit=60.0 PlayerProfile=Counter-Striker AddedBots=Counter-Striker Bot PEEKER.bot;Counter-Striker Bot PEEKER.bot PlayerMaxLives=0 BotMaxLives=0;0 PlayerTeam=1 BotTeams=1;1 MapName=Lijiang-CC.map MapScale=5.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=true TimeRefilledByKill=5.0 ScoreToWin=100.0 ScorePerDamage=0.0 ScorePerKill=100.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=true ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Run'n and Gun'n WeaponHeroTag=Pistol and a Rifle DifficultyTag=4 AuthorsTag=Mdog864 BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=true Description=Move through the map gunning down anything that moves! Work on small clip high damage 6 shooter, or 30 rounds spraying targets with the Scar. GameVersion=1.0.8.0 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false [Aim Profile] Name=cs MinReactionTime=0.18 MaxReactionTime=0.3 MinSelfMovementCorrectionTime=0.007 MaxSelfMovementCorrectionTime=0.035 FlickFOV=10.0 FlickSpeed=1.0 FlickError=3.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=90.0 MinRecenterTime=0.25 MaxRecenterTime=0.4 OptimalAimFOV=35.0 OuterAimPenalty=1.1 MaxError=35.0 ShootFOV=1.0 VerticalAimOffset=-5.0 MaxTolerableSpread=2.0 MinTolerableSpread=0.0 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=Counter-Striker Bot PEEKER DodgeProfileNames=cs peek DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=10.0 DodgeProfileMinChangeTime=0.1 WeaponProfileWeights=1.5;1.5;1.5;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=cs;cs;cs;cs;cs;Default;Default;Default WeaponSwitchTime=5.0 UseWeapons=true CharacterProfile=Counter-Striker SeeThroughWalls=true NoDodging=false NoAiming=false [Character Profile] Name=Player MaxHealth=500.0 WeaponProfileNames=Six Shooter;SCAR;Bow & Arrow;;;;; MinRespawnDelay=3.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.75 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=1.0 MovementType=Base MaxSpeed=1100.0 MaxCrouchSpeed=250.0 Acceleration=6000.0 AirAcceleration=16000.0 Friction=7.5 BrakingFrictionFactor=1.25 JumpVelocity=800.0 Gravity=2.5 AirControl=1.0 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=true EnemyBodyColor=X=0.468 Y=0.195 Z=0.095 EnemyHeadColor=X=0.847 Y=0.012 Z=0.018 TeamBodyColor=X=0.016 Y=0.440 Z=0.072 TeamHeadColor=X=0.016 Y=0.440 Z=0.072 BlockSelfDamage=true InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=true AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=250.0 MainBBRadius=35.0 MainBBHasHead=true MainBBHeadRadius=25.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=250.0 ProjBBRadius=35.0 ProjBBHasHead=true ProjBBHeadRadius=25.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.5 JetpackFullFuelTime=1000.0 JetpackFuelIncPerSec=100.0 JetpackFuelRegensInAir=true JetpackThrust=6000.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=5.0 BlockedSpawnRadius=256.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=200.0 HealthRegenPerSec=25.0 HealthRegenDelay=7.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Character Profile] Name=Counter-Striker MaxHealth=100.0 WeaponProfileNames=pistol;M4A4;Projectile Rifle;Six Shooter;SCAR;;; MinRespawnDelay=3.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.75 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=1.0 MovementType=Base MaxSpeed=1100.0 MaxCrouchSpeed=250.0 Acceleration=6000.0 AirAcceleration=16000.0 Friction=7.5 BrakingFrictionFactor=1.25 JumpVelocity=800.0 Gravity=2.5 AirControl=1.0 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=true EnemyBodyColor=X=0.468 Y=0.195 Z=0.095 EnemyHeadColor=X=0.847 Y=0.012 Z=0.018 TeamBodyColor=X=0.016 Y=0.440 Z=0.072 TeamHeadColor=X=0.016 Y=0.440 Z=0.072 BlockSelfDamage=true InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=true AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=250.0 MainBBRadius=35.0 MainBBHasHead=true MainBBHeadRadius=25.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=250.0 ProjBBRadius=35.0 ProjBBHasHead=true ProjBBHeadRadius=25.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.5 JetpackFullFuelTime=1000.0 JetpackFuelIncPerSec=100.0 JetpackFuelRegensInAir=true JetpackThrust=6000.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=5.0 BlockedSpawnRadius=256.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=200.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Dodge Profile] Name=cs peek MaxTargetDistance=10000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.125 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.01 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.25 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=1.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.0 BlockedMovementReactionMax=0.125 [Weapon Profile] Name=Six Shooter Type=Hitscan ShotsPerClick=1 DamagePerShot=200.0 KnockbackFactor=0.1 TimeBetweenShots=0.5 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=6 AmmoPerShot=1 ReloadTimeFromEmpty=1.5 ReloadTimeFromPartial=1.5 DamageFalloffStartDistance=2200.0 DamageFalloffStopDistance=4500.0 DamageAtMaxRange=20.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.5 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=true DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Quake/Source ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=5.0 MinRecoilUp=5.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=2 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=0.5 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.01 TriggerBotFOV=0.1 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Weapon Profile] Name=SCAR Type=Hitscan ShotsPerClick=1 DamagePerShot=25.0 KnockbackFactor=4.0 TimeBetweenShots=0.096 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=87000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=87000.000 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=0.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=30 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=None ProjectileGraphic=Arrow VisualLifetime=0.1 WallParticleEffect=None HitParticleEffect=Flare BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=0.01 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=0 DecalSize=20.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.2 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Quake/Source ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 Explosive=false Radius=100.0 DamageAtCenter=0.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=0.0,0.1,-1.0,0.0 SpreadSCA=0.0,0.1,-1.0,0.0 SpreadMSA=0.0,0.1,-1.0,0.0 SpreadMCA=0.0,0.1,-1.0,0.0 SpreadSSH=0.0,0.1,-1.0,0.0 SpreadSCH=0.0,0.1,-1.0,0.0 SpreadMSH=0.0,0.1,-1.0,0.0 SpreadMCH=0.0,0.1,-1.0,0.0 MaxRecoilUp=0.8 MinRecoilUp=0.8 MinRecoilHoriz=-0.6 MaxRecoilHoriz=0.6 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=Bow & Arrow Type=Projectile ShotsPerClick=1 DamagePerShot=125.0 KnockbackFactor=0.1 TimeBetweenShots=0.5 Pierces=false Category=Charge BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=29.0 ChargeStartVelocity=X=3500.000 Y=0.000 Z=150.000 ChargeTimeToAutoRelease=99.0 ChargeTimeToCap=0.5 ChargeMoveSpeedModifier=0.7 MuzzleVelocityMin=X=15000.000 Y=0.000 Z=150.000 MuzzleVelocityMax=X=15000.000 Y=0.000 Z=150.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=3 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=80.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Arrow VisualLifetime=0.5 WallParticleEffect=None HitParticleEffect=Blood BounceOffWorld=false BounceFactor=0.0 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=true DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Quake/Source ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.1 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=2 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=180.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=true VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Map Data]
25543e8ec7ab575aa053ed3ee5ec150b139f42f3
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/2777/CH4/EX4.16/Ex4_16.sce
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FOSSEE/Scilab-TBC-Uploads
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Ex4_16.sce
// ELECTRICAL MACHINES // R.K.Srivastava // First Impression 2011 // CENGAGE LEARNING INDIA PVT. LTD // CHAPTER : 4 : DIRECT CURRENT MACHINES // EXAMPLE : 4.16 clear ; clc ; close ; // Clear the work space and console // GIVEN DATA Out_hp = 20; // Output of the Motor in HP eta = 90/100; // Full load efficiency of the Motor V = 220; // Motor voltage in Volts ns = 5; // Number of the step of Starter Rf = 220; // Field Resistance in Ohms cr = 1.8; // Lowest Current rating is 1.8 times of the Full load current Cu = 5/100; // Total Copper loss is 5% of the Input // CALCULATIONS Out = 20 * 746; .. // Output of the Motor in Watt Inp = (Out/eta); // Input of the Motor in KiloWatt I = Inp/Rf; // Full-Load Current in Amphere Cu_l = Inp*Cu; // Total Copper loss in Watts olf = (V ^ 2)/Rf; // Ohmic loss in the Fiels in the Watts Acu = Cu_l - olf; // Armature Copper loss in Watts Ra = Acu/(I * I); // Armature Resistance in Ohms I2 = I * cr; // Lower Current in Amphere n = ns - 1; // Number of the Resistance gama = ( (I2 * Ra)/Rf ) ^ (1/(n + 1)); // Current Ratio I1 = I2/gama; // Initial Current in amphere R1 = V/I1; // Initial Resistance in Ohms R2 = gama * R1; // Initial Resistance in Ohms r1 = R1 - R2; // Graded Resistance in Ohms R3 = gama * R2; // Initial Resistance in Ohms r2 = gama * r1; // Graded Resistance in Ohms r3 = gama ^ 2 * r1; // Graded Resistance in Ohms r4 = gama ^ 3 * r1; // Graded Resistance in Ohms // DISPLAY RESULTS disp("EXAMPLE : 4.16 : SOLUTION :-") ; printf("\n (a) Graded Resistances are %.4f Ohms, %.4f Ohms, %.4f Ohms and %.4f Ohms \n",r1,r2,r3,r4);
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/SquareWaveFunc.sce
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santushtisharma10/AppliedMathematics_with_Scilab
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2023-05-29T04:40:42.507269
2021-06-04T13:25:58
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SquareWaveFunc.sce
clc; x = [1 2 3 4 5 6 7 8 9 10 ]; y = [5 0 5 0 5 0 5 0 5 0 ]; plot2d2(x,y) xlabel('VALUES OF x'); ylabel('VALUES OF y'); title('SQUARE WAVE FUNCTION');
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/3682/CH7/EX7.4/Ex7_4.sce
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FOSSEE/Scilab-TBC-Uploads
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Ex7_4.sce
// Exa 7.4 clc; clear; // Given data n=2; // Second order Butterworth filter fH=1000; // Lower cut off frequency(Hz) // Solution printf('Let C = 0.1 μF. \n'); C=0.1*10^-6; // Farads // Since fH = 1/(2 * %pi * R*C); // Therefore; R = 1/(2*%pi*fH*C); printf(' The calculated value of R = %.1f kΩ. \n',R/1000); printf(' From Table 7.1, for n=2, the damping factor alpha = 1.414.'); alpha=1.414; A0 = 3-alpha; printf('\n Then the pass band gain A0 = %.3f. \n',A0); printf('\n'); printf(' The transfer function of the normalized second order low-pass Butterworth filter is 1.586 '); printf('\n ----------------'); printf('\n Sn^2+1.414*Sn+1'); // Since Af= 1 + Rf/Ri = 1 + 0.586; printf('\n Since A0= 1.586 so Let Rf = 5.86 kΩ and Ri = 10 kΩ to make A0 = 1.586.' ); printf(' \n The circiuit realized is as shown in Fig. 7.4 with component value as mentioned above.'); printf('\n By considering minimum DC offset condition, the modified value of R and C comes out to be R = 1.85 kΩ and C=0.086 μF.'); printf('\n\n\n Frequency, f in Hz Gain magnitude in dB 20 log(vo/vi)\n'); // Frequency Response x=[0.1*fH,0.2*fH,0.5*fH,1*fH,5*fH,10*fH] for i = 1:1:6 response(i) = 20*log10(A0/(sqrt(1+(x(i)/fH)^4))); printf(' %d %.2f \n',x(i),response(i)); end
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/1088/CH2/EX2.1/Example1.sce
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Example1.sce
clear() clc disp('Example 1 : Display the current working shell ') disp('***************************************************************************') disp('Answer : ') printf('The current Working Shell is ') if (getos()=='Linux') then unix_w("echo $SHELL") else printf("%s",getshell()) end disp('***************************************************************************')
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/564/DEPENDENCIES/3_2data.sci
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sci
3_2data.sci
a=4;//major axis,in mm b=3;//minor axis of bar,in mm T=100000;//applied torque,in N.mm G=76923;//shear modulus,in N/mm^2
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//Example 5_4 clc(); clear; //To calculate the inter planar distance a=0.82 //units in nm b=0.94 //units in nm c=0.75 //units in nm h=1 k=2 l=3 d=1/sqrt((((h/a)^2)+((k/b)^2)+((l/c)^2))) //units in nm printf("The Distance between (1,2,3) planes and (2,4,6) planes is d123=%.2fnm and d246=%.2fnm",d,d/2) //In textbook the answer is printed wrong as d123=0.11nm and d246=0.055nm but the correct answers are d123=0.21nm and d246=0.11nm
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errcatch(-1,"stop");mode(2);//Example 3.16 : volume ; ; format('v',7) //given data : a=0.2665; // in mm c=0.4947;// in mm V=(3*sqrt(3)*a^2*c)/2; disp(V,"volume,V(mm^3) = ") exit();
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// Scilab code Ex3.2: Pg.125 (2008) clc; clear; T = 5800; // Temperature of sun, K b = 2.898e-003; // Wein's constant, m-K lamda_m = b/T; // Peak wavelength of solar spectrum, m printf("\nPeak wavelength of solar spectrum = %5.1f nm", lamda_m/1e-009); // Result // Peak wavelength of solar spectrum = 499.7 nm
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<?xml version="1.0" encoding="utf-8"?> <test> <description>3D homogeneous 1D Channel Flow, SEM parallelisation (2 proc)</description> <executable>IncNavierStokesSolver</executable> <parameters>ChanFlow_3DH1D_Parallel_mode1.xml</parameters> <processes>2</processes> <files> <file description="Session File">ChanFlow_3DH1D_Parallel_mode1.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="u" tolerance="1e-6">3.44241e-14</value> <value variable="v" tolerance="1e-6">2.09484e-13</value> <value variable="w" tolerance="1e-6">0</value> <value variable="p" tolerance="1e-6">4.8457e-11</value> </metric> <metric type="Linf" id="2"> <value variable="u" tolerance="1e-6">2.72504e-13</value> <value variable="v" tolerance="1e-6">3.29175e-13</value> <value variable="w" tolerance="1e-6">1.22076e-18</value> <value variable="p" tolerance="1e-6">1.33911e-10</value> </metric> </metrics> </test>
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//Example 2-8, Page No- 38 clear clc gain_dB = 40 pout_W= 100 pin_W = pout_W/10^4 printf('The input power is %.2f watt',pin_W);
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Turbomachinery Design and Theory,Rama S. R. Gorla and Aijaz A. Khan, Chapter 2, Example 8") //D2 is siameter in meter, N is rpm, Cr2 in m/s and Cw2=U2 in m/s , V velocity of flow in m/s D2 = 0.6; N = 550; Cr2 = 3.5; U2 = %pi*D2*N/60 Cw2 = U2 g = 9.81; V=2.5; disp("Head in meters from where water is being lifted is :") H = Cw2 * U2/ g - (V^2)/(2*g) //b2 is width //Qis discharge Q=piD2b2Cr2 in m3/s b2 = 0.082; disp("Discharge Q is in m3/s:") Q = %pi * D2 * b2 * Cr2 disp("Power P in Kilowatts is given as :") rho = 1000; //density of water 1000kg/m3 P = rho*g*Q*H/1000
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a^4*m11^2 - 2*a^2*b^2*m11^2 + b^4*m11^2 + 4*a^3*b*m11*m12 - 4*a*b^3*m11*m12 + 4*a^2*b^2*m12^2 + 2*a^4*m11*m13 - 2*b^4*m11*m13 + 4*a^3*b*m12*m13 + 4*a*b^3*m12*m13 + a^4*m13^2 + 2*a^2*b^2*m13^2 + b^4*m13^2 + a^4*m21^2 - 2*a^2*b^2*m21^2 + b^4*m21^2 + 4*a^3*b*m21*m22 - 4*a*b^3*m21*m22 + 4*a^2*b^2*m22^2 + 2*a^4*m21*m23 - 2*b^4*m21*m23 + 4*a^3*b*m22*m23 + 4*a*b^3*m22*m23 + a^4*m23^2 + 2*a^2*b^2*m23^2 + b^4*m23^2 - a^4*m31^2 + 2*a^2*b^2*m31^2 - b^4*m31^2 - 4*a^3*b*m31*m32 + 4*a*b^3*m31*m32 - 4*a^2*b^2*m32^2 - 2*a^4*m31*m33 + 2*b^4*m31*m33 - 4*a^3*b*m32*m33 - 4*a*b^3*m32*m33 - a^4*m33^2 - 2*a^2*b^2*m33^2 - b^4*m33^2 getVariablePowers(a,b)=a^4 + a^3*b + a^2*b^2 + a*b^3 + b^4 groupBy(a,b)= + a^4*(m11^2 + 2*m11*m13 + m13^2 + m21^2 + 2*m21*m23 + m23^2 - m31^2 - 2*m31*m33 - m33^2) + 4*a^3*b*(m11*m12 + m12*m13 + m21*m22 + m22*m23 - m31*m32 - m32*m33) + 2*a^2*b^2*( - m11^2 + 2*m12^2 + m13^2 - m21^2 + 2*m22^2 + m23^2 + m31^2 - 2*m32^2 - m33^2) + 4*a*b^3*( - m11*m12 + m12*m13 - m21*m22 + m22*m23 + m31*m32 - m32*m33) + b^4*(m11^2 - 2*m11*m13 + m13^2 + m21^2 - 2*m21*m23 + m23^2 - m31^2 + 2*m31*m33 - m33^2)
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// Exa 3.8 clc; clear; close; // Given data V_BE= 0.7;// in V V_CE= 3;// in V I_C= 1;// in mA I_C=I_C*10^-3;// in A bita= 100; I_B= I_C/bita;// in A // V_CE= V_BE+V_CB and V_CB= I_B*R_B R_B= (V_CE-V_BE)/I_B;// in Ω disp(R_B*10^-3,"The value of R_B in kΩ is : ")
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//Exa_2.10 // TO find ABS/BH(average busy season per busy hour) calling rates, design cell capacity for the switch and design Erlangs. clc; clear all; Rlines=15000;//Residential lines Blines=80000;//Business lines PWElines=5000;//PBX, WATS, and Foreign Exchange (FX) lines CR_R=2;//Call rates for Rlines CR_B=3;// call rates for Blines CR_PWE=10;//call rates for PWElines HT_R=140;//average holding time for Rlines(sec) HT_B=160;//average holding time for Blines(sec) HT_PWE=200;//average holding time for PWE lines(sec) Slines=100000;// no of lines carried by switch HD_ABS=1.5;// HD/ABS for the switch //solution percentR_lines=Rlines/Slines; percentB_lines=Blines/Slines; percentPWE_lines=PWElines/Slines; CCSR=CR_R*HT_R/100; CCSB=CR_B*HT_B/100; CCSPWE=CR_PWE*HT_PWE/100; CR=CR_R*percentR_lines+CR_B*percentB_lines+CR_PWE*percentPWE_lines; printf('The call rate is %.1f calls per line \n ',CR); CCS=CCSR*percentR_lines+CCSB*percentB_lines+CCSPWE*percentPWE_lines; AvgHTperline=CCS*100/CR; ABS_BH_calls=CR*Slines; ABS_BH_usage=CCS/36*Slines; printf('Design cell capacity based on HD is %d calls \n',HD_ABS*ABS_BH_calls); printf(' DESIGN Erlangs based on HD is %d \n',round(HD_ABS*ABS_BH_usage));
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clear // //variable declaration P1=20.0 P2=30.0 P3=20.0 theta3=60.0*%pi/180.0 //Taking horizontal direction towards left as x axis and the vertical downward direction as y axis. ////sum of vertical Fy & sum of horizontal forces Fx is zero //Assume direction of Fx is right //Assume direction of Fy is up Fx=20.0*cos(theta3) Fy=P1+P2+P3*sin(theta3) R=sqrt((Fx**2)+(Fy**2)) printf("\n R= %0.4f KN",R) alpha=atan(Fy/Fx)*180/%pi printf("\n alpha= %0.2f °",alpha) //moment at A MA=P1*1.5+P2*3.0+P3*sin(theta3)*6.0 //The distance of the resultant from point O is given by: d=MA/R x=d/sin(alpha*%pi/180) printf("\n x= %0.3f m",x)
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A = 0.5; Na = 10^17; p0 = Na; ni = 1.5*10^10; dp = 5*10^16; x = 10^-5; up = 500; Tp = 10^-10; kT = 0.0259; q0 = 1; q = 1.6*10^-19; Dp = kT*up/q0; Lp = sqrt(Dp*Tp); p = p0 + dp*exp(-x/Lp); E = kT*log(p/ni); E0 = 1.1/2 + E; Ip = q*A*Dp*dp*exp(-x/Lp)/Lp; Qp = q*A*dp*Lp; Qp0 = Qp*10^6; disp(E0,"steady state separation between Fp and Ec (in eV)=") disp(Ip,"hole current (in ampere)=") disp(Qp,"excess stored hole charge (in coulomb)=") disp(Qp0,"excess stored hole charge (in micro-coulomb)=")
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clc // Given that P_in = 100 // power of input signal in mW P_out = 50 // power of output signal in mW // Sample Problem 12 on page no. 280 printf("\n # PROBLEM 12 # \n") alpha = (10 * log10(P_in / P_out))//calculation for absorption coefficient printf("\n Standard formula used \n alpha=10/L*log(Pi/Po).\n") printf("\n Attenuation loss is %f dB. ",alpha)
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clc clear close deff('y2dot=f(ydot,y)','y2dot=-4*y-0.8*ydot'); y(1)=5e-3; ydot(1)=0; y2dot(1)=f(ydot(1),y(1)); dt=.05; t=0:dt:10; for i=2:length(t) ydot(i)=ydot(i-1)+dt*y2dot(i-1); y(i)=y(i-1)+dt*ydot(i-1); y2dot(i)=f(ydot(i),y(i)); end Y=[y ydot y2dot]; // [azul,verde,vermelho] X=[t' t' t']; plot(X,Y)
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clc clear //Initialization of variables dH=-2369859 //Btu r=1.986 //Gas constant dn=5.5 //Change in number of moles T=536.7 //R //calculations dQ=dH+dn*r*T //results printf("Higher heating value = %d Btu",dQ)
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syms R1 R2 R3 C1 C2 C3 L1 L2 s; T1=1/(R3*(R1+s*L1)*(R2+s*L2)*C1*C2*C3*s^3) L1=-1/(s*(R1+s*L1)*C1); L2=-1/(s*(R2+s*L2)*C1); L3=1/(-(s*L2+R2)*s*C2); L4=1/(-s*R3*C2) L5=-1/(s*R3*C3) delta=1-(L1+L2+L3+L4+L5)+(L1*L3 + L1*L4 + L1*L5 + L2*L4 + L2*L5 + L3*L5)-(L1*L3*L5) del1=1; TF=(T1*del1)/delta ; disp(TF,"Vo/VI = ")
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Example5_11.sce
clear; clc; printf("\t Example 5.11\n"); Q=14; //steady heat transfer,W D=0.06; //diameter of heat source,m l=0.3;; // length of source below surface ,m T=308; //temperature of heat source,K T1=294; //temperature of surface,K k=(Q/(T-T1))*(1-(D/2)/(D*10))/(4*3.14*D/2)+0.025; // thermal conductivity of soil printf("\t thermal conductivity is : %.3f W/(m*K)\n",k); //end
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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 13.11w //calculation of the velocity of the water coming out of the opening //given data AA=.5//area(in m^2) of the tank AB=1*10^-4//area(in m^2) of the cross section at the bottom m=20//mass(in kg) of the load h=50*10^-2//height(in m)of the water level g=10//gravitational acceleration(in m/s^2) of the earth rho=1000//density of the water(in kg/m^3) //calculation //from the equation............P = P0 + (h*rho*g)//pressure at the bottom r=m*g/AA//in above equation it is the value of (h*rho*g) //on solving,we get............PA = P0 + (400 N/m^2) //from Bernoulli equtation.....P1 + (rho*g*h1) + (rho*v1^2/2) = P2 + (rho*g*h2) + (rho*v2^2/2) //we get vB=sqrt((2*(r+(rho*g*h)))/rho) printf('the velocity of the water coming out of the opening is %3.1f m/s',vB)
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Ch02Ex7.sci
// Scilab Code Ex2.7 Bond formation Energy for K+ and Cl- ion pair: Page-70 (2010) eps_0 = 8.854D-12; // Absolute electrical permittivity of free space, coulomb sqaure per newton per metre square e = 1.6D-19; // Electronic charge, C IP_K = 4.1; // Ionization potential of potassium, electron-volt EA_Cl = 3.6; // Electron affinity of chlorine, electron-volt delta_E = IP_K - EA_Cl; // Net energy required to produce the ion-pair, electron-volt Ec = delta_E; // Coulomb energy equals net energy required to produce the ion pair, in electron-volt // Since Ec = -e/(4*%pi*eps_0*R), solving for R R = -e/(4*%pi*eps_0*Ec); // Separation between K+ and Cl- ion pair, m disp(Ec,"The bond formation energy for K+ and Cl- ion pair, in eV, is : "); disp(R/1D-10, "The separation between K+ and Cl- ion pair, in angstrom, is : "); //Result // The bond formation energy for K+ and Cl- ion pair, in eV, is : // 0.5 // The separation between K+ and Cl- ion pair, in angstrom, is : // - 28.760776
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ex3_12.sce
// Exa 3.12 clc; clear; close; // Given data N_A = 2*10^16;// in /cm^3 N_D = 10^16;// in /cm^3 C = N_A-N_D;// in /cm^3 disp(C,"Carrier concentration in holes/cm^3 is");
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ex_3_12.sce
//example no. 3.12 //solve system by decomposition method A=[1 1 -1;2 2 5;3 2 -3] b=[2;-3;6] // hence we can observe that LU decomposition method fails to solve this system since the pivot L(2,2)=0; //we note that the coefficient matrix is not a positive definite matrix and hence its LU decomposition is not guaranteed, //if we interchange the rows of A as shown below the LU decomposition would work, A=[3 2 -3;2 2 5;1 1 -1] b=[6;-3;2] [U,L]=LandU(A,3) // call LandU function to evaluate U,L of A, n=3; Z=fore(L,b); X=back(U,Z)
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Ex4_32.sce
clc; Vt=230;//Supply voltage P=4;//No of poles A=2;//No of parallel paths for armature conductors Z=500;//No of armature conductors Ra=0.2;//armature circuit resistance in ohm Rs=0.1;//field resistance in ohm Il=40;//line current N=1000;//rated speed in rpm Ia1=40;//armature current for dc series motor at 40 A line current Ia2=20;//armature current for dc series motor at 20 A line current //For 40A line current Ea1=Vt-Ia1*(Ra+Rs);//counter emf //For 20A line current Ea2=Vt-Ia2*(Ra+Rs);//counter emf //Let, phi_1=flux at 40 A, phi_2=flux at 20 A line current //phi_2=0.6*(phi_1) //(Ea1/Ea2)=(n1*phi_1)/(n2*phi_2) //(218/224)=(1000*(phi_1))/(n2*(0.6*(phi_1)) n2=(1000*224)/(218*0.6);//speed of motor at line current of 20 A at 230 V printf('Speed of motor at line current of 20 A at 230 V is %f rpm.',round(n2));
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9_1_1.sce
clc //initialisation of variables d= 1.6 //lb/ft^3 vk= 6.2*10^-6 //ft^2/sec R= 1.8 //lbf v= 100 //ft/sec d1= 64 //lb/ft^3 vk1= 1.7*10^-5 //ft62/sec l= 10 //ft //CALCULATIONS u= v*vk1/(vk*l) u1= v*vk1/(vk*l*1.98) r= d1*l^2*(u/100)^2/d F= r*R //RESULTS printf (' resistance= %.f lbf ',F)
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clf; c=3.986e+5; function[y]=f16(x,u) y(1)=u(2); y(2)=-c*u(1)/((u(1)^2+u(3)^2)^(3/2)); y(3)=u(4); y(4)=-c*u(3)/((u(1)^2+u(3)^2)^(3/2)); endfunction T=2*24*60*60; //Q1 teta=linspace(0,2*%pi,1001); r=6400; plot2d(r*cos(teta),r*sin(teta),2); y0=[6400+35786;0;0;3.07]; t=linspace(0,T,5001); y=ode(y0,0,t,f16); comet(y(1,:),y(3,:))
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split.tst
## Test the split command set echo set interactive set quiet read <mergeinfo.svn :6 split at 2 prefer git inspect
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Ex2_2.sce
//Example 2.2, page 49 clc h=6.63*10^-34//Joule-sec vo=5.6*10^14 w=h*vo printf("\npower is %e per sec",w) ev=(1/(1.6*10^-19)) wo=w*ev printf("\nEnergy is %f ev",wo)
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ex2_37.sce
errcatch(-1,"stop");mode(2);//Caption:In a dc machine calculate speed at which the induced emf will be 250 Volts and also calculate the increase in main flux of field in percentage for induced emf of 250 Volts and speed 700 rpm //Exam:2.37 ; ; E_1=220;//Primary emf(in Volts) N_1=750;//Speed of the machine at 220 Volts E_2=250;//Secondary emf(in Volts) N_2=(E_2/E_1)*N_1;//Speed of the machine at which emf will be 250 Volts disp(N_2,'Speed of the machine at which emf will be 250 Volts='); N_3=700;//Speed of the machine when main field flux increase E_3=250;//induced emf when flux increase(in Volts) F_x=(E_3/E_2)*(N_2/N_3);//Ratio of flux when speed is N_3 and N_2 F=(F_x-1)*100;//Percentage change in flux for induced emf of 250 Volts and speed 700 rpm(in %) disp(F,'Percentage change in flux when induced emf 250 Volts and speed 700 rpm(in %)='); exit();
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EX5_14.sce
//chapter 5 //example 5.14 //page 443 clear; clc; disp("example 5.14"); disp("star connected alternator") printf("\n"); KVA=1500; //rating ph=3; //3-phase V_l=6600; //voltage Ra=0.4 //armature resistance Xs=6; //reactance Ia=(KVA*1000)/(sqrt(3)*V_l); printf("Full-load current= %d A\n",Ia); V=V_l/sqrt(3); printf("Voltage per phase=%d V\n",V); disp("for 0.8 lagging power facor"); pf=0.8; //power factor phi=acosd(pf); E=sqrt((V*cosd(phi)+Ia*Ra)^2+(V*sind(phi)+Ia*Xs)^2) printf("induced emf=%f V\n\n",E); disp("then at 0.8 leading power factor"); Vt=4743; //solved manually printf("termial Voltage, line-to-line=%d V\n",(sqrt(3)*Vt))
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dgn=figure('figure_position',[300,300],'figure_size',[300,300],'auto_resize','on','background',[27],'figure_name','Design Metrics'); delmenu(dgn.figure_id,gettext('File')) delmenu(dgn.figure_id,gettext('?')) delmenu(dgn.figure_id,gettext('Tools')) delmenu(dgn.figure_id,gettext('Edit')) toolbar(dgn.figure_id,'off') dgn.color_map = hotcolormap(32) handles.dummy = 0; handles.Power=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.26,0.86,0.22,0.14],'Relief','flat','SliderStep',[0.01,0.1],'String','Power','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Power','Callback',''); handles.Power_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.41,0.86,0.28,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Power_val','Callback',''); handles.Power_w=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','bold','ForegroundColor',[0,0,0],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.7,0.86,0.22,0.14],'Relief','flat','SliderStep',[0.01,0.1],'String','W','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Power_w','Callback',''); handles.Area=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','bold','ForegroundColor',[0,0,0],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.15,0.76,0.7,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','FPAA Area Percentage Utilized','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Area','Callback',''); handles.Area_Si=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.03,0.64,0.22,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','Elements','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Area_Si','Callback',''); handles.AreaSi_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.25,0.63,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','AreaSi_val','Callback',''); handles.AreaSi_per=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[16],'FontUnits','points','FontWeight','bold','ForegroundColor',[0,0,0],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.35,0.64,0.05,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','%','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','AreaSi_per','Callback',''); handles.Area_Tile1=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.43,0.64,0.1,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','CAB','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Area_Tile1','Callback',''); handles.AreaTile_val1=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.54,0.63,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','AreaTile_val1','Callback',''); handles.AreaTile_per1=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[16],'FontUnits','points','FontWeight','bold','ForegroundColor',[0,0,0],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.64,0.64,0.15,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','%','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','AreaTile_per1','Callback',''); handles.Area_Tile2=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.71,0.64,0.1,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','CLB','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Area_Tile2','Callback',''); handles.AreaTile_val2=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.82,0.63,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','AreaTile_val2','Callback',''); handles.AreaTile_per2=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[16],'FontUnits','points','FontWeight','bold','ForegroundColor',[0,0,0],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.92,0.64,0.4,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','%','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','AreaTile_per2','Callback',''); handles.Enum=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','bold','ForegroundColor',[0,0,0],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.033,0.52,0.93,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','Number of Individual FPAA Components','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Enum','Callback',''); handles.Eota=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.08,0.4,0.11,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','OTA','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Eota','Callback',''); handles.Eota_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.19,0.39,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Eota_val','Callback',''); handles.Efgota=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.36,0.4,0.18,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','FGOTA','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Efgota','Callback',''); handles.Efgota_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.54,0.39,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Efgota_val','Callback',''); handles.Ecap=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.71,0.4,0.1,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','CAP','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Ecap','Callback',''); handles.Ecap_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.82,0.39,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Ecap_val','Callback',''); handles.Enfet=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.06,0.22,0.13,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','NFET','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Enfet','Callback',''); handles.Enfet_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.19,0.22,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Enfet_val','Callback',''); handles.Epfet=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.36,0.22,0.13,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','PFET','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Epfet','Callback',''); handles.Epfet_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.49,0.22,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Epfet_val','Callback',''); handles.Etgate=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.65,0.22,0.17,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','TGATE','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Etgate','Callback',''); handles.Etgate_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.82,0.22,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Etgate_val','Callback',''); handles.Enmirror=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.06,0.05,0.23,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','NMIRROR','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Enmirror','Callback',''); handles.Enmirror_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.29,0.05,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Enmirror_val','Callback',''); handles.Eble=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.44,0.05,0.13,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','BLE','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Eble','Callback',''); handles.Eble_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.54,0.05,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Eble_val','Callback',''); handles.Efg=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,1],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.68,0.05,0.1,0.12],'Relief','flat','SliderStep',[0.01,0.1],'String','FGs','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Efg','Callback',''); handles.Efg_val=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,1],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[14],'FontUnits','points','FontWeight','normal','ForegroundColor',[0,0,0],'HorizontalAlignment','center','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.78,0.05,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Efg_val','Callback',''); handles.Efg_per=uicontrol(dgn,'unit','normalized','BackgroundColor',[1,1,0.4],'Enable','on','FontAngle','normal','FontName','mukti narrow','FontSize',[16],'FontUnits','points','FontWeight','bold','ForegroundColor',[0,0,0],'HorizontalAlignment','left','ListboxTop',[],'Max',[1],'Min',[0],'Position',[0.88,0.05,0.1,0.13],'Relief','flat','SliderStep',[0.01,0.1],'String','%','Style','text','Value',[0],'VerticalAlignment','middle','Visible','on','Tag','Efg_per','Callback','');
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/2138/CH3/EX3.9/ex_3_9.sce
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ex_3_9.sce
//Example 3.9 // resistance and current clc; clear; close; //given data : V=240; // voltage in volts r1=2; // resistance in ohm r2=3; // resistance in ohm r3=8.8; // resistance in ohm r4=10; // resistance in ohm r5=3; // resistance in ohm R1=(r1*r2)/(r1+r2); // equivalent resistance of parallel branch R2=R1+r3; // equivalent resistance of section ABC R3=(R2*r4)/(R2+r4); R=R3+r5; // total resistance of section AD I=V/R; V1=I*r5; // voltage drop across r5 V2=V-V1; // voltage drop across section ABC I1=V2/r4; // current flowing through r4 resistance I2=I-I1; // current in r3 resistance V3=I2*r3; // voltage drop across r3 resistance, section ABC V4=V2-V3; // voltage drop between section AB I3=V4/r1; // current flowing through r1 resistance I4=V4/r2; // current flowing through r2 resistance disp(I3,"current flowing through r1 (2 ohms) resistance,I3(A) = ") disp(I4,"current flowing through r2 (3 ohms)resistance,I4(A) = ") disp(R,"total resistance,R(ohm) = ") disp(V1,"voltage drop across r5(3 ohms) resistance,V1(V) = ") disp(V2,"voltage drop across section ABC,V2(V) = ") disp(V3,"voltage drop across r3 resistance(8.8 ohms),V3(V) = ") disp(V4," voltage drop between section AB,V4(V) = ")
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/172/CH11/EX11.1/ex1.sce
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ex1.sce
//Ques 1 //To determine the efficiency of Rankine cycle clc clear //1-Inlet state of pump //2-Exit state of pump P2=2000;//Exit pressure in kPa P1=10;//Inlet pressure in kPa v=0.00101;//specific weight of water in m^3/kg wp=v*(P2-P1);//work done in pipe in kJ/kg h1=191.8;//Enthalpy in kJ/kg from table h2=h1+wp;//enthalpy in kJ/kg //2-Inlet state for boiler //3-Exit state for boiler h3=2799.5;//Enthalpy in kJ/kg //3-Inlet state for turbine //4-Exit state for turbine //s3=s4(Entropy remain same) s4=6.3409;//kJ/kg sf=0.6493;//Entropy at liquid state in kJ/kg sfg=7.5009;//Entropy difference for vapor and liquid state in kJ/kg x4=(s4-sf)/sfg;//x-factor hfg=2392.8;//Enthalpy difference in kJ/kg for turbine h4=h1+x4*hfg;//Enthalpy in kJ/kg nth=((h3-h2)-(h4-h1))/(h3-h2); printf('Percentage efficiency = %.1f ',nth*100);
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/2339/CH8/EX8.23.1/Ex8_23.sce
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Ex8_23.sce
clc clear V1=5; P1=1; P2=5; n=1.25; Em=0.9; IP=[n/(n-1)]*[P1*100*V1/60]*[((P2/P1)^((n-1)/n))-1]; SP=IP/Em; printf('Shaft Power: %3.1f kW',SP); printf('\n'); IsoP=P1*100*V1*(log(P2/P1))*(1/60); Eo=IsoP/SP; printf('Overall Efficiency: %3.0f Percent',Eo*100); printf('\n');
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clc clear //input data u=2800 //rocket speed in m/s Cj=1400 //effective exhaust velocity in m/s mp=5 //propellent flow rate in kg/s q=6500 //heat of propellent per kg of propellant mixture in kJ/kg //calculation s=u/Cj //effective jet speed ratio np=(2*s)/(1+s^2) //propulsive efficiency F=Cj*mp*10^-3 //thrust in kN Pt=F*10^3*u*10^-6 //Thrust power in MW, F in N Pe=Pt/np //engine outputin MW nth=Pe*10^3/(mp*q) //thermal efficiency, Pe in kW no=np*nth //overall efficiency //output printf('(A)propulsive efficiency is %3.1f \n (B)propulsive power is %3.1f MW\n (C)engine outut is %3.1f MW\n (D)thermal efficiency is %3.4f \n (E)overall efficiency is %3.3f',np,Pt,Pe,nth,no)
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/2498/CH2/EX2.22/ex2_22.sce
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ex2_22.sce
// Exa 2.22 clc; clear; close; format('v',7) // Given data V_L = 25;// in V I_L = 200;// in mA I_L = I_L * 10^-3;// in A R_L = V_L/I_L;// in ohm Gamma = 3/100; //Gamma = 1/(6*sqrt(2)*(omega^2)*L*C); f = 50;// in Hz omega = 2*%pi*f;// in rad/sec //LC = 1/( 6*sqrt(2)*(omega^2)*Gamma ) L = R_L/(3*omega);// in H disp(L,"The value of L in H is"); C = 1/( 6*sqrt(2)*(omega^2)*Gamma*L );// in F C = C * 10^6;// in µF disp(C,"The value of C in µF is");
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clc; clear; format('v',6); V1=60; V2=20; r1=2; //in cm r2=6; //in cm r=4; //in cm disp("where A and B are constants.","V=A*ln(r)+B","The potential V as a function of coordinates is "); disp("B=85.2","A=-36.4","using the given data,we get"); V=-36.4*log(r)+85.2; disp(V,"The potential at r=4 cm,V(in volt)=");
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/libs/lib_interLinear.sce
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// Topografia IV // Allan Turini Speroto 78233 // Fernando Martins Pimenta 80018 // Gabriel Batista Freitas 82718 // Matheus Lopes Vieira 80020 // Funções para o processamento da interseção linear function [Lb, Xa, sigma_d_xy] = getParams(Xp, Yp) /* Retorna os vetores Lb, Xa e sigma_d_xy Lb: vetor das observações injuncionadas Xa: vetor dos parâmetros injuncionados sigma_d_xy: vetor dos desvios padrão das distâncias e coordenadas */ for i = 1:num.dists Lb(i) = dist(i).dist; sigma_d_xy(i) = dist(i).stdd; end for i = 1:num.coords py = 2*i+num.coords px = py-1 //inj(i).X inj(i).Y Lb(px) = inj(i).X; Lb(py) = inj(i).Y; sigma_d_xy(px) = inj(i).stdd_x sigma_d_xy(py) = inj(i).stdd_y end Xa = [Xp;Yp;Lb(num.dists+1:length(Lb))]; endfunction function [CLb, P] = getMVC_P(varianciaPriori, sigma_d_xy) CLb = diag(sigma_d_xy^2); P = varianciaPriori*inv(CLb); endfunction function F = inters_linear_2D_red(Xa) /* Retorna o modelo funcional das distâncias F: resultado do modelo funcional (Distâncias + Injunções) */ for i = 1:num.coords px = 2*i+1; py = px+1; dx(i) = Xa(px) - Xa(1); dy(i) = Xa(py) - Xa(2); D(i) = sqrt(dx(i)^2 + dy(i)^2); end //Injunções for i = 1:(num.coords) px = 2*i+1; py = px+1; n = 2*i-1; I(n) = Xa(px); I(n+1) = Xa(py); end F = [D; I] endfunction function [X0] = getX0(Lb, Xa, pos) /* Retorna o vetor de parametros X0 */ dx = Lb(num.dists+3)-Lb(num.dists+1); dy = Lb(num.dists+4)-Lb(num.dists+2); D = sqrt(dx^2 + dy^2); Az = azimute(dx, dy); aux1 = D^2+(Lb(1)^2)-(Lb(2)^2); aux2 = 2*D; S = sqrt(4*(D^2)*Lb(1)^2-aux1^2); if pos ~= 'esquerda' // ponto à direita de A-> B X0(1) = Lb(num.coords+1) + aux1*sin(Az)/aux2 + S*cos(Az)/aux2; X0(2) = Lb(num.coords+2) + aux1*cos(Az)/aux2 - S*sin(Az)/aux2; else X0(1) = Lb(num.coords+1) + aux1*sin(Az)/aux2 - S*cos(Az)/aux2; X0(2) = Lb(num.coords+2) + aux1*cos(Az)/aux2 + S*sin(Az)/aux2; end X0 = [X0; Xa(3:length(Xa))]; endfunction function [varianciaPosteriori] = getVarPost(V, P, GL) /* Retorna a variância à posteriori */ varianciaPosteriori = (V'*P*V)/GL; endfunction function X_quad(var_pri, var_post, nc, gl,fig) /* Executa o teste de X-quadrado var_pri: variância a priori var_post: variância a posteriori nc: nível de confiança gl: graus de liberdade fig: objeto onde será plotado o resultado do teste (info_bar) */ X_calc = var_post*gl/var_pri; niv_sig = 1 - nc /100; lim_esq = 0.5*niv_sig; lim_dir = 1-lim_esq; [X_inf] = cdfchi("X", gl, lim_esq, lim_dir); [X_sup] = cdfchi("X", gl, lim_dir, lim_esq); if (X_calc> X_inf & X_calc < X_sup) then fig.info_message=msprintf("Hipótese básica, H0: %3.0f = %8.3f, NÃO REJEITADA ao nível de significância de %3.0f%%", var_pri, var_post, 100*niv_sig); else fig.info_message=msprintf("Hipótese básica, H0: %3.0f = %8.3f, REJEITADA ao nível de significância de %3.0f%%", var_pri, var_post, 100*niv_sig); end endfunction function geraGrafico(handles, Xa, MVCxy) /* Plota o gráfico na interface e as elipses dos erros Xa: Vetor com as coordenadas ajustadas MCVxy: Matriz variância covariância das coordenadas ajustadas */ handles.grafico.visible = 1; //Cria vetores com apenas as coordenasdas X e Y for i=1:(length(Xa)-2)/2 px = 2*i+1; py = px+1; vetx(i) = Xa(px); vety(i) = Xa(py); end // Extensão do gráfico Xmin = -min(abs(vetx))-1000; Ymin = -min(abs(vety))-1000; Xmax = max(abs(vetx))+1000; Ymax = max(abs(vety))+1000; plot2d(Xp,Yp,-1,"031", " ", [Xmin, Ymin, Xmax, Ymax]); for i=1:(length(Xa)-2)/2 xstring(vetx(i), vety(i), inj(i).ponto); end // Plotagem dos vértices e alinhamestos xpoly(vetx, vety, "lines", 1); xy = get("hdl"); xy.mark_background=1; xy.foreground=1; xy.thickness=1; xy.mark_style=6; xy.mark_size=4; xy.closed = 'off'; // Plotagem dos vértices em relação ao ponto p for i=1:(length(Xa)-2)/2 px = 2*i+1; py = px+1; vetxp(1) = Xa(1); vetyp(1) = Xa(2); vetxp(2) = Xa(px); vetyp(2) = Xa(py); xpoly(vetxp, vetyp, "lines", 1); xyp = get("hdl"); xyp.mark_background=1; xyp.foreground=1; xyp.thickness=1; xyp.line_style=6; xyp.closed = 'off'; end //Desenha as elipses absolutas for i=1:length(Xa)/2 py=2*i; px= py-1; MVCponto = MVCxy(px:py, px:py); // Matriz 2x2 [ae(i), be(i), aza(i)] = error_elipse(MVCponto, nc); draw_elipse(Xa(px), Xa(py), ae(i), be(i), aza(i)); end // Plotagem do ponto p xpoly(Xa(1), Xa(2), "marks"); p = get("hdl"); p.mark_background=1; p.foreground=0; p.mark_style=9; p.mark_size=1; xstring(Xa(1), Xa(2), "p"); endfunction
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clear; clc; disp("--------------Example 3.15---------------") printf("Another example of a nonperiodic composite signal is the signal received by an old-fashioned analog black-and-white TV.\n"); s=30; // screen is scanned 30 times per second //screen resolution = 525 x 700 vl=525; hl=700; pixels=vl*hl; // total number of pixels pixels_per_second=pixels*s; // pixels scanned per second cycles_per_second=pixels_per_second/2; // 2 pixels per cycle in the worst-case scenario i.e alternating black and white pixels bandwidth = cycles_per_second*10^-6; b7=bandwidth*0.7; // 70% of the bandwidth final =ceil(b7); // final rounded bandwidth // display the result printf("The bandwidth needed in the worst-case scenario i.e alternating black and white pixels where we need to represent \none color by the minimum amplitude and the other color by the maximum amplitude is %5.4f MHz.\n\n",bandwidth); printf("This worst-case scenario has such a low probability of occurrence that the assumption is that we need only 70 percent\nof this bandwidth, which is %3.2f MHz. Since audio and synchronization signals are also needed, a %d MHz bandwidth\nhas been set aside for each black and white TV channel.\nAn analog color TV channel has a 6-MHz bandwidth.",b7,final);
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//Example 13.5 //Stirlings Central Difference Derivatives //Page no. 426 clc;close;clear; printf(' x\t\t y\t\t d\t\t d2\t\t d3\n') printf('---------------------------------------------------------------------------') h=0.01;s=0.5; deff('y=f1(x,s)','y=((z(x,3)+z(x-1,3))/2+s*z(x-1,4)+(z(x-1,5)+z(x-2,5))*(3*s^2-1)/12)/h') deff('y=f2(x,s)','y=(z(x-1,4))/h^2') deff('y=f3(x,s)','y=(z(x-1,5)+z(x-2,5))/(2*h^3)') z=[1.00,1.00000;1.01,1.00499;1.02,1.00995;1.03,1.01489;1.04,1.01980;1.05,1.02470;1.06,1.02956;1.07,1.03441;1.08,1.03923;1.09,1.04403;1.10,1.04881;1.11,1.05357;1.12,1.05830;1.13,1.06301;1.14,1.06771;1.15,1.07238;1.16,1.07703]; for i=3:5 for j=1:19-i z(j,i)=z(j+1,i-1)-z(j,i-1) end end printf('\n') for i=1:17 for j=1:5 if z(i,j)==0 then printf(' \t') else printf('%.7f\t',z(i,j)) end end printf('\n') end printf('\n\ny1(1.125) = %g (exact value = 0.4771404)',f1(13,0.5)) printf('\n\ny2(1.125) = %g (exact value = -0.20951)',f2(13,0.5)) printf('\n\ny3(1.125) = %g (exact value = 0.27935)',f3(13,0.5))
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//Example6.13 // Determine the time constant of the integrator clc; clear; close; Vo = 20 ; t = 1*10^-3 ; VI = -1 ; // at t =0 ; // The output voltage of an integrator is define as RC = t/10 ; disp(' The time constant of the given filter is RC = '+string(RC)+ ' sec '); R = 1*10^3 ; // we assume C = RC/R ; disp('The capacitor value is = '+string(C)+ ' F');
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// Function dlyapchol //lyapunov equation a =[-0.25 0.25; 0.6 -0.4]; b=[1.5442;0]; r=dlyapchol(a,b) //generalized lyapunov equation a =[-0.25 0.25; 0.6 -0.4]; b=[1.5442;0]; e=[11 22 ;33 44]; r1=dlyapchol(a,b,e)
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// Example No. 2.16 // To find the length of DCF so that the pulse width (FWHM) at the output of the DCF is twice the pulse width at the input of the TF // Page No. 84 clc; clear; // Given data beta2TF=-21*(10^(-12))^2; // Dispersion coefficient of transmission fiber in s^2/km beta2DCF=130*(10^(-12))^2; // Dispersion coefficient of dispersion compensating fiber in s^2/km LTF=80; // Length of transmission fiber in km TFWHM=12.5*10^(-12); // Full-width at half-maximum T0=TFWHM/1.665; // Half-width // The length of required DCF LDCF1=(sqrt(3)*T0^2-beta2TF*LTF)/beta2DCF; // Length of dispersion compensating fiber in km LDCF2=(-sqrt(3)*T0^2-beta2TF*LTF)/beta2DCF; // Length of dispersion compensating fiber in km // Displaying the result in command window printf('\n The length of DCF so that the pulse width (FWHM) at the output of the DCF is twice the pulse width at the input of the TF = %0.2f km',LDCF1); printf(' or = %0.2f km',LDCF2);
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// Calculate the range of readings clc; fsd=1000; TP=100; Efsd=(1/100)*1000; disp(Efsd,'magnitude of Error when specified in terms of full scale deflection (w)=') disp('Thus the meter will read between 90W and 110W') Etv=(1/100)*100; disp(Etv,'magnitude of Error when specified in terms of true value (w)=') disp('Thus the meter will read between 99W and 101W')
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//example2.3 clc disp("Consider shunt generator as shown in the fig 2.29") disp("I_a=(I_L)+(I_sh)") disp("I_sh=(V_t)/(R_sh)") disp("Now, V_t=250 V") disp("and, R_sh=100 ohm") i=250/100 disp(i,"Therefore, I_sh(in A)=") disp("Load power=5 kW") disp("Therefore, P=(V_t)*(I_L)") i=(5*10^3)/250 disp(i,"I_L(in A)=P/(V_t)=") i=20+2.5 disp(i,"(I_a)[in A]=(I_L)+(I_sh)=") disp("E=(V_t)+((I_a)*(R_a))[neglect V_brush]") E=250+(22.5*0.22) disp(E,"Therefore, E(in V)=") disp("This is the induced emf to supply the given load.")
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//Example No. 4_03 //Pg No. 64 clear ; close ; clc ; a = 0.1 b = 0.4 for i = 1:8 afrac(i) = floor(a*2) a = a*2 - floor(a*2) bfrac(i) = floor(b*2) b = b*2 - floor(b*2) end afrac_s = '0' + '.' + strcat(string(afrac)) //string form binary equivalent of a i.e 0.1 bfrac_s = '0' + '.' + strcat(string(bfrac)) mprintf('\n 0.1_10 = %s \n 0.4_10 = %s \n ', afrac_s , bfrac_s) for j = 8:-1:1 summ(j) = afrac(j) + bfrac(j) if summ(j) > 1 then summ(j) = summ(j)-2 afrac(j-1) = afrac(j-1) + 1 end end summ_dec = 0 for k = 8:-1:1 summ_dec = summ_dec + summ(k) summ_dec = summ_dec*1/2 end disp(summ_dec,'sum =') disp('Note : The answer should be 0.5, but it is not so.This is due to the error in conversion from decimal to binary form.')
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clc VLB=2400 //line to base voltage in volts Ix=2005 //current in amperes xda=VLB/(sqrt(3)*Ix) mprintf("xda=%fΩ\n",xda)//ans may vary due to roundoff error Ifv=116 //current in amperes ma1=VLB/(sqrt(3)*Ifv)//equal to ma` in textbook mprintf("má=V1B/Ifv=%fΩ\n",ma1)//ans may vary due to roundoff error //from ex 2_7 V1=VLB/sqrt(3) //reference phasor in volts kVAB=9375 //rated kVA I1B=(kVAB*1000)/(sqrt(3)*VLB)//current in amperes pf=0.8 //power factor I1=I1B*exp((-1)*%i*(acos(pf)))//current in amperes Ef=V1+%i*I1*xda disp('Ef='+string(Ef)+'V')//ans may vary due to roundoff error mprintf("If=|Ef|/má=%fA\n",abs(Ef)/ma1)//ans may vary due to roundoff error Voc=2960 //line to line volatge in Volts mprintf("V1oc=%fV\n",Voc/sqrt(3))//ans may vary due to roundoff error If=240 //current in amperes Efmax=ma1*If mprintf("Efmax=%dV\n",Efmax)//ans in textbook is wrong I1max=(Efmax-V1)/xda //ans in textbook is wrong mprintf("I1max=%fA\n",I1max)//ans may vary due to roundoff error mprintf("Qmax=%fMVAR",sqrt(3)*VLB*I1max*(10^-6))//ans may vary due to roundoff error
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//Example_a_9_6 page no:406 clc; Vl=400; Vrnmag=400/sqrt(3); Vrnang=0; Vynmag=400/sqrt(3); Vrnang=-120; Vbnmag=400/sqrt(3); Vrnang=-240; R=10; omega=314; L=1; C=100*10^-6; Yph=(1/R)+(1/(%i*omega*L))+(%i*omega*C); Iph=Vrnmag*Yph;//multiplication of Vrnmag and Yph is rounded off in text book so output line current varies sligthly Iphmag=sqrt(real(Iph)^2+imag(Iph)^2); Iphang=atand(imag(Iph)/real(Iph)); P=sqrt(3)*Vl*Iphmag*cosd(Iphang); pf=cosd(Iphang); disp(Iphmag,"the magnitude of line current is (in A)"); disp(Iphang,"the angle of line current is (in degree)"); disp(P,"the power is (in W)"); disp(pf,"the power factor is"); //multiplication of Vrnmag and Yph is rounded off in text book so output line current varies sligthly //Iphmag and Iphang are rounded off in text book so calculated power varies with the textbook
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// Variable Declaration TMS = 0.5 //Time multiplier setting I_f = 5000.0 //Fault current(A) CT = 500.0/5 //CT ratio set_plug = 1.0 //Relay plug set I_relay = 5.0 //Rated relay current(A) // Calculation Section PSM = I_f/(CT*set_plug*I_relay) //Plug setting multiplier T1 = 1.0 //Time of operation for obtained PSM & TMS of 1 from graph.Refer Fig 14.22 T2 = TMS*3/T1 //Time of operation(sec) // Result Section printf('Operating time of the relay = %.1f sec' ,T2)
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<?xml version="1.0" encoding="utf-8"?> <test> <description>3D channel flow, Hexahedral elements, P=3, Successive RHS(5), par(2)</description> <executable>IncNavierStokesSolver</executable> <parameters>--use-scotch Hex_channel_m3_srhs.xml</parameters> <processes>2</processes> <files> <file description="Session File">Hex_channel_m3_srhs.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="u" tolerance="1e-8">4.54205e-13</value> <value variable="v" tolerance="1e-8">5.92873e-13</value> <value variable="w" tolerance="1e-8">2.56712e-12</value> <value variable="p" tolerance="1e-8">8.8739e-11</value> </metric> <metric type="Linf" id="2"> <value variable="u" tolerance="1e-8">1.89675e-12</value> <value variable="v" tolerance="1e-8">2.84934e-12</value> <value variable="w" tolerance="1e-8">1.51304e-11</value> <value variable="p" tolerance="1e-8">3.4398e-10</value> </metric> </metrics> </test>
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// Example 4.15, page no-156 clear clc p=10000 //power fed to the antenna in W ag=60 //Antenna gain loss=2 //Power lossin feed system adb=10*log10(p) EIRP=adb+ag-loss printf("Earth station EIRP = %ddB",EIRP)
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clc //initialisation of variables r= 82.4 //ohms k= 0.002768 //ohm^-1 R1= 326 //ohm //CALCULATIONS K= r*k K1= (K/R1) //RESULTS printf ('cell constant= %.4f cm^-1',K) printf ('\n specific conductance= %.3e ohm^-1 cm^-1',K1)
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function [txt]=indentsci(txt) // //! // Copyright INRIA bl=' ' txt=bl(ones(prod(size(txt)),1))+txt
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errcatch(-1,"stop");mode(2);//Initilization of variables W=32.2 //lb T=120 //lb m=1 //slug r=6/12 //ft //Calculations w=sqrt((T*(3/5)*4)/(m*r*3)) //rad/s //Result printf('The angular speed permissible is %f rad/s',w) exit();
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errcatch(-1,"stop");mode(2);//Chapter 12 //page no 432 //given ; all; Pt1=-18; //in dBm for 50/125 micron fiber Pt2=-10; //in dBm for 100/125 micron fiber Pd=Pt1-Pt2; printf("\n Additional Power = %0.0f dBm",Pd); exit();
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function out=S2(x,p) somme=0; for i=0:p somme=somme+cos((2*i+1)*x)/(2*i+1)^2; end out=%pi/2-somme*4/%pi; endfunction //pas de discontinuite, donc pas d'effet Gibbs clf; x=linspace(-%pi,%pi,10000); n=100; plot(x,S2(x,n)); title("n=100");
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# vio_chsize.tst # # (virtual IO: operations that change file size) # read 0 5716 1.tmp expect 0 5716 0 compare_file 1.tmp data1.dat # shrink file set_size 0x1500 expect 0 read 0x1400 0x100 1.tmp expect 0 0x100 0 compare_file 1.tmp result13.dat read 0x1400 0x100 1p.tmp portion expect 0 0x100 0 compare_file 1p.tmp result13.dat read 0x1400 0x100 1b.tmp iobuf expect 0 0x100 0 compare_file 1b.tmp result13.dat read 0x1400 0x100 1bp.tmp iobuf portion expect 0 0x100 0 compare_file 1bp.tmp result13.dat read 0x1400 0x200 2.tmp expect 0x800000CA 0 0 read 0x1400 0x200 2p.tmp portion expect 0 0x100 0 compare_file 2p.tmp result13.dat read 0x1400 0x200 2b.tmp iobuf expect 0x800000CA 0 0 read 0x1400 0x200 2bp.tmp iobuf portion expect 0 0x100 0 compare_file 2bp.tmp result13.dat # grow file set_size 0x2000 expect 0 get_size expect 0 0x2000 read 0x1584 0xD0 3.tmp expect 0 0xD0 0 compare_file 3.tmp result3.dat read 0x1584 0xD0 3p.tmp portion expect 0 0xD0 0 compare_file 3p.tmp result3.dat read 0x1584 0xD0 3b.tmp iobuf expect 0 0xD0 0 compare_file 3b.tmp result3.dat read 0x1584 0xD0 3bp.tmp portion iobuf expect 0 0xD0 0 compare_file 3bp.tmp result3.dat # read block at the end of real IO read 0x1584 0x100 4.tmp expect 0 0x100 0 compare_file 4.tmp result14.dat read 0x1584 0x100 4p.tmp portion expect 0 0x100 0 compare_file 4p.tmp result14.dat read 0x1584 0x100 4b.tmp iobuf expect 0 0x100 0x0 compare_file 4b.tmp result14.dat read 0x1584 0x100 4bp.tmp iobuf portion expect 0 0x100 0x0 compare_file 4bp.tmp result14.dat # read block at the end of virtual IO read 0x1F00 0x100 5.tmp expect 0 0x100 0 compare_file 5.tmp zero256.dat read 0x1F00 0x100 5p.tmp portion expect 0 0x100 0 compare_file 5p.tmp zero256.dat read 0x1F00 0x100 5b.tmp iobuf expect 0 0x100 0x0 compare_file 5b.tmp zero256.dat read 0x1F00 0x100 5bp.tmp iobuf portion expect 0 0x100 0x0 compare_file 5bp.tmp zero256.dat # read block overlapping end of virtual IO read 0x1F00 0x200 6.tmp expect 0x800000CA 0 0 read 0x1F00 0x200 6p.tmp portion expect 0 0x100 0 compare_file 6p.tmp zero256.dat read 0x1F00 0x200 6b.tmp iobuf expect 0x800000CA 0 0 read 0x1F00 0x200 6bp.tmp iobuf portion expect 0 0x100 0x0 compare_file 6bp.tmp zero256.dat # read block past the end of virtual IO read 0x2000 0x100 7.tmp expect 0x800000CA 0 0 read 0x2000 0x100 7p.tmp portion expect 0 0 0 read 0x2000 0x100 7b.tmp iobuf expect 0x800000CA 0 0 read 0x2000 0x100 7bp.tmp iobuf portion expect 0 0 0x0 # auto-grow file by writing past EOF write 0x4000 data3.dat expect 0 0x2000 get_size expect 0 0x6000 read 0x4000 0x2000 8.tmp expect 0 0x2000 0 compare_file 8.tmp data3.dat read 0x4000 0x2000 8p.tmp portion expect 0 0x2000 0 compare_file 8p.tmp data3.dat read 0x4000 0x2000 8b.tmp iobuf expect 0 0x2000 0x0 compare_file 8b.tmp data3.dat read 0x4000 0x2000 8bp.tmp iobuf portion expect 0 0x2000 0x0 compare_file 8bp.tmp data3.dat # read past new EOF read 0x4000 0x3000 9.tmp expect 0x800000CA 0 0 read 0x4000 0x3000 9p.tmp portion expect 0 0x2000 0 compare_file 9p.tmp data3.dat read 0x4000 0x3000 9b.tmp iobuf expect 0x800000CA 0 0 read 0x4000 0x3000 9bp.tmp iobuf portion expect 0 0x2000 0x0 compare_file 9bp.tmp data3.dat # shrink file and grow it again, the data should be cleared set_size 0x5F00 expect 0 get_size expect 0 0x5F00 set_size 0x6000 expect 0 get_size expect 0 0x6000 read 0x5F00 0x100 10_1.tmp expect 0 0x100 0 compare_file 10_1.tmp zero256.dat read 0x5F00 0x100 10_1p.tmp portion expect 0 0x100 0 compare_file 10_1p.tmp zero256.dat read 0x5F00 0x100 10_1b.tmp iobuf expect 0 0x100 0x0 compare_file 10_1b.tmp zero256.dat read 0x5F00 0x100 10_1bp.tmp iobuf portion expect 0 0x100 0x0 compare_file 10_1bp.tmp zero256.dat # this data should be retained read 0x5E00 0x100 10_2.tmp expect 0 0x100 0 compare_file 10_2.tmp data4.dat read 0x5E00 0x100 10_2p.tmp portion expect 0 0x100 0 compare_file 10_2p.tmp data4.dat read 0x5E00 0x100 10_2b.tmp iobuf expect 0 0x100 0x0 compare_file 10_2b.tmp data4.dat read 0x5E00 0x100 10_2bp.tmp iobuf portion expect 0 0x100 0x0 compare_file 10_2bp.tmp data4.dat set_size 0x2000 expect 0 get_size expect 0 0x2000 read 0x4000 0x2000 10.tmp expect 0x800000CA 0 0 read 0x4000 0x2000 10p.tmp portion expect 0 0 0 read 0x4000 0x2000 10b.tmp iobuf expect 0x800000CA 0 0 read 0x4000 0x2000 10bp.tmp iobuf portion expect 0 0 0x0 set_size 0x6000 expect 0 get_size expect 0 0x6000 read 0x4000 0x100 11.tmp expect 0 0x100 0 compare_file 11.tmp zero256.dat read 0x4000 0x100 11p.tmp portion expect 0 0x100 0 compare_file 11p.tmp zero256.dat read 0x4000 0x100 11b.tmp iobuf expect 0 0x100 0x0 compare_file 11b.tmp zero256.dat read 0x4000 0x100 11bp.tmp iobuf portion expect 0 0x100 0x0 compare_file 11bp.tmp zero256.dat
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function lagrangre() endfunction
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//Example 4.10.a//total load of lights and fans clc; clear; close; lp=50;//no. of light points lw=60;//wattage of light points fp=20;//no. of fan points fw=100;//wattage of fan points wpp=10;//no. of wall plug points wppw=60;//wattage of wall plug points bp=5;//no. of bell points bpw=40;//wattage of bell points ppp=8;//power plug points pppw=5000;//wattage of power plug points lpw=lp*lw;//wattage of 50 lamps fpw=fp*fw;//wattage of 20 fans wpppw=wpp*wppw;//wattage of wall plug points bpww=bp*bpw;//wattage of bell points tl=lpw+fpw+wpppw+bpww;//total wattage disp(tl,"total wattage of lightning load is in watts ")
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//Force P required to raise the load eta=0.70 W=2500 //N //refer fig. 6.17 //For third order pulley //VR=2^2-1 //For whole system VR=3+3 P=W/(eta*VR) //N printf("Required force p=%.2f N",P)
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//exapple 1.25 clc; funcprot(0); // Initialization of Variable time=4+20/60+30/3600; accn=time*9.8565/3600;//acceleration stime=time+accn;//sideral time disp("local mean time in past midnight observed:"); a=modulo(stime*3600,60); printf("seconds %.3f",a); b=modulo(stime*3600-a,3600)/60; printf(" minutes %i",b); c=(stime*3600-b*60-a)/3600; if c>24 then c=c-24; end printf(" hours %i",c);
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CSpeech_Session2_SDL.sce
####### INITIATION ####### # Initiation of the scenario and the main PCL-file scenario = "CSpeech"; scenario_type = fMRI_emulation;# set to fMRI at the scanner! pcl_file = "CSpeech_Session1_MAIN.pcl"; pulse_code = 255; pulses_per_scan = 1; scan_period = 2000; write_codes = true; default_output_port = 1; # !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! # !! at the scanner, uncomment all lines with port_code (use search function) #!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! # the resolution of the screen/ adapt to fit projector screen_height = 768; screen_width = 1024; screen_bit_depth = 32; # keep SDL as simple as possible and stay clear of the parallel port response_matching = simple_matching; response_port_output = true; active_buttons = 4; button_codes = 1,2,3,4; # 1 = ENTER-exp-subj # 2 yes # 3 no # 4 SPACEBAR-exp # basic colours and fonts default_background_color = 82,82,82; # grey as in PPM, adjust to picture background default_font = "arial"; default_font_size = 20; default_text_color = 0,0,0; # black default_text_align = align_center; ######### BEGIN ########## begin; ########################## picture {} default; # blank screen picture { box { height = 3; width = 30; color = 0, 0, 0; } horz_s; x = 0; y = 0; box { height = 30; width = 3; color = 0, 0, 0; } vert_s; x = 0; y = 0; box { height = 3; width = 3; color = 255, 255, 255; } dot_s; x = 0; y = 0; } fixation; # fixation cross picture { text { caption = " "; } t_info1; x = 0; y = 50; text { caption = " "; } t_info2; x = 0; y = 0; text { caption = "Druk [ENTER] om door te gaan of [Esc] om te onderbreken. "; } t_info3; x = 0; y = -50; } p_info; # text picture { text { caption = "Wachten op de scanner... "; } t_countdown; x = 0; y = 0; } p_countdown; # countdown picture for when the scanner is collecting 30 volume-weighting volumes before the exp. starts. ######## GENERAL PICTURES ######## picture { text {caption = "Welkom bij dit experiment. De eerste taak duurt ongeveer drie kwartier (4 delen met 3x pauze), de tweede taak duurt ook ongeveer drie kwartier, en tot slot maken we een anatomische scan van tien minuten. Als eerste komt nu een kalibratie van de oogcamera. OK (wijsvinger) >"; } t_instruction_1; x = 0; y = 0; } p_welcome; picture { text { caption = "Deel 1: Plaatjes Benoemen Je krijgt een serie plaatjes te zien. Het is de bedoeling dat je stil (in je hoofd) de plaatjes benoemt (dus: als je een vleermuis ziet, zeg je in je hoofd 'vleermuis'). Af en toe komt er na het plaatje een stip in beeld. Terwijl die stip er staat, moet je het woord hardop uitspreken. We nemen je respons op, spreek s.v.p. luid en duidelijk. (wijsvinger) >"; } t_instruction_naming_1; x = 0; y = 0; } p_instr_naming; picture { text { caption = "Je krijgt nu eerst een oefenronde, zodat je kunt wennen aan de taak in de scanner. Het is tijdens het hele experiment BELANGRIJK DAT JE JE BLIK IN HET MIDDEN HOUDT, op het kruis of de stip, ook als het plaatje komt. De plaatjes in de oefenronde zijn andere dan in het experiment. (wijsvinger) >"; } t_traininginstr_1; x = 0; y = 0; } p_instr_training; picture { text { caption = "Wil je nog een ronde oefenen? Druk wijsvinger voor ja, middelvinger voor nee."; } t_training_1; x = 0; y = 0; } p_training; picture { text { caption = "Prima! Druk wijsvinger om door te gaan met het experiment."; } t_training_1b; x = 0; y = 0; } p_aftertraining; picture { text { caption = "Bedankt! Deel 1 is klaar. Druk wijsvinger om door te gaan naar de instructies voor het tweede (laatste) deel."; } t_end_part11; x = 0; y = 0; } p_end_part1; picture { text { caption = "Deel 2: Kleur benoemen Nu ga je dezelfde plaatjes bekijken, maar dit keer zeg je in jezelf de typische kleur van het object (bijv. 'zwart' voor vleermuis of 'wit' voor sneeuwpop). Als de stip in beeld is moet je hetzelfde hardop zeggen. (wijsvinger) >"; } t_instruction_judgement_1; x = 0; y = 0; } p_instr_judgement; picture { text { caption = "PAUZE"; } t_pause_1a; x = 0; y = 30; text { caption = "Je hebt nu pauze. Blijf stil liggen s.v.p.";}t_pause_1b; x = 0; y = 0; text { caption = "De proefleider zal zo verdergaan met [ENTER].";}t_pause_1c; x = 0; y = -30; } p_pauze; picture { text { caption = "Oogkalibratie? [SPATIE] ja, [ENTER] nee."; } t_eyeQuest; x=0; y=0; } p_eyeQuest; picture { text { caption = "Het experiment is nu afgelopen. Bedankt voor het meedoen! Wij drukken straks op [ENTER]. Dan volgt nog één oogkalibratie, en tot slot de anatomische scan (10 minuten)."; } t_end_1; x = 0; y = 0; } p_end_1; ###################### for the eyetracker calibration ############################ trial { #instructions trial_duration = 5000; stimulus_event { picture{ text { caption = "Kalibratie oogcamera In deze taak moet je je blik op het kruisje fixeren "; } introtext; x=0;y=0; } textpic; code = "instr_text"; }instr_event; }text_eyetr; trial { #Show focus point trial_duration = 2000; stimulus_event { picture { box {height = 3; width = 30; color = 250, 250, 250;}horizontal; x=0;y=0; box {height = 30; width = 3; color = 250, 250, 250;}vertical; x=0;y=0; }cross; code = "calibr_cross"; port_code = 15; # needs to be there at scanner!! (for proper log file eyetracker) } crossevent; }eyetrial; ######## STIMULI ######### ##### sound file(s) ###### sound { wavefile { filename = "WAV-files\\Beep.wav"; preload = true;} w_beep; } s_beep; sound_recording { duration = 5000; use_date_time = false; } recording; ####### array that preloads all the pictures before starting the experiment ######### array { bitmap { filename = "pictures\\bat1_.jpg"; }bat1; bitmap { filename = "pictures\\box1_.jpg"; }box1; bitmap { filename = "pictures\\cactus1_.jpg"; }cactus1; bitmap { filename = "pictures\\cactus2_.jpg"; }cactus2; bitmap { filename = "pictures\\cactus3_.jpg"; }cactus3; bitmap { filename = "pictures\\carrot1_.jpg"; }carrot1; bitmap { filename = "pictures\\cherry1_.jpg"; }cherry1; bitmap { filename = "pictures\\cherry2_.jpg"; }cherry2; bitmap { filename = "pictures\\cherry3_.jpg"; }cherry3; bitmap { filename = "pictures\\crocodile1_.jpg"; }crocodile1; bitmap { filename = "pictures\\crocodile2_.jpg"; }crocodile2; bitmap { filename = "pictures\\crocodile3_.jpg"; }crocodile3; bitmap { filename = "pictures\\fire_truck1_.jpg"; }fire_truck1; bitmap { filename = "pictures\\fire_truck2_.jpg"; }fire_truck2; bitmap { filename = "pictures\\fire_truck3_.jpg"; }fire_truck3; bitmap { filename = "pictures\\frog1_.jpg"; }frog1; bitmap { filename = "pictures\\frog2_.jpg"; }frog2; bitmap { filename = "pictures\\frog3_.jpg"; }frog3; bitmap { filename = "pictures\\igloo1_.jpg"; }igloo1; bitmap { filename = "pictures\\lobster1_.jpg"; }lobster1; bitmap { filename = "pictures\\lobster2_.jpg"; }lobster2; bitmap { filename = "pictures\\lobster3_.jpg"; }lobster3; bitmap { filename = "pictures\\mouse1_.jpg"; }mouse1; bitmap { filename = "pictures\\pineapple1_.jpg"; }pineapple1; bitmap { filename = "pictures\\snowman1_.jpg"; }snowman1; bitmap { filename = "pictures\\strawberry1_.jpg"; }strawberry1; bitmap { filename = "pictures\\strawberry2_.jpg"; }strawberry2; bitmap { filename = "pictures\\strawberry3_.jpg"; }strawberry3; bitmap { filename = "pictures\\swan1_.jpg"; }swan1; bitmap { filename = "pictures\\tank1_.jpg"; }tank1; bitmap { filename = "pictures\\tank2_.jpg"; }tank2; bitmap { filename = "pictures\\tank3_.jpg"; }tank3; bitmap { filename = "pictures\\tomato1_.jpg"; }tomato1; bitmap { filename = "pictures\\tomato2_.jpg"; }tomato2; bitmap { filename = "pictures\\tomato3_.jpg"; }tomato3; bitmap { filename = "pictures\\tooth1_.jpg"; }tooth1; bitmap { filename = "pictures\\turtle1_.jpg"; }turtle1; bitmap { filename = "pictures\\turtle2_.jpg"; }turtle2; bitmap { filename = "pictures\\turtle3_.jpg"; }turtle3; } stimuli; ####### visual stimuli trials ######## picture { bitmap { filename = "Pictures\\empty.bmp"; preload = true; } b_target; #width = 222; height = 222; } b_target; x = 0; y = 0; box { height = 3; width = 30; color = 0, 0, 0; } horz_s_pic; x = 0; y = 0; box { height = 30; width = 3; color = 0, 0, 0; } vert_s_pic; x = 0; y = 0; box { height = 3; width = 3; color = 255, 255, 255; } dot_s_pic; x = 0; y = 0; } p_target; trial { trial_duration = stimuli_length; stimulus_event { picture p_target; code = "target"; port_code = 20; # needs to be there at scanner!! (for proper log file eyetracker) time = 0; duration = 690;# 700 ms minus security (hard coded because SDL has to precede PCL) }target_event; }trial_target; picture {ellipse_graphic {ellipse_width = 20; ellipse_height = 20; color = 0, 0, 0; rotation = 30;} circle; x = 0; y = 0; } cue; # speech cue trial { trial_duration = stimuli_length; stimulus_event { picture cue; code = "speech_cue"; port_code = 60; time = 0; duration = 1990;# 2000 ms minus security }cue_event; }trial_cue;
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main function fibo(n); array[10] f; var i; { let f[0] <- 0; let f[1] <- 1; let i <- 2; while i < 10 do let f[i] <- f[i - 1] + f[i - 2]; let i <- i + 1 od; return f[n] }; { call outputnum(call fibo(9)) }.
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//<>=errbar(x,y,em,ep) //<>=errbar(x,y,em,ep) // Rajoute des barres d'erreur sur un graphique 2D // x et y decrivent les courbes (voir plot2d) // em et ep sont deux matrices la barre d'erreur au point // <x(i,j),y(i,j)> va de <x(i,j),y(i,j)-em(i,j)> a <x(i,j),y(i,j)+em(i,j)> // x,y,em et ep sont donc des matrices (p,q), q courbes contenant chacunes // p points. // Exemple : taper errbar() // x=0:0.1:2*%pi; // y=<sin(x);cos(x)>';x=<x;x>';plot2d(x,y); // errbar(x,y,0.05*ones(x),0.03*ones(x)); //! [lhs,rhs]=argn(0) if rhs<=0,write(%io(2),'x=0:0.1:2*%pi;'); write(%io(2),'y=[sin(x);cos(x)]'';x=[x;x]'''); write(%io(2),'plot2d(x,y);'); write(%io(2),'errbar(x,y,0.05*ones(x),0.03*ones(x));'); x=0:0.1:2*%pi; y=[sin(x);cos(x)]';x=[x;x]';plot2d(x,y); errbar(x,y,0.05*ones(x),0.03*ones(x)); return;end; xselect(); [n1,n2]=size(x); y1=matrix(y-em,1,n1*n2); x1=matrix(x,1,n1*n2); y2=matrix(y+ep,1,n1*n2); [frect,f1rect]=xgetech(); xclip(f1rect(1),f1rect(4),f1rect(3),abs(f1rect(4)-f1rect(2))); xsegs([x1;x1],[y1;y2]); xclip(); //end
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//////////////////////////////////////////////////////////////////////////////// //// Неделя 8. //// Формирующий фильтр. //// Моделирование динамики матрицы ковариаций в байесовском подходе. //// Рекуррентный метод. Векторный случай //////////////////////////////////////////////////////////////////////////////// clear; deff('[numd] = roundd(num,n)','numd = round(num *10^n) / 10^n'); rand("seed",getdate("s")); grand("setsd",getdate("s")); //// Параметры //// mn = 100; //Количество измерений dt = 1; //Интервал дискретизации x_0 = [roundd(5000+rand(1,'nor')*100,1); roundd(rand(1,'nor')*3,1)]; //Начальное значение P_0 = [10 0; //Начальная матрица ковариаций 0 0.1]; F = [1 dt; //Матрица динамики 0 1]; G = [0; roundd(0.5+rand(1,'uin'),2)];//Матрица шумов Q = 1; //Матрица ковариаций шумов //Выделение памяти x = zeros(2,mn); x(:,1) = x_0; x_ex = zeros(2,mn,5); P = zeros(2,2,mn); P(:,:,1) = P_0; //// Моделирование //// //Мат. ожидание и матрица ковариаций for i = 2:mn x(:,i) = F*x(:,i-1); P(:,:,i) = F*P(:,:,i-1)*F'+G*Q*G'; end //Реализации for j = 1:5 x_ex(:,1,j) = x_0+sqrt(P_0)*rand(2,1,'nor'); for i = 2:mn x_ex(:,i,j) =F*x_ex(:,i-1,j)+sqrt(G)*rand(1,'nor'); end end //// Графики //// figure(1); clf; subplot(2,1,2); title('Динамика и СКО высоты') set(gca(),"auto_clear","off"); xgrid(1,0.1,10); plot(1:mn,x(1,:),'b'); plot(1:mn,3*sqrt(squeeze(P(1,1,:)))'+x(1,:),'r'); for j = 1:5 plot(1:mn,x_ex(1,:,j),'g'); end plot(1:mn,-3*sqrt(squeeze(P(1,1,:)))'+x(1,:),'r'); legend('Математическое ожидание','3 sigma','Примеры возможных реализаций'); subplot(2,1,1); title('Динамика и СКО вертикальной скорости') set(gca(),"auto_clear","off"); xgrid(1,0.1,10); plot(1:mn,x(2,:),'b'); plot(1:mn,3*sqrt(squeeze(P(2,2,:)))'+x(2,:),'r'); for j = 1:5 plot(1:mn,x_ex(2,:,j),'g'); end plot(1:mn,-3*sqrt(squeeze(P(2,2,:)))'+x(2,:),'r'); legend('Математическое ожидание','3 sigma','Примеры возможных реализаций'); mprintf('Математическое ожидание высоты через 100 секунд %f \n',x(1,100)); mprintf('3*СКО высоты через 100 секунд %f \n',3*sqrt(squeeze(P(1,1,100)))); mprintf('3*СКО высоты > 300 через %f секунд \n',find(3*sqrt(P(1,1,:))>300,1)); //// Запись данных //// deletefile('data.txt'); deletefile('fillings.txt'); deletefile('answer.txt'); answer = [x(1,100); 3*sqrt(squeeze(P(1,1,100)));find(3*sqrt(P(1,1,:))>300,1)]; fillings = [x_0; G(2)]; write('answer.txt',answer); write('fillings.txt',fillings); write('data.txt',[]);
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Tint 255 0 0 0 Label Here1 TintAlphaChange 100 0.5 Linear Wait 0.5 TintAlphaChange 0 0.5 Linear Wait 0.5 Goto Here1
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clear// //Variables RC = 250.0 * 10**-12 //Time constance (in seconds) Vomax = 50.0 //Maximum output voltage (in volts) tau = 0.05 * 10**-6 //time (in seconds) //Calculation alpha = Vomax / RC //alpha (in volt per second) Vp = alpha * tau //Peak voltage (in volts) //Result printf("\n The peak value of input voltage is %0.3f kV.",Vp * 10**-3)
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clc clear clf() t=[0:%pi/20:2*%pi]'; z=sin(t)*cos(t'); plot3d(t,t,z)
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// Example 2.30 page no-95 clear clc B=0.1 //Wb/m^2 Vh=50 //mV I=10 //mA rho=2*10^5 //Ohm-cm w=3*10^-3 //m x=B*I*10^-3/(Vh*10^-2*w) printf("\n1/RH=%.3f",x) y=1/(rho*10^-2) printf("\nConductivity = %f mhos/meter\nmu=%.0f cm^2/V-sec",y,(y/x)*10^6)
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//to calculate syncronising power/elec deg,pu sync torque/mech deg clc; j=sqrt(-1); Xd=.8; Xq=.5; Vt=1; pf=.8; phi=acosd(pf); Ia=1*complex(cosd(phi),sind(phi)); Ef=Vt-j*Ia*Xq; Eff=abs(Ef); dl=atand(imag(Ef)/real(Ef)); w=-dl+phi; Id=abs(Ia)*sind(w); Ef=Eff+Id*(Xd-Xq); Psyn=abs(Ef)*Vt*cosd(dl)/Xd+Vt^2*((Xd-Xq)/(Xd*Xq))*cosd(2*dl); disp(Psyn*(%pi/180),'syncronising power(pu)/elec deg'); f=50; P=12; n_s=(120*f/P)*(2*%pi/60); Tsyn=Psyn/n_s;disp(Tsyn,'pu sync torque/mech deg');
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clc; clear all; u0=4*%pi*1e-7; b=9.27*1e-24; H=1e3;//homogeneous field k=1.38*1e-23;//boltzmann constant T=303;//temp in kelvin T1 = T - 273; // Temp In Degree x=u0*b*H/(k*T);//avg magnetic moment disp('bohr magneton/spin',x,'avg magnetic moment is=');
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function a=f2t(S,fs) N=length(S); T=1/fs*N; t=[-(T/2):1/fs:(T/2-1/fs)]; temp1=fft(S)/T; temp2=N*ifft(S)/T; a(1:N/2)=temp1(N/2+1:-1:2); a(N/2+1:N)=temp2(1:N/2); a=a.*exp((-%i*%pi)*fs*t); endfunction
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Ex9_5.sce
//Example 9.5 m_ub=55.0;//Mass of upper body (kg) m_box=30.0;//Mass of box (kg) r_ub=35*10^-2;//Distance of CG of upper body from pivot (m) r_box=50*10^-2;//Distance of CG of box from pivot (m) r_B=8*10^-2;//Distance of force F_B from pivot (m) g=9.80;//Acceleration due to gravity (m/s) F_B=((r_ub*m_ub*g)+(r_box*m_box*g))/r_B;//Force in the back muscles (N) printf('a.Force in the back muscles = %0.2e N',F_B) ratio=F_B/(m_ub*g+m_box*g); printf('\nRatio of the force in the back muscles to the weight of the upper body plus the load = %0.2f',ratio) ///////////////////////////////////// theta=29;//Direction of F_B (deg) F_Vy=(m_ub*g)+(m_box*g)+F_B*sind(theta);//Vertical component of force on vertebrae (N) F_Vx=F_B*cosd(theta);//Horizontal component of force on vertebrae (N) F_V=sqrt(F_Vx^2+F_Vy^2);//Force on vertebrae (N) printf('\nb.Force exerted by vertebrae = %0.2e N',F_V) THETA=atand(F_Vy/F_Vx);//Direction of F_V (deg) printf('\nDirection of force exerted by vertebrae = %0.1f deg',THETA) ratio1=F_V/(m_ub*g+m_box*g); printf('\nRatio of the force exerted by the vertebrae to the weight of the upper body plus the load = %0.2f',ratio1) //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest