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Ex4_19.sce
//Electric Drives:concepts and applications by V.subrahmanyam //Publisher:Tata McGraw-Hill //Edition:Second //Ex4_19 clc; clear; V=400;// voltage in V R1=10;// Resistance in ohm R2=5;// Resistance in ohm X1=2.6*%i;//Reactance in ohm X2=2.4*%i;//Reactance in ohm Xm=36.4*%i;//Reactance in ohm Z=0.06;//zigma value C=486;//constant F4=2.5;//frequency in Hz F2=25;//frequency in Hz Z1=(1+X1)+((Xm*(R1+X2))/(R1+X2+Xm)); [M, P] = polar(Z1); M * exp(%i * P); Ieff1=sqrt(1+(M/(Z*Xm))^2*(((R2*(%pi)^4)/C)-1)); disp(Ieff1,"The rms value of current I1 in A:") Z2=(1+(X1/2))+(((Xm/2)*((R1/2)+(X2/2)))/((R1/2)+X2+(Xm/2))); [M, P] = polar(Z2); M * exp(%i * P); Ieff2=sqrt(1+(M/(Z*(Xm/2)))^2*(((R2*(%pi)^4)/C)-1)); disp(Ieff2,"The rms value of current I2 in A:") S=(F4/F2); Z3=(1+(X1*S))+(((Xm*S)*((R1*S)+(X2*S)))/((R1*S)+(X2*S)+(Xm*S))); [M, P] = polar(Z3); M * exp(%i * P); Ieff3=sqrt(1+(M/(Z*(Xm*S)))^2*(((R2*(%pi)^4)/C)-1)); disp(Ieff3,"The rms value of current I3 in A:")
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//Example2.8// //From Appendix 2 rAl=0.057;//nm //Ionic radius of Aluminium rB=0.02;//nm //Ionic radius of Boron rCa=0.106;//nm //Ionic radius of Calcium rMg=0.078;//nm// Ionic radius of Magnesium rSi=0.039;//nm //Ionic radius of Silicon rTi=0.064;//nm //Ionic radius of Titanium rO=0.132//nm //Ionic radius of Oxygen r=rAl/rO mprintf("r = %f ",r) //For B2O3 r1=rB/rO mprintf("\nr1 = %f ,giving CN=2",r1) //For CaO r2=rCa/rO mprintf("\nr2 = %f ,giving CN=8",r2) //For MgO r3=rMg/rO mprintf("\nr3 = %f ,giving CN=6",r3) //For SiO2 r4=rSi/rO mprintf("\nr4 = %f ,giving CN=4",r4) //For TiO2 r5=rTi/rO mprintf("\nr5 = %f ,giving CN=6",r5) mprintf("\nThe coordination number for the cation is obtain from Table 2.1")
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// Example 4.6;/Pulse broadning due to material dispersion clc; clear; close; c=3*10^5;// speed of light in km/s Dh=0.025;//Material dispersion L=1;//distance in km h=0.85;//Wavelength micro meters Sh=20;// Spectral width in nano meter M=Dh/(c*h*10^3);// Sm=M*L*Sh//Pulse broadning due to material dispersion in nano second per kilometer disp(Sm*10^9,"Pulse broadning due to material dispersion in nano second per kilometer")
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//chapter 2 //Pavg=0.5*|E|^2/etta0,Prmax=2*10^-6W,Aem=Prmax/Pavg printf("\n"); E=50*10^-3; Etta0=120*(%pi); printf("the electric field is %eV/m",E); Pavg=0.5*(50*10^-3)^2/(120*(%pi)); printf("\nthe average power is %gW",Pavg); Aem=(2*10^-6)/(3.315*10^-6); printf("\nthe maximum effective aperture area is %gm^2",Aem);
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function [signo,mantisa,exponente] = convertirIEEE(valor) // inicializacion //mode(0) signo = %nan; mantisa = ''; exponente = 0; // obteniendo el signo if valor<0 then signo = '1'; else signo = '0'; end // obteniendo el exponente valor = abs(valor); while(valor>=2) valor = valor/2; exponente = exponente + 1; end exponente = exponente + 127; exponente = dec2bin(exponente,8); // obteniendo la mantisa valor = valor - 1; for i=1:23 if (valor == 1) then mantisa = mantisa + '0'; elseif (valor ~= 1) then valor = valor*2; if (valor < 1) then mantisa = mantisa + '0'; else valor = valor - 1; mantisa = mantisa + '1'; end end end endfunction
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// Chapter 6_The pn junction //Caption_Space charge width //Ex_3//page 227 Na=10^16 //acceptor ion concentration T=300 //temperature in kelvin Nd=10^15 ni=1.5*(10^10) //intrinsic ion concentration Vr=5 //Reverse applied voltage Vbi=0.635 V=Vr+Vbi W=(2*eps*V/e*(Na+Nd)/(Na*Nd))^0.5 printf('The space charge width is %f cm ',W)
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@relation vehicle @attribute COMPACTNESS integer[73,119] @attribute CIRCULARITY integer[33,59] @attribute DISTANCECIRCULARITY integer[40,112] @attribute RADIUSRATIO integer[104,333] @attribute PRAXISASPECTRATIO integer[47,138] @attribute MAXLENGTHASPECTRATIO integer[2,55] @attribute SCATTERRATIO integer[112,265] @attribute ELONGATEDNESS integer[26,61] @attribute PRAXISRECTANGULAR integer[17,29] @attribute LENGTHRECTANGULAR integer[118,188] @attribute MAJORVARIANCE integer[130,320] @attribute MINORVARIANCE integer[184,1018] @attribute GYRATIONRADIUS integer[109,268] @attribute MAJORSKEWNESS integer[59,135] @attribute MINORSKEWNESS integer[0,22] @attribute MINORKURTOSIS integer[0,41] @attribute MAJORKURTOSIS integer[176,206] @attribute HOLLOWSRATIO integer[181,211] @attribute class{van,saab,bus,opel} @inputs COMPACTNESS,CIRCULARITY,DISTANCECIRCULARITY,RADIUSRATIO,PRAXISASPECTRATIO,MAXLENGTHASPECTRATIO,SCATTERRATIO,ELONGATEDNESS,PRAXISRECTANGULAR,LENGTHRECTANGULAR,MAJORVARIANCE,MINORVARIANCE,GYRATIONRADIUS,MAJORSKEWNESS,MINORSKEWNESS,MINORKURTOSIS,MAJORKURTOSIS,HOLLOWSRATIO @outputs class @data van bus van van bus bus saab saab saab van saab saab opel van bus saab bus van van bus opel opel saab saab van van van van bus bus van bus opel van van van van van saab van saab opel bus bus saab saab opel bus opel saab bus bus opel van saab saab opel saab opel opel van bus bus saab saab van saab saab van van opel bus opel opel van van saab saab opel saab saab opel bus bus saab saab opel opel bus bus opel saab bus bus bus bus saab saab bus saab van van van van opel opel bus bus opel bus opel saab opel saab bus bus van van van van saab van van van opel opel saab saab saab saab opel bus saab bus bus bus opel opel bus saab bus bus bus bus bus bus opel opel van van saab saab saab bus saab opel bus bus saab van van van van van bus bus bus bus
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integral = integrate('(4*x)-(2*x*x)' , 'x', 0, 2); C = 1/integral; disp(C, "The value of C is") integral_new = integrate('C*((4*x)-(2*x*x))' , 'x', 0, 1); disp(1-integral_new , "Probability that X is greater than 1 is")
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// Scilab Code Ex1.30:: Page-1.33 (2009) clc; clear; h = 6.6e-034; // Planck's constant, Js e = 1.6e-019; // Energy equivalent of 1 eV, J/eV c = 3e+08; // Speed of light, m/s v = 3e+07; // Velocity of the electron, m/s m0 = 9.1e-031; // Rest mass of electron, kg m = m0/sqrt(1-v^2/c^2); // Mass of moving electron, kg delta_p_max = m*v; // Maximum uncertainty in momentum of the particle, m/s // delta_x_min*delta_p_max = h/(4*%pi), solving for delta_x_min delta_x_min = h/(4*%pi*delta_p_max); // Minimum position uncertainty of particle, m printf("\nThe smallest possible uncertainty in position of the electron = %5.3f angstrom", delta_x_min/1e-010); // Result // The smallest possible uncertainty in position of the electron = 0.019 angstrom
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// Scilab code Ex10.5: Pg.424 (2008) clc; clear; lamda = 0.38e-09; // Mean free path, m v = 1.08e+05; // Average speed of electrons, m/s t = lamda/v; // Relaxation time, s e = 1.6e-19; // Electronic charge, C m_e = 9.11e-31; // Mass of electrons, kg n = 8.47e+28; // Density of electrons, electrons/m^3 rho = m_e/(n*e^2*t); // Resistivity of Copper, ohm-m sigma = 1/rho; // Conductivity of Copper, (ohm-m)^(-1) printf("\nThe resistivity of copper = %4.2e ohm-m", rho); printf("\nThe conductivity of copper = %4.2e per ohm-m", sigma); // Result // The resistivity of copper = 1.19e-007 ohm-m // The conductivity of copper = 8.37e+006 per ohm-m
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--INFO: Reading startup configuration from file PulsarLogOn.act_ssl_config -- Fuzzy Logix, LLC: Functional Testing Script for DB Lytix functions on Teradata Aster -- -- Copyright (c): 2016 Fuzzy Logix, LLC -- -- NOTICE: All information contained herein is, and remains the property of Fuzzy Logix, LLC. -- The intellectual and technical concepts contained herein are proprietary to Fuzzy Logix, LLC. -- and may be covered by U.S. and Foreign Patents, patents in process, and are protected by trade -- secret or copyright law. Dissemination of this information or reproduction of this material is -- strictly forbidden unless prior written permission is obtained from Fuzzy Logix, LLC. -- Functional Test Specifications: -- -- Test Category: Matrix Operations -- -- Last Updated: 05-30-2017 -- -- Author: <kamlesh.meena@fuzzyl.com> -- -- BEGIN: TEST SCRIPT -----**************************************************************** -----**************************************************************** ---Product of Two Matrices -----**************************************************************** TRUNCATE TABLE tblMatrixResult; INSERT INTO tblMatrixResult SELECT a.Row_ID, a.Col_ID, FLMatrixInv(a.Row_ID, a.Col_ID, a.CELL_VAL) OVER (PARTITION BY 1) AS Inverse FROM tblMatrixMulti a WHERE a.Matrix_ID=5 ORDER BY 1, 2; SELECT a.Row_ID, b.Col_ID, FLSumProd(a.CELL_VAL, b.CELL_VAL) AS Product FROM tblMatrixResult a, tblMatrixMulti b WHERE a.Col_ID = b.Row_ID AND b.Matrix_ID=5 GROUP BY a.Row_ID, b.Col_ID ORDER BY 1, 2;
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//Example 1.15.3 //To find the cutoff wavelength.. clc; clear; n1= 1.46; //RI of core.. a = 4.5; //radius of core in um.. del= 0.0025; //relative RI difference.. V= 2.405; // Normalisd frequency for single mode.. lamda= 2*%pi*a*n1*sqrt(2*del)/V; //cutoff wavelength... printf('The cut off wavelength for the given fibre is %.3f um',lamda);
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clc //given that E_eV = 510 // Energy of gamma ray in keV h = 6.63e-34 // Planks constant m_e = 9.1e-31 // mass of electron in kg c = 3e8 // speed of light in m/sec theta = 90 // scattering angle in degree printf("Example 3.18") E_j = E_eV*1e3*1.6e-19 // Energy of gamma ray in Joule lambda = h*c/E_j // Calculation of wavelength in meter d_lambda= h*(1-cos(theta*%pi/180))*1e10/(m_e*c) // calculation of wavelength shift in angstrom lambda_n = lambda+d_lambda/1e10 // Calculation of recoiled electron wavelength d_E = h*c*(d_lambda/1e10)/(1.6e-19*lambda_n*lambda)// Calculation of recoiled electron energy in eV psi= atan(1/(tan((theta*%pi/180)/2)/(1+(h/(lambda*m_e*c))))) phi_deg = 90 - psi*180/%pi // Calculation of degree part of angle of recoiled electron phi_min = 60*(phi_deg - floor(phi_deg))// Calculation of minute part of angle of recoiled electron printf("\nWavelength of scattered radiation is %e m ",lambda_n) printf("\nEnergy of recoiled electron is %f MeV.",d_E/1e6) printf("\nRecoiled electron angle is %d degree%d minute \n\n\n",phi_deg,phi_min)
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// Example 4.14, page no-155 clear clc c=3*10^8 //speed of light f=2.5*10^9 //operating frequency s=0.1 //inter element spacing theta =10 //10° right towards array axis l=c/f fi=(360*s/l)*ceil(10000*sind(theta))/10000 fi=ceil(10*fi)/10 printf("The phase angle for elements 1,2,3,4 and 5 \n are respecively 0°,%.1f°,%.1f°,%.1f° and %.1f°",fi,2*fi,3*fi,4*fi)
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/2267/CH7/EX7.3/ex7_3.sce
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ex7_3.sce
//Part A Chapter 7 Example 3 clc; clear; close; m=5;//kg cp_super_heat=2.1;//kJ/kgK cp_water=4.18;//kJ/kgK Tsuper_heat=300+273.15;//K Tsat=212.42;//degreeC(at 2 MPa) Tsat=Tsat+273.15;//K hfg=1890.7;//kJ/kg(For 2 MPa & Tsat)\ S=cp_water*log(Tsat/273.15)+hfg/Tsat+cp_super_heat*log(Tsuper_heat/Tsat);//kJ/kgK S_5kg=S*5;//kJ/K disp("Entropy of 5 kg steam = "+string(S_5kg)+" kJ/K");
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/635/CH5/EX5.11/Ch05Ex11.sci
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FOSSEE/Scilab-TBC-Uploads
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Ch05Ex11.sci
// Scilab Code Ex5.11 Dependence of applied stress on the slip direction of a copper: Page-169 (2010) tau_critical = 1; // Critical shear stress for the <-110>{111} slip system, mega-pascal (MPa) // For directions [001] and [-111] h1 = 0; k1 = 0; l1 = 1 // Miller indices for first set of planes h2 = -1; k2 = 1; l2 = 1; // Miller indices for second set of planes cos_phi = (h1*h2+k1*k2+l1*l2)/(sqrt(h1^2+k1^2+l1^2)*sqrt(h2^2+k2^2+l2^2)); // Cosine of angle between [001] and [-111] directions // For directions [001] and [101] h1 = 0; k1 = 0; l1 = 1 // Miller indices for first set of planes h2 = 1; k2 = 0; l2 = 1; // Miller indices for second set of planes cos_lambda = (h1*h2+k1*k2+l1*l2)/(sqrt(h1^2+k1^2+l1^2)*sqrt(h2^2+k2^2+l2^2)); // Cosine of angle between [001] and [101] directions sigma = tau_critical/(cos_phi*cos_lambda); // Stress along [001] direction, newton per metre square printf("\nThe stress required to be applied along [001] direction to produce slip in the [101] direction on the (-111) plane = %4.2f MPa", sigma); // For directions [001] and [110] h1 = 0; k1 = 0; l1 = 1 // Miller indices for first set of planes h2 = 1; k2 = 1; l2 = 0; // Miller indices for second set of planes cos_lambda = (h1*h2+k1*k2+l1*l2)/(sqrt(h1^2+k1^2+l1^2)*sqrt(h2^2+k2^2+l2^2)); // Cosine of angle between [001] and [110] directions if cos_lambda <> 0 then sigma = tau_critical/(cos_phi*cos_lambda); // Stress along [001] direction, newton per metre square printf("\nThe stress required to be applied along [001] direction to produce slip in the [110] direction on the (-111) plane = %4.2f MPa", sigma); else printf("\nSince cos_lambda = 0, this implies that slip cannot occur in [110] direction when the stress is applied along [001] direction"); end // Result // The stress required to be applied along [001] direction to produce slip in the [101] direction on the (-111) plane = 2.45 MPa // Since cos_lambda = 0, this implies that slip cannot occur in [110] direction when the stress is applied along [001] direction
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/Statistics with R - Coursera/SkeletonBMI.Quantitative.tst
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SkeletonBMI.Quantitative.tst
Observation Sex BMIcat BMIquant Age DGEstimate DGDifference 1 2 underweight 15.66 78 44 -34 2 1 normal 23.03 44 32 -12 3 1 overweight 27.92 72 32 -40 4 1 overweight 27.83 59 44 -15 5 1 normal 21.41 60 32 -28 6 1 underweight 13.65 34 25 -9 7 1 overweight 25.86 50 32 -18 8 1 underweight 14.56 73 50 -23 9 1 normal 22.44 70 39 -31 10 1 normal 19.88 60 44 -16 11 1 normal 23.24 58 32 -26 12 1 overweight 25.09 61 32 -29 13 2 overweight 25.68 52 44 -8 14 1 normal 24.97 67 44 -23 15 1 normal 23.32 60 44 -16 16 1 normal 23.29 68 50 -18 17 2 overweight 27.37 35 12 -23 18 2 obese 34.82 81 39 -42 19 2 underweight 12.29 73 44 -29 20 1 normal 23.85 65 39 -26 21 1 normal 24.89 57 57 0 22 2 normal 24.69 67 32 -35 23 2 normal 23.18 60 44 -16 24 1 normal 24.71 35 32 -3 25 1 overweight 26.62 64 32 -32 26 1 normal 23.85 76 32 -44 27 2 underweight 17.92 39 32 -7 28 1 overweight 29.45 60 44 -16 29 1 normal 22.98 41 61 20 30 1 obese 40.03 55 32 -23 31 2 normal 19.81 38 57 19 32 1 normal 23.08 60 61 1 33 1 normal 20.61 70 50 -20 34 1 normal 22.65 70 44 -26 35 1 normal 24.54 50 44 -6 36 1 overweight 26.13 28 25 -3 37 2 underweight 17.48 66 44 -22 38 1 normal 24.3 45 39 -6 39 1 overweight 26.98 44 32 -12 40 2 normal 18.63 43 15 -28 41 2 normal 20.26 52 50 -2 42 1 underweight 16.6 63 32 -31 43 2 normal 19.68 36 32 -4 44 1 normal 24.52 54 44 -10 45 1 normal 22.62 26 25 -1 46 1 normal 23.52 65 32 -33 47 1 underweight 17.82 68 25 -43 48 2 underweight 14.85 25 25 0 49 1 normal 23.48 32 25 -7 50 1 underweight 17.27 33 39 6 51 1 overweight 25.86 45 32 -13 52 1 overweight 26.62 32 15 -17 53 1 normal 18.66 46 32 -14 54 1 normal 19.03 50 32 -18 55 1 overweight 29 34 32 -2 56 2 underweight 17.69 45 15 -30 57 1 normal 19.24 64 44 -20 58 1 normal 24.41 63 44 -19 59 2 normal 22.79 71 32 -39 60 2 normal 22.42 60 44 -16 61 1 overweight 27.14 58 32 -26 62 2 normal 21.26 60 44 -16 63 1 obese 31.75 60 66 6 64 1 normal 24.41 39 32 -7 65 2 underweight 10.06 37 25 -12 66 1 overweight 27.12 39 32 -7 67 1 overweight 26.45 33 25 -8 68 2 normal 21.56 43 25 -18 69 2 overweight 27.78 52 32 -20 70 1 normal 22.43 63 50 -13 71 1 normal 18.88 49 30 -19 72 1 overweight 27.15 40 32 -8 73 1 underweight 17.18 35 44 9 74 1 underweight 16.4 50 32 -18 75 2 underweight 17.04 65 32 -33 76 2 normal 23.89 46 50 4 77 2 normal 21.12 49 32 -17 78 2 obese 33.84 50 57 7 79 1 overweight 29.62 50 44 -6 80 1 normal 22.02 50 44 -6 81 1 underweight 14.95 29 32 3 82 2 normal 19.9 39 25 -14 83 1 underweight 14.05 51 32 -19 84 1 normal 21.73 38 32 -6 85 2 underweight 16.66 50 44 -6 86 1 normal 22.53 19 16 -3 87 1 underweight 14.95 67 32 -35 88 1 normal 21.99 47 44 -3 89 1 normal 19.26 22 44 22 90 2 underweight 17.01 50 32 -18 91 1 normal 23.24 65 44 -21 92 1 normal 24.2 82 50 -32 93 1 obese 34.53 44 32 -12 94 1 normal 19.61 70 32 -38 95 1 normal 20.3 49 44 -5 96 2 overweight 29.72 47 32 -15 97 1 normal 20.14 61 39 -22 98 1 normal 19.75 47 32 -15 99 1 overweight 25.25 30 32 2 100 2 underweight 23.68 70 61 -9 101 1 normal 23.94 55 32 -23 102 2 overweight 29.07 38 44 6 103 1 normal 23.73 53 32 -21 104 1 normal 23.61 46 32 -14 105 1 normal 23.78 40 32 -8 106 1 normal 20.4 71 39 -32 107 1 normal 20.27 50 44 -6 108 2 underweight 14.84 85 50 -35 109 1 normal 24.59 48 44 -4 110 1 normal 24.99 70 32 -38 111 1 normal 19.96 50 44 -6 112 1 normal 24.76 50 32 -18 113 2 overweight 26.58 70 25 -45 114 1 overweight 28.69 39 32 -7 115 1 normal 23.02 45 44 -1 116 1 normal 22.81 45 32 -13 117 1 normal 24.47 38 44 6 118 1 overweight 28.7 61 44 -17 119 1 normal 21.09 59 44 -15 120 1 overweight 27.6 55 44 -11 121 2 underweight 18.15 61 25 -36 122 1 normal 22.73 23 32 9 123 2 normal 20.23 75 32 -43 124 1 underweight 16.54 70 44 -26 125 2 underweight 17.9 50 25 -25 126 1 normal 22.77 59 50 -9 127 1 normal 19.67 39 50 11 128 2 obese 35.51 72 44 -28 129 1 normal 21.69 41 44 3 130 1 normal 20.09 74 44 -30 131 1 overweight 25.12 35 25 -10 132 1 normal 24.95 38 32 -6 133 1 normal 23.52 38 57 19 134 1 normal 21.7 54 57 3 135 1 underweight 16.3 41 32 -9 136 1 overweight 27.38 35 32 -3 137 2 overweight 26.63 40 57 17 138 1 obese 31.85 38 25 -13 139 2 normal 20.78 56 39 -17 140 2 normal 20.39 48 44 -4 141 2 normal 24.64 27 16 -11 142 1 normal 24.03 49 32 -17 143 1 normal 23.43 64 57 -7 144 1 underweight 16.77 60 39 -21 145 1 overweight 26.65 68 32 -36 146 2 underweight 14.57 40 25 -15 147 1 underweight 16.37 42 50 8 148 1 normal 24.77 40 32 -8 149 1 normal 22.42 78 32 -46 150 1 normal 19.46 53 50 -3 151 1 underweight 12.92 68 44 -24 152 1 normal 20.26 41 50 9 153 1 normal 24.61 64 44 -20 154 1 overweight 27.38 30 25 -5 155 2 normal 19.72 68 32 -36 156 1 normal 24.33 25 32 7 157 2 normal 20.57 50 32 -18 158 2 obese 31.57 34 32 -2 159 1 normal 21.72 39 44 5 160 1 overweight 26.25 38 25 -13 161 1 normal 22.81 58 25 -33 162 1 normal 19.77 43 32 -11 163 2 normal 22.25 44 32 -12 164 1 overweight 29.84 36 32 -4 165 1 underweight 14.2 49 44 -5 166 1 underweight 15.58 26 32 6 167 2 normal 18.53 67 32 -35 168 1 normal 22.49 44 32 -12 169 1 normal 20.51 70 44 -26 170 2 normal 19.77 69 25 -44 171 2 normal 22.97 43 39 -4 172 1 overweight 29.44 44 32 -12 173 2 obese 30.79 54 61 7 174 1 normal 19.04 40 32 -8 175 1 overweight 25.29 53 32 -21 176 2 overweight 29.23 50 32 -18 177 1 underweight 15.06 68 32 -36 178 2 overweight 25.68 68 25 -43 179 1 normal 22.28 45 32 -13 180 2 overweight 27.3 35 25 -10 181 1 obese 31.32 46 57 11 182 1 normal 23.99 56 39 -17 183 1 overweight 26.61 62 57 -5 184 2 normal 22.87 42 32 -10 185 1 normal 22.86 50 32 -18 186 1 overweight 29.82 47 32 -15 187 2 normal 21.18 60 39 -21 188 2 normal 18.7 76 25 -51 189 1 normal 22.77 44 44 0 190 1 underweight 14.9 62 32 -30 191 1 normal 24.67 69 58 -11 192 2 normal 20.6 40 32 -8 193 2 underweight 15.71 33 25 -8 194 1 normal 22.38 58 44 -14 195 1 underweight 17.38 84 57 -27 196 1 normal 21.23 64 57 -7 197 1 underweight 17.21 60 44 -16 198 1 overweight 25.79 19 16 -3 199 2 normal 24.22 25 12 -13 200 1 normal 22.87 59 44 -15 201 1 underweight 16.02 51 44 -7 202 1 normal 18.72 51 44 -7 203 2 overweight 25.39 35 32 -3 204 1 normal 18.97 57 39 -18 205 2 normal 22.43 35 44 9 206 1 overweight 29.99 43 32 -11 207 1 overweight 26.96 67 50 -17 208 1 overweight 29.08 78 50 -28 209 1 normal 19.97 43 39 -4 210 2 underweight 11.79 51 32 -19 211 2 normal 21.27 78 20 -58 212 2 overweight 29.26 66 50 -16 213 2 normal 20.5 65 32 -33 214 1 normal 21.32 63 57 -6 215 1 normal 22.46 57 32 -25 216 1 normal 18.82 60 44 -16 217 2 normal 20.81 40 32 -8 218 1 underweight 18.16 58 44 -14 219 1 overweight 29.38 62 44 -18 220 1 overweight 28.08 68 44 -24 221 2 obese 33.72 60 32 -28 222 1 normal 19.9 30 25 -5 223 2 underweight 16.86 42 30 -12 224 1 overweight 29.2 56 39 -17 225 1 overweight 26.6 51 32 -19 226 1 normal 19.18 70 32 -38 227 2 underweight 14.17 31 20 -11 228 2 normal 23.03 71 57 -14 229 1 normal 23.68 73 44 -29 230 1 normal 21 20 25 5 231 1 overweight 28.35 54 50 -4 232 1 underweight 14.85 35 25 -10 233 1 underweight 16.85 68 32 -36 234 1 overweight 26.63 54 57 3 235 1 obese 31.2 44 32 -12 236 1 underweight 16.25 59 44 -15 237 1 normal 19.41 35 25 -10 238 2 underweight 15.94 85 61 -24 239 1 overweight 29.11 38 44 6 240 1 normal 23.92 55 32 -23 241 2 overweight 29.3 51 25 -26 242 1 normal 20.05 43 44 1 243 2 normal 24.72 38 25 -13 244 2 underweight 17.55 42 32 -10 245 1 normal 22.4 60 39 -21 246 1 normal 23.13 74 44 -30 247 2 normal 20.45 53 20 -33 248 2 underweight 15.79 32 25 -7 249 2 normal 21.92 58 50 -8 250 1 obese 32.89 63 57 -6 251 2 normal 19.57 44 32 -12 252 2 obese 34.96 73 61 -12 253 1 normal 20.67 61 58 -3 254 2 overweight 26.82 47 32 -15 255 1 normal 24.25 50 32 -18 256 1 normal 19.08 40 44 4 257 1 normal 21.56 78 61 -17 258 1 normal 21.55 52 32 -20 259 2 normal 24.08 37 32 -5 260 1 normal 18.25 66 44 -22 261 2 normal 19.88 39 44 5 262 2 overweight 25.3 38 44 6 263 2 normal 23.76 78 61 -17 264 1 normal 21.46 71 57 -14 265 1 overweight 26.39 51 50 -1 266 1 underweight 16.67 62 32 -30 267 2 overweight 29.24 49 58 9 268 1 underweight 17.97 55 50 -5 269 1 normal 21.57 45 32 -13 270 1 normal 19.07 46 32 -14 271 2 normal 22.94 50 32 -18 272 1 normal 19.15 28 12 -16 273 1 overweight 27.24 48 39 -9 274 2 obese 33.74 60 44 -16 275 2 overweight 27.46 64 32 -32 276 1 obese 35.2 50 50 0 277 2 normal 23.33 45 44 -1 278 1 normal 22.19 59 32 -27 279 1 overweight 28.7 40 32 -8 280 1 normal 23.62 78 61 -17 281 1 underweight 16.38 78 44 -34 282 2 normal 21.9 38 25 -13 283 1 normal 19.52 72 32 -40 284 1 normal 23.11 67 32 -35 285 1 normal 18.97 55 44 -11 286 2 normal 20.25 30 32 2 287 1 normal 18.76 55 32 -23 288 2 normal 21.85 79 50 -29 289 1 underweight 17.54 47 32 -15 290 1 normal 22.81 20 32 12 291 1 normal 20.54 58 39 -19 292 1 normal 21.13 53 39 -14 293 1 normal 21.97 25 32 7 294 1 overweight 26.58 35 32 -3 295 1 normal 23.52 60 32 -28 296 1 normal 19.09 68 32 -36 297 1 normal 23.97 49 32 -17 298 2 normal 21.26 81 39 -42 299 1 underweight 18.38 53 44 -9 300 1 normal 23.53 63 57 -6 301 1 normal 22.8 68 39 -29 302 2 obese 37.87 38 25 -13 303 1 obese 31.01 59 44 -15 304 2 overweight 26.51 57 57 0 305 1 normal 20.74 79 50 -29 306 1 underweight 18.43 74 44 -30 307 1 normal 22.45 60 57 -3 308 1 normal 24.51 50 50 0 309 1 underweight 16.29 48 44 -4 310 1 overweight 28.48 46 44 -2 311 1 normal 20.15 73 50 -23 312 2 underweight 15.28 37 25 -12 313 1 underweight 14.62 72 57 -15 314 1 normal 22.91 32 32 0 315 1 normal 23.64 36 44 8 316 1 overweight 25.12 61 44 -17 317 1 underweight 16.46 25 57 32 318 1 underweight 16.87 60 32 -28 319 1 normal 21.22 58 44 -14 320 1 underweight 17.4 32 32 0 321 1 overweight 28.64 63 44 -19 322 1 normal 18.64 43 44 1 323 1 overweight 29.04 52 57 5 324 1 overweight 25.76 74 50 -24 325 1 normal 20.09 24 32 8 326 1 normal 24.29 35 25 -10 327 1 normal 21.08 61 39 -22 328 1 normal 24.75 62 32 -30 329 1 overweight 26.74 52 50 -2 330 2 normal 21.16 28 12 -16 331 1 normal 19.58 39 57 18 332 1 obese 30.83 54 50 -4 333 1 overweight 25.34 40 32 -8 334 1 normal 27.89 56 44 -12 335 2 overweight 26.58 43 32 -11 336 1 normal 20.96 28 32 4 337 2 normal 19.38 45 44 -1 338 2 normal 19.21 73 44 -29 339 2 underweight 15.93 85 25 -60 340 1 normal 22.08 70 32 -38 341 2 underweight 17.97 77 25 -52 342 1 normal 22.91 56 44 -12 343 1 normal 20.3 68 50 -18 344 1 underweight 14.31 61 32 -29 345 2 underweight 10.88 47 32 -15 346 1 normal 21.87 66 44 -22 347 2 underweight 14.02 60 32 -28 348 2 overweight 25.3 24 15 -9 349 1 normal 19.4 32 32 0 350 2 obese 34.93 50 32 -18 351 1 underweight 16.8 45 32 -13 352 1 normal 20.59 63 50 -13 353 1 overweight 25.11 49 44 -5 354 1 normal 23.4 35 50 15 355 2 normal 19.45 45 32 -13 356 1 overweight 27.24 53 57 4 357 1 overweight 28.3 71 58 -13 358 1 normal 22.17 60 44 -16 359 2 normal 19.92 54 32 -22 360 1 underweight 17.25 76 44 -32 361 1 normal 20.43 31 20 -11 362 2 overweight 29.72 47 44 -3 363 1 normal 22.62 37 44 7 364 2 underweight 15.21 29 15 -14 365 1 normal 21.07 43 44 1 366 1 normal 21.98 41 25 -16 367 1 normal 23.21 56 39 -17 368 2 normal 23.07 34 32 -2 369 2 normal 22.71 53 25 -28 370 2 normal 19.15 79 66 -13 371 1 normal 22.85 35 32 -3 372 2 normal 24.8 80 61 -19 373 1 underweight 13.95 45 44 -1 374 1 underweight 16.25 81 32 -49 375 1 overweight 25.9 35 32 -3 376 1 normal 22.96 44 32 -12 377 1 overweight 26.07 84 44 -40 378 1 normal 24.04 36 39 3 379 1 normal 19.13 65 50 -15 380 1 normal 21.63 35 32 -3 381 1 normal 20.79 77 44 -33 382 1 overweight 27.06 55 50 -5 383 1 underweight 13.68 39 32 -7 384 1 overweight 28.9 30 32 2 385 2 normal 20.07 76 50 -26 386 1 normal 22.52 47 44 -3 387 1 normal 24.3 76 39 -37 388 2 normal 23.41 70 50 -20 389 1 normal 23.05 43 44 1 390 1 normal 22.13 32 25 -7 391 1 underweight 14.46 52 32 -20 392 1 normal 24.16 55 32 -23 393 1 normal 22.81 47 39 -8 394 1 underweight 16.6 60 32 -28 395 1 normal 24.41 69 44 -25 396 1 normal 18.83 74 32 -42 397 2 normal 20.9 73 32 -41 398 2 normal 23.1 65 50 -15 399 1 underweight 17.58 40 32 -8 400 2 overweight 28.1 31 25 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/Hardware/MALU.tst
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z2512690268/nand2teris
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2023-04-19T00:21:49.516211
2021-05-05T12:10:30
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MALU.tst
load MALU.hdl, output-file MALU.out, output-list x%B1.16.1 y%B1.16.1 zx nx zy ny f no out%B1.16.1; set x %B1100111111011111, set y %B1011101010110011, set zx 1, set zy 1, set nx 1, set ny 0, set f 0, set no 0, eval, output; set x %B0110110111110011, set y %B0110110011101001, set zx 0, set zy 1, set nx 1, set ny 1, set f 0, set no 0, eval, output; set x %B1001110101011001, set y %B0000110100100000, set zx 1, set zy 1, set nx 1, set ny 0, set f 0, set no 1, eval, output; set x %B1101111101110011, set y %B1111111010000000, set zx 0, set zy 0, set nx 1, set ny 0, set f 1, set no 1, eval, output; set x %B0011110100111000, set y %B1010011010111000, set zx 0, set zy 0, set nx 1, set ny 1, set f 0, set no 0, eval, output; set x %B0000000100011011, set y %B1011101011011011, set zx 0, set zy 1, set nx 0, set ny 0, set f 1, set no 0, eval, output; set x %B1101010011000111, set y %B0001101101100100, set zx 1, set zy 0, set nx 0, set ny 0, set f 0, set no 1, eval, output; set x %B0011110001011010, set y %B1100000100010100, set zx 0, set zy 0, set nx 1, set ny 0, set f 0, set no 1, eval, output; set x %B0010111011000110, set y %B1000001111000001, set zx 1, set zy 0, set nx 1, set ny 0, set f 1, set no 1, eval, output; set x %B1111101010110000, set y %B0100100101100010, set zx 1, set zy 0, set nx 1, set ny 0, set f 0, set no 1, eval, output; set x %B1010110000110101, set y %B1010000000111010, set zx 1, set zy 0, set nx 1, set ny 0, set f 0, set no 1, eval, output; set x %B0100100000110110, set y %B0111110111100100, set zx 1, set zy 1, set nx 0, set ny 0, set f 1, set no 1, eval, output; set x %B1001010011000001, set y %B1011000101001000, set zx 0, set zy 0, set nx 0, set ny 0, set f 1, set no 0, eval, output; set x %B1010110101010110, set y %B0001010100001101, set zx 0, set zy 1, set nx 0, set ny 1, set f 1, set no 0, eval, output; set x %B0110110110001111, set y %B1100010101000001, set zx 1, set zy 1, set nx 1, set ny 1, set f 1, set no 1, eval, output; set x %B1110111101111010, set y %B0011000000100001, set zx 1, set zy 1, set nx 0, set ny 1, set f 1, set no 0, eval, output;
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/2915/CH2/EX2.16/Ex2_16.sce
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Ex2_16.sce
//Example 2.16 //To determine area of triangle when 3 sides are given clc,clear c=0.0000029 //side oposite to vertex C a=1000000 //side opposite to vertex A b=999999.9999979 //side opposite to vertex B s= (a+b+c)/2 //semi perimeter area_K = sqrt(s*(s-a)*(s-b)*(s-c)) //using herons formula printf('Area of triangle ABC = %.3f square units\n\n',area_K) printf('Note:\n') printf('In calculators like TI-83 plus, due to rounding off etc s will be 1000000\n') printf('Therefore (s-a) is zero. And area will be zero according to herons formula\n') printf('Due to large number of digits in scilab,(s-a) is not zero. Thus, area is non-zero above.')
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Ex11_5.sce
clc //initialization of new variables clear R=0.5 U=290 //m/s c1=150 //m/s alpha1=37 //degrees beta2=alpha1 cp=0.24 eta=0.85 gama=1.4 T01=280 //k //calculations cp=cp*4200 alpha1=alpha1*%pi/180 Cth1=c1*sin(alpha1) DCth=U-2*c1*sin(alpha1) beta1=atan((U-Cth1)/c1*cos(alpha1)) Cp=1-cos(beta1)^2/cos(beta2)^2 Pr=(1+eta*U*DCth/(cp*T01))^(gama/(gama-1)) //results printf('The compression ratio is %.2f',Pr)
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/acmp.ru/307, Athletes/test-01.tst
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3 3 4 3 1 1 2 1 3 3 2 ~~~~~~~~~~~~~~~~~~~~~~~~~~ 3
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clc; clear all; disp("Volatge at burnout point") d=0.001;//m diameter of wire I=190;//amp L=0.4;//m length of wire rhol=958.4;//kg/m^3 rhov=0.5955;//kg/m^3 hfg=2257*10^3;//J/kg s=58.9*10^(-3);// N/m g=9.81;//m/s^2 qsc=0.18*rhov^0.5*hfg*(g*s*(rhol-rhov))^0.25;// at burnout i.e. points of critical flux A=%pi*d*L; Q=A*qsc; Vb=Q/I;// V disp("V",Vb,"Voltage at burnout point =")
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// Example 10-7 // Designing a controller using a full order observer clear; clc; xdel(winsid()); //close all windows mode(0); function smallplot(i) subplot(2,2,i);xgrid(color('gray')); plot(t,x(i,:)); endfunction s = %s; A = [0 1; 20.6 0]; B = [0; 1]; C = [1 0]; D = [0]; P = [-1.8 + %i*2.4 ,-1.8 - %i*2.4 ]; Q = [-8 -8]; // observer poles K = ppol(A,B,P) Ke = ppol(A',C',Q)' // The transfer function of observer controller A1 = A - B*K - Ke*C M = s*eye(A1) - A1 UbyE = K * inv(M) * Ke; disp(UbyE, 'U(s) / E(s) ='); // Plant dynamics Gp = syslin('c',A,B,C,D); disp('plant dynamics'); ssprint(Gp); YbyU = ss2tf(Gp) // Observer controller dynamics disp('observer controller dynamics (x = xbar) ,(u = y), (y = u)'); Goc = syslin('c',A1,Ke,-K,[0]); ssprint(Goc); // Overall System transfer funtion GsFullsystem = UbyE * YbyU /. 1 // Overall System x0 = [1; 0; 0.5; 0]; // initial state As = [A-B*K, B*K ; zeros(2,2) , A-Ke*C]; Gss = syslin('c',As,[1;0;0;0], [1 0 0 0], [0],x0); // Unit step response t = 0:0.01:4; u = zeros(1,length(t)); [y x] = csim(u,t,Gss); smallplot(1); xtitle('Response to initial condition','t (sec)','x1'); smallplot(2); xtitle('Response to initial condition','t (sec)','x2'); smallplot(3); xtitle('','t (sec)','e1'); smallplot(4); xtitle('','t (sec)','e2');
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i=linspace(0,2.5,6) V=[0 50 84 105 120 131] plot(i,V) xtitle("Magnetization curve for example 18.3","Field Current","Generated emf") //refer Fig.18.6 in the textbook //OE is the field resistance line of critical resistance Rc=100 //solving (iii) Rsh=70//field resistance N=750//speed in rpm Nc=Rsh/Rc*N mprintf("When the field resistance is 70 ohm, critical speed=%d rpm\n",round(Nc)) //solving (iv) Eg=100//open-circuit voltage Rsh=55//shunt field resistance //now, the operating point is M instead of A //LM/LN=N1/N //from the graph, LM/LN=100/115 N1=100/115*N//desired speed mprintf("With shunt field resistance of 55 ohm, reduction in speed to make the open circuit voltage equal to 100 V=%d rpm",round(N-N1))
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clc clear //Input data p1=100;//Pressure at the inlet of the compressor in kPa p2=500;//Pressure at the outlet of the compressor in kPa v1=3;//Volume of the air at the inlet of the compressor in m^3/kg v2=0.8;//Volume of the air at the outlet of the compressor in m^3/kg c1=25;//The velocity of air at the inlet of the compressor in m/s c2=130;//The velocity of air at the outlet of the compressor in m/s z=12;//The height of delivery connection above the inlet in m g=9.81;//Gravitational constant in m/s^2 n=1.3;//Polytropic index //Calculations W=[(n)*(p1*v1-p2*v2)]/(n-1);//Workdone for open system polytropic process in kJ/kg K=[(c2^2-c1^2)/2000];//Change in kinetic energy of the system in kJ/kg P=g*(z)/1000;//Change in potential energy of the system in kJ/kg w=W-K-P;//The shaft work of the compressor in kJ/kg //Output printf('The Shaft work of the compressor w = %3.3f kJ/kg \n It is the power absorbing system',w)
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clc //initialisation of variables g= 32.2 //ft/sec^2 H= 100//ft L= 1000 //ft h1= 0.03 h= 0.05 h2= 0.4 d= 6//in le= 1021 //ft //CALCULATIONS u1= sqrt((2*g*H)/(1+h+h2+(h1*L/0.5))) Q= %pi*(d/12)^2*u1/4 u2= sqrt((H*2*g)/(1+h+(1/16)*(1+h+h2+(h1*L/0.5)))) Q1= %pi*(d/24)^2*u2/4 r= sqrt((d/12)/(2*h1*le)) //RESULTS printf (' rate of discharge without a nozzle= %.2f ft^3/sec',Q) printf (' \n rate of discharge= %.2f ft^3/sec',Q1) printf (' \n diameter of nozzle= %.2f in',r)
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function outputVoltage = helperHarmonicDistortion(inputVoltage) //helperHarmonicDistortionADC Helper function for HarmonicDistortionExample.m //Calling Sequence // outputVoltage=helperHarmonicDistortionAmplifier(inputVoltage) //Description //Analizing the harmonic distortion of a weakly non-linear system in the presence of noise. //Example //VmaxPk = 2; //Fi = 2000; //Fs = 44.1e3; //Tstop = 50e-3; //t = 0:1/Fs:Tstop; //inputVmax = VmaxPk*sin(2*%pi*Fi*t);z //outputVmax = helperHarmonicDistortionAmplifier(inputVmax); //plot(t, outputVmax);replot([0,-2.5,0.005,2.5]); //xlabel('Time') //ylabel('Output Voltage') //title('Amplifier output') // model parameters noiseVrms = 0.4e-6; // RMS voltage of input noisefloor // polynomial coefficients a0 = 25e-3; // dc bias (25mV) a1 = 1; // voltage gain a2 = 6e-5; // second order term a3 = -1e-3; // third order term a4 = 5e-6; // fourth order term a5 = 1e-5; // fifth order term // polyval function has constant term at the end. polyCoeff = [a5 a4 a3 a2 a1 a0]; // get number of input samples n = size(inputVoltage,2); // add noise at input inputNoise = noiseVrms*rand(1,n,"normal"); distortedInput = inputVoltage + inputNoise; // adjust input by DC bias, voltage gain and higher order terms outputVoltage = polyval(polyCoeff, distortedInput); endfunction
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FL=0.4*exp(-%i*30*%pi/180) Fin=0.2*exp(%i*45*%pi/180) Z_L=(1+FL)/(1-FL) Z_in=(1+Fin)/(1-Fin) Y_in=(1-Fin)/(1+Fin) disp(Z_L,"Z_L=") disp(Z_in,"Z_in=") disp(Y_in,"Y_in=") //Y_in=(1+%i*Z_L*tan(Bl))/(Z_L+%i*tan(Bl)) Y_in=1/Z_in disp(Y_in,"Y_in=")
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// Chapter 13_Optical Devices //Caption_Solar concentration //Ex_4//page 605 JL==150*10^-3 //PHOTOCURRENT DENSITY Js=3.6*10^-11 //reverse saturation current density Voc=0.0259*log(1+JL/Js) printf('Open circuit voltage when solar concentration is used is %1.3f V',Voc)
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clear // Resolve sist.triangular U function [x]=solveU(U,b) n=size(U,1) // # de linhas x(n)=b(n)/U(n,n) for i=n-1:-1:1 x(i)=(b(i)-U(i,i+1:n)*x(i+1:n))/U(i,i) end endfunction // Resolve sist.triangular function [x]=solveL(L,b) n=size(L,1) // # de linhas x(1)=b(1)/L(1,1) for i=2:n x(i)=(b(i)-L(i,1:i-1)*x(1:i-1))/L(i,i) end endfunction // Fatora matriz function [L,A]=fatoracaoLU(A) n=size(A,1) L=eye(n,n) for j=1:n-1 for i=j+1:n //coluna j L(i,j)=A(i,j)/A(j,j) A(i,j+1:n)=A(i,j+1:n)-L(i,j)*A(j,j+1:n) A(i,j)=0 end end endfunction // Resolve sistema Ax=b function x=resolve(A,b) [L,U]=fatoracaoLU(A); y=solveL(L,b); x=solveU(U,y); endfunction
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clear; clc; TY=1;seno=0;coss=0; ANG=input('ANGULO EM RADIANO='); function X=FAT(N) if N==0 X=1; else X=N*FAT(N-1); end endfunction for T=0:1:100 TY=TY+3; seno=seno+((-1)^TY*((ANG^((T*2)+1))/FAT((T*2)+1))); coss=coss+((-1)^TY*((ANG^(T*2)/FAT(T*2)))); end MZ= %e^(%i*ANG); SP= cos(ANG)+%i*sin(ANG); GG=[SP MZ]; disp(GG); disp(seno); disp(sin(ANG)); disp(coss); disp(cos(ANG)); //14) n=13; M= (cos(ANG)+%i*sin(ANG))^n; C= (cos(ANG*n)+%i*sin(ANG*n)); RED=[M C]; disp(RED);
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close; clc; clear; n=0:3; x=cos(%pi*n/2); subplot(4,1,1) plot2d3(n,x) xtitle('x[n]','n') a=gca(); a.x_location="origin"; a.y_location="right"; poly1=a.children.children; poly1.thickness=3; poly1.foreground=2; plot(n,x,'r.') subplot(4,1,2) h=.5^n; plot2d3(n,h); xtitle('h[n]','n') a=gca(); a.x_location="origin"; a.y_location="right"; poly1=a.children.children; poly1.thickness=3; poly1.foreground=2; plot(n,h,'r.') y=convol(x,h) subplot(4,1,3) plot2d3(n,y(1:4)); xtitle('y[n]','n') plot(n,y(1:4),'r.') a=gca(); a.x_location="origin"; a.y_location="right"; poly1=a.children.children; poly1.thickness=3; poly1.foreground=2; clear y; X=fft(x,-1); H=fft(h,-1); Y=H.*X; y=fft(Y,1); subplot(4,1,4) plot2d3(n,y); xtitle('y[n]','n') plot(n,y,'r.') a=gca(); a.x_location="origin"; a.y_location="right"; poly1=a.children.children; poly1.thickness=3; poly1.foreground=2; plot(n,x,'r.')
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// exa 7.4 Pg 204 clc;clear;close; // Given Data d=75;// mm tau=50;// MPa sigma_c=75;// MPa printf('for key to be equally strong in shear & crushing - \n') b=d/4;// mm printf(' b= %.2f mm. Use b=20 mm.',b) b=20;//mm //2*b/t=sigma_c/tau for key to be equally strong in shear & crushing t=2*b/(sigma_c/tau);// mm printf('\n t=%.2f mm. Use t=27 mm',t) l= %pi*d**2/8/b;// mm (for key to be equally strong in shear as shaft) printf('for key to be equally strong in shear as shaft - \n') printf(' l=%.1f mm. Use l=115 mm',l)
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// Exa 10.5 clc; clear; close; format('v',5) // Given data V_CC = 10;// in V V_BB = -10;// in V R_C2 = 1.2* 10^3;// in ohm R_C1 = R_C2;// in ohm R_B1 = 39 * 10^3;// in ohm R_B2 = R_B1;// in ohm R2 = 10* 10^3;// in ohm R1 = R2;// in ohm h_fe = 30;// unit less V_CE2sat = 0;// in V I1 = (V_CC-V_CE2sat)/R_C2;// in A I2 = (V_CE2sat-V_BB)/(R1+R_B2);// in A I_C2 = I1-I2;// in A I_B2min = I_C2/h_fe;// in A V_C2 = 0;// in V V_B1 = V_C2 - (I2*R1);// in V V_B2 = 0;// in V V_C1 = 10;// in V I3 = (V_CC-V_C1)/R_C1;// in A V_BE2sat = 0;// in V I4 = (V_C1-V_BE2sat)/R2;// in A I_D = I3-I4;// in A I5 = (V_BE2sat-V_BB)/R_B1;// in A I_B2actual = I4-I5;// in A I_B2actual= I_B2actual*10^3;// in mA I_C1 = 0;// in mA I_B1 = 0;// in mA I_C2= I_C2*10^3;// in mA disp(V_C1,"The value of V_C1 in V is"); disp(V_C2,"The value of V_C2 in V is"); disp(V_B1,"The value of V_B1 in V is"); disp(V_B2,"The value of V_B2 in V is"); disp(I_C1,"The value of I_C1 in mA is"); disp(I_C2,"The value of I_C2 in mA is"); disp(I_B1,"The value of I_B1 in mA is"); disp(I_B2actual,"The value of I_B2 in mA is");
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11_10.sce
clc //ex11.10 t=[0:0.000001:0.002]; V_i=3*cos(2000*%pi*t)-2*cos(6000*%pi*t); //for A A_1000_A_peak=10; A_1000_A_phi=0; A_3000_A_peak=10; A_3000_A_phi=0; V_o_A=A_1000_A_peak*3*cos(2000*%pi*t+A_1000_A_phi)-A_3000_A_peak*2*cos(6000*%pi*t+A_3000_A_phi); //for B A_1000_B_peak=10; A_1000_B_phi=-%pi/4; A_3000_B_peak=10; A_3000_B_phi=-3*%pi/4; V_o_B=A_1000_B_peak*3*cos(2000*%pi*t+A_1000_B_phi)-A_3000_B_peak*2*cos(6000*%pi*t+A_3000_B_phi); //for C A_1000_C_peak=10; A_1000_C_phi=-%pi/4; A_3000_C_peak=10; A_3000_C_phi=-%pi/4; V_o_C=A_1000_C_peak*3*cos(2000*%pi*t+A_1000_C_phi)-A_3000_C_peak*2*cos(6000*%pi*t+A_3000_C_phi); disp('VoA(t)=30cos(2000%pit)-10cos(6000%pit)') disp('VoB(t)=30cos(2000%pit-%pi/4)-10cos(6000%pit-3%pi/4)') disp('VoC(t)=30cos(2000%pit-%pi/4)-10cos(6000%pit-%pi/4)') subplot(221) xtitle('Output-voltage vs time for A','time in ms','Output-voltage for A in volts') plot(t*10^3,V_o_A) subplot(222) xtitle('Output-voltage vs time for B','time in ms','Output voltage for B in volts') plot(t*10^3,V_o_B) subplot(223) xtitle('Output-voltage vs time for C','time in ms','Output voltage for C in volts') plot(t*10^3,V_o_C)
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test2.tst
'second test file' i write text with many spaces. Space Space Space.
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/scripts/egalisation.sci
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egalisation.sci
function image_out=egalisation(matrice,hist_cum) SizeX = size(matrice,"r"); SizeY = size(matrice,"c"); nb_pixel = SizeX*SizeY; disp (nb_pixel); coef = nb_pixel/255; disp(coef); table = zeros(1,256); for i = 1:256, table(i)= round(hist_cum(i)/coef); end disp(table); image_out= zeros(SizeX,SizeY); for i = 1:SizeX, for j = 1:SizeY, pixel_value = matrice(i,j); image_out(i,j)= table(pixel_value+1); end; end; endfunction
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Ex4_1.sce
// Exa 4.1 clc; clear; // Given data // To design an adder circuit as shown in Fig. 4.2(a) // Vo = -(0.1*V1+V2+10*V3); // V1,V2,V3 are the inputs // Solution printf(' The output in Fig. 4.2(a) is - \n Vo = -[(Rf/R1)*V1 + (Rf/R2)*V2 + (Rf/R3)*V3].'); printf('\n The desired output is -\n Vo = [(0.1)*V1 + (1)*V2 + (10)*V3].'); printf('\n\n Comparing above two equations,'); printf('\n We can say, Let Rf = 10 kΩ, R1 = 100 kΩ and R2 = 10 kΩ and R3 = 1 kΩ.\n'); printf('\n Thus, the desired output expression is obtained.');
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/tests/test_ods_fsed_1_a.tst
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test_ods_fsed_1_a.tst
cd / branch objects dump Total index levels = 0 Total number of nodes = 0 Total number of items = 0 exit
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Example_16_1a.sce
clear; clc; x=poly([0],'x'); printf("\tExample 16.1\n"); printf("\n\tPart A"); E_gf=69; // in GPa Elasticity of glass fibre mf_gf=0.4; //Vol % of glass fibre E_pr=3.4; // in GPa Elasticity of poyester resin mf_pr=0.6; //Vol % of polyester resin E_cl=(E_pr*mf_pr)+(E_gf*mf_gf); printf("\nModulus of elasticity of composite is : %f GPa\n",E_cl); //End
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/3547/CH7/EX7.2/Ex7_2.sce
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Ex7_2.sce
// Example no. 7.2 // To calculate exact and approximate Q-factor if the signal is (a)OOK, (b) PSK // Page no. 311 clc; clear; // Given data lambda=1.55*10^(-6); // Wavelength of given signal meanPin=1; // Mean fiber launch power in dBm alpha=0.2; // fiber loss in dB/km l=240; // fiber length in km neta=0.7; // quantum efficiency T = 290; // Tempearture in K RL=100; // Length resistance in Ω PLOdBm = 10; // Power at local oscillator in dBm Be = 7.5*10^9; // Efficient bandwidth of filter in Hz c=3*10^8; // Speed of ligth in air in m/s loss=alpha*l; // Total fiber loss q=1.602*10^(-19); // Charge of electron h=6.626*10^(-34); // Planck constant kB=1.38*10^(-23); // Bolzman constant f=c/lambda; // mean frequency R=(neta*q)/(h*f); // Responsivity //For OOK Pin=10*log10(2)+meanPin; // peak power in dBm P1rdBm=Pin-loss; // received peak power in dBm P1r=(10^(P1rdBm/10))*10^(-3); // received peak power in W PLO=(10^(PLOdBm/10))*10^(-3); // Power at local oscillator in W I1=2*R*sqrt(P1r*PLO); // mean of bit 1 sigma1=2*q*Be*R*(P1r+PLO)+(4*kB*T*Be)/RL; // Square of variance of bit 1 I0=0; // mean of bit 0 sigma0=sigma1; // Square of variance of bit 0 Q1=(I1-I0)/(2*sqrt(sigma1)); // Exact Q-factor Q2=sqrt((neta*P1r)/(2*h*f*Be)); // Approximate Q-factor // Displaying the result in command window printf('\n Exact Q-factor if the signal is OOK = %0.1f',Q1); printf('\n Approximate Q-factor if the signal is OOK = %0.1f',Q2); // For PSK P1rdBm=meanPin-loss; // received peak power in dBm P1r=(10^(P1rdBm/10))*10^(-3); // received peak power in W I1=2*R*sqrt(P1r*PLO); // mean of bit 1 sigma1=2*q*Be*R*(P1r+PLO)+(4*kB*T*Be)/RL; // Square of variance of bit 1 I0=-I1; // mean of bit 0 sigma0=sigma1; // Square of variance of bit 0 Q1=I1/sqrt(sigma1); // Exact Q-factor Q2=sqrt((2*neta*P1r)/(h*f*Be)); // Approximate Q-factor // Displaying the result in command window printf('\n Exact Q-factor if the signal is PSK = %0.2f',Q1); printf('\n Approximate Q-factor if the signal is PSK = %0.2f',Q2);
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ques2_1.sce
//ques1(ii) disp('To find the laplace of given function in t '); syms t s f=exp(-3*t)*(2*cos(5*t)-3*sin(5*t)); disp(laplace(f,t,s));
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example1.sce
//Chapter-11 example 1 //============================================================================= clc; clear; //Given data F = 10*10^9; //radar operating frequency in Hz Vo = 3*10^8; //vel in m/s; G = 20; //antenna gain in dBi; R = 20*10^3; //distance of radar reflected signal from target Pt = 10*10^3 //Tx power in watts CS = 10; //cross sectional area in m^2 // Calculations Gain = 10^(G/10) //G = 10log(Gain) ==>gain - antilog(20/10); Gr = Gain; //gain of tx antenna and Rx antenna Gt = Gain lamda = Vo/F Pr= (lamda*lamda*Pt*Gt*Gr*CS)/((4*4*4*%pi*%pi*%pi)*(R^4))//received power in watts // Output mprintf('Received signal Power is %g',Pr); mprintf('\n Note : Calculation error in Textbook');
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Example_11_1.sce
//Example 11.1 clear; clc; printf("\tExample 11.1\n"); p0_A=106; //Vapour pressure of n-heptane in kN/m^2 p0_B=73.7; //Vapour pressure of toluene in kN/m^2 P=101.3; //Total pressure in kN/m^2 xA=(P-p0_B)/(p0_A-p0_B); yA=p0_A*xA/P; printf("\nMole fraction in liquid phase is : %.3f",xA); printf("\nMole fraction in vapour phase is : %.3f\n",yA); //End
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Program11_5.sce
//Program 11.5 //Program To Calculate the value of the function //Y=A*X1+B*X2+C*X3 clear; clc; close; //Data A=1; B=2; C=3; X1=4; X2=5; X3=6; //Compute the function Y=A*X1+B*X2+C*X3; //Display the result in command window disp(Y,"Y = A*X1+B*X2+C*X3 = ");
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/New LSTMAttn Model/.data/lemma-split/GOLD-TEST/crh.tst
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şayba şaybadan N;ABL şayba şaybada N;LOC şayba şayba N;NOM şayba şaybanı N;ACC şayba şaybağa N;DAT şayba şaybanıñ N;GEN bal balğa N;DAT bal baldan N;ABL bal balda N;LOC bal balnı N;ACC bal balnıñ N;GEN bal bal N;NOM kontsentratsiya kontsentratsiyanı N;ACC kontsentratsiya kontsentratsiyadan N;ABL kontsentratsiya kontsentratsiya N;NOM kontsentratsiya kontsentratsiyağa N;DAT kontsentratsiya kontsentratsiyada N;LOC kontsentratsiya kontsentratsiyanıñ N;GEN kiraz kirazda N;LOC kiraz kiraznıñ N;GEN kiraz kiraz N;NOM kiraz kiraznı N;ACC kiraz kirazdan N;ABL kiraz kirazğa N;DAT reaktiv reaktivni ADJ;ACC reaktiv reaktivde N;LOC reaktiv reaktivni N;ACC reaktiv reaktivde ADJ;LOC reaktiv reaktivge N;DAT reaktiv reaktiv ADJ;NOM reaktiv reaktivniñ N;GEN reaktiv reaktivge ADJ;DAT reaktiv reaktivden ADJ;ABL reaktiv reaktivniñ ADJ;GEN reaktiv reaktiv N;NOM reaktiv reaktivden N;ABL arnavut arnavutnıñ ADJ;GEN arnavut arnavutqa ADJ;DAT arnavut arnavutta N;LOC arnavut arnavutqa N;DAT arnavut arnavuttan ADJ;ABL arnavut arnavutta ADJ;LOC arnavut arnavuttan N;ABL arnavut arnavutnıñ N;GEN arnavut arnavut N;NOM arnavut arnavut ADJ;NOM arnavut arnavutnı N;ACC arnavut arnavutnı ADJ;ACC yanvar yanvarniñ N;GEN yanvar yanvar N;NOM yanvar yanvarni N;ACC yanvar yanvarde N;LOC yanvar yanvarden N;ABL yanvar yanvarge N;DAT şoqmar şoqmardan N;ABL şoqmar şoqmarğa N;DAT şoqmar şoqmarnı N;ACC şoqmar şoqmarnıñ N;GEN şoqmar şoqmar N;NOM şoqmar şoqmarda N;LOC filatelist filatelistni N;ACC filatelist filatelistniñ N;GEN filatelist filatelistten N;ABL filatelist filatelist N;NOM filatelist filatelistte N;LOC filatelist filatelistke N;DAT çot çotnı N;ACC çot çotqa N;DAT çot çottan N;ABL çot çot N;NOM çot çotta N;LOC çot çotnıñ N;GEN nam namnıñ N;GEN nam namğa N;DAT nam namnı N;ACC nam nam N;NOM nam namda N;LOC nam namdan N;ABL riñg riñgdan N;ABL riñg riñgga N;DAT riñg riñgda N;LOC riñg riñgnıñ N;GEN riñg riñg N;NOM riñg riñgnı N;ACC yel yelniñ N;GEN yel yelden N;ABL yel yelge N;DAT yel yelde N;LOC yel yelni N;ACC yel yel N;NOM rahit rahitniñ N;GEN rahit rahitte N;LOC rahit rahitni N;ACC rahit rahit N;NOM rahit rahitke N;DAT rahit rahitten N;ABL qolçaq qolçaqnıñ N;GEN qolçaq qolçaqta N;LOC qolçaq qolçaq N;NOM qolçaq qolçaqtan N;ABL qolçaq qolçaqnı N;ACC qolçaq qolçaqqa N;DAT qımırsqa qımırsqa N;NOM qımırsqa qımırsqanıñ N;GEN qımırsqa qımırsqada N;LOC qımırsqa qımırsqadan N;ABL qımırsqa qımırsqanı N;ACC qımırsqa qımırsqağa N;DAT elevator elevatordan N;ABL elevator elevatorğa N;DAT elevator elevatornıñ N;GEN elevator elevator N;NOM elevator elevatorda N;LOC elevator elevatornı N;ACC erkmen erkmenge N;DAT erkmen erkmenden N;ABL erkmen erkmende N;LOC erkmen erkmenni N;ACC erkmen erkmen N;NOM erkmen erkmenniñ N;GEN gaz gazğa N;DAT gaz gaz N;NOM gaz gaznı N;ACC gaz gazda N;LOC gaz gazdan N;ABL gaz gaznıñ N;GEN öküz öküznı N;ACC öküz öküzden N;ABL öküz öküzde N;LOC öküz öküznıñ N;GEN öküz öküz N;NOM öküz öküzge N;DAT testimal testimal N;NOM testimal testimalğa N;DAT testimal testimalnı N;ACC testimal testimalda N;LOC testimal testimalnıñ N;GEN testimal testimaldan N;ABL kvartal kvartalda N;LOC kvartal kvartaldan N;ABL kvartal kvartal N;NOM kvartal kvartalnı N;ACC kvartal kvartalnıñ N;GEN kvartal kvartalğa N;DAT kurs kurs N;NOM kurs kurstan N;ABL kurs kursqa N;DAT kurs kursnıñ N;GEN kurs kursnı N;ACC kurs kursta N;LOC şpatel şpatelniñ N;GEN şpatel şpatelden N;ABL şpatel şpatelni N;ACC şpatel şpatelge N;DAT şpatel şpatelde N;LOC şpatel şpatel N;NOM pite piteni N;ACC pite piteden N;ABL pite piteniñ N;GEN pite pitede N;LOC pite pitege N;DAT pite pite N;NOM kassir kassirden N;ABL kassir kassirde N;LOC kassir kassir N;NOM kassir kassirniñ N;GEN kassir kassirni N;ACC kassir kassirge N;DAT rekordçı rekordçınıñ N;GEN rekordçı rekordçı N;NOM rekordçı rekordçıda N;LOC rekordçı rekordçığa N;DAT rekordçı rekordçıdan N;ABL rekordçı rekordçını N;ACC etika etikağa N;DAT etika etikadan N;ABL etika etika N;NOM etika etikanıñ N;GEN etika etikanı N;ACC etika etikada N;LOC çinke çinkege N;DAT çinke çinkeni N;ACC çinke çinkeniñ N;GEN çinke çinkeden N;ABL çinke çinkede N;LOC çinke çinke N;NOM sır sırnıñ N;GEN sır sırnı N;ACC sır sırdan N;ABL sır sırğa N;DAT sır sır N;NOM sır sırda N;LOC calanğaş calanğaşqa N;DAT calanğaş calanğaş ADJ;NOM calanğaş calanğaşta N;LOC calanğaş calanğaşnı N;ACC calanğaş calanğaşnıñ N;GEN calanğaş calanğaşnı ADJ;ACC calanğaş calanğaşnıñ ADJ;GEN calanğaş calanğaştan N;ABL calanğaş calanğaşqa ADJ;DAT calanğaş calanğaşta ADJ;LOC calanğaş calanğaş N;NOM calanğaş calanğaştan ADJ;ABL kreditor kreditordan N;ABL kreditor kreditornıñ N;GEN kreditor kreditornı N;ACC kreditor kreditor N;NOM kreditor kreditorğa N;DAT kreditor kreditorda N;LOC şipşe şipşede N;LOC şipşe şipşege N;DAT şipşe şipşe N;NOM şipşe şipşeni N;ACC şipşe şipşeden N;ABL şipşe şipşeniñ N;GEN semantika semantikanıñ N;GEN semantika semantika N;NOM semantika semantikanı N;ACC semantika semantikağa N;DAT semantika semantikada N;LOC semantika semantikadan N;ABL repetitorlıq repetitorlıqta N;LOC repetitorlıq repetitorlıqnıñ N;GEN repetitorlıq repetitorlıqnı N;ACC repetitorlıq repetitorlıq N;NOM repetitorlıq repetitorlıqqa N;DAT repetitorlıq repetitorlıqtan N;ABL fırçı fırçığa N;DAT fırçı fırçıda N;LOC fırçı fırçıdan N;ABL fırçı fırçı N;NOM fırçı fırçınıñ N;GEN fırçı fırçını N;ACC amam amamğa N;DAT amam amam N;NOM amam amamnıñ N;GEN amam amamnı N;ACC amam amamdan N;ABL amam amamda N;LOC aleket aleketniñ N;GEN aleket alekette N;LOC aleket aleketni N;ACC aleket aleket N;NOM aleket aleketten N;ABL aleket aleketke N;DAT konstruktsiya konstruktsiya N;NOM konstruktsiya konstruktsiyadan N;ABL konstruktsiya konstruktsiyanı N;ACC konstruktsiya konstruktsiyada N;LOC konstruktsiya konstruktsiyanıñ N;GEN konstruktsiya konstruktsiyağa N;DAT kirişmek kirişmek V;NFIN kirişmek kiriş V;IMP;SG;2 kirişmek kirişe V;SG;3;PRS kirişmek kirişti V;SG;3;PST yer yerden N;ABL yer yerde N;LOC yer yerge N;DAT yer yerni N;ACC yer yerniñ N;GEN yer yer N;NOM repetitor repetitornı N;ACC repetitor repetitorğa N;DAT repetitor repetitordan N;ABL repetitor repetitor N;NOM repetitor repetitorda N;LOC repetitor repetitornıñ N;GEN emce emceni N;ACC emce emce N;NOM emce emceden N;ABL emce emcege N;DAT emce emcede N;LOC emce emceniñ N;GEN qonaq qonaqnı N;ACC qonaq qonaqqa N;DAT qonaq qonaqnıñ N;GEN qonaq qonaqta N;LOC qonaq qonaq N;NOM qonaq qonaqtan N;ABL bereket berekette N;LOC bereket bereketni N;ACC bereket bereket N;NOM bereket bereketke N;DAT bereket bereketniñ N;GEN bereket bereketten N;ABL cuqmaq cuqdı V;SG;3;PST cuqmaq cuqmaq V;NFIN cuqmaq cuqa V;SG;3;PRS cuqmaq cuq V;IMP;SG;2 kölek köleknı N;ACC kölek kölekden N;ABL kölek kölekde N;LOC kölek kölek N;NOM kölek kölekıñ N;GEN kölek kölekge N;DAT fikir fikirden N;ABL fikir fikirge N;DAT fikir fikirde N;LOC fikir fikir N;NOM fikir fikirniñ N;GEN fikir fikirni N;ACC çavke çavke N;NOM çavke çavkeni N;ACC çavke çavkeden N;ABL çavke çavkege N;DAT çavke çavkeniñ N;GEN çavke çavkede N;LOC tırnak tırnaknı N;ACC tırnak tırnakdan N;ABL tırnak tırnakda N;LOC tırnak tırnakga N;DAT tırnak tırnak N;NOM tırnak tırnaknıñ N;GEN bağ bağnı N;ACC bağ bağdan N;ABL bağ bağğa N;DAT bağ bağnıñ N;GEN bağ bağ N;NOM bağ bağda N;LOC komissariat komissariatnıñ N;GEN komissariat komissariatqa N;DAT komissariat komissariatta N;LOC komissariat komissariatnı N;ACC komissariat komissariattan N;ABL komissariat komissariat N;NOM capmaq capdı V;SG;3;PST capmaq capa V;SG;3;PRS capmaq cap V;IMP;SG;2 capmaq capmaq V;NFIN sıyırcıq sıyırcıq N;NOM sıyırcıq sıyırcıqqa N;DAT sıyırcıq sıyırcıqnı N;ACC sıyırcıq sıyırcıqnıñ N;GEN sıyırcıq sıyırcıqtan N;ABL sıyırcıq sıyırcıqta N;LOC kupon kuponda N;LOC kupon kupondan N;ABL kupon kuponnıñ N;GEN kupon kuponnı N;ACC kupon kupon N;NOM kupon kuponğa N;DAT elva elvanıñ N;GEN elva elvadan N;ABL elva elvağa N;DAT elva elvada N;LOC elva elva N;NOM elva elvanı N;ACC miy miyden N;ABL miy miyniñ N;GEN miy miyge N;DAT miy miy N;NOM miy miyni N;ACC miy miyde N;LOC kodein kodeinniñ N;GEN kodein kodeinge N;DAT kodein kodeinde N;LOC kodein kodein N;NOM kodein kodeinni N;ACC kodein kodeinden N;ABL registr registrniñ N;GEN registr registrge N;DAT registr registrde N;LOC registr registrni N;ACC registr registrden N;ABL registr registr N;NOM karp karptan N;ABL karp karpnı N;ACC karp karp N;NOM karp karpta N;LOC karp karpnıñ N;GEN karp karpqa N;DAT cımırta cımırta N;NOM cımırta cımırtanı N;ACC cımırta cımırtadan N;ABL cımırta cımırtada N;LOC cımırta cımırtağa N;DAT cımırta cımırtanıñ N;GEN radiotehnika radiotehnikada N;LOC radiotehnika radiotehnika N;NOM radiotehnika radiotehnikağa N;DAT radiotehnika radiotehnikanı N;ACC radiotehnika radiotehnikadan N;ABL radiotehnika radiotehnikanıñ N;GEN filcan filcan N;NOM filcan filcanğa N;DAT filcan filcannı N;ACC filcan filcannıñ N;GEN filcan filcanda N;LOC filcan filcandan N;ABL ant anttan N;ABL ant ant N;NOM ant antqa N;DAT ant antnıñ N;GEN ant antnı N;ACC ant antta N;LOC büst büstke N;DAT büst büstte N;LOC büst büstten N;ABL büst büst N;NOM büst büstni N;ACC büst büstniñ N;GEN caş caşnı ADJ;ACC caş caşnıñ N;GEN caş caştan N;ABL caş caş N;NOM caş caş ADJ;NOM caş caşnı N;ACC caş caştan ADJ;ABL caş caşqa N;DAT caş caşnıñ ADJ;GEN caş caşta N;LOC caş caşqa ADJ;DAT caş caşta ADJ;LOC relâtivizm relâtivizmden N;ABL relâtivizm relâtivizm N;NOM relâtivizm relâtivizmge N;DAT relâtivizm relâtivizmni N;ACC relâtivizm relâtivizmniñ N;GEN relâtivizm relâtivizmde N;LOC qol qoldan N;ABL qol qol N;NOM qol qolnıñ N;GEN qol qolğa N;DAT qol qolda N;LOC qol qolnı N;ACC kâtip kâtipniñ N;GEN kâtip kâtip N;NOM kâtip kâtipten N;ABL kâtip kâtipni N;ACC kâtip kâtipke N;DAT kâtip kâtipte N;LOC energiya energiyadan N;ABL energiya energiya N;NOM energiya energiyanıñ N;GEN energiya energiyada N;LOC energiya energiyanı N;ACC energiya energiyağa N;DAT küç küç N;NOM küç küçte N;LOC küç küçke N;DAT küç küçniñ N;GEN küç küçni N;ACC küç küçten N;ABL kuzov kuzov N;NOM kuzov kuzovnıñ N;GEN kuzov kuzovğa N;DAT kuzov kuzovnı N;ACC kuzov kuzovdan N;ABL kuzov kuzovda N;LOC zeer zeerde N;LOC zeer zeerniñ N;GEN zeer zeerni N;ACC zeer zeer N;NOM zeer zeerge N;DAT zeer zeerden N;ABL faşizm faşizm N;NOM faşizm faşizmniñ N;GEN faşizm faşizmge N;DAT faşizm faşizmde N;LOC faşizm faşizmni N;ACC faşizm faşizmden N;ABL qudababay qudababaydan N;ABL qudababay qudababaynıñ N;GEN qudababay qudababaynı N;ACC qudababay qudababay N;NOM qudababay qudababayda N;LOC qudababay qudababayğa N;DAT may maydan N;ABL may maynıñ N;GEN may maynı N;ACC may mayğa N;DAT may may N;NOM may mayda N;LOC ağır ağırnıñ ADJ;GEN ağır ağırda ADJ;LOC ağır ağırnı ADJ;ACC ağır ağırdan ADJ;ABL ağır ağır ADJ;NOM ağır ağırğa ADJ;DAT kvitantsiya kvitantsiyanı N;ACC kvitantsiya kvitantsiyanıñ N;GEN kvitantsiya kvitantsiya N;NOM kvitantsiya kvitantsiyada N;LOC kvitantsiya kvitantsiyağa N;DAT kvitantsiya kvitantsiyadan N;ABL vazife vazifeniñ N;GEN vazife vazifeden N;ABL vazife vazifege N;DAT vazife vazifede N;LOC vazife vazifeni N;ACC vazife vazife N;NOM banq banq N;NOM banq banqtan N;ABL banq banqta N;LOC banq banqqa N;DAT banq banqnı N;ACC banq banqnıñ N;GEN sviter sviterden N;ABL sviter sviterniñ N;GEN sviter sviterge N;DAT sviter sviter N;NOM sviter sviterni N;ACC sviter sviterde N;LOC kontsert kontsertke N;DAT kontsert kontsertniñ N;GEN kontsert kontsert N;NOM kontsert kontsertni N;ACC kontsert kontsertte N;LOC kontsert kontsertten N;ABL kontributsiya kontributsiyağa N;DAT kontributsiya kontributsiya N;NOM kontributsiya kontributsiyanı N;ACC kontributsiya kontributsiyada N;LOC kontributsiya kontributsiyanıñ N;GEN kontributsiya kontributsiyadan N;ABL kostüm kostümge N;DAT kostüm kostüm N;NOM kostüm kostümden N;ABL kostüm kostümniñ N;GEN kostüm kostümni N;ACC kostüm kostümde N;LOC köpek köpekte N;LOC köpek köpekten N;ABL köpek köpekni N;ACC köpek köpekniñ N;GEN köpek köpekke N;DAT köpek köpek N;NOM marinad marinadğa N;DAT marinad marinadnıñ N;GEN marinad marinad N;NOM marinad marinadda N;LOC marinad marinadnı N;ACC marinad marinaddan N;ABL kommunist kommunistniñ ADJ;GEN kommunist kommunistniñ N;GEN kommunist kommunistten N;ABL kommunist kommunistke N;DAT kommunist kommunistte N;LOC kommunist kommunistte ADJ;LOC kommunist kommunist ADJ;NOM kommunist kommunist N;NOM kommunist kommunistni ADJ;ACC kommunist kommunistni N;ACC kommunist kommunistten ADJ;ABL kommunist kommunistke ADJ;DAT dımlıq dımlıqta N;LOC dımlıq dımlıqqa N;DAT dımlıq dımlıqnıñ N;GEN dımlıq dımlıq N;NOM dımlıq dımlıqnı N;ACC dımlıq dımlıqtan N;ABL bita bitanıñ N;GEN bita bitadan N;ABL bita bitağa N;DAT bita bitada N;LOC bita bitanı N;ACC bita bita N;NOM qudret qudretniñ N;GEN qudret qudrette N;LOC qudret qudretten N;ABL qudret qudret N;NOM qudret qudretke N;DAT qudret qudretni N;ACC egeşmek egeşmek V;NFIN egeşmek egeş V;IMP;SG;2 egeşmek egeşti V;SG;3;PST egeşmek egeşe V;SG;3;PRS isveç isveçni N;ACC isveç isveçten N;ABL isveç isveçniñ N;GEN isveç isveçke N;DAT isveç isveçte N;LOC isveç isveç N;NOM minder minderni N;ACC minder minderden N;ABL minder minder N;NOM minder minderge N;DAT minder minderde N;LOC minder minderniñ N;GEN klub klubnıñ N;GEN klub klubda N;LOC klub klubnı N;ACC klub klubdan N;ABL klub klub N;NOM klub klubğa N;DAT aydayıcı aydayıcınıñ N;GEN aydayıcı aydayıcıdan N;ABL aydayıcı aydayıcını N;ACC aydayıcı aydayıcı N;NOM aydayıcı aydayıcıda N;LOC aydayıcı aydayıcığa N;DAT jüri jüriniñ N;GEN jüri jürini N;ACC jüri jüriden N;ABL jüri jürige N;DAT jüri jüride N;LOC jüri jüri N;NOM şura şuranıñ N;GEN şura şuradan N;ABL şura şura N;NOM şura şurağa N;DAT şura şuranı N;ACC şura şurada N;LOC müzey müzey N;NOM müzey müzeyni N;ACC müzey müzeyden N;ABL müzey müzeyde N;LOC müzey müzeyniñ N;GEN müzey müzeyge N;DAT litvan litvannıñ N;GEN litvan litvanğa N;DAT litvan litvandan N;ABL litvan litvan N;NOM litvan litvannı N;ACC litvan litvanda N;LOC flora floradan N;ABL flora floranıñ N;GEN flora florağa N;DAT flora floranı N;ACC flora florada N;LOC flora flora N;NOM revizionizm revizionizmni N;ACC revizionizm revizionizm N;NOM revizionizm revizionizmge N;DAT revizionizm revizionizmden N;ABL revizionizm revizionizmniñ N;GEN revizionizm revizionizmde N;LOC bestekâr bestekârnıñ N;GEN bestekâr bestekârnı N;ACC bestekâr bestekârğa N;DAT bestekâr bestekâr N;NOM bestekâr bestekârda N;LOC bestekâr bestekârdan N;ABL börü börüde N;LOC börü börüniñ N;GEN börü börü N;NOM börü börüden N;ABL börü börüni N;ACC börü börüge N;DAT abbat abbatnı N;ACC abbat abbatnıñ N;GEN abbat abbattan N;ABL abbat abbat N;NOM abbat abbatqa N;DAT abbat abbatta N;LOC aşıtmaq aşıtdı V;SG;3;PST aşıtmaq aşıta V;SG;3;PRS aşıtmaq aşıt V;IMP;SG;2 aşıtmaq aşıtmaq V;NFIN capma capmañ N;GEN capma capmaga N;DAT capma capmanı N;ACC capma capmada N;LOC capma capmadan N;ABL capma capma N;NOM evakuatsiya evakuatsiyağa N;DAT evakuatsiya evakuatsiya N;NOM evakuatsiya evakuatsiyanı N;ACC evakuatsiya evakuatsiyada N;LOC evakuatsiya evakuatsiyanıñ N;GEN evakuatsiya evakuatsiyadan N;ABL avtomat avtomat N;NOM avtomat avtomattan N;ABL avtomat avtomatqa N;DAT avtomat avtomatnıñ N;GEN avtomat avtomatta N;LOC avtomat avtomatnı N;ACC biber biberni N;ACC biber biberde N;LOC biber biberniñ N;GEN biber biberge N;DAT biber biberden N;ABL biber biber N;NOM madde maddeyi N;ACC madde maddede N;LOC madde maddeden N;ABL madde madde N;NOM madde maddenin N;GEN madde maddeye N;DAT devir devir N;NOM devir devirde N;LOC devir devirniñ N;GEN devir devirni N;ACC devir devirge N;DAT devir devirden N;ABL qurna qurnanıñ N;GEN qurna qurnağa N;DAT qurna qurnanı N;ACC qurna qurnadan N;ABL qurna qurna N;NOM qurna qurnada N;LOC bilyard bilyardğa N;DAT bilyard bilyardnı N;ACC bilyard bilyardda N;LOC bilyard bilyard N;NOM bilyard bilyarddan N;ABL bilyard bilyardnıñ N;GEN sol sol ADJ;NOM sol solnıñ ADJ;GEN sol soldan N;ABL sol sol N;NOM sol soldan ADJ;ABL sol solğa N;DAT sol solnıñ N;GEN sol solda N;LOC sol solnı ADJ;ACC sol solnı N;ACC sol solğa ADJ;DAT sol solda ADJ;LOC materializm materializmdan N;ABL materializm materializmnı N;ACC materializm materializmnıñ N;GEN materializm materializmğa N;DAT materializm materializm N;NOM materializm materializmda N;LOC mikrofon mikrofonğa N;DAT mikrofon mikrofonnıñ N;GEN mikrofon mikrofon N;NOM mikrofon mikrofondan N;ABL mikrofon mikrofonda N;LOC mikrofon mikrofonnı N;ACC defter defterni N;ACC defter defter N;NOM defter defterniñ N;GEN defter defterde N;LOC defter defterden N;ABL defter defterge N;DAT domatis domatiske N;DAT domatis domatisniñ N;GEN domatis domatiste N;LOC domatis domatis N;NOM domatis domatisni N;ACC domatis domatisten N;ABL qapıcı qapıcını N;ACC qapıcı qapıcıdan N;ABL qapıcı qapıcınıñ N;GEN qapıcı qapıcı N;NOM qapıcı qapıcığa N;DAT qapıcı qapıcıda N;LOC emçek emçek N;NOM emçek emçekten N;ABL emçek emçekte N;LOC emçek emçekniñ N;GEN emçek emçekni N;ACC emçek emçekke N;DAT tize tizeden N;ABL tize tizede N;LOC tize tize N;NOM tize tizege N;DAT tize tizeni N;ACC tize tizeniñ N;GEN kurator kuratorda N;LOC kurator kuratorğa N;DAT kurator kurator N;NOM kurator kuratordan N;ABL kurator kuratornıñ N;GEN kurator kuratornı N;ACC sabalıq aş sabalıq aşta N;LOC sabalıq aş sabalıq aşnı N;ACC sabalıq aş sabalıq aş N;NOM sabalıq aş sabalıq aşnıñ N;GEN sabalıq aş sabalıq aşqa N;DAT sabalıq aş sabalıq aştan N;ABL uçucı uçucıdan N;ABL uçucı uçucını N;ACC uçucı uçucınıñ N;GEN uçucı uçucı N;NOM uçucı uçucığa N;DAT uçucı uçucıda N;LOC şlak şlakqa N;DAT şlak şlakta N;LOC şlak şlaknı N;ACC şlak şlak N;NOM şlak şlaktan N;ABL şlak şlaknıñ N;GEN kulminatsiya kulminatsiyada N;LOC kulminatsiya kulminatsiyanıñ N;GEN kulminatsiya kulminatsiyağa N;DAT kulminatsiya kulminatsiyanı N;ACC kulminatsiya kulminatsiya N;NOM kulminatsiya kulminatsiyadan N;ABL sıçan sıçannıñ N;GEN sıçan sıçanğa N;DAT sıçan sıçan N;NOM sıçan sıçannı N;ACC sıçan sıçandan N;ABL sıçan sıçanda N;LOC aborigen aborigenden N;ABL aborigen aborigenge N;DAT aborigen aborigenniñ N;GEN aborigen aborigende N;LOC aborigen aborigen N;NOM aborigen aborigenni N;ACC uçaq uçaqqa N;DAT uçaq uçaqnı N;ACC uçaq uçaqnıñ N;GEN uçaq uçaq N;NOM uçaq uçaqtan N;ABL uçaq uçaqta N;LOC kabinet kabinette N;LOC kabinet kabinet N;NOM kabinet kabinetni N;ACC kabinet kabinetniñ N;GEN kabinet kabinetten N;ABL kabinet kabinetke N;DAT baza bazadan N;ABL baza bazanı N;ACC baza bazanıñ N;GEN baza bazada N;LOC baza bazağa N;DAT baza baza N;NOM reproduktor reproduktornı N;ACC reproduktor reproduktor N;NOM reproduktor reproduktorğa N;DAT reproduktor reproduktordan N;ABL reproduktor reproduktornıñ N;GEN reproduktor reproduktorda N;LOC noyabr noyabr N;NOM noyabr noyabrni N;ACC noyabr noyabrniñ N;GEN noyabr noyabrge N;DAT noyabr noyabrden N;ABL noyabr noyabrde N;LOC linza linzanı N;ACC linza linzağa N;DAT linza linzada N;LOC linza linza N;NOM linza linzadan N;ABL linza linzanıñ N;GEN qaar qaarni N;ACC qaar qaar N;NOM qaar qaarden N;ABL qaar qaarde N;LOC qaar qaarge N;DAT qaar qaarniñ N;GEN radiatsiya radiatsiyanıñ N;GEN radiatsiya radiatsiyağa N;DAT radiatsiya radiatsiya N;NOM radiatsiya radiatsiyanı N;ACC radiatsiya radiatsiyadan N;ABL radiatsiya radiatsiyada N;LOC semafor semafor N;NOM semafor semaforda N;LOC semafor semafornıñ N;GEN semafor semafordan N;ABL semafor semafornı N;ACC semafor semaforğa N;DAT restavratsiya restavratsiyanı N;ACC restavratsiya restavratsiyadan N;ABL restavratsiya restavratsiyanıñ N;GEN restavratsiya restavratsiya N;NOM restavratsiya restavratsiyağa N;DAT restavratsiya restavratsiyada N;LOC atmaca atmacanıñ N;GEN atmaca atmacadan N;ABL atmaca atmacada N;LOC atmaca atmaca N;NOM atmaca atmacanı N;ACC atmaca atmacağa N;DAT dua duanı N;ACC dua duağa N;DAT dua duadan N;ABL dua dua N;NOM dua duanıñ N;GEN dua duada N;LOC kontora kontorada N;LOC kontora kontorağa N;DAT kontora kontoradan N;ABL kontora kontora N;NOM kontora kontoranıñ N;GEN kontora kontoranı N;ACC molla mollanıñ N;GEN molla mollada N;LOC molla mollanı N;ACC molla mollağa N;DAT molla molladan N;ABL molla molla N;NOM krossvord krossvordnı N;ACC krossvord krossvordğa N;DAT krossvord krossvord N;NOM krossvord krossvordnıñ N;GEN krossvord krossvorddan N;ABL krossvord krossvordda N;LOC tirsek tirsekte N;LOC tirsek tirsekni N;ACC tirsek tirsek N;NOM tirsek tirsekke N;DAT tirsek tirsekten N;ABL tirsek tirsekniñ N;GEN şorap şorapdan N;ABL şorap şorapnıñ N;GEN şorap şorapnı N;ACC şorap şorap N;NOM şorap şorapğa N;DAT şorap şorapda N;LOC mehanizm mehanizmden N;ABL mehanizm mehanizmde N;LOC mehanizm mehanizmniñ N;GEN mehanizm mehanizmge N;DAT mehanizm mehanizm N;NOM mehanizm mehanizmni N;ACC bücet bücetten N;ABL bücet bücet N;NOM bücet bücetni N;ACC bücet bücetke N;DAT bücet bücette N;LOC bücet bücetniñ N;GEN yüzbez yüzbezni N;ACC yüzbez yüzbezden N;ABL yüzbez yüzbezge N;DAT yüzbez yüzbezde N;LOC yüzbez yüzbezniñ N;GEN yüzbez yüzbez N;NOM bronhit bronhitniñ N;GEN bronhit bronhitke N;DAT bronhit bronhitte N;LOC bronhit bronhitten N;ABL bronhit bronhit N;NOM bronhit bronhitni N;ACC mehanizatsiya mehanizatsiya N;NOM mehanizatsiya mehanizatsiyağa N;DAT mehanizatsiya mehanizatsiyadan N;ABL mehanizatsiya mehanizatsiyanıñ N;GEN mehanizatsiya mehanizatsiyanı N;ACC mehanizatsiya mehanizatsiyada N;LOC şortı şortığa N;DAT şortı şortı N;NOM şortı şortını N;ACC şortı şortıdan N;ABL şortı şortınıñ N;GEN şortı şortıda N;LOC rupor ruporğa N;DAT rupor rupor N;NOM rupor ruporda N;LOC rupor rupordan N;ABL rupor rupornı N;ACC rupor rupornıñ N;GEN düve düve N;NOM düve düveniñ N;GEN düve düvege N;DAT düve düvede N;LOC düve düveni N;ACC düve düveden N;ABL qolbez qolbezde N;LOC qolbez qolbezden N;ABL qolbez qolbezni N;ACC qolbez qolbez N;NOM qolbez qolbezge N;DAT qolbez qolbezniñ N;GEN süt sütte N;LOC süt süt N;NOM süt sütni N;ACC süt sütke N;DAT süt sütniñ N;GEN süt sütten N;ABL zeytün zeytünge N;DAT zeytün zeytünden N;ABL zeytün zeytünniñ N;GEN zeytün zeytünni N;ACC zeytün zeytünde N;LOC zeytün zeytün N;NOM qısqaayaq qısqaayaqta N;LOC qısqaayaq qısqaayaqnı N;ACC qısqaayaq qısqaayaqtan N;ABL qısqaayaq qısqaayaqqa N;DAT qısqaayaq qısqaayaqnıñ N;GEN qısqaayaq qısqaayaq N;NOM şahmat şahmatnıñ N;GEN şahmat şahmatta N;LOC şahmat şahmat N;NOM şahmat şahmatnı N;ACC şahmat şahmatqa N;DAT şahmat şahmattan N;ABL kamera kamera N;NOM kamera kamerada N;LOC kamera kameranı N;ACC kamera kameradan N;ABL kamera kamerağa N;DAT kamera kameranıñ N;GEN regress regressten N;ABL regress regressniñ N;GEN regress regresske N;DAT regress regress N;NOM regress regresste N;LOC regress regressni N;ACC faktor faktorğa N;DAT faktor faktornıñ N;GEN faktor faktor N;NOM faktor faktordan N;ABL faktor faktorda N;LOC faktor faktornı N;ACC fara farağa N;DAT fara fara N;NOM fara faranı N;ACC fara faranıñ N;GEN fara farada N;LOC fara faradan N;ABL keşe keşede N;LOC keşe keşeniñ N;GEN keşe keşege N;DAT keşe keşeni N;ACC keşe keşeden N;ABL keşe keşe N;NOM ekspress ekspressden N;ABL ekspress ekspressni N;ACC ekspress ekspresske N;DAT ekspress ekspress N;NOM ekspress ekspressniñ N;GEN ekspress ekspresste N;LOC estoniyalı estoniyalıda N;LOC estoniyalı estoniyalıdan N;ABL estoniyalı estoniyalığa N;DAT estoniyalı estoniyalını N;ACC estoniyalı estoniyalı N;NOM estoniyalı estoniyalınıñ N;GEN bas basta N;LOC bas bastan N;ABL bas basnı N;ACC bas bas N;NOM bas basnıñ N;GEN bas basqa N;DAT regata regatadan N;ABL regata regatağa N;DAT regata regatada N;LOC regata regatanıñ N;GEN regata regata N;NOM regata regatanı N;ACC yuvğuç yuvğuçtan N;ABL yuvğuç yuvğuçta N;LOC yuvğuç yuvğuçqa N;DAT yuvğuç yuvğuçnu N;ACC yuvğuç yuvğuç N;NOM yuvğuç yuvğuçnıñ N;GEN ziytin ziytinni N;ACC ziytin ziytinin N;GEN ziytin ziytinge N;DAT ziytin ziytin N;NOM ziytin ziytinde N;LOC ziytin ziytinden N;ABL advokat advokatnıñ N;GEN advokat advokatta N;LOC advokat advokatnı N;ACC advokat advokat N;NOM advokat advokatqa N;DAT advokat advokattan N;ABL tiz tizni N;ACC tiz tizden N;ABL tiz tizde N;LOC tiz tiz N;NOM tiz tizniñ N;GEN tiz tizge N;DAT selitra selitra N;NOM selitra selitrada N;LOC selitra selitranıñ N;GEN selitra selitranı N;ACC selitra selitrağa N;DAT selitra selitradan N;ABL mobilizatsiya mobilizatsiyağa N;DAT mobilizatsiya mobilizatsiyada N;LOC mobilizatsiya mobilizatsiyanı N;ACC mobilizatsiya mobilizatsiyanıñ N;GEN mobilizatsiya mobilizatsiya N;NOM mobilizatsiya mobilizatsiyadan N;ABL şirket şirket N;NOM şirket şirkette N;LOC şirket şirketten N;ABL şirket şirketniñ N;GEN şirket şirketni N;ACC şirket şirketke N;DAT süyrü balıq süyrü balıqtan N;ABL süyrü balıq süyrü balıqqa N;DAT süyrü balıq süyrü balıqta N;LOC süyrü balıq süyrü balıqnıñ N;GEN süyrü balıq süyrü balıqnı N;ACC süyrü balıq süyrü balıq N;NOM kendir kendirge N;DAT kendir kendirde N;LOC kendir kendir N;NOM kendir kendirniñ N;GEN kendir kendirden N;ABL kendir kendirni N;ACC medal medalge N;DAT medal medalni N;ACC medal medalde N;LOC medal medal N;NOM medal medalniñ N;GEN medal medalden N;ABL qan qanğa N;DAT qan qannı N;ACC qan qannıñ N;GEN qan qandan N;ABL qan qan N;NOM qan qanda N;LOC rükzak rükzak N;NOM rükzak rükzaknıñ N;GEN rükzak rükzaknı N;ACC rükzak rükzakqa N;DAT rükzak rükzakta N;LOC rükzak rükzaktan N;ABL şimşir şimşirge N;DAT şimşir şimşirde N;LOC şimşir şimşirniñ N;GEN şimşir şimşirni N;ACC şimşir şimşir N;NOM şimşir şimşirden N;ABL sanitar sanitarnı ADJ;ACC sanitar sanitarğa N;DAT sanitar sanitarda ADJ;LOC sanitar sanitardan ADJ;ABL sanitar sanitar N;NOM sanitar sanitardan N;ABL sanitar sanitarnıñ N;GEN sanitar sanitarnıñ ADJ;GEN sanitar sanitarda N;LOC sanitar sanitarnı N;ACC sanitar sanitarğa ADJ;DAT sanitar sanitar ADJ;NOM şaynik şaynikni N;ACC şaynik şaynikke N;DAT şaynik şaynikniñ N;GEN şaynik şaynik N;NOM şaynik şaynikte N;LOC şaynik şaynikten N;ABL rezervatsiya rezervatsiyadan N;ABL rezervatsiya rezervatsiya N;NOM rezervatsiya rezervatsiyanıñ N;GEN rezervatsiya rezervatsiyanı N;ACC rezervatsiya rezervatsiyada N;LOC rezervatsiya rezervatsiyağa N;DAT sanktsiya sanktsiyadan N;ABL sanktsiya sanktsiyağa N;DAT sanktsiya sanktsiyada N;LOC sanktsiya sanktsiyanıñ N;GEN sanktsiya sanktsiyanı N;ACC sanktsiya sanktsiya N;NOM dişi dişi N;NOM dişi dişiniñ N;GEN dişi dişige N;DAT dişi dişide N;LOC dişi dişiden N;ABL dişi dişini N;ACC toramaq toradı V;SG;3;PST toramaq tora V;IMP;SG;2 toramaq toray V;SG;3;PRS toramaq toramaq V;NFIN el elni N;ACC el el N;NOM el elge N;DAT el elde N;LOC el elden N;ABL el elniñ N;GEN say say N;NOM say sayğa N;DAT say saynıñ N;GEN say saydan N;ABL say sayda N;LOC say saynı N;ACC abonement abonementke N;DAT abonement abonement N;NOM abonement abonementte N;LOC abonement abonementten N;ABL abonement abonementni N;ACC abonement abonementniñ N;GEN bagaj bagajğa N;DAT bagaj bagajda N;LOC bagaj bagajnıñ N;GEN bagaj bagaj N;NOM bagaj bagajnı N;ACC bagaj bagajdan N;ABL salüt salütqa N;DAT salüt salüttan N;ABL salüt salüt N;NOM salüt salütnı N;ACC salüt salütta N;LOC salüt salütnıñ N;GEN avdarmaq avdarmaq V;NFIN avdarmaq avdara V;SG;3;PRS avdarmaq avdar V;IMP;SG;2 avdarmaq avdardı V;SG;3;PST cıltıramaq cıltıramaq V;NFIN cıltıramaq cıltıray V;SG;3;PRS cıltıramaq cıltıradı V;SG;3;PST cıltıramaq cıltıra V;IMP;SG;2 yemiş yemişte N;LOC yemiş yemişniñ N;GEN yemiş yemişni N;ACC yemiş yemişten N;ABL yemiş yemişke N;DAT yemiş yemiş N;NOM brak brakqa N;DAT brak brak N;NOM brak brakta N;LOC brak braknıñ N;GEN brak braktan N;ABL brak braknı N;ACC sentâbr sentâbr N;NOM sentâbr sentâbrde N;LOC sentâbr sentâbrden N;ABL sentâbr sentâbrni N;ACC sentâbr sentâbrge N;DAT sentâbr sentâbrniñ N;GEN fleyta fleyta N;NOM fleyta fleytanıñ N;GEN fleyta fleytadan N;ABL fleyta fleytada N;LOC fleyta fleytağa N;DAT fleyta fleytanı N;ACC fizika fizikağa N;DAT fizika fizikada N;LOC fizika fizikanıñ N;GEN fizika fizikadan N;ABL fizika fizikanı N;ACC fizika fizika N;NOM qısqaç qısqaçtan N;ABL qısqaç qısqaçta N;LOC qısqaç qısqaçqa N;DAT qısqaç qısqaçnıñ N;GEN qısqaç qısqaçnı N;ACC qısqaç qısqaç N;NOM missiya missiyanıñ N;GEN missiya missiya N;NOM missiya missiyadan N;ABL missiya missiyanı N;ACC missiya missiyada N;LOC missiya missiyağa N;DAT aqsüyek aqsüyekniñ N;GEN aqsüyek aqsüyek N;NOM aqsüyek aqsüyekten N;ABL aqsüyek aqsüyekni N;ACC aqsüyek aqsüyekte N;LOC aqsüyek aqsüyekke N;DAT reyting reyting N;NOM reyting reytingni N;ACC reyting reytingden N;ABL reyting reytingge N;DAT reyting reytingde N;LOC reyting reytingniñ N;GEN isviçriyalı isviçriyalıdan N;ABL isviçriyalı isviçriyalıda N;LOC isviçriyalı isviçriyalı N;NOM isviçriyalı isviçriyalığa N;DAT isviçriyalı isviçriyalınıñ N;GEN isviçriyalı isviçriyalını N;ACC avurmaq avur V;IMP;SG;2 avurmaq avurmaq V;NFIN avurmaq avurdı V;SG;3;PST avurmaq avura V;SG;3;PRS burçaq burçaq N;NOM burçaq burçaqnı N;ACC burçaq burçaqqa N;DAT burçaq burçaqtan N;ABL burçaq burçaqta N;LOC burçaq burçaqnıñ N;GEN bufer bufer N;NOM bufer buferni N;ACC bufer buferde N;LOC bufer buferniñ N;GEN bufer buferden N;ABL bufer buferge N;DAT refleksologiya refleksologiyanı N;ACC refleksologiya refleksologiyanıñ N;GEN refleksologiya refleksologiyadan N;ABL refleksologiya refleksologiya N;NOM refleksologiya refleksologiyağa N;DAT refleksologiya refleksologiyada N;LOC mandarin mandarinden N;ABL mandarin mandarinni N;ACC mandarin mandarin N;NOM mandarin mandaringe N;DAT mandarin mandarinniñ N;GEN mandarin mandarinde N;LOC kiyev kiyevniñ N;GEN kiyev kiyevde N;LOC kiyev kiyevden N;ABL kiyev kiyevni N;ACC kiyev kiyevge N;DAT kiyev kiyev N;NOM avantürist avantüristni N;ACC avantürist avantürist N;NOM avantürist avantüristke N;DAT avantürist avantüristten N;ABL avantürist avantüristte N;LOC avantürist avantüristniñ N;GEN element elementke N;DAT element elementniñ N;GEN element elementten N;ABL element elementni N;ACC element element N;NOM element elementte N;LOC yavluq yavluq N;NOM yavluq yavluqqa N;DAT yavluq yavluqnı N;ACC yavluq yavluqtan N;ABL yavluq yavluqnıñ N;GEN yavluq yavluqta N;LOC ayvan ayvan N;NOM ayvan ayvannıñ N;GEN ayvan ayvandan N;ABL ayvan ayvannı N;ACC ayvan ayvanğa N;DAT ayvan ayvanda N;LOC frenk frenkniñ ADJ;GEN frenk frenkke ADJ;DAT frenk frenkten N;ABL frenk frenkni N;ACC frenk frenkni ADJ;ACC frenk frenkniñ N;GEN frenk frenkte N;LOC frenk frenkten ADJ;ABL frenk frenk ADJ;NOM frenk frenk N;NOM frenk frenkte ADJ;LOC frenk frenkke N;DAT cuqa cuqadan ADJ;ABL cuqa cuqada ADJ;LOC cuqa cuqanı ADJ;ACC cuqa cuqanıñ ADJ;GEN cuqa cuqa ADJ;NOM cuqa cuqağa ADJ;DAT kotlet kotletni N;ACC kotlet kotlet N;NOM kotlet kotletke N;DAT kotlet kotlette N;LOC kotlet kotletniñ N;GEN kotlet kotletten N;ABL kibernetika kibernetikadan N;ABL kibernetika kibernetikağa N;DAT kibernetika kibernetikanı N;ACC kibernetika kibernetikanıñ N;GEN kibernetika kibernetikada N;LOC kibernetika kibernetika N;NOM kreyser kreyserde N;LOC kreyser kreyser N;NOM kreyser kreyserden N;ABL kreyser kreyserge N;DAT kreyser kreyserni N;ACC kreyser kreyserniñ N;GEN cuvurmaq cuvura V;SG;3;PRS cuvurmaq cuvurmaq V;NFIN cuvurmaq cuvurdı V;SG;3;PST cuvurmaq cuvur V;IMP;SG;2 eşelon eşelondan N;ABL eşelon eşelonda N;LOC eşelon eşelonnıñ N;GEN eşelon eşelon N;NOM eşelon eşelonğa N;DAT eşelon eşelonnı N;ACC reket reketniñ N;GEN reket reket N;NOM reket rekette N;LOC reket reketke N;DAT reket reketten N;ABL reket reketni N;ACC arslan arslannıñ N;GEN arslan arslanda N;LOC arslan arslanğa N;DAT arslan arslannı N;ACC arslan arslandan N;ABL arslan arslan N;NOM domates domatesi N;ACC domates domatese N;DAT domates domates N;NOM domates domatesin N;GEN domates domateste N;LOC domates domatesten N;ABL dondurma dondurma N;NOM dondurma dondurmada N;LOC dondurma dondurmadan N;ABL dondurma dondurmağa N;DAT dondurma dondurmanıñ N;GEN dondurma dondurmanı N;ACC poçta poçtanıñ N;GEN poçta poçtadan N;ABL poçta poçta N;NOM poçta poçtanı N;ACC poçta poçtağa N;DAT poçta poçtada N;LOC cılıtmaq cılıt V;IMP;SG;2 cılıtmaq cılıta V;SG;3;PRS cılıtmaq cılıtmaq V;NFIN cılıtmaq cılıtdı V;SG;3;PST keks kekste N;LOC keks keks N;NOM keks keksten N;ABL keks kekske N;DAT keks keksniñ N;GEN keks keksni N;ACC rentabellik rentabellikten N;ABL rentabellik rentabellikke N;DAT rentabellik rentabellikni N;ACC rentabellik rentabellikte N;LOC rentabellik rentabellik N;NOM rentabellik rentabellikniñ N;GEN maşna maşna N;NOM maşna maşnada N;LOC maşna maşnağa N;DAT maşna maşnadan N;ABL maşna maşnanıñ N;GEN maşna maşnanı N;ACC kapitulâtsiya kapitulâtsiyanıñ N;GEN kapitulâtsiya kapitulâtsiyağa N;DAT kapitulâtsiya kapitulâtsiyada N;LOC kapitulâtsiya kapitulâtsiya N;NOM kapitulâtsiya kapitulâtsiyadan N;ABL kapitulâtsiya kapitulâtsiyanı N;ACC müyüz müyüzde N;LOC müyüz müyüzni N;ACC müyüz müyüzden N;ABL müyüz müyüzge N;DAT müyüz müyüzniñ N;GEN müyüz müyüz N;NOM qartana qartanadan N;ABL qartana qartananı N;ACC qartana qartananıñ N;GEN qartana qartana N;NOM qartana qartanağa N;DAT qartana qartanada N;LOC egoizm egoizmde N;LOC egoizm egoizmni N;ACC egoizm egoizmniñ N;GEN egoizm egoizmden N;ABL egoizm egoizm N;NOM egoizm egoizmge N;DAT bavını tapmaq bavını tapdı V;SG;3;PST bavını tapmaq bavını tap V;IMP;SG;2 bavını tapmaq bavını tapa V;SG;3;PRS bavını tapmaq bavını tapmaq V;NFIN batalyon batalyonda N;LOC batalyon batalyonğa N;DAT batalyon batalyon N;NOM batalyon batalyonnı N;ACC batalyon batalyonnıñ N;GEN batalyon batalyondan N;ABL relaksatsiya relaksatsiyanı N;ACC relaksatsiya relaksatsiyada N;LOC relaksatsiya relaksatsiyağa N;DAT relaksatsiya relaksatsiyadan N;ABL relaksatsiya relaksatsiya N;NOM relaksatsiya relaksatsiyanıñ N;GEN manövr manövrge N;DAT manövr manövr N;NOM manövr manövrni N;ACC manövr manövrniñ N;GEN manövr manövrden N;ABL manövr manövrde N;LOC böcek böcekke N;DAT böcek böcekte N;LOC böcek böcekten N;ABL böcek böcekniñ N;GEN böcek böcekni N;ACC böcek böcek N;NOM reforma reformağa N;DAT reforma reformadan N;ABL reforma reforma N;NOM reforma reformanı N;ACC reforma reformanıñ N;GEN reforma reformada N;LOC til til N;NOM til tilde N;LOC til tilden N;ABL til tilge N;DAT til tilni N;ACC til tilniñ N;GEN konduktor konduktornıñ N;GEN konduktor konduktorda N;LOC konduktor konduktorğa N;DAT konduktor konduktordan N;ABL konduktor konduktornı N;ACC konduktor konduktor N;NOM getto gettonı N;ACC getto gettonıñ N;GEN getto gettoğa N;DAT getto gettodan N;ABL getto gettoda N;LOC getto getto N;NOM körük körükten N;ABL körük körükni N;ACC körük körükke N;DAT körük körük N;NOM körük körükte N;LOC körük körükniñ N;GEN gerdanlıq gerdanlıqnıñ N;GEN gerdanlıq gerdanlıqta N;LOC gerdanlıq gerdanlıqtan N;ABL gerdanlıq gerdanlıq N;NOM gerdanlıq gerdanlıqqa N;DAT gerdanlıq gerdanlıqnı N;ACC rumın rumınnı N;ACC rumın rumınnıñ N;GEN rumın rumından N;ABL rumın rumında N;LOC rumın rumın N;NOM rumın rumınğa N;DAT sarkoma sarkomanı N;ACC sarkoma sarkomada N;LOC sarkoma sarkomadan N;ABL sarkoma sarkoma N;NOM sarkoma sarkomanıñ N;GEN sarkoma sarkomağa N;DAT
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[ "BSD-2-Clause" ]
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round.sce
// Calculating the round. y = [1.2, 1, 1.9; 4, 2.6, 5; 2.3, 8, 7]; roundres = armaMat("round",y)
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refs/heads/master
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clear; clc; //Example 4.2 V_pi=50;//(V) Icq=1;//(mA) ro=V_pi/Icq; printf('\nsmall signal output resistance=%.1f KOhm\n',ro) Rc=6; g_m=38.5; r_pi=2.6; Rb=50; Av=-(g_m)*(Rc*ro/(Rc+ro))*r_pi/(r_pi+Rb); printf('\nsmall signal voltage gain=%.2f \n',Av)
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function [p,cap]=max_cap_path(i,j,g) // Copyright INRIA [lhs,rhs]=argn(0) if rhs<>3 then error(39), end // check i and j if prod(size(i))<>1 then error('First argument must be a scalar') end if prod(size(j))<>1 then error('Second argument must be a scalar') end // check g check_graph(g) // compute lp, la and ls n=g('node_number') ma=prod(size(g('tail'))) if g('directed')==1 then [lp,la,ls]=m6ta2lpd(g('tail'),g('head'),n+1,n) else [lp,la,ls]=m6ta2lpu(g('tail'),g('head'),n+1,n,2*ma) end // check max capacity if g('edge_max_cap')==[] then cap=0 p=[] return end // compute max capacity path [c,v]=m6chcm(i,la,lp,ls,n,g('edge_max_cap')) p=m6prevn2p(i,j,v,la,lp,ls,g('directed')) cap=c(j)
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// Scilab Code Ex6.5: Page-371 (2011) clc;clear; lambda = 3.6e-011;....// Wavelength of X-rays, m n = 1; // Order of diffraction theta = 4.8; // Angle of diffraction, degrees // Braggs equation for X-rays is n*lambda = 2*d*sin(theta), solving for d d = n*lambda/(2*sind(theta)); // Interplanar spacing, m printf("\nThe interplanar separation of atomic planes in the crystal = %4.2f angstrom", d/1e-010); // Result // The interplanar separation of atomic planes in the crystal = 2.15 angstrom
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clc; //Example 17.1 //Page No 690 //solution p1=10*10^-3; p2=0.5*10^-3; disp("(a)The power levels, "); P1=10*log10(p1/0.001); disp('dBm',P1,"P = "); P2=10*log10(p2/0.001) disp('dBm',round(P2),"P = "); disp("(b)The difference "); P=10*log10(p1/p2); disp('dBm',round(P),"diff = "); disp("The 10mW power level is 13dB higher than 0.5W power level. ");
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//Ex3_5 clc BF1=100 disp("BF1 = "+string(BF1)+" ") //BJT gain VCC=20 disp("VCC = "+string(VCC)+" volts") // collector supply voltage VBB=VCC RL=5*(10^3) disp("resistance,RL= "+string(RL)+ " ohm") //initialization RB=965*(10^3) disp("resistance,RB = "+string(RB)+ " ohm") //initialization VBE=(0.7) disp("VBE = "+string(VBE)+" volts") // value of base-emitter voltage ICO=10*10^(-9) disp("ICO = "+string(ICO)+" ampere") // collector reverse bias current Vi=0 disp("Vi = "+string(Vi)+" volts") // value of input IBQ=(VCC-VBE)/RB //base current as operating point disp("IBQ = "+string(IBQ)+" ampere") ICQ1=BF1*IBQ //operating point (collector current) disp("ICQ1 =BF1*IBQ= "+string(ICQ1)+" ampere") // calculation VCEQ1=VCC-ICQ1*RL // collector-emitter voltage as operating point disp("VCEQ1 =VCC-ICQ1*RL = "+string(VCEQ1)+" volts") //calculation
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function [x,y] = myfunc(a,b) m = a^2 + b^2; x = a + m; y = b + m; endfunction
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// Example 24_32 clc;funcprot(0); //Given data T_1=15+273;// K p_1=1;// bar p_r=6;// Pressure ratio T_4=750+273;// K e=0.75;// Effectiveness of heat exchanger n_c=0.80;// Isentropic efficiency of compressor n_t=0.85;// Isentropic efficiency of turbine C_pa=1;// kJ/kg.K C_pg=1;// kJ/kg.K r=1.4;// Specific heat ratio //Calculation T_2a=T_1*(p_r)^((r-1)/r);// K T_2=((T_2a-T_1)/n_c)+T_1;// K p_2=p_1*p_r;// bar p_3=sqrt(p_1*p_2);// bar p_r1=p_2/p_3;// Pressure ratio p_r2=p_r1; T_5a=T_4/(p_r1)^((r-1)/r);// K T_5=T_4-(n_t*(T_4-T_5a));// K T_6=T_4;// K T_7=T_5;// K T_3=T_2+(e*(T_7-T_2));// K W_c=C_pa*(T_2-T_1);// The work of compression in kJ/kg W_t=2*C_pg*(T_4-T_5);// The work developed by both turbines in kJ/kg W_n=W_t-W_c;// Net work in kJ/kg Q_1=C_pg*(T_4-T_3);// kJ/kg Q_2=C_pa*(T_6-T_5);// kJ/kg Q_s=Q_1+Q_2;// The total heat supplied in kJ/kg W_r=W_n/W_t;// Work ratio n_p=(W_n/Q_s)*100;// The plant efficiency in % printf('\nEfficiency of the plant=%0.1f percentage \nWork ratio=%0.4f',n_p,W_r); // The answer vary due to round off error
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// A Texbook on POWER SYSTEM ENGINEERING // A.Chakrabarti, M.L.Soni, P.V.Gupta, U.S.Bhatnagar // DHANPAT RAI & Co. // SECOND EDITION // PART II : TRANSMISSION AND DISTRIBUTION // CHAPTER 7: UNDERGROUND CABLES // EXAMPLE : 7.9 : // Page number 215 clear ; clc ; close ; // Clear the work space and console // Given data d = 2.5 // Conductor diameter(cm) D = 6.0 // Sheath diameter(cm) V_l = 66.0 // Line Voltage(kV) // Calculations alpha = (D/d)**(1.0/3) // α d_1 = d*alpha // Best position of first intersheath(cm) d_2 = d_1*alpha // Best position of second intersheath(cm) V = V_l/3**0.5*2**0.5 // Peak voltage on core(kV) V_2 = V/(1+(1/alpha)+(1/alpha**2)) // Peak voltage on second intersheath(kV) V_1 = (1+(1/alpha))*V_2 // Voltage on first intersheath(kV) stress_max = 2*V/(d*log(D/d)) // Maximum stress without intersheath(kV/cm) stress_min = stress_max*d/D // Minimum stress without intersheath(kV/cm) g_max = V*3/(1+alpha+alpha**2) // Maximum stress with intersheath(kV/cm) // Results disp("PART II - EXAMPLE : 7.9 : SOLUTION :-") printf("\nMaximum stress without intersheath = %.2f kV/cm", stress_max) printf("\nBest position of first intersheath, d_1 = %.2f cm", d_1) printf("\nBest position of second intersheath, d_2 = %.3f cm", d_2) printf("\nMaximum stress with intersheath = %.2f kV/cm", g_max) printf("\nVoltage on the first intersheath, V_1 = %.2f kV", V_1) printf("\nVoltage on the second intersheath, V_2 = %.2f kV \n", V_2) printf("\nNOTE: Changes in the obtained answer is due to more precision here")
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// Scilab Code Ex6.9 : X-ray Diffraction by crystal planes: Page-137 (2010) // For (221) planes h = 2; k = 2; l = 1; // Miller Indices for planes in a cubic crystal a = 2.68e-010; // Interatomic spacing, m n = 1; // First Order of diffraction theta = 8.5; // Glancing angle at which Bragg's reflection occurs, degrees d = a/(h^2+k^2+l^2)^(1/2); // The interplanar spacing for cubic crystal, m lambda = 2*d*sind(theta); // Bragg's Law for wavelength of X-rays, m n = 2; // Second order of diffraction theta = asind(n*lambda/(2*d)); // Angle at which second order Bragg reflection occurs, degrees printf("\nThe interplanar spacing between consecutive (221) planes = %5.3e", d); printf("\nThe wavelength of X-rays = %5.3f angstrom", lambda/1e-010); printf("\nThe angle at which second order Bragg reflection occurs = %4.1f degrees", theta); // Result // The interplanar spacing between consecutive (221) planes = 8.933e-011 // The wavelength of X-rays = 0.264 angstrom // The angle at which second order Bragg reflection occurs = 17.2 degrees
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clc; delt=80-20; //change in temp in celcius m=3; //mass in lb c=4185; //specific heat in J/kg.celcius Q=m*c*delt; //calculating heat required disp(Q,"Heat required in Joule = "); //displaying result
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//Example 2.8 // the density of magnetic field clc; clear; close; //given data : Va=6000; // in volts l=.033; // in m L=.22; // in m D=0.044; // in m m=9.109*10^-31; // in kg e=1.602*10^-19; A=sqrt(e/(2*m*Va)); C=(L*l*A); B=(D/C)*10^3; disp(B,"the density magnetic field,B(mWb/m^2) = ")
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; acos.tst ; ; Copyright 2009-2023, Arm Limited. ; SPDX-License-Identifier: MIT OR Apache-2.0 WITH LLVM-exception func=acos op1=7ff80000.00000001 result=7ff80000.00000001 errno=0 func=acos op1=fff80000.00000001 result=7ff80000.00000001 errno=0 func=acos op1=7ff00000.00000001 result=7ff80000.00000001 errno=0 status=i func=acos op1=fff00000.00000001 result=7ff80000.00000001 errno=0 status=i func=acos op1=7ff00000.00000000 result=7ff80000.00000001 errno=EDOM status=i func=acos op1=fff00000.00000000 result=7ff80000.00000001 errno=EDOM status=i func=acos op1=00000000.00000000 result=3ff921fb.54442d18.469 errno=0 func=acos op1=80000000.00000000 result=3ff921fb.54442d18.469 errno=0 func=acos op1=3ff00000.00000000 result=00000000.00000000 errno=0 func=acos op1=bff00000.00000000 result=400921fb.54442d18.469 errno=0 func=acos op1=3ff00000.00000001 result=7ff80000.00000001 errno=EDOM status=i func=acos op1=bff00000.00000001 result=7ff80000.00000001 errno=EDOM status=i
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// Function Name: inplaceTrans // Returns transposed matrix // Calculating the inplaceTrans inputMat = [ 1, 2; 3, 4;] result = armaMatFunc("inplaceTrans",inputMat)
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//Chapter 2,Ex2.55,Pg2.68 clc; disp("Refer to the diagram shown in the figure") //Calculation of Vth //The network is divided into meshes and Kirchoff's laws are applied to the meshes to obtain simultaneous equations A=[4 -2;-1 4] B=[-25;10] I=A\B printf("\n I1=%.0f A \n",I(1)) printf("\n I2=%.0f A \n",I(2)) Vth=(2*I(1))+(2*I(2)) printf("\n Vth=%.0f V \n",Vth) //Calculation of Rth //Convert star resistances formed by 2 ohms, 2 ohms and 1 ohm into an equivalent delta network R1=2*2/(2+2+1) R2=R1 //R1=R2 since the resistances are of equal value R3=2*1/(2+1+2) Rth=8*(2*(4*1/(4+1)))/(8+(2*(4*1/(4+1)))) printf("\n Rth=%.2f ohms \n",Rth) //Calculation of load current Il=Vth/(Rth+10) printf("\n Il=%.2f A \n",Il)
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Engineering Thermodynamics by Onkar Singh Chapter 4 Example 11") n_carnot=0.5;//efficiency of carnot power cycle m=0.5;//mass of air in kg p2=7*10^5;//final pressure in pa v2=0.12;//volume in m^3 R=287;//gas constant in J/kg K Q_23=40*1000;//heat transfer to the air during isothermal expansion in J Cp=1.008;//specific heat at constant pressure in KJ/kg K Cv=0.721;//specific heat at constant volume in KJ/kg K disp("let thermodynamic properties be denoted with respect to salient states;") disp("n_carnot=1-T1/T2") disp("so T1/T2=1-0.5") 1-0.5 disp("so T1/T2=0.5") disp("or T2=2*T1") disp("corresponding to state 2,p2*v2=m*R*T2") disp("so temperature(T2)=p2*v2/(m*R) in K") T2=p2*v2/(m*R) disp("heat transferred during process 2-3(isothermal expansion),Q_23=40 KJ") disp("Q_23=W_23=p2*v2*log(v3/v2)") disp("so volume(v3)=v2*exp(Q_23/(p2*v2)) in m^3") v3=v2*exp(Q_23/(p2*v2)) disp("temperature at state 1,T1=T2/2 in K") T1=T2/2 disp("during process 1-2,T2/T1=(p2/p1)^((y-1)/y)") disp("here expansion constant(y)=Cp/Cv") y=Cp/Cv disp("so pressure(p1)=p2/(T2/T1)^(y/(y-1)) in pa") p1=p2/(T2/T1)^(y/(y-1)) disp("p1 in bar") p1=p1/10^5 disp("thus p1*v1=m*R*T1") disp("so volume(v1)=m*R*T1/(p1*10^5) in m^3") v1=m*R*T1/(p1*10^5) disp("heat transferred during process 4-1(isothermal compression)shall be equal to the heat transferred during process2-3(isothermal expansion).") disp("for isentropic process,dQ=0,dW=dU") disp("during process 1-2,isentropic process,W_12=-m*Cv*(T2-T1)in KJ") disp("Q_12=0,") W_12=-m*Cv*(T2-T1) disp("W_12=-105.51 KJ(-ve work)") disp("during process 3-4,isentropic process,W_34=-m*Cv*(T4-T3)in KJ") disp("Q_31=0,") T4=T1; T3=T2; W_34=-m*Cv*(T4-T3) disp("ANS:") disp("W_34=+105.51 KJ(+ve work)") disp("so for process 1-2,heat transfer=0,work interaction=-105.51 KJ") disp("for process 2-3,heat transfer=40 KJ,work intercation=40 KJ") disp("for process 3-4,heat transfer=0,work interaction=+105.51 KJ") disp("for process 4-1,heat transfer=-40 KJ,work interaction=-40 KJ") disp("maximum temperature of cycle=585.36 KJ") disp("minimum temperature of cycle=292.68 KJ") disp("volume at the end of isothermal expansion=0.1932 m^3")
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ex12_3.sce
// Exa 12.3 format('v',6) clc; clear; close; // Given data memory = 16;// in K memory= memory*1024;// in bits // Number of bits of storage, Req_add_bits= log(memory)/log(2); disp(Req_add_bits,"Number of bits of storage is : ") disp(Req_add_bits,"Number of lines in address bus is : ")
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13_7.sce
//To find revolutions of arm clc //Given: TA=40, TD=90 //Solution: //Calculating the number of teeth on gears B and C //From geometry of the Fig. 13.11, dA+2*dB=dD. //Since the number of teeth are proportional to their pitch circle diameters, TB=(TD-TA)/2 TC=TB //Refer Table 13.6 //Speed of arm when A makes 1 revolution clockwise and D makes half revolution anticlockwise: //Calculating the values of x and y //From the fourth row of the table, -x-y = -1, or x+y = 1 .....(i) //The gear D makes half revolution anticlockwise, i.e., x*(TA/TD)-y = 1/2 .....(ii) A=[1 1; TA/TD -1] B=[1; 1/2] V=A \ B x=V(1) y=V(2) //Calculating the speed of arm varm=-y //Speed of arm, revolutions //Results: printf("\n\n Speed of arm when A makes 1 revolution clockwise and D makes half revolution anticlockwise = %.2f revolution anticlockwise.\n\n",varm) //Speed of arm when A makes 1 revolution clockwise and D is stationary: //Calculating the values of x and y //From the fourth row of the table, -x-y = -1, or x+y = 1 .....(iii) //The gear D is stationary, i.e., x*(TA/TD)-y = 0 .....(iv) A=[1 1; TA/TD -1] B=[1; 0] V=A \ B x=V(1) y=V(2) //Calculating the speed of arm varm=-y //Speed of arm, revolutions //Results: printf(" Speed of arm when A makes 1 revolution clockwise and D is stationary = %.3f revolution clockwise.\n\n",-varm)
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Example43_5.sce
//Given that M = 2.71 //in g R = 4490 //in Bq fraction = 1.17/100 Mo = 74.555 //gm/mol Na = 6.023*10^23 //n /mol //Sample Problem 43-5 txt = mopen('Example43_5_result.txt','wt') mfprintf(txt, '**Sample Problem 43-5**\n') Nk = Na * M * fraction/Mo Th = log(2)*Nk/R mfprintf(txt, 'The half life of the substance is %eSec', Th)
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ex_2_9.sce
//Example 2.9:Convolution Integral clear; close; clc; t =-2:1/100:2; for i=1:length(t) if t(i)<-1|t(i)>1 then x(i)=0; else x(i)=1; end end ty=-2:1/100:4; for i=1:length(ty) if ty(i)<-1|ty(i)>3 then y(i)=0; elseif ty(i)<1 y(i)=1+ty(i); else y(i)=3-ty(i); end end figure a=gca(); a.x_location="origin"; a.y_location="origin"; plot2d(t,x) xtitle('Input Response','t','x(t)'); a.children.children.thickness = 3; a.children.children.foreground= 2; figure a=gca(); a.y_location="origin"; a.x_location="origin"; plot2d(ty,y) xtitle('Output Response','t','y(t)'); a.children.children.thickness = 3; a.children.children.foreground= 2; //since it is a time invariant system for x(t-2) o/p is y(t-2) ty1=ty+2; figure a=gca(); a.y_location="origin"; a.x_location="origin"; plot2d(ty1,y) xtitle('Output Response','t','y(t-2)'); a.children.children.thickness = 3; a.children.children.foreground= 2; //since the system is linear,for x(t)/2 o/p is y(t)/2 figure a=gca(); a.y_location="origin"; a.x_location="origin"; plot2d(ty,y./2) xtitle('Output Response','t','.5*y(t)'); a.children.children.thickness = 3; a.children.children.foreground= 2;
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exa14_1.sce
// Example 14.1 // From figure 14.7(a) // Let us assume some Values to R's and C for illustration purpose R=5; C=0.1*10^-6; s=%s; // Conductance matrix from figure 14.7(b) Y_11=s*C+1/R; Y_12=-s*C; Y_21=Y_12; Y_22=Y_11; Y=[Y_11,Y_12;Y_21,Y_22]; delta=det(Y); // Solving matrix equation // Y*[V_1;V_2]=[I_1;I_2] // On application of Cramer's Rule we get // V_1=(Y_22/delta)*I_1-(Y_12/delta)*I_2 ----equqtion(1) //V_2=-(Y_21/delta)*I_1+(Y_11/delta)*I_2 ----equation(2) // comparing above equations with z-parameter matrix equation z_11=Y_11/delta; z_22=z_11; z_12=-Y_12/delta; z_21=z_12; Z=[z_11,z_12;z_21,z_22]; disp(Z,"Z-Parameters=")
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ex2_9.sce
// Example 2.9 page no-58 clear clc A=60.2*10^4 //A/m^2/°K^2 B=52400 //°K T1=2400 //°K T2=2410 //°K js1=A*T1^2*(%e^(-B/T1)) js2=A*T2^2*(%e^(-B/T2)) js1=floor(js1) js2=floor(js2) printf("\nJS1=%d A/m^2\nJS2=%d A/m^2",js1,js2) p=(js2-js1)*100/js1 printf("\nPercentage Increase=%.2f%%",p)
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example_3_6.sce
//Chapter 3 //Example 3-6 //ProbonOutputVoltage //Page 51 clear;clc; Ei=-5;//input voltage Acl=-2;//Voltage Gain Vout=Ei*Acl;//output voltage printf("\n\n Value of Output Voltage = %.4f V \n\n",Vout)
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pathname=get_absolute_file_path('9_2.sce') filename=pathname+filesep()+'9_2_data.sci' exec(filename) //Duration of injection t=Tc/(360*N/60) //Specific gravity SG=141.5/(131.5+API) //Velocity of injection Vinj=Cd*sqrt((2*(pinj-pcyl)*10^5)/(SG*1000)) //Vol of fuel injected per cycle V=((bsfc/60)*P)/((N/2)*(SG*1000)) //Nozzle orifice area Af=V/(Vinj*t) //Orifice diameter d=sqrt((4*Af)/%pi) printf("\n\nRESULTS\n\n") printf("\norifice diameter:%f\n",d)
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degsubcool.tst
# Simple distilation column test units SI $thermo = VirtualMaterials.Peng-Robinson / -> $thermo thermo + PROPANE n-BUTANE ISOBUTANE n-PENTANE col = Tower.Tower() col.Stage_0 + 20 # twenty two stages` /col.MaxOuterLoops = 50 /col.Damping = 0.9 cd col.Stage_10 f = Tower.Feed() f.Port.T = 30 f.Port.P = 720 f.Port.MoleFlow = 10 f.Port.Fraction = .4 .05 .4 .15 f.Port cd ../Stage_0 l = Tower.LiquidDraw() l.Port.P = 700 l.Port.MoleFlow = 5 cond = Tower.EnergyFeed(0) reflux = Tower.StageSpecification('Reflux') reflux.Value = 1 cd ../Stage_21 l = Tower.LiquidDraw() l.Port.P = 720 reb = Tower.EnergyFeed(1) cd .. TryToSolve = 1 # start calculation # since there was little output here, I will put some profile stuff here L_MassFraction.PROPANE V_MoleFraction.ISOBUTANE L_MassFlow L_Viscosity L_StdVolFraction.PROPANE V_StdVolFraction.PROPANE L_VolumeFlow L_StdLiqVolumeFlow V_StdLiqVolumeFlow cd / #Create streams s_feed = Stream.Stream_Material() s_liqdraw_0 = Stream.Stream_Material() s_liqdraw_21 = Stream.Stream_Material() s_vapdraw_0 = Stream.Stream_Material() ene_cond = Stream.Stream_Energy() ene_reb = Stream.Stream_Energy() s_intvap_1 = Stream.Stream_Material() s_intliq_0 = Stream.Stream_Material() #Create clones in streams cd /s_feed clone = Stream.ClonePort(0) cd /s_liqdraw_0 clone = Stream.ClonePort() cd /s_liqdraw_21 clone = Stream.ClonePort() cd /s_vapdraw_0 clone = Stream.ClonePort() cd /ene_cond clone = Stream.ClonePort() cd clone cd /ene_reb clone = Stream.ClonePort(0) cd /s_intvap_1 clone = Stream.ClonePort(0) cd /s_intliq_0 clone = Stream.ClonePort() cd /s_liqdraw_0 clone2 = Stream.ClonePort() cd /ene_cond clone2 = Stream.ClonePort() #Create clones in tower cd /col.Stage_1 vaporclone = Tower.InternalVapourClone() cd /col.Stage_0 liquidclone = Tower.InternalLiquidClone() #Create a balance for the overall tower cd / bal = Balance.BalanceOp() cd bal NumberStreamsInMat = 1 NumberStreamsOutMat = 2 NumberStreamsInEne = 1 NumberStreamsOutEne = 2 BalanceType = 4 #Create a balance for the top stage cd / stagebalance = Balance.BalanceOp() cd stagebalance BalanceType = 4 NumberStreamsInMat = 1 NumberStreamsOutMat = 2 NumberStreamsOutEne = 2 #Connect the streams to the tower and the clones to the balance /s_feed.Out -> /col.Feed_10_f /s_liqdraw_0.In -> /col.LiquidDraw_0_l /s_liqdraw_21.In -> /col.LiquidDraw_21_l /ene_cond.In -> /col.EnergyFeed_0_cond /ene_reb.Out -> /col.EnergyFeed_21_reb /bal.In0 -> /s_feed.clone /bal.Out0 -> /s_liqdraw_0.clone /bal.Out1 -> /s_liqdraw_21.clone /bal.InQ0 -> /ene_reb.clone /bal.OutQ0 -> /ene_cond.clone /stagebalance.In0 -> /s_intvap_1.clone /stagebalance.Out0 -> /s_intliq_0.clone /stagebalance.Out1 -> /s_liqdraw_0.clone2 /stagebalance.OutQ0 -> /ene_cond.clone2 /s_intliq_0.In -> /col.InternalLiquid_0_liquidclone /s_intvap_1.In -> /col.InternalVapour_1_vaporclone cd /col MaxOuterError = 1e-6 MaxInnerError = 1e-6 TryToRestart = 1 /col.LiquidDraw_0_l #Add degrees of subcooling cd /col.Stage_0 degsubcool = Tower.DegSubCooling() /col.DegSubCool_0_degsubcool.DT = 2 /col.LiquidDraw_0_l /bal.OutQ1 /stagebalance.OutQ1 /col.DegSubCool_0_degsubcool.DT = 4 /col.LiquidDraw_0_l /bal.OutQ1 /stagebalance.OutQ1 /col.DegSubCool_0_degsubcool.DT = 0 /col.LiquidDraw_0_l /bal.OutQ1 /stagebalance.OutQ1 /col.DegSubCool_0_degsubcool.DT = /col.LiquidDraw_0_l.T = 18 /col.DegSubCool_0_degsubcool /bal.OutQ1 /stagebalance.OutQ1 /col.LiquidDraw_0_l.MoleFlow = /col.DegSubCool_0_degsubcool.DT = 2 /col.DegSubCool_0_degsubcool /col.LiquidDraw_0_l /bal.OutQ1 /stagebalance.OutQ1 #Now add a vapour draw and make sure it doesnt break anything /col.TryToSolve = 0 /col.TryToRestart = 0 cd /col.Stage_0 vap = Tower.VapourDraw() cd / #Should solve fine even for vap flow > 0.0 /col.DegSubCool_0_degsubcool.DT = 0 /col.TryToSolve = 1 /col.VapourDraw_0_vap.MoleFlow = 1 /bal.OutQ1 /stagebalance.OutQ1 #Solve with an inconcistency /col.LiquidDraw_0_l.T = /col.LiquidDraw_0_l.MoleFlow = 5 /col.DegSubCool_0_degsubcool.DT = 1 /bal.OutQ1 /stagebalance.OutQ1 #Solve fine again /col.DegSubCool_0_degsubcool.DT = 0 #Should attempt to solve for vapour draw even if TryToSolve = 0 /col.DegSubCool_0_degsubcool.DT = /col.TryToSolve = 0 /col.DegSubCool_0_degsubcool.DT = 1 /col.VapourDraw_0_vap.MoleFlow = /col.VapourDraw_0_vap.MoleFlow /col.TryToSolve = 1 #Solve fine. A DegSubcooling > 0.0 puts a zero lfow in the vap flow /col.VapourDraw_0_vap.MoleFlow = /bal.OutQ1 /stagebalance.OutQ1 # Can not solve because the liquid is subcooled and the vap is > 0.0 /col.DegSubCool_0_degsubcool.DT = /col.LiquidDraw_0_l.T = 18 C /col.VapourDraw_0_vap.MoleFlow = 1 /bal.OutQ1 /stagebalance.OutQ1 #Solve fine /col.VapourDraw_0_vap.MoleFlow = 0 /bal.OutQ1 /stagebalance.OutQ1 #Get rid of the vapour draw wich should not have been there at all to begin with delete /col.Stage_0.vap /bal.OutQ1 /stagebalance.OutQ1 copy / paste /
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//(13.9) Liquid octane at 25C, 1 atm enters a well-insulated reactor and reacts with air entering at the same temperature and pressure. The products of combustion exit at 1 atm pressure. For steady-state operation and negligible effects of kinetic and potential energy, determine the rate of entropy production, in kJ/K per kmol of fuel, for complete combustion with (a) the theoretical amount of air, (b) 400% theoretical air. //solution //part(a) Tp = 2395 //in kelvin, from example 13.8 //For combustion of liquid octane with the theoretical amount of air, the chemical equation is //C8H18(l) + 12.5O2 + 47N2 ----> 8CO2 + 9H2O(g) + 47N2 //from table A-25 sFbar = 360.79 //absolute entropy of liquid octane in kj/kmol.K //from table A-23 //for reactant side sbarO2atTref = 205.03 //in kj/kmol.K sbarN2atTref = 191.5 //in kj/kmol.K Rbar = 8.314 //universal gas constant in SI units yO2 = .21 yN2 = .79 sbarO2 = sbarO2atTref - Rbar*log(yO2) //in kj/kmol.K sbarN2 = sbarN2atTref - Rbar*log(yN2) //in kj/kmol.K //for product side yCO2 = 8/64 yH2O = 9/64 yN2p = 47/64 //with the help from table A-23 sbarCO2 = 320.173 - Rbar*log(yCO2) sbarH2O = 273.986 - Rbar*log(yH2O) sbarN2p = 258.503 - Rbar*log(yN2p) sigmadot = (8*sbarCO2 + 9*sbarH2O + 47*sbarN2p) - sFbar - (12.5*sbarO2 + 47*sbarN2) printf(' the rate of entropy production, in kJ/K per kmol of fuel with theoretical amount of air is: %f',sigmadot) //part(b) //The complete combustion of liquid octane with 400% theoretical air is described by the following chemical equation: //C8H18(l) + 50 O2 + 188N2 -----> 8 CO2 + 9H2O(g) + 37.5O2 + 188N2 //for product side yCO2 = 8/242.5 yH2O = 9/242.5 yO2 = 37.5/242.5 yN2p = 188/242.5 //with help from table A-23 sbarCO2 = 267.12 - Rbar*log(yCO2) sbarH2O = 231.01 - Rbar*log(yH2O) sbarO2p = 242.12 - Rbar*log(yO2) sbarN2p = 226.795 - Rbar*log(yN2p) sigmadot = (8*sbarCO2 + 9*sbarH2O + 37.5*sbarO2p +188*sbarN2p) -sFbar - (50*sbarO2 + 188*sbarN2) printf('\n\nthe rate of entropy production, in kJ/K per kmol of fuel with 400 percent theoretical air is: %f',sigmadot)
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clear //Variable declaration n=7046 //Hex number //Calculations h = dec2hex(n) //decimal to hex conversion //Result printf ("The hexadecimal equivalent of 7046 is %s ",h)
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Bt=12.5*10^6 Bc=30*10^3 K=7//frequency reuse factor N=Bt/Bc//total no. of available channels M=N*(1/K)//user capacity per cell Nu=3//no. of users/channel NU=N*Nu K1=4 M1=NU*(1/K1) disp(M,'capacity of 1G AMPS FDMA analog cellular system in users/cell') disp(M1,'capacity of 2G IS-136 TDMA digital cellular system in users/cell')
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// Function Name: fliplr and flipud // fliplr(): generate a copy of matrix X, with the order of the columns reversed // flipud(): generate a copy of matrix X, with the order of the rows reversed // Calculating the inplaceTrans inputMat = [ 1, 2; 3, 4;] result = armaMatFunc("fliplr",inputMat) result = armaMatFunc("flipud",inputMat)
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#+++++++++++++++++++++++++++++++++++++++++++++++++++ menu "SCI Config" depends on HI_SCI_SUPPORT choice prompt "Clock Mode" depends on HI_SCI_SUPPORT help HI_UNF_SCI_MODE_CMOS means CMOS output, HI_UNF_SCI_MODE_OD means OD output. default HI_SCI_CLK_MODE_CMOS config HI_SCI_CLK_MODE_CMOS bool "CMOS" config HI_SCI_CLK_MODE_OD bool "OD" endchoice choice prompt "VccEn Mode" depends on HI_SCI_SUPPORT help HI_UNF_SCI_MODE_CMOS means CMOS output, HI_UNF_SCI_MODE_OD means OD output. default HI_SCI_VCCEN_MODE_CMOS config HI_SCI_VCCEN_MODE_CMOS bool "CMOS" config HI_SCI_VCCEN_MODE_OD bool "OD" endchoice choice prompt "Reset Mode" depends on HI_SCI_SUPPORT help HI_UNF_SCI_MODE_CMOS means CMOS output, HI_UNF_SCI_MODE_OD means OD output. default HI_SCI_RESET_MODE_CMOS config HI_SCI_RESET_MODE_CMOS bool "CMOS" config HI_SCI_RESET_MODE_OD bool "OD" endchoice choice prompt "VccEn Pin Active Level" depends on HI_SCI_SUPPORT help Low level active or high level active. default HI_SCI_VCCEN_LOW config HI_SCI_VCCEN_LOW bool "Low Level" config HI_SCI_VCCEN_HIGH bool "High Level" endchoice choice prompt "Detect Pin Active Level" depends on HI_SCI_SUPPORT help Low level active or high level active. default HI_SCI_DETECT_LOW config HI_SCI_DETECT_LOW bool "Low Level" config HI_SCI_DETECT_HIGH bool "High Level" endchoice endmenu #+++++++++++++++++++++++++++++++++++++++++++++++++++
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# Test lookup table lkp = Pump.LookupTable() # setup table lkp.NumberSeries = 3 lkp.NumberTables = 1 lkp.TableType = P lkp.SpecTagValue = 100.0 # specified table tag value lkp.Extrapolate0 = 0 # do not extrapolate series 0 lkp.SeriesType0 = P lkp.SeriesType1 = T lkp.SeriesType2 = H lkp.Table0.TagValue = 32.0 # tag value for the input table 0 lkp.Table0.Series0 = 1.0 2.0 3.0 4.0 5.0 6.0 7.0 lkp.Table0.Series1 = 2.0 4.0 6.0 8.0 10.0 12.0 14.0 lkp.Table0.Series2 = 10.0 9.5 9.0 8.5 8.0 7.5 7.0 lkp # interpolate the table # expecting: 5.75, 11.5, 7.625 lkp.Signal1 = 11.5 lkp.Signal0 lkp.Signal1 lkp.Signal2 # extrapolate down the table # Expecting: 1.0, 0.0, 10.5 lkp.Signal1 = 0.0 lkp.Signal0 lkp.Signal1 lkp.Signal2 # extrapolate up the table # expecting: 7.0, 16.0, 6.5 lkp.Signal1 = 16.0 lkp.Signal0 lkp.Signal1 lkp.Signal2 # try specifying Signal0 instead of Signal1 # expecting 1.5, 3.0, 9.75 lkp.Signal1 = None lkp.Signal0 = 1.5 lkp.Signal0 lkp.Signal1 lkp.Signal2 # multiple entry, input both Signal0 and Signal1 # expecting 1.5, (4.0 vs 3.0), 9.75 with inconsistency for signal1 lkp.Signal1 = 4.0 lkp.Signal0 lkp.Signal1 lkp.Signal2
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// Test # 10 : Valid input test case #2 exec('./allpasslp2bpc.sci',-1); [n,d]=allpasslp2bpc(0.17,[0.9,0.95]); disp(d); disp(n); // //Scilab Output //d=1. 0.7281417 - 0.1748114i //n=-0.7488320 -0.9723699 + 0.2334454i //Matlab Output //n= -0.7488 + 0.0000i -0.9724 + 0.2334i //d= 1.0000 + 0.0000i 0.7281 - 0.1748i
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clear; clc; //page no. 12 funcprot(0); gamma = 1.4; T1 = 60;//temperature of air in degree F p1 = 14.7;//pressure in psia k = 0.5;//(final volume/initial volume) = k R = 53.3;//Engineering gas constant gam1 = p1*(144/R)*(1/(460+T1));//lb/cuft gam2 = gam1/k;//lb/cuft p2 = (p1/(gam1^(gamma)))*(gam2^(gamma));// in psia T2 = p2*(144/R)*(1/gam2);//in degree F a1 = sqrt(gamma*32.2*R*(460+T1));// in fps a2 = sqrt(gamma*32.2*R*(T2));// in fps printf('Final pressure = %.1f psia\n Final temperature = %d degreeR \n Sonic velocity before compression = %d fps\n Sonic velocity after compression = %d fps',p2,T2,a1,a2); //there are small errors in the answers given in textbook
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Aerror =28; Berror = 18; common =10; N2 = Aerror - common; N3 =Berror- common; pval = 1- cdfbin("PQ", N2-1, N2 + N3, 0.5, 0.5); disp(pval, "P-value is")
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function f=%r_s(f) // %r_s(f) -f, f rational //! // Copyright INRIA f(2)=-f(2)
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//Given that R = 2*10^-3 //in meter J = 2*10^5 //in A/m^2 //Sample Problem 27-2a printf("**Sample Problem 27-2a**\n") //As current density is uniform A = %pi*(R^2 - (R/2)^2) I = J*A printf("The current flowing through the outer portion is %fA\n", I) //Sample Problem 27-2b printf("\n**Sample Problem 27-2b**\n") a = 3*10^11 //in SI unit Iv = integrate('a*r^2*2*%pi*r', 'r', R/2, R) printf("Now the current will be %fA", Iv)
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grade = input("Enter your grade : ") if grade>90 then disp("O") elseif grade>=80 & grade<=89 then disp("E") elseif grade>=70 & grade<=79 then disp("A") elseif grade>=60 & grade<=69 then disp("B") elseif grade>=50 & grade<=59 then disp("Poor") elseif grade>=40 & grade<=49 then disp("Very Poor") else disp("F") end
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clear; clc; //page no.20 T = 70;//degreeF del_p = 0.1;// in psi sigma = 0.00498;// lb/ft R = (sigma*2)/(del_p*144);//in ft d = 12*2*R;// in inches printf('Diameter of the droplet of water, d = %.4f in',d);
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//Find (a) the final-stage voltage gain Av2  vo=vo1; (b) the final-stage input impedance Zin2; //(c) the initial-stage voltage gain Av1  vo1=vin; (d) the amplifier input impedance Zin1; and //(e) the amplifier voltage gain Av  vo=vi. //Example 6.22 page no 189 clear clc hfe=40 Rc2=20*10^3 //Ω Rc1=10^4 //Ω hie=1500 hoe=30*10^-6 Av2=-((hfe*Rc2)/(hie*(1+hoe*Rc2))) //final-stage voltage gain printf("\n The value of Av2=%0.3f " ,Av2) Rb2=5*10^3 //Ω hie=1500 hfe=40 Zin2=(((Rb2*hie)/(Rb2+hie)))/1000 //final-stage input impedance Zin2 printf("\n The value of Zin2=%0.3f Kohm " ,Zin2) Zin2=Zin2*1000 Av1=-((hfe*Zin2*Rc1)/(hie*(Rc1+Zin2+hoe*Zin2*Rc1))) //initial-stage voltage gain printf("\n The value of Av1=%0.3f " ,Av1)
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<?xml version="1.0" encoding="utf-8"?> <test> <description>LocProject_Diff3D Lin. Deformed Hex Lagrange Basis, P=6, Q=7</description> <executable>LocProject_Diff3D</executable> <parameters>8 8 8 8 6 6 6 7 7 7 0 0 0 1 0 0 1 1.5 0 0 1 0 0 0 1 1.5 0 1 1 1 1 0 1 1.5</parameters> <metrics> <metric type="L2" id="1"> <value tolerance="1e-12">0.0353098</value> </metric> <metric type="Linf" id="2"> <value tolerance="1e-12">0.446618</value> </metric> </metrics> </test>
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//Problem 20.01: A transformer has 500 primary turns and 3000 secondary turns. If the primary voltage is 240 V, determine the secondary voltage, assuming an ideal transformer. //initializing the variables: N1 = 500; // primary turns N2 = 3000; // secondary turns V1 = 240; // in Volts //calculation: //For an ideal transformer, voltage ratio = turns ratio V2 = V1*N2/N1 printf("\n\n Result \n\n") printf("\n secondary voltage %.2E V",V2)
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function[x]=dcgain(p) //function is to find the dc gain of LTI system //k = dcgain(sys) computes the DC gain k of the LTI model sys. //DC gain is infinite for systems with integrators. //author:- Paresh Yeole emailid:-yeoleparesh@students.vnit.ac.in [lhs rhs]=argn(0); if rhs<1 then error("dcgain:input parameter as a dynamic system is expected"); end select typeof(p) case "rational" then case "state-space" then p=ss2tf(p) else msprintf("\n") error(97,1), end; if(p.dt=='c') then //if system is continuous then put s=o for dc gain if(ndims(p)==3) then //x=cell(size(p,'r'),size(p,'c'),size(p,3)); //t=cell(size(p,'r'),size(p,'c'),size(p,3)); for i=1:size(p,'r') for j=1:size(p,'c') for k=1:size(p,3) try t=horner(p(i,j,k),0); catch //x(i,j,k).entries=1; //continue; x(i,j,k)=%inf; //disp(t); continue; //return; end x(i,j,k)=t; //=y; // if(t==1) then // x(i,j,k).entries=%inf; // end end end end elseif(ndims(p)==2) then //x=cell(size(p,'r'),size(p,'c')); for i=1:size(p,'r') for j=1:size(p,'c') try t=horner(p(i,j),0); catch x=%inf; continue; end x(i,j)=t end end else try x=horner(p,0) catch x=%inf; end end else //discrete systems if(ndims(p)==3) then // x=cell(size(p,'r'),size(p,'c'),size(p,3)); for i=1:size(p,'r') for j=1:size(p,'c') for k=1:size(p,3) try t=horner(p(i,j,k),1); catch x(i,j,k)=%inf; continue; end x(i,j,k)=t; end end end elseif(ndims(p)==2) then //x=cell(size(p,'r'),size(p,'c')); for i=1:size(p,'r') for j=1:size(p,'c') try t=horner(p(i,j),1); catch x(i,j)=%inf; continue; end x(i,j,k)=t; end end else //if system is discrete then put z=1 for dc gain try x=horner(p,1) catch x=%inf; end end end endfunction
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clc; printf("Example 3.1\n\n"); sap=1.25; //Sulphuric acid pumped d=25e-3; //Diameter of pipe l=30; //length of pipe meu=25e-3; //Viscosity of acid rho_a=1840; //Density of acid printf(" Given :\n Sulphuric acid pumped = %.2f kg/s\n Diameter of pipe = %.3f m\n length of pipe = %d m\n Viscosity of acid = %d x 10^-3 N s/m^2\n Density of acid = %d kg/m^3",sap,d,l,meu*1000,rho_a); Re=4*sap/(%pi*meu*d); printf("\n\n\n Reynolds number , Re=(u*d*rho)/meu = 4G/(pi*meu*d)= %d",Re); //For a mild steel pipe, suitable for conveying the acid, the roughness e will be between 0.05 and 0.5 mm (0.00005 and 0.0005 m). //The relative roughness is thus: e/d = 0.002 to 0.02 //From Figure 3.7: R/(rho*u^2) = 0.006 over this range of e/d u=sap/(rho_a*%pi/4*d^2); printf("\n Velocity is , u=G/(rho *A) = %.2f m/s",u); //calculating pressure drop from the energy balance equation and equation 3.19 Dp=rho_a*((0.5+4*0.006*30/0.025)*u^2+9.81*12); printf("\n Pressure Drop = %.0f N/m^2",Dp); printf("\n Pressure drop = %.0f kN/m^2",(Dp/10^3));
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clear clc //Example 17.5 disp('Example 17.5') deltaT=[0.05 0.25 0.5 1]';//sampling time K=-20; theta=1+(deltaT/2);//Add half of sampling time to delay for finding PI settings tau=5; //Table 11.3 ITAE disturbance settings //Note that there is an error in book solution saying Table 11.2 //It should be table 11.3 Y=0.859*(theta/tau)^(-0.977);Kc=Y/K; taui=tau*(0.674*(theta/tau)^-0.680).^-1; mprintf('\n ITAE(disturbance) \n') mprintf(' deltaT Kc tauI') mprintf('\n %f %f %f',deltaT,Kc,taui) //Finding digital controller settings //Eqn 17-55 a0=1+deltaT./taui; a1=-(1); //since tauD=0 a2=0; z=%z; Gcz=Kc.*(a0+a1*z^-1)./(1-z^-1); //Refer to table 17.1 to convert continuous transfer function to digital form Gp=K*(1-exp(-1/tau*deltaT)).*z^(-1+(-1)./deltaT)./(1-exp((-1)/tau*deltaT)*z^-1);//z^(-1/deltaT) for delay G_CL=syslin('d',((Gp)./(Gcz.*Gp+1))); t=0:deltaT(1):15 u=ones(1,length(t)); yt=flts(u,G_CL(1,1)); plot(t,yt,'-') t=0:deltaT(2):15 u=ones(1,length(t)); yt=flts(u,G_CL(2,1)); plot(t,yt,'green--') t=0:deltaT(3):15 u=ones(1,length(t)); yt=flts(u,G_CL(3,1)); plot(t,yt,'black-.') t=0:deltaT(4):15 u=ones(1,length(t)); yt=flts(u,G_CL(4,1)); plot(t,yt,'red:') set(gca(),"data_bounds",[0 15 -8 1]); //putting bounds on display l=legend("$\Delta t=0.05\ min$","$\Delta t=0.25\ min$","$\Delta t=0.5\ min$","$\Delta t=1\ min$",position=4); xtitle("Example 17.5","Time(min)","$y$"); a=get("current_axes"); c=a.y_label;c.font_size=5; mprintf("\nNote that there is a mismatch between the book simulation and what\n... what we get from SCILAB. The book is wrong. This has been crosschecked using\n... simulation in SIMULINK(MATLAB)")
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// Scilab Code Ex5.1: Page-176 (2006) clc; clear; h = 6.626e-34; // Planck's constant, Js h_bar = h/(2*%pi); // Reduced Planck's constant, Js e = 1.6e-019; // Energy equivalent of 1 eV, J/eV m = 9.1e-031; // Mass of an electron, kg // For Na n_Na = 2.65e+28; // electronic concentration of Na, per metre cube k_F = (3*%pi^2*n_Na)^(1/3); // Fermi wave vector, per cm E_F = h_bar^2*k_F^2/(2*m*e); // Fermi energy of Na, eV printf("\nThe fermi energy of Na = %4.2f eV", E_F); printf("\nThe band structure value of Na = %4.2f eV", 0.263*13.6); // For K n_K = 1.4e+28; // electronic concentration of K, per metre cube k_F = (3*%pi^2*n_K)^(1/3); // Fermi wave vector, per cm E_F = h_bar^2*k_F^2/(2*m*e); // Fermi energy of K, eV printf("\nThe fermi energy of K = %4.2f eV", E_F); printf("\nThe band structure value of K = %4.2f eV", 0.164*13.6); printf("\nThe agreement between the free electron and band theoretical values are fairly good both for Na and K"); // Result // The fermi energy of Na = 3.25 eV // The band structure value of Na = 3.58 eV // The fermi energy of K = 2.12 eV // The band structure value of K = 2.23 eV // The agreement between the free electron and band theoretical values are fairly good both for Na and K
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// Electric Machinery and Transformers // Irving L kosow // Prentice Hall of India // 2nd editiom // Chapter 4: DC Dynamo Torque Relations-DC Motors // Example 4-9 clear; clc; close; // Clear the work space and console. // Given data I_l_orig = 40; // original Line current in A I_l_final = 66; // Final Line current in A phi_orig = 1; // field flux is increased by 12% so EMF produced and terminal // voltage will also increase by 12% phi_final = 1.12; V_a = 120; R_sh_orig = 60; // Original Field ckt resistance in ohm R_sh_final = 50 ; // Decreased final field ckt resistance in ohm R_a = 0.2; // Armature resistance in ohm BD = 3; // Brush voltage drop in volt S_orig = 1800; // Rated full-load speed // Calculations I_f_orig = V_a / R_sh_orig ; // Original Field current in A I_a_orig = I_l_orig - I_f_orig ; // Original Armature current @ full load E_c_orig = V_a - ( I_a_orig * R_a + BD ) ; // Back EMF @ full load I_f_final = V_a / R_sh_final ; // Final field current in A I_a_final = I_l_final - I_f_final ; // Final Armature current in A E_c_final = V_a - ( I_a_final * R_a + BD ) ; // Final EMF induced S = S_orig * ( E_c_final / E_c_orig ) * ( phi_orig / phi_final ) ; // Final speed of the motor // Display the result disp("Example 4-9 Solution : "); printf(" \n S = %.1f rpm ", S );
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// Chapter9 // Maximum and minimum Frequency of oscillation // Page.No-307 // Example9_2 //Figure 9.9 // Given clear;clc; // for minimium frequency R=11100; //in Ohm C=0.1*10^-6; //in F f=1/(2*%pi*R*C); printf("\n The mimimum frequency of oscillation = %.1f Hz\n",f); // Result // for maximum frequency R=1100; //in Ohm C=0.1*10^-6; //in F fm=1/(2*%pi*R*C); printf("\n The maximum frequency of oscillation = %.0f Hz\n",fm); // Result printf("\n For C=0.001microF, the range is from %.1f Hz to %.0f Hz\n ", f*10,fm*10);//Result printf("\n For C=0.0001microF, the range is from %.1f Hz to %.0f Hz\n ", f*100,fm*100);//Result Rf=10000+2700; //in ohm Ri=5600; //in Ohm Av=1+Rf/Ri; printf("\n Gain ,Av is %.2f \n ", Av);//Result
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% Vector test routine % Author: David Harper (algebra@liverpool.ac.uk) % Computer Algebra Support Officer % University of Liverpool Computer Laboratory. % Please compare carefully the output from running this test file with the % log file provided to make sure your implementation is correct. linelength 72; off allfac; on div; vec a,b,c; matrix q; a := avec(ax,ay,az); b := avec(bx,by,bz); q := mat((q11,q12,q13),(q21,q22,q23),(q31,q32,q33)); c := a+b; c := a-b; c := a cross b; d := a dot b; a dot c; b dot c; q*a; c:=2*f*a - b/7; c(0); c(1); c(2); 1/vmod(a); b/vmod(a); (a cross b)/(a dot b); 2/3*vmod(a)*a*(a dot c)/(vmod(a cross c)); a := avec(x**2*y**3,log(z+x),13*z-y); df(a,x); df(a,x,y); int(a,x); exp(a); log sin b; a := avec(ax,ay,az); depend ax,x,y,z; depend ay,x,y,z; depend az,x,y,z; depend p,x,y,z; c := grad p; div c; delsq p; div a; curl a; delsq a; depend h1,x,y,z; depend h2,x,y,z; depend h3,x,y,z; scalefactors(h1,h2,h3); grad p; div a; curl a; dp1 := delsq p; dp2 := div grad p; dp1-dp2; delsq a; curl grad p; grad div a; div curl a; % Examples of integration : (1) Volume integrals getcsystem 'spherical; % Example 1 : integration of r**n over a sphere origin := avec(0,0,0); upperbound := avec(rr,pi,2*pi); volintegral(r**n,origin,upperbound); % Substitute n=0 to get the volume of a sphere sub(n=0,ws); % Example 2 : volume of a right-circular cone getcsystem 'cylindrical; upperbound := avec(pp*z,h,2*pi); volintorder := avec(2,0,1); % Integrate in the order : phi, r, z cone := volintegral(1,origin,upperbound); % Now we replace P*Z by RR to get the result in the familiar form let pp*h=rr; cone := cone; % This is the familiar form clear pp*h; % Example 3 : line integral to obtain the length of a line of latitude % on a sphere getcsystem 'spherical; a := avec(0,0,1); % Function vector is the tangent to the % line of latitude curve := avec(rr,latitude,phi); % Path is round a line of latitude deflineint(a,curve,phi,0,2*pi); end;
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DIT_DIF_FFT.sce
clc; clear; close; function [X]=DIT_FFT(x) t = nextpow2(length(x)); j = [x zeros(1,(2^t)-length(x))] ; N = length(j); S = log2(N); j = j(:,$:-1:1); for stage=1:S a = 1; b = 1+2^(stage-1); n=0; while(n<=2^(stage-1)-1 && b<=N) e = exp((-1*%i)*2*%pi*n/(2^stage)); y = j(a)+e*j(b); z = j(a)-e*j(b); j(a) = y; j(b) = z; a = a+1; b = b+1; n = n+1; if(modulo(b,2^stage)== 1) a = a+2^(stage-1); b = b+2^(stage-1); n = 0; end end end X = j; endfunction function [X]=DIF_FFT(x) t = nextpow2(length(x)); j = [x zeros(1,(2^t)-length(x))] ; N = length(j); S = log2(N); for stage=S:-1:1 a = 1; b = 1+2^(stage-1); n = 0; while( n<=2^(stage-1)-1 && a<=N && b<=N) l = (n).*(2^(S+1-stage))./2; e = exp((-1*%i)*2*%pi*l/(16)); y = j(a)+j(b); z = (j(a)-j(b)).*e; j(a) = y; j(b) = z; a = a+1; b = b+1; n = n+1; if (stage == 1) if(modulo(1,a) == 1) a = a+2^(stage-1); b = b+2^(stage-1); n=0; end end if(stage~=1) if(modulo(a,2^(stage-1))==1) a = a+2^(stage-1); b = b+2^(stage-1); n = 0; end end end end X = j(:,$:-1:1); endfunction //Four point sequence x4=[1, 2+2*%i,2,2-2*%i,1-1*%i,0,1+1*%i,0]; N1=length(x4); r=[0:N1-1]; scf(0); plot2d3(r,abs(x4)); title('Plot of magnitude of x(n)','FontSize'); xlabel('n','FontSize'); ylabel('|x|','FontSize'); e = gce(); e.children.thickness = 4; a=gca() a.x_location = "origin"; a.y_location = "origin"; scf(1); r=[0:N1-1]; plot2d3(r,atan(imag(x4),real(x4))); title('Plot of phase of x(n)','FontSize'); xlabel('n','FontSize'); ylabel('angel(x)','FontSize'); e = gce(); e.children.thickness = 4; //a=gca() //a.x_location = "origin"; //a.y_location = "origin"; X4=DIT_FFT(x4); disp("DIT FFT of x : "); disp(X4); scf(2); r=[0:N1-1]; plot2d3(r,abs(X4)); title('Plot of magnitude of X(k)','FontSize'); xlabel('n','FontSize'); ylabel('angel(x)','FontSize'); e = gce(); e.children.thickness = 4; a=gca() a.x_location = "origin"; a.y_location = "origin"; scf(3); r=[0:N1-1]; plot2d3(r,atan(imag(X4),real(X4))); title('Plot of phase of X(k)','FontSize'); xlabel('n','FontSize'); ylabel('angel(x)','FontSize'); e = gce(); e.children.thickness = 4; a=gca() a.x_location = "origin"; a.y_location = "origin"; X_4 = DIF_FFT(x4) disp("DIF FFT of x : "); disp(X_4); scf(4); r=[0:N1-1]; plot2d3(r,abs(X_4)); title('Plot of magnitude of X(k)','FontSize'); xlabel('n','FontSize'); ylabel('angel(x)','FontSize'); e = gce(); e.children.thickness = 4; a=gca() a.x_location = "origin"; a.y_location = "origin"; scf(5); r=[0:N1-1]; plot2d3(r,atan(imag(X_4),real(X_4))); title('Plot of phase of X(k)','FontSize'); xlabel('n','FontSize'); ylabel('angel(x)','FontSize'); e = gce(); e.children.thickness = 4; a=gca() a.x_location = "origin"; a.y_location = "origin";
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ex15_2.sce
clc;clear; //Example 15.2 //given data E=200;//energy released per fission in MeV e=1.6*10^-19;//the charge on electron in C Na=6.02*10^26;//Avgraodo no. in 1/kg mole //calculations CE=E*e*10^6;//conversion in J RF=1/CE; disp(RF,'fission rate of one watt in fissions/second'); Ekg=CE*Na/235; disp(Ekg,'Energy realeased in complete fission of 1 kg in J')
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3_8.sci
//3.8 clc; Sp_constant=10.5*10^-6*%pi/180; deflection=83; Td=Sp_constant*deflection; I1=10; K=0.078; I2=(Td/(K*I1))*10^6; printf("Current in the voltage coil=%.2f uA",I2)
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Ex5_8.sce
clear all; clc; disp("Scilab Code Ex 5.8 : ") //Given: T = 45; //N G = 80; //GPa d = 20/1000; //m r = d/2; //m l_dc = 1.5; //m l_ab = 2; //m r1 = 75/1000; //m r2 = 150/1000; //m //Internal Torque: F = T/r2; T_d_x = F*r1; //Angle of twist: J = (%pi/2)*(r^4); phi_c = (T*l_dc)/(2*J*G*10^9); phi_b = (phi_c*r1)/r2; phi_ab = (T*l_ab)/(J*G*10^9); phi_a = phi_b + phi_ab; //Display: printf('\n\nThe angle of twist of end A of shaft AB = + %1.4f rad',phi_a); //----------------------------------------------------------------------------END--------------------------------------------------------------------------------
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Ex4_3.sce
//problem 3 pagenumber 4.38 //given n=4;format(6); z=['0111','1111']; vref=5;//volt //determine v0 r=vref/(2^n-1); i=1; while i<3 v0=r*base2dec(z(i),2); disp('Output voltage '+string(z(i))+' = '+string(v0)+' volt'); i=i+1; end