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//Example 6.8(c) clear; clc; Vs=15; A=10; Vim=40*10^(-3); SR=0.5*10^6; fmax=SR/(2*%pi*Vim*A); ft=1*10^6; fB=ft/A; printf("Useful Frequency Range of Operation f<=%.2f kHz",fB*10^(-3));
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// Exa 4.15 clc; clear; close; format('v',5) // Given data S = 12; V_CC = 16;// in V R_C = 1.5 * 10^3;// in ohm V_CE = 8;// in V V_BE= 0.2;// in V I_C = 4;// in mA I_C = I_C * 10^-3;// in A Beta = 50; // Vth = V_CC*(R2/(R1+R2)) and Rth = (R1*R2)/(R1+R2); //Applying KVL to input side, Vth - I_B*Rth - V_BE - I_E*R_E = 0 (i) I_B = I_C/Beta;// in A I_E = I_B*(1+Beta);// in A // Applying KVL to output section, R_E = (V_CC - (I_C*R_C) - V_CE)/I_E;// in ohm //S = ((Rth+R3)*(1+Beta))/(Rth + ((1+Beta)*R_E)) (ii) Rth= R_E*(1+Beta-S-Beta*S)/(S-1-Beta);// in ohm V_BN= V_BE+I_E*R_E;//in V Vth= V_BN+I_B*Rth;// in V // Vth= V_CC*R2/(R1+R2) and Rth= R2*R1/(R1+R2), So Vth= V_CC*Rth/R1 R1= V_CC*Rth/Vth;// in ohm R2= R1*Rth/(R1-Rth);// in ohm R1= round(R1*10^-3);// in k ohm R2= R2*10^-3;// in k ohm R_E= R_E*10^-3;// in k ohm disp(R1,"The value of R1 in kΩ is : ") disp(R2,"The value of R2 in kΩ is : ") disp(R_E,"The value of R_E in kΩ is : ")
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//Example 9-6,Page No- 330 clear clc R= 75 T=31+273 k=1.38*106-23 B=6*10^6 Vs = 8.3*10^-6 NF=2.8 Vn = (4*k*T*B*R)^0.5 Pn = Vn^2/R Ps = Vs^2/R SN = (Ps*10^12)/(Pn/10^12) SN_dB =10*log10(SN) NR = 10^0.28 SN_op = SN/NR Tn = 290*(NR-1) printf('The input noise power is %.1f pW',Pn/10^12) printf('\n The input signal power is %.3f pW',Ps*10^12) printf('\n Signal to noise ratio in decibels %f',SN) printf('\n The noise factor is %.1f',NR) printf('\n Signal to noise ratio of the amplifier is %f',SN_op) printf('\n The noise temperature of the amplifier %.1f K',Tn)
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//Variable declaration N=3*10**25; //number of atoms(per m**3) r=0.2*10**-9; //radius(m) epsilon0=8.85*10**-12; E=1; //electric field //Calculation p=4*%pi*epsilon0*r**3; //dipole moment(F m**2) P=N*p; //polarization(C m) epsilonr=(P/(epsilon0*E))+1; //dielectric constant alpha_e=epsilon0*(epsilonr-1)/N; //polarizability(F m**2) //Result printf('dipole moment is %0.3f *10**-40 F m**2 \n',(p*10**40)) printf('polarization is %0.3f *10**-15 C m \n',(P*10**15)) printf('dielectric constant is %0.3f \n',(epsilonr)) printf('polarizability is %0.3f *10**-40 F m**2 \n',(alpha_e*10**40))
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clear; path_rna = get_absolute_file_path('rna.sce'); exec( path_rna+"\_input_data_file.sce" ); exec( path_rna+"\..\RNA_ANALISE_TECNICA.sce" ); printf( 'Iniciando rna...\n' ); input_data = getInputDataFile(); output_data = rna_indicador(input_data(1),input_data(2),input_data(3),input_data(4),input_data(5),input_data(6),input_data(7),input_data(8),input_data(9)); gravarDados( path_rna + '\output_data.txt', output_data ); printf( 'Rna executada com sucesso.' ); exit;
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Expanding for base=2, level=7, reasons+features=base,similiar invall,norm Refined variables=x,y [0+1x,0+1y]: unknown -> [1] [0,0] x²-y²+3 ---------------- level 0 expanding queue[0]^-1,meter=[2,2]: x²-y²+3 [1+2x,0+2y]: unknown -> [1] [1,0] x+x²-y²+1 -> solution [1,2],NONTRIVIAL endexp[0] ---------------- level 1 expanding queue[1]^0,meter=[2,2]: x+x²-y²+1 [1+4x,2+4y]: unknown -> [2] [0,1] x+2x²-2y-2y² -> solution [1,2],NONTRIVIAL [3+4x,2+4y]: unknown -> [3] [1,1] 3x+2x²-2y-2y²+1 endexp[1] ---------------- level 2 expanding queue[2]^1,meter=[2,2]: x+2x²-2y-2y² [1+8x,2+8y]: unknown -> [4] [0,0] x+4x²-2y-4y² -> solution [1,2],NONTRIVIAL [1+8x,6+8y]: unknown -> [5] [0,1] x+4x²-6y-4y²-2 endexp[2] expanding queue[3]^1,meter=[2,2]: 3x+2x²-2y-2y²+1 [7+8x,2+8y]: unknown -> [6] [1,0] 7x+4x²-2y-4y²+3 [7+8x,6+8y]: unknown -> [7] [1,1] 7x+4x²-6y-4y²+1 endexp[3] ---------------- level 3 expanding queue[4]^2,meter=[2,2]: x+4x²-2y-4y² [1+16x,2+16y]: unknown -> [8] [0,0] x+8x²-2y-8y² -> solution [1,2],NONTRIVIAL [1+16x,10+16y]: unknown -> [9] [0,1] x+8x²-10y-8y²-3 endexp[4] expanding queue[5]^2,meter=[2,2]: x+4x²-6y-4y²-2 [1+16x,6+16y]: unknown -> [10] [0,0] x+8x²-6y-8y²-1 [1+16x,14+16y]: unknown -> [11] [0,1] x+8x²-14y-8y²-6 endexp[5] expanding queue[6]^3,meter=[2,2]: 7x+4x²-2y-4y²+3 [15+16x,2+16y]: unknown -> [12] [1,0] 15x+8x²-2y-8y²+7 [15+16x,10+16y]: unknown -> [13] [1,1] 15x+8x²-10y-8y²+4 endexp[6] expanding queue[7]^3,meter=[2,2]: 7x+4x²-6y-4y²+1 [15+16x,6+16y]: unknown -> [14] [1,0] 15x+8x²-6y-8y²+6 [15+16x,14+16y]: unknown -> [15] [1,1] 15x+8x²-14y-8y²+1 endexp[7] ---------------- level 4 expanding queue[8]^4,meter=[2,2]: x+8x²-2y-8y² [1+32x,2+32y]: unknown -> [16] [0,0] x+16x²-2y-16y² -> solution [1,2],NONTRIVIAL [1+32x,18+32y]: unknown -> [17] [0,1] x+16x²-18y-16y²-5 endexp[8] expanding queue[9]^4,meter=[2,2]: x+8x²-10y-8y²-3 [17+32x,10+32y]: unknown -> [18] [1,0] 17x+16x²-10y-16y²+3 [17+32x,26+32y]: unknown -> [19] [1,1] 17x+16x²-26y-16y²-6 endexp[9] expanding queue[10]^5,meter=[2,2]: x+8x²-6y-8y²-1 [17+32x,6+32y]: unknown -> [20] [1,0] 17x+16x²-6y-16y²+4 [17+32x,22+32y]: unknown -> [21] [1,1] 17x+16x²-22y-16y²-3 endexp[10] expanding queue[11]^5,meter=[2,2]: x+8x²-14y-8y²-6 [1+32x,14+32y]: unknown -> [22] [0,0] x+16x²-14y-16y²-3 [1+32x,30+32y]: unknown -> [23] [0,1] x+16x²-30y-16y²-14 endexp[11] expanding queue[12]^6,meter=[2,2]: 15x+8x²-2y-8y²+7 [31+32x,2+32y]: unknown -> [24] [1,0] 31x+16x²-2y-16y²+15 [31+32x,18+32y]: unknown -> [25] [1,1] 31x+16x²-18y-16y²+10 endexp[12] expanding queue[13]^6,meter=[2,2]: 15x+8x²-10y-8y²+4 [15+32x,10+32y]: unknown -> [26] [0,0] 15x+16x²-10y-16y²+2 [15+32x,26+32y]: unknown -> [27] [0,1] 15x+16x²-26y-16y²-7 endexp[13] expanding queue[14]^7,meter=[2,2]: 15x+8x²-6y-8y²+6 [15+32x,6+32y]: unknown -> [28] [0,0] 15x+16x²-6y-16y²+3 [15+32x,22+32y]: unknown -> [29] [0,1] 15x+16x²-22y-16y²-4 endexp[14] expanding queue[15]^7,meter=[2,2]: 15x+8x²-14y-8y²+1 [31+32x,14+32y]: unknown -> [30] [1,0] 31x+16x²-14y-16y²+12 [31+32x,30+32y]: unknown -> [31] [1,1] 31x+16x²-30y-16y²+1 endexp[15] ---------------- level 5 expanding queue[16]^8,meter=[2,2]: x+16x²-2y-16y² [1+64x,2+64y]: unknown -> [32] [0,0] x+32x²-2y-32y² -> solution [1,2],NONTRIVIAL [1+64x,34+64y]: unknown -> [33] [0,1] x+32x²-34y-32y²-9 endexp[16] expanding queue[17]^8,meter=[2,2]: x+16x²-18y-16y²-5 [33+64x,18+64y]: unknown -> [34] [1,0] 33x+32x²-18y-32y²+6 [33+64x,50+64y]: unknown -> [35] [1,1] 33x+32x²-50y-32y²-11 endexp[17] expanding queue[18]^9,meter=[2,2]: 17x+16x²-10y-16y²+3 [49+64x,10+64y]: unknown -> [36] [1,0] 49x+32x²-10y-32y²+18 [49+64x,42+64y]: unknown -> [37] [1,1] 49x+32x²-42y-32y²+5 endexp[18] expanding queue[19]^9,meter=[2,2]: 17x+16x²-26y-16y²-6 [17+64x,26+64y]: unknown -> [38] [0,0] 17x+32x²-26y-32y²-3 [17+64x,58+64y]: unknown -> [39] [0,1] 17x+32x²-58y-32y²-24 endexp[19] expanding queue[20]^10,meter=[2,2]: 17x+16x²-6y-16y²+4 [17+64x,6+64y]: unknown -> [40] [0,0] 17x+32x²-6y-32y²+2 [17+64x,38+64y]: unknown -> [41] [0,1] 17x+32x²-38y-32y²-9 endexp[20] expanding queue[21]^10,meter=[2,2]: 17x+16x²-22y-16y²-3 [49+64x,22+64y]: unknown -> [42] [1,0] 49x+32x²-22y-32y²+15 [49+64x,54+64y]: unknown -> [43] [1,1] 49x+32x²-54y-32y²-4 endexp[21] expanding queue[22]^11,meter=[2,2]: x+16x²-14y-16y²-3 [33+64x,14+64y]: unknown -> [44] [1,0] 33x+32x²-14y-32y²+7 [33+64x,46+64y]: unknown -> [45] [1,1] 33x+32x²-46y-32y²-8 endexp[22] expanding queue[23]^11,meter=[2,2]: x+16x²-30y-16y²-14 [1+64x,30+64y]: unknown -> [46] [0,0] x+32x²-30y-32y²-7 [1+64x,62+64y]: unknown -> [47] [0,1] x+32x²-62y-32y²-30 endexp[23] expanding queue[24]^12,meter=[2,2]: 31x+16x²-2y-16y²+15 [63+64x,2+64y]: unknown -> [48] [1,0] 63x+32x²-2y-32y²+31 [63+64x,34+64y]: unknown -> [49] [1,1] 63x+32x²-34y-32y²+22 endexp[24] expanding queue[25]^12,meter=[2,2]: 31x+16x²-18y-16y²+10 [31+64x,18+64y]: unknown -> [50] [0,0] 31x+32x²-18y-32y²+5 [31+64x,50+64y]: unknown -> [51] [0,1] 31x+32x²-50y-32y²-12 endexp[25] expanding queue[26]^13,meter=[2,2]: 15x+16x²-10y-16y²+2 [15+64x,10+64y]: unknown -> [52] [0,0] 15x+32x²-10y-32y²+1 [15+64x,42+64y]: unknown -> [53] [0,1] 15x+32x²-42y-32y²-12 endexp[26] expanding queue[27]^13,meter=[2,2]: 15x+16x²-26y-16y²-7 [47+64x,26+64y]: unknown -> [54] [1,0] 47x+32x²-26y-32y²+12 [47+64x,58+64y]: unknown -> [55] [1,1] 47x+32x²-58y-32y²-9 endexp[27] expanding queue[28]^14,meter=[2,2]: 15x+16x²-6y-16y²+3 [47+64x,6+64y]: unknown -> [56] [1,0] 47x+32x²-6y-32y²+17 [47+64x,38+64y]: unknown -> [57] [1,1] 47x+32x²-38y-32y²+6 endexp[28] expanding queue[29]^14,meter=[2,2]: 15x+16x²-22y-16y²-4 [15+64x,22+64y]: unknown -> [58] [0,0] 15x+32x²-22y-32y²-2 [15+64x,54+64y]: unknown -> [59] [0,1] 15x+32x²-54y-32y²-21 endexp[29] expanding queue[30]^15,meter=[2,2]: 31x+16x²-14y-16y²+12 [31+64x,14+64y]: unknown -> [60] [0,0] 31x+32x²-14y-32y²+6 [31+64x,46+64y]: unknown -> [61] [0,1] 31x+32x²-46y-32y²-9 endexp[30] expanding queue[31]^15,meter=[2,2]: 31x+16x²-30y-16y²+1 [63+64x,30+64y]: unknown -> [62] [1,0] 63x+32x²-30y-32y²+24 [63+64x,62+64y]: unknown -> [63] [1,1] 63x+32x²-62y-32y²+1 endexp[31] ---------------- level 6 expanding queue[32]^16,meter=[2,2]: x+32x²-2y-32y² [1+128x,2+128y]: unknown -> [64] [0,0] x+64x²-2y-64y² -> solution [1,2],NONTRIVIAL [1+128x,66+128y]: unknown -> [65] [0,1] x+64x²-66y-64y²-17 endexp[32] expanding queue[33]^16,meter=[2,2]: x+32x²-34y-32y²-9 [65+128x,34+128y]: unknown -> [66] [1,0] 65x+64x²-34y-64y²+12 [65+128x,98+128y]: unknown -> [67] [1,1] 65x+64x²-98y-64y²-21 endexp[33] expanding queue[34]^17,meter=[2,2]: 33x+32x²-18y-32y²+6 [33+128x,18+128y]: unknown -> [68] [0,0] 33x+64x²-18y-64y²+3 [33+128x,82+128y]: unknown -> [69] [0,1] 33x+64x²-82y-64y²-22 endexp[34] expanding queue[35]^17,meter=[2,2]: 33x+32x²-50y-32y²-11 [97+128x,50+128y]: unknown -> [70] [1,0] 97x+64x²-50y-64y²+27 [97+128x,114+128y]: unknown -> [71] [1,1] 97x+64x²-114y-64y²-14 endexp[35] expanding queue[36]^18,meter=[2,2]: 49x+32x²-10y-32y²+18 [49+128x,10+128y]: unknown -> [72] [0,0] 49x+64x²-10y-64y²+9 [49+128x,74+128y]: unknown -> [73] [0,1] 49x+64x²-74y-64y²-12 endexp[36] expanding queue[37]^18,meter=[2,2]: 49x+32x²-42y-32y²+5 [113+128x,42+128y]: unknown -> [74] [1,0] 113x+64x²-42y-64y²+43 [113+128x,106+128y]: unknown -> [75] [1,1] 113x+64x²-106y-64y²+6 endexp[37] expanding queue[38]^19,meter=[2,2]: 17x+32x²-26y-32y²-3 [81+128x,26+128y]: unknown -> [76] [1,0] 81x+64x²-26y-64y²+23 [81+128x,90+128y]: unknown -> [77] [1,1] 81x+64x²-90y-64y²-6 endexp[38] expanding queue[39]^19,meter=[2,2]: 17x+32x²-58y-32y²-24 [17+128x,58+128y]: unknown -> [78] [0,0] 17x+64x²-58y-64y²-12 [17+128x,122+128y]: unknown -> [79] [0,1] 17x+64x²-122y-64y²-57 endexp[39] expanding queue[40]^20,meter=[2,2]: 17x+32x²-6y-32y²+2 [17+128x,6+128y]: unknown -> [80] [0,0] 17x+64x²-6y-64y²+1 [17+128x,70+128y]: unknown -> [81] [0,1] 17x+64x²-70y-64y²-18 endexp[40] expanding queue[41]^20,meter=[2,2]: 17x+32x²-38y-32y²-9 [81+128x,38+128y]: unknown -> [82] [1,0] 81x+64x²-38y-64y²+20 [81+128x,102+128y]: unknown -> [83] [1,1] 81x+64x²-102y-64y²-15 endexp[41] expanding queue[42]^21,meter=[2,2]: 49x+32x²-22y-32y²+15 [113+128x,22+128y]: unknown -> [84] [1,0] 113x+64x²-22y-64y²+48 [113+128x,86+128y]: unknown -> [85] [1,1] 113x+64x²-86y-64y²+21 endexp[42] expanding queue[43]^21,meter=[2,2]: 49x+32x²-54y-32y²-4 [49+128x,54+128y]: unknown -> [86] [0,0] 49x+64x²-54y-64y²-2 [49+128x,118+128y]: unknown -> [87] [0,1] 49x+64x²-118y-64y²-45 endexp[43] expanding queue[44]^22,meter=[2,2]: 33x+32x²-14y-32y²+7 [97+128x,14+128y]: unknown -> [88] [1,0] 97x+64x²-14y-64y²+36 [97+128x,78+128y]: unknown -> [89] [1,1] 97x+64x²-78y-64y²+13 endexp[44] expanding queue[45]^22,meter=[2,2]: 33x+32x²-46y-32y²-8 [33+128x,46+128y]: unknown -> [90] [0,0] 33x+64x²-46y-64y²-4 [33+128x,110+128y]: unknown -> [91] [0,1] 33x+64x²-110y-64y²-43 endexp[45] expanding queue[46]^23,meter=[2,2]: x+32x²-30y-32y²-7 [65+128x,30+128y]: unknown -> [92] [1,0] 65x+64x²-30y-64y²+13 [65+128x,94+128y]: unknown -> [93] [1,1] 65x+64x²-94y-64y²-18 endexp[46] expanding queue[47]^23,meter=[2,2]: x+32x²-62y-32y²-30 [1+128x,62+128y]: unknown -> [94] [0,0] x+64x²-62y-64y²-15 [1+128x,126+128y]: unknown -> [95] [0,1] x+64x²-126y-64y²-62 endexp[47] expanding queue[48]^24,meter=[2,2]: 63x+32x²-2y-32y²+31 [127+128x,2+128y]: unknown -> [96] [1,0] 127x+64x²-2y-64y²+63 [127+128x,66+128y]: unknown -> [97] [1,1] 127x+64x²-66y-64y²+46 endexp[48] expanding queue[49]^24,meter=[2,2]: 63x+32x²-34y-32y²+22 [63+128x,34+128y]: unknown -> [98] [0,0] 63x+64x²-34y-64y²+11 [63+128x,98+128y]: unknown -> [99] [0,1] 63x+64x²-98y-64y²-22 endexp[49] expanding queue[50]^25,meter=[2,2]: 31x+32x²-18y-32y²+5 [95+128x,18+128y]: unknown -> [100] [1,0] 95x+64x²-18y-64y²+34 [95+128x,82+128y]: unknown -> [101] [1,1] 95x+64x²-82y-64y²+9 endexp[50] expanding queue[51]^25,meter=[2,2]: 31x+32x²-50y-32y²-12 [31+128x,50+128y]: unknown -> [102] [0,0] 31x+64x²-50y-64y²-6 [31+128x,114+128y]: unknown -> [103] [0,1] 31x+64x²-114y-64y²-47 endexp[51] expanding queue[52]^26,meter=[2,2]: 15x+32x²-10y-32y²+1 [79+128x,10+128y]: unknown -> [104] [1,0] 79x+64x²-10y-64y²+24 [79+128x,74+128y]: unknown -> [105] [1,1] 79x+64x²-74y-64y²+3 endexp[52] expanding queue[53]^26,meter=[2,2]: 15x+32x²-42y-32y²-12 [15+128x,42+128y]: unknown -> [106] [0,0] 15x+64x²-42y-64y²-6 [15+128x,106+128y]: unknown -> [107] [0,1] 15x+64x²-106y-64y²-43 endexp[53] expanding queue[54]^27,meter=[2,2]: 47x+32x²-26y-32y²+12 [47+128x,26+128y]: unknown -> [108] [0,0] 47x+64x²-26y-64y²+6 [47+128x,90+128y]: unknown -> [109] [0,1] 47x+64x²-90y-64y²-23 endexp[54] expanding queue[55]^27,meter=[2,2]: 47x+32x²-58y-32y²-9 [111+128x,58+128y]: unknown -> [110] [1,0] 111x+64x²-58y-64y²+35 [111+128x,122+128y]: unknown -> [111] [1,1] 111x+64x²-122y-64y²-10 endexp[55] expanding queue[56]^28,meter=[2,2]: 47x+32x²-6y-32y²+17 [111+128x,6+128y]: unknown -> [112] [1,0] 111x+64x²-6y-64y²+48 [111+128x,70+128y]: unknown -> [113] [1,1] 111x+64x²-70y-64y²+29 endexp[56] expanding queue[57]^28,meter=[2,2]: 47x+32x²-38y-32y²+6 [47+128x,38+128y]: unknown -> [114] [0,0] 47x+64x²-38y-64y²+3 [47+128x,102+128y]: unknown -> [115] [0,1] 47x+64x²-102y-64y²-32 endexp[57] expanding queue[58]^29,meter=[2,2]: 15x+32x²-22y-32y²-2 [15+128x,22+128y]: unknown -> [116] [0,0] 15x+64x²-22y-64y²-1 [15+128x,86+128y]: unknown -> [117] [0,1] 15x+64x²-86y-64y²-28 endexp[58] expanding queue[59]^29,meter=[2,2]: 15x+32x²-54y-32y²-21 [79+128x,54+128y]: unknown -> [118] [1,0] 79x+64x²-54y-64y²+13 [79+128x,118+128y]: unknown -> [119] [1,1] 79x+64x²-118y-64y²-30 endexp[59] expanding queue[60]^30,meter=[2,2]: 31x+32x²-14y-32y²+6 [31+128x,14+128y]: unknown -> [120] [0,0] 31x+64x²-14y-64y²+3 [31+128x,78+128y]: unknown -> [121] [0,1] 31x+64x²-78y-64y²-20 endexp[60] expanding queue[61]^30,meter=[2,2]: 31x+32x²-46y-32y²-9 [95+128x,46+128y]: unknown -> [122] [1,0] 95x+64x²-46y-64y²+27 [95+128x,110+128y]: unknown -> [123] [1,1] 95x+64x²-110y-64y²-12 endexp[61] expanding queue[62]^31,meter=[2,2]: 63x+32x²-30y-32y²+24 [63+128x,30+128y]: unknown -> [124] [0,0] 63x+64x²-30y-64y²+12 [63+128x,94+128y]: unknown -> [125] [0,1] 63x+64x²-94y-64y²-19 endexp[62] expanding queue[63]^31,meter=[2,2]: 63x+32x²-62y-32y²+1 [127+128x,62+128y]: unknown -> [126] [1,0] 127x+64x²-62y-64y²+48 [127+128x,126+128y]: unknown -> [127] [1,1] 127x+64x²-126y-64y²+1 endexp[63] ---------------- level 7 Maximum level 7 [128] mod 2: x²-y²+3
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clear // //Initilization of Variables t=40 //degree celsius //temperature A_s=400 //mm**2 //Area of steel bar A_c=600 //mm**2 //Area of copper bar E_s=2*10**5 //N/mm**2 //Modulus of Elasticity of steel bar E_c=1*10**5 //N/mm**2 //Modulus of Elasticity of copper bar alpha_s=12*10**-6 //degree celsius //Temperature coeff of steel bar alpha_c=18*10**-6 //degree celsius //Temperature coeff of copper bar L_c=800 //mm //Length of copper bar L_s=600 //mm //Length of steel bar //Calculations //Let P_s be the tensile force in steel bar and P_c be the compressive force in copper bar //Static Equilibrium obtained by taking moment about A //P_c=2*P_s //From property of similar triangles we get //(alpha_c*Lc-dell_c)*1**-1=(alpha_s*L_s-dell_s)*2**-1 //After substituting values in above equations and further simplifying we get P_s=(2*alpha_c*L_c-alpha_s*L_s)*t*(L_s*(A_s*E_s)**-1+4*L_c*(A_c*E_c)**-1)**-1 P_c=2*P_s //Stress in steel rod sigma_s=P_s*A_s**-1 //N/mm**2 //Stress in copper rod sigma_c=P_c*A_c**-1 //N/mm**2 //Result printf("\n Stress in steel rod is %0.2f N/mm**2",sigma_s) printf("\n STress in copper rod is %0.2f N/mm**2",sigma_c)
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R=1.987;//universal gas constant// T=473;//temperature in kelvin// A=2.75*10^15;//frequency factor in per sec// K=1.38*10^-16;//boltzmans constant// h=6.625*10^-27;//planks constant// dn=0; dS=4.57*(log10(A)-log10(exp(1))-log10(9.85*10^12));//entropy change in cal per deg// printf('The entropy of activation=dS=%f=9.19eu',dS); printf('\nSince A is independent of concentration units dS does not sepend on the concentration units used\nand hence the standard state.\nHowever if the time were expressed in different units A will assume a different value\nand consequently the value of dS will be different\nIf time were expressed in minutes A=2.75*10^15*60 per min\ndS=9.19+4.57*log10(60)=17.32eu\nfor bimolecular reaction e^2=7.4*10^10 \nso dS will result in dS=-10.1eu or mol per litre.'); printf('\nIf the concentration were expressed in mol per millilitre A would be 7.4*10^13 \nso dS will result in dS=-10.1+13.6=3.5eu or mol per millilitre\nIf the concentration were expressed in molecules per millilitre the value of A will be multiplied by 6.023*10^23 \nso dS would result in as dS=-10.1-94.9=-105eu or -105molecules per millilitre');
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a b d u l 압 둘 a b e l 아 벨 a b r a m s 아 브 람 스 a d o l f 아 돌 프 a g r i p p i n a 아 그 리 피 나 a h m a d 아 마 드 a i l e e n 에 일 린 a l b a 알 바 a l b a n 알 반 a l b a n i 알 바 니 a l b e r s 알 베 르 스 a l d e r 알 더 a l l a r d 알 라 드 a l l o n 알 론 a l t 알 트 a l t e n b e r g 알 텐 베 르 크 a l v a 알 바 a m a l i a 아 말 리 아 a m a r a 아 마 라 a n a t o l i a 아 나 톨 리 아 a n d e r s o n 앤 더 슨 a n d r e w s 앤 드 루 스 a n g e l i k a 앙 겔 리 카 a n n 앤 a n n a 안 나 a n n a p o l i s 아 나 폴 리 스 a n t w e r p 앤 트 워 프 a n w a r i 안 와 리 a r n h e m 아 른 헴 a s k e 아 스 케 a s t a n a 아 스 타 나 a t l a s 아 틀 라 스 a u g u s t 아 우 구 스 트 a u g u s t 어 거 스 트 b a b b i t t 바 비 트 b a f f i n 배 핀 b a k e r 베 이 커 b a k h t i n 바 흐 친 b a l b o a 발 보 아 b a l c h 볼 치 b a l m e r 발 머 b a m b e r 뱀 버 b a n g 방 b a n j u l 반 줄 b a r n a r d 바 너 드 b a r r i e 배 리 b a s i n 바 신 b a s o v 바 소 프 b a t t l e 배 틀 b a y a r d 바 야 르 b a y l e 벨 b e a r d 비 어 드 b e a u m o n t 바 몬 트 b e a u m o n t 보 몬 트 b e a u v o i r 보 부 아 르 b e e r n a e r t 베 르 나 르 트 b e l f a s t 벨 파 스 트 b e l f o r t 벨 포 b e l g r a d e 벨 그 라 드 b e n z 벤 츠 b e r e n g e r 베 린 저 b e r n 베 른 b e r n a r d i n o 베 르 나 르 디 노 b e r n h a r d 번 하 드 b e r t r a n d 베 르 트 랑 b e t h e s d a 베 데 스 다 b e t h l e h e m 베 들 레 헴 b e t t i n o 베 티 노 b e t t y 베 티 b i l b a o 빌 바 오 b i n d i n g 빈 딩 b l a c h e 블 라 슈 b l a c k b u r n 블 랙 번 b l i n d e r 블 라 인 더 b l o o m b e r g 블 룸 버 그 b l o u n t 블 라 우 트 b l u m b e r g 블 럼 버 그 b o e r 보 어 b o i s e 보 이 시 b o r c h a r d t 보 르 하 르 트 b o r c h e r t 보 르 헤 르 트 b o r g e s 보 르 헤 스 b o s s u e t 보 쉬 에 b r a c t o n 브 랙 턴 b r e c h t 브 레 히 트 b r e n t a n o 브 렌 타 노 b r i g g s 브 리 그 스 b r i g h t o n 브 라 이 튼 b r o a d w a y 브 로 드 웨 이 b r o w n e 브 라 운 b r u s s e l s 브 뤼 셀 b u j u m b u r a 부 줌 부 라 b u r g u n d y 부 르 고 뉴 b u r k e 버 크 b u r m a n 버 마 c a e t a n o 까 에 따 누 c a l d e r o n 깔 데 론 c a m b r i d g e 케 임 브 리 지 c a m d e s s u s 캉 드 쉬 c a n o v a 카 노 바 c a r d e n a s 카 르 데 나 스 c a r m i c h a e l 카 마 이 클 c a r o l e 캐 롤 c a r v a l h o 카 르 발 료 c a s a l s 카 살 스 c a s t i g l i o n e 카 스 틸 리 오 네 c a v a l c a n t i 카 발 칸 티 c e c h 체 크 c e c i l i a 세 실 리 아 c e r v a n t e s 세 르 반 테 스 c h a t t a n o o g a 채 터 누 가 c h a u n c e y 첸 시 c h i p p e n d a l e 치 펜 데 일 c h u r c h i l l 처 칠 c i c e r o 키 케 로 c l a u d e 클 라 우 데 c l a u d i u s 클 라 우 디 우 스 c l e a r w a t e r 클 리 어 워 터 c l e m e n s 클 레 멘 스 c l e v e l a n d 클 리 블 랜 드 c o b u r n 코 번 c o l e t t e 콜 레 트 c o l l i n 콜 린 c o o p e r 쿠 퍼 c o r n e i l l e 코 르 네 유 c o r n e l i u s 코 르 넬 리 우 스 c o u t o 코 투 c r i s p i 크 리 스 피 c r i s p i n 크 리 스 피 누 스 c r o a t i a 크 로 아 티 아 c r o m m e l y n c k 크 롬 랭 크 c r u y f f 크 루 이 프 c u g n o t 퀴 뇨 c u v i e r 퀴 비 에 d a f o e 데 포 d a n 단 d a n z i g 단 치 히 d a w e s 도 스 d e b s 데 브 스 d e d e k i n d 데 데 킨 트 d e h m e l 데 멜 d e l a n e 딜 레 인 d e l t a 델 타 d e n n i s 데 니 스 d e r z h a v i n 데 르 자 빈 d i c k e n s 디 킨 즈 d i o c l e t i a n u s 디 오 클 레 티 아 누 스 d i x 딕 스 d l a m i n i 들 라 미 니 d o d o m a 도 도 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미 j o a c h i m 요 아 킴 j o e 조 j o n a h 요 나 j o n g k i n d 용 킨 트 j o u h a u x 주 오 j o u v e 주 브 j o x e 족 스 j u g l a r 쥐 글 라 j u n k e r 융 커 k a h n 칸 k a r a j a n 카 라 얀 k a r a k h a n 카 라 한 k a r l f e l d t 칼 펠 트 k a t z 카 츠 k a u f m a n 코 프 먼 k a z a k h s t a n 카 자 흐 스 탄 k e n t o n 켄 턴 k e s s l e r 케 슬 러 k e s w i c k 케 스 윅 k e y n e s 케 인 스 k h o r a n a 코 라 나 k i p l i n g 키 플 링 k o b l e n z 코 블 렌 츠 k o l l w i t z 콜 비 츠 k o l t s o v 콜 초 프 k o n r a d 콘 라 트 k o r n e i c h u k 코 르 네 이 추 크 k o r o l e n k o 코 롤 렌 코 k r o e m e r 크 로 머 k u p r i n 쿠 프 린 k u t t e r 쿠 터 l a h o r e 라 호 르 l a n c e 랜 스 l a n g 랑 l a n g u e d o c 랑 그 도 크 l a n s i n g 랜 싱 l a p l a c e 라 플 라 스 l a p t e v 랍 테 프 l a t h a m 레 이 담 l a u g h l i n 로 플 린 l a u r e n 로 렌 l a v o i s i e r 라 부 아 지 에 l e o n a r d o 레 오 나 르 도 l e o p a r d i 레 오 파 르 디 l e w e s 루 이 스 l i a m 리 엄 l i b b y 리 비 l i l l i a n 릴 리 언 l i m 림 l i m b u r g 림 부 르 흐 l i m e r i c k 리 머 릭 l o e b 러 브 l o n g 롱 l o r e n z e n 로 렌 젠 l o t t 롯 l u i g i 루 이 지 l y e l l 라 이 엘 m a c k a y 맥 케 이 m a c l e o d 매 클 라 우 드 m a d e i r a 마 데 이 라 m a g d a l e n a 막 달 레 나 m a l a m u d 맬 러 머 드 m a l h e r b e 말 레 르 브 m a l i p i e r o 말 리 피 에 로 m a n a m a 마 나 마 m a n e t 마 네 m a n g 망 m a n z o n i 만 초 니 m a r g a r e t 마 거 릿 m a r g o l i s 마 골 리 스 m a r g u l i s 마 굴 리 스 m a r i 마 리 m a r k o w i t z 마 코 위 츠 m a r l e n e 마 를 레 네 m a r l o w e 말 로 m a s s o n 마 송 m a s t e r s 마 스 터 스 m a s u r 마 주 어 m a t t h i a s 마 티 아 스 m a u r r a s 모 라 스 m a u r u s 모 뤼 스 m a y h e w 메 이 휴 m b a b a n e 음 바 바 네 m e a d o w s 미 도 우 스 m e d a w a r 메 더 워 m e g 맥 m e h t a 메 타 m e l 멜 m e l a n c h t h o n 멜 란 히 톤 m e l v i l 멜 빌 m e r y l 메 릴 m e s o p o t a m i a 메 소 포 타 미 아 m e t z l e r 메 츠 러 m i l a n o 밀 라 노 m i l l a y 밀 레 이 m i l t 밀 트 m i n n e s o t a 미 네 소 타 m i s s i s s i p p i 미 시 시 피 m i t t e r r a n d 미 테 랑 m o n i c a 모 니 카 m o n r o e 먼 로 m o n t a i g n e 몽 테 뉴 m o n t a n a 몬 태 나 m o n t e v e r d i 몬 테 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y 피 어 리 p e i r c e 퍼 스 p e l e g r i n 펠 레 그 린 p e n c k 펭 크 p e n g 펑 p e n r o s e 펜 로 스 p e p e 페 페 p e r e c 페 렉 p e r r e t 페 레 p e t e r 베 드 로 p e t e r b o r o u g h 피 터 버 러 p f l e i d e r e r 플 라 이 테 러 p h i l l i p s 필 립 스 p i a t i g o r s k y 피 아 티 고 르 스 키 p i a z z i 피 아 치 p i c c a r d 피 카 르 p i c k 피 크 p i e r o 피 에 로 p i e t e r 피 터 p i s a 피 사 p i s a n o 피 사 노 p o l i z i a n o 폴 리 치 아 노 p o n s 퐁 스 p o n t o p p i d a n 폰 토 피 단 p o r t a 포 르 타 p o r t s m o u t h 포 츠 머 스 p o t s d a m 포 스 담 p o u l 포 울 p o y n t i n g 포 인 팅 p r a i a 프 라 이 아 p r a n d t l 프 란 틀 p r a s a d 프 라 사 드 p r e n d e r g a s t 프 렌 더 가 스 트 p r o k h o r o v 프 로 호 로 프 p u i g 프 이 그 p y o n g y a n g 평 양 q u e e n 퀸 r a b e l a i s 라 블 레 r a c e 레 이 스 r a m a n 라 만 r a n d a l l 랜 달 r a w l i n g s 롤 링 스 r a z i n 라 진 r e e l 릴 r e m i n g t o n 레 밍 턴 r e n a t a 레 나 타 r e n n 렌 r e s p i g h i 레 스 피 기 r i c e 라 이 스 r i c h e l i e u 리 슐 리 외 r i c h m o n d 리 치 먼 드 r i c k e n 리 켄 r i d e l 리 델 r i p l e y 리 플 리 r i t z 리 츠 r o b i n s o n 로 빈 슨 r o g e r 로 저 r o m a 로 마 r o m e o 로 메 오 r o m m e l 로 멜 r o s e n b e r g 로 젠 베 르 크 r o u x 루 r u g b y 럭 비 r u p e r t 루 퍼 트 r u s s o 루 소 r w a n d a 르 완 다 r y z h k o v 리 슈 코 프 s a c h s 색 스 s a i n t 샌 트 s a i n t 세 인 트 s a l a z a r 살 라 자 르 s a l e h 살 레 s a l z b u r g 잘 츠 부 르 크 s a m m y 새 미 s a m p s o n 샘 슨 s a n d b u r g 샌 드 버 그 s a n d e r s o n 샌 더 슨 s a n t a y a n a 산 타 야 나 s a p i r 사 피 어 s a r a h 사 라 s a r n e y 사 르 네 이 s a r t o n 사 턴 s c a l i a 스 캘 리 아 s c h e e l e 셸 레 s c h e i d e m a n n 샤 이 데 만 s c h i e l e 실 레 s c h i l l i n g 실 링 s c h l i e m a n n 슐 리 만 s c h o n b e r g 쇤 베 르 크 s c h o n g a u e r 숀 가 우 어 s c h w a r z k o p f 슈 워 츠 코 프 s e g a l 시 갈 s e g o v i a 세 고 비 아 s e n 센 s e n i o r 시 니 어 s e r g e 세 르 게 s e r v a i s 세 르 베 s e r v e t u s 세 르 베 투 스 s h a d w e l l 섀 드 웰 s h a r a f 셰 라 프 s h a w 쇼 s i c k e l 지 켈 s i e g e n 지 겐 s i m m o n d s 시 먼 즈 s i n a i 시 나 이 s i n a i 시 내 s i n o 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r i n 투 린 t u r k 터 키 t u r n e r 터 너 t u v a l u 투 발 루 t w a r d o w s k i 트 와 르 도 프 스 키 u c c e l l o 우 첼 로 u l a a n b a a t a r 울 란 바 토 르 u n a m u n o 우 나 무 노 u n g a r o 웅 가 로 u n s w o r t h 언 스 워 스 u p d i k e 업 다 이 크 u t e 우 트 v a l e n t i n o 발 렌 티 노 v a l e r a 발 레 라 v e l a y a t i 벨 라 야 티 v e n t u r i 벤 투 리 v e r e s a e v 베 레 사 예 프 v e r n e t 베 르 네 v i c 빅 v i c t o r i a 빅 토 리 아 v i e n t i a n e 비 엔 티 안 v i l a 빌 라 v i l l a n i 빌 라 니 v i n c e n z o 빈 첸 초 v i r t a n e n 비 르 타 넨 v o s s 포 스 v o u e t 부 에 w a l d 월 드 w a l e s 웨 일 스 w a l k e r 워 커 w a l l a c e 월 리 스 w a t s o n 왓 슨 w e b s t e r 웹 스 터 w e i n h e b e r 바 인 헤 버 w e i s m a n n 바 이 스 만 w e i s s 바 이 스 w e l c h 웰 치 w e n d y 웬 디 w e r t h 웰 스 w e r t h e i m e r 베 르 트 하 이 머 w e s l e y 웨 슬 리 w e y g a n d 베 강 w h o r f 워 프 w i e c h e r t 비 헤 르 트 w i e s b a d e n 비 스 바 덴 w i l f r e d 윌 프 레 드 w i l m 빌 름 w i l t s h i r e 윌 트 셔 w i m 빔 w i n k l e r 빙 클 러 w i s c o n s i n 위 스 콘 신 w i t t e n b e r 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// Exa 6.21 clc; clear; close; // Given data T_sat = 99.6;// in degree C h_fg = 2258;// in kJ/kg m = 1;// steam output of the boiler in (assumed) m1 = 0.03;// exhaust steam x = 0.9; T1 = 21;// in degree C Cp = 4.187;// kJ/kg-K // Formula m1*(Cp*(T_sat-t)+x*h_fg)= m*Cp*(t-T1) t= (m1*(Cp*T_sat+x*h_fg)+m*Cp*T1)/(Cp*(m+m1)) disp(t,"Temperature of the feed water leaving the heater in degree C is");
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//Example 29.9 delta_t=1*10^-10;//Uncertainty in time (s) h=6.63*10^-34;//Planck's constant (J.s) delta_E=h/(4*%pi*delta_t);//Uncertainty in energy (J) delta_E=delta_E*1/(1.6*10^-19);//Uncertainty in energy (eV) printf('Minimum uncertainty in energy = %0.1e eV',delta_E) //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest
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clear; // Echantillons N=100; // Intervalles de temps t=(0 :N-1); // Signal s=squarewave(t); // sin(t); // FFT manual Sf1=sum(s'*ones(1,N).*exp(-2*%pi*%i*t'*t/N),'r'); // FFT function Sf2=fft(s,-1); subplot(1,2,1); plot(t,s,'-r'); // .dg xlabel("Signal"); subplot(1,2,2); plot(t,Sf1,'-r'); xlabel("FFT");
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// Copyright (C) 2015 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author: Nihar Rao // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in function[stats] = graycoprops(srcImg, varargin) // This function computes the Properties of gray-level co-occurrence matrix. // // Calling Sequence // z=imread("lena.jpeg"); //in grayscale or color // //Note: z can be a image or simply a Matrix. // gray=graycoprops(z) //get all 4 properties // gray=graycoprops(z,"contrast") //compute only contrast // gray=graycoprops(z,["contrast" "energy"]) //compute contrast and energy.the properties can be passed in any order // gray=graycoprops(z,["contrast" "correlation" "energy"]) // gray=graycoprops(z,["contrast" "correlation" "energy" "homogeneity"]) // // Parameters // // gray: A struct containing all the parameters // z: A image or a matrix // contrast: a measure of the intensity contrast between a pixel and its neighbor over the whole image. // energy: the sum of squared elements // homogeneity: a value that measures the closeness of the distribution of elements. // correlation:a measure of how correlated a pixel is to its neighbor over the whole image // // Description // This function computes the Properties of gray-level co-occurrence matrix.The properties being "correlation","contrast","energy" and "homogeneity". // // // Examples // //compute for a image // z=imread("lena.jpeg",0); // sss=graycoprops(z,["contrast"]) // // //compute for a matrix // glcm = [0 1 2 3;1 1 2 3;1 0 2 0;0 0 0 3] // sss=graycoprops(glcm,["contrast" "energy" "correlation"]) [lhs, rhs] = argn(0) srcMat = mattolist(srcImg) select rhs case 1 then [contrast correlation energy homo] = raw_graycoprops(srcMat); stats=struct('Contrast',contrast,'Correlation',correlation,'Energy',energy,'Homogeniety',homo); case 2 then [rows cols]=size(varargin(1)); n=rows*cols; if n>4 error(msprintf("the string matrix must have maximimum of 4 entries")); end inputString=varargin(1); if n==1 [out]=raw_graycoprops(srcMat,varargin(1)); stats=struct(inputString(1),out); elseif n==2 [out out1]=raw_graycoprops(srcMat,varargin(1)); stats=struct(inputString(1),out,inputString(2),out1); elseif n==3 [out out1 out2]=raw_graycoprops(srcMat,varargin(1)); stats=struct(inputString(1),out,inputString(2),out1,inputString(3),out2); elseif n==4 [out out1 out2 out3]=raw_graycoprops(srcMat,varargin(1)); stats=struct(inputString(1),out,inputString(2),out1,inputString(3),out2,inputString(4),out3); end end endfunction
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// Exa 1.6 clc; clear; close; // Given data V_o = 0.7;// in V disp(V_o,"The value of V_o in V is"); E = 10;// in V V_D = V_o;// in V R = 330;// in ohm I1 = (E - V_D)/R;// in A I1 = I1*10^3;// in mA disp(I1,"The value of I1 in mA is"); I_D1 = I1/2;// in mA disp(I_D1,"The value of I_D1 in mA is"); I_D2 = I_D1;// in mA disp(I_D2,"The value of I_D2 in mA is");
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//Example 10.17 //Fourth Order Runge Kutta Method for system of 1st order equations //Page no. 327 clc;clear;close; deff('y=f(x,y,z)','y=x+z') deff('y=g(x,y,z)','y=x-y') y=0;h=0.1;z=1; for i=1:2 x=(i-1)*h K(1)=h*f(x,y,z); L(1)=h*g(x,y,z); K(2)=h*f(x+h/2,y+K(1)/2,z+L(1)/2); L(2)=h*g(x+h/2,y+K(1)/2,z+L(1)/2); K(3)=h*f(x+h/2,y+K(2)/2,z+L(2)/2); L(3)=h*g(x+h/2,y+K(2)/2,z+L(2)/2); K(4)=h*f(x+h,y+K(3),z+L(3)); L(4)=h*g(x+h,y+K(3),z+L(3)); y=y+(K(1)+2*K(2)+2*K(3)+K(4))/6 z=z+(L(1)+2*L(2)+2*L(3)+L(4))/6 for j=1:4 printf('\n K%i = %g\t\tL%i = %g\n',j,K(j),j,L(j)) end printf('\ny(%g) = %.8f\t\tz(%g) = %.8f\n\n\n\n',x+h,y,x+h,z) end
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//Pressure at entry(in psia): p1=14.7; //Temperature at entry(in F): T1=70; //Pressure at exit(in psia): p2=50; //Temprature a exit(in F): T2=100; //Cross sectional area of the pipe at exit(in ft^2): A2=1; //Mass flow rate(in lbf/sec): m=20; //Power input to the compressor(in hp): Ws=-600; //Value of cp(in Btu/lbm-R): cp=0.24; //Value of gas constant(in ft-lbf/(lbm-R)) R=53.3;
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load Comparator8bit.hdl; output-file Comparator8bit.out; output-list x7 x6 x5 x4 x3 x2 x1 x0 y7 y6 y5 y4 y3 y2 y1 y0 z; set x0 0,set x1 1,set x2 0,set x3 1,set x4 0,set x5 0,set x6 0,set x7 0,set y0 0,set y1 1,set y2 0,set y3 1,set y4 0,set y5 0,set y6 0,set y7 0,eval,output; set x0 1,set x1 1,set x2 0,set x3 1,set x4 0,set x5 0,set x6 0,set x7 0,set y0 1,set y1 1,set y2 0,set y3 1,set y4 0,set y5 0,set y6 0,set y7 0,eval,output; set x0 0,set x1 1,set x2 1,set x3 1,set x4 0,set x5 0,set x6 0,set x7 0,set y0 0,set y1 1,set y2 0,set y3 1,set y4 0,set y5 0,set y6 0,set y7 0,eval,output; set x0 0,set x1 0,set x2 1,set x3 1,set x4 1,set x5 0,set x6 0,set x7 0,set y0 0,set y1 0,set y2 0,set y3 0,set y4 0,set y5 0,set y6 0,set y7 0,eval,output;
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clc; //e.g 18.2 Vbb=10; Rb=50*10**3; Vcc=20; Rc=300; beta=200; Ic=Vcc/Rc;//saturation current disp('mA',Ic*10**3,"Ic="); Vce=Vcc;//cut-off voltage disp('V',Vce*1,"Vce="); Ib=(Vbb-0.7)/Rb; disp('10^-3A',Ib*10**3,"Ib="); Ic=beta*Ib; disp('10^-3A',Ic*10**3,"Ic="); Vce=Vcc-Ic*Rc; disp('V',Vce*1,"Vce="); i=21:-0.1:0; plot2d(i); a=gca() //get the current axes a.box="off"; xlabel("VCE"); ylabel( "IC");
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Chapter3_Example31.sce
//Chapter-3, Example 3.31, Page 109 //============================================================================= clc clear //INPUT DATA t=0.025;//Thickness of fin in m L=0.1;//Length of fin in m k=17.7;//Thermal conductivity of the fin material in W/m.K p=7850;//Density in kg/m^3 Tw=600;//Temperature of the wall in degree C Ta=40;//Temperature of the air in degree C h=20;//Heat transfer coefficient in W/m^2.K I0(1.9)=2.1782;//Io value taken from table 3.2 on page no.108 I1(1.9)=1.48871;//I1 value taken from table 3.2 on page no. 108 //CALCULATIONS B=sqrt((2*L*h)/(k*t));//Calculation of B for determining temperature distribution X=((Tw-Ta)/I0(2*B*sqrt(0.1)));//Calculation of X for determining temperature distribution Y=(2*B);//Calculation of Y for determining temperature distribution Q=(sqrt(2*h*k*t)*(Tw-Ta)*((I1(2*B*sqrt(0.1)))/(I0(2*B*sqrt(0.1))))); m=((p*t*L)/2);//Mass of the fin per meter of width in kg/m q=(Q/m);//Rate of heat flow per unit mass in W/kg //OUTPUT mprintf('Temperature distribution is T=%i+%3.1f(%3.4f√x)\nRate of heat flow per unit mass of the fin is %3.2f W/kg',Ta,X,Y,q) //=================================END OF PROGRAM==============================
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// key is to look for the feature you want to extract :) S = imread('four.jpg'); ShowColorImage(S,'0'); S2 = rgb2gray(S); ShowImage(S2,'0'); S3 = S2>180; ShowImage(S3,'0'); se = CreateStructureElement('vertical_line', 10); S4 = ErodeImage(S3, se); se = CreateStructureElement('horizontal_line', 10); S4 = ErodeImage(S4, se); ShowImage(S4,'0'); S5 = S4.*1; IsCalculated = CreateFeatureStruct(%f); IsCalculated.Centroid = %t; S6 = AnalyzeBlobs(S5, IsCalculated); ShowColorImage(S,'0'); plot(S6(1).Centroid(1),S6(1).Centroid(2),'r*');
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//find clc //solution //given P=22000//W Np=1800//rpm Ng=600//rpm a=(%pi/180)*30 q=(%pi/180)*20 Tp=24 vr=3 fo=50//N/mm^2 //b=4*pc oh=150//mm..overhang t=50//N/mm^2 T=P*60*1000/(2*%pi*Np)//N-mm printf("torque acting is,%f N-mm\n",T) Te=T/(cos(a))^3//N yb=0.154-(0.912/Te) //Wt=T/(Dp/2)=(2T/m/Tp)....Dp=m*Tp //Wt=9725/m....eq1 //v=%pi*m*Tp*Np=135.735*m//m/min //Cv=350/(350+v) //Wt=fo*Cv*b*%pi*m*yp//N...eq2 //Wt=(fo*Cv)*4*%pi*m*%pi*m*yb...eq3 //using hit and trial in eq2 and eq3,we egt m=4.75..say 6 m=6 b=4*%pi*m printf("module and face width is,%f mm\n,%f mm\n",m,b) Dp=m*Tp Tg=3*Tp printf("numbr of teeeth on gear is,%f \n",Tg) Dg=m*Tg printf("pitch circle dia of pinion and gear is is,%f mm\n,%f mm\n",Dp,Dg) Tg=3*Tp printf("numbr of teeeth on gear is,%f \n",Tg) //let dp be dia of pinion shaft Wt=9725/m printf("Wt is,%f N\n",Wt) Wa=Wt*tan(a) printf("Wa is,%f N\n",Wa) M1=Wt*oh//N-mm M2=Wa*Dp/2//N-mm M=sqrt(M1^2 +M2^2) printf("equivalnet bendng moment is,%f N-mm\n",M) Te=sqrt(T^2 +M^2) //dp=(Te*16/(%pi*t))^(1/3)//mm printf("dia of pinion shaft is,%f mm\n",(Te*16/(%pi*t))^(1/3)) printf("dia of pinion shaft is,say 35mm\n") dp=35//mm printf("dia of pinion hub is,%f mm\n",1.8*dp) printf("length of hub is,%f mm\n",1.25*dp) T1=T*vr//torque on gear shaft M22=Wa*Dg/2 Mr=sqrt(M1^2 +M22^2) Te1=sqrt(Mr^2 + T1^2) //let dg be dia of gear shfat //dg=(Te1*16/(%pi*t))^(1/3)//mm printf("dia of gear shaft is,%f mm\n",(Te1*16/(%pi*t))^(1/3)) printf("dia of gear shaft is,say 40 mm\n") dg=40//mm printf("dia of gear hub is,%f mm\n",1.8*dg) printf("length of hub is,%f mm\n",1.25*dg) //let a1 be major axis and b1 minor axis //b1=a1/2 //Z=%pi*b1*a1^2/32=0.05*a1^3 v=135.735*m Cv=350/(350+v) Ws=Wt/Cv//N Mb=Ws/4*Dg/2//N-mm printf("max bending moment acting is,%f N-mm\n",Mb) fb=42//N/mm^2 //fb=M/Z a1=(Mb/(0.05*fb))^(1/3)//mm printf("major and minor axis of section is,%f mm\n,%f mm\n",a1,a1/2)
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// Measurement of Circuit Voltage changes // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 4-10 in page 211 clear; clc; close; // Given Data Vb=-5; // Base Voltage of BJT in V Rc=1*10^3; // Collector Resistance in K-ohms Ie=2*10^-3; // Emitter Current of BJT in mA delB=+0.4; // Change in Base Voltage // Calculations delE=+0.4; delC=0; printf("(a)Change in Emitter voltage is +%0.2f V\n",delE); printf("(b)Change in Collector Voltage is %0.2f V\n",delC); // Results // (a) Change in Emitter Voltage in the Circuit = +0.4 V // (b) Change in Collector Voltage in the Circuit = 0.0 V
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// Example 14_10 clc;clear;funcprot(0); //Given data omega_a=1;// Unit Speed // Calculation omega_b=2*omega_a;// Speed bhp_ratio=(omega_b/omega_a)^3; printf('\nThe power to the pump motor must be increased by a factor of %0.0f.',bhp_ratio);
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// Calculate voltage gain Av // Basic Electronics // By Debashis De // First Edition, 2010 // Dorling Kindersley Pvt. Ltd. India // Example 7-57 in page 359 clear; clc; close; // Given data gm=2*10^-3; // Transconductance in mA/V rd=10*10^3; // Dynamic resistance in K-ohms C=0.025*10^-6; // Capacitance in microF // Calculation Rl=(30*30)/(30+30); Av=(-gm*rd*Rl*10^3)/(Rl+rd); f1=1/(2*%pi*37.5*10^3*C); Avl=Av/sqrt(1+(f1/(5*10^3))^2); printf("(a)Av = %0.0f\n(b)Avl = %0.2f",Av,Avl); // Result // (a) Av = -30 // (b) Avl = -29.94
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// Given data: clc T1=40+273.0 // ambient temp in kelvin T2=-10+273.0 // freezer temp in kelvin Q2=2 // heat loss rate for freezer in kJ/s Q1=T1*(Q2/T2) // heat transfer rate in kJ/s W=Q1-Q2 // work in kW printf("The least power required is %0.2f kW",W)
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// Exa 2.1 clc; clear; close; // Given data R_L = 1000;// in ohm N2byN1= 4; Vi= '10*sin(omega*t)' // V2= N2byN1*V1 // V2= 40*sin(omega*t) Vm= N2byN1*10;// in V V_Lav= Vm/%pi;// in V disp(V_Lav,"The average load voltage in volts is : ") Im= Vm/R_L;// in A I_dc= Im/%pi;// in A I_av = I_dc;// in A I_av= I_av*10^3;// in mA disp(I_av,"Average load current in mA is"); V_Lrms = Vm/2;// in V disp(V_Lrms,"RMS load voltage in V is"); I_rms = V_Lrms/R_L;// in A I_rms= I_rms*10^3;// in mA disp(I_rms,"RMS load current in mA is"); Eta = I_av^2/I_rms^2*100;// in % disp(Eta,"Efficiency in % is"); V2rms= Vm/sqrt(2);// in V TUF = ((I_av )^2)/(V2rms*I_rms)*100;// in % disp(TUF,"Transformer utilization factor in % is"); Gamma= sqrt(V_Lrms^2-I_av^2)/V_Lav*100; disp(round(Gamma),"Ripple factor in % is");
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// Scilab code Ex8.8: Pg.350 (2008) clc; clear; // Part (a) // For simplicity let kT be unity kT = 1; // Product of Boltzmann constant & temperature, J hf = 2*kT; // Product of Plank's constant & frequency, J-s-Hz E = hf/(exp(hf/kT)-1); // Average energy of vibration of molecules, J printf("\nThe average energy of vibration of molecules at temperature T = hf/2k = %4.2f kT", E); // Part (b) // For simplicity let kT be unity kT = 1; // Product of Boltzmann constant & temperature, J hf = 0.25*kT; // Product of Plank's constant & frequency, J-s-Hz E = hf/(exp(hf/kT)-1); // Average energy of vibration of molecules, J printf("\nThe average energy of vibration of molecules at temperature T = 4hf/2k = %4.2f kT", E); // Result // The average energy of vibration of molecules at temperature T = hf/2k = 0.31 kT // The average energy of vibration of molecules at temperature T = 4hf/2k = 0.88 kT
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// Example 8.1 format('v',6) clc; clear; close; // given data V_EE= 10;// in V V_BE= 0.7;// in V R_E= 20*10^3;// in Ω V_CC= 25;// in V R_C= 10*10^3;// in Ω // The emitter current I_E= (V_EE-V_BE)/R_E;// in A I_C= I_E;// in A // The collector to base voltage, V_CB= V_CC-I_C*R_C;// in V disp(V_CB,"The value of V_CB in volts is : ")
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// Aim:To Determine velocity through pipe. // Given: // Diameter of pipe: D=30; //mm // Flow through pipe: Q=60; //lpm
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clc; lamda=5893*1e-10;//wavelength of monocromatic light n=4000; x=n*lamda/2;//distance moved by mirror M1 disp(+'meter',x,'distance moved by mirror M1 =')
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function [vertex,face] = check_face_vertex(vertex,face, options) // check_face_vertex - check that vertices and faces have the correct size // // [vertex,face] = check_face_vertex(vertex,face); // // Copyright (c) 2007 Gabriel Peyre vertex = check_size(vertex); face = check_size(face); endfunction ////////////////////////////////////////////////////////// function a = check_size(a) if isempty(a) return; end if size(a,1)>size(a,2) a = a'; end if size(a,1)<3 & size(a,2)==3 a = a'; end if size(a,1)<=3 & size(a,2)>=3 & sum(abs(a(:,3)))==0 // for flat triangles a = a'; end if size(a,1)~=3 & size(a,1)~=4 error('face or vertex is not of correct size'); end endfunction
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@relation unknow @attribute mcg real[0.11,1.0] @attribute gvh real[0.13,1.0] @attribute alm real[0.21,1.0] @attribute mit real[0.0,1.0] @attribute erl real[0.5,1.0] @attribute pox real[0.0,0.83] @attribute vac real[0.0,0.73] @attribute nuc real[0.0,1.0] @attribute class{MIT,NUC,CYT,ME1,ME2,ME3,EXC,VAC,POX,ERL} @inputs mcg,gvh,alm,mit,erl,pox,vac,nuc @outputs class @data NUC NUC CYT CYT NUC CYT NUC CYT CYT CYT CYT CYT MIT MIT EXC ME2 CYT MIT CYT CYT NUC NUC CYT CYT EXC EXC MIT ME1 CYT CYT CYT CYT POX MIT NUC ME3 NUC NUC MIT MIT MIT MIT MIT MIT NUC CYT MIT MIT NUC CYT CYT CYT CYT CYT CYT CYT ME3 NUC CYT CYT CYT CYT MIT ME1 MIT MIT MIT MIT MIT ME1 MIT MIT MIT MIT MIT EXC VAC NUC ME3 ME3 CYT CYT CYT CYT NUC CYT NUC MIT EXC EXC CYT CYT MIT CYT CYT NUC MIT CYT MIT MIT NUC CYT NUC NUC ME3 ME3 ME3 ME3 NUC NUC CYT CYT NUC NUC ME3 ME3 CYT NUC ME3 ME3 ME1 NUC NUC CYT CYT NUC CYT EXC CYT NUC CYT NUC NUC NUC ME3 ME3 ME2 ME3 CYT MIT MIT MIT NUC NUC MIT MIT NUC MIT NUC CYT CYT CYT NUC MIT ME3 ME3 ME3 ME3 ME3 ME3 CYT CYT MIT MIT MIT MIT NUC NUC ME1 NUC MIT CYT ME3 ME3 ERL ME2 ME3 NUC ME1 ME2 VAC NUC NUC NUC ME2 NUC MIT MIT MIT MIT MIT ME2 NUC NUC MIT MIT ME3 MIT MIT CYT NUC CYT MIT MIT MIT MIT MIT MIT CYT CYT POX POX ME2 MIT MIT NUC MIT MIT MIT CYT MIT CYT MIT MIT MIT MIT NUC CYT MIT CYT MIT MIT CYT CYT ME1 ME1 CYT NUC MIT MIT CYT NUC NUC NUC NUC CYT NUC CYT CYT CYT NUC CYT NUC NUC NUC ME2 NUC CYT NUC CYT NUC EXC NUC ME2 NUC ME2 NUC CYT ME2 ME2 MIT CYT ME3 CYT NUC NUC MIT NUC ME2 ME1 CYT CYT ME3 ME3 CYT CYT CYT CYT NUC NUC VAC CYT NUC NUC MIT ME2 MIT MIT MIT NUC MIT MIT CYT CYT CYT CYT EXC EXC NUC CYT ME3 ME3 NUC CYT POX CYT CYT CYT VAC NUC VAC MIT CYT CYT CYT ME2 NUC CYT NUC CYT NUC NUC NUC NUC CYT NUC CYT NUC MIT MIT NUC CYT NUC CYT NUC NUC NUC CYT NUC CYT NUC NUC NUC NUC NUC CYT NUC CYT NUC ME3 MIT MIT NUC CYT CYT NUC NUC CYT NUC NUC NUC NUC NUC CYT CYT CYT CYT CYT CYT CYT CYT MIT CYT CYT CYT CYT CYT EXC CYT CYT CYT CYT CYT CYT CYT NUC CYT CYT CYT CYT CYT CYT CYT CYT CYT CYT CYT CYT CYT CYT CYT MIT CYT MIT NUC NUC CYT NUC CYT NUC ME3 ME3 CYT CYT ME2 ME3 ME2 ME3 ME3 ME3 ME3 ME3 NUC CYT NUC CYT ME3 ME3 NUC ME3 NUC NUC CYT CYT NUC NUC NUC NUC CYT CYT NUC NUC NUC CYT NUC CYT NUC CYT NUC NUC NUC NUC CYT NUC MIT MIT NUC NUC EXC EXC EXC EXC NUC CYT CYT CYT CYT NUC ME1 ME1 CYT CYT CYT CYT CYT CYT CYT MIT NUC NUC CYT NUC CYT NUC NUC NUC CYT CYT CYT NUC CYT CYT ME1 ME1 NUC NUC CYT CYT ME3 MIT ME3 NUC CYT ME2 NUC CYT NUC NUC CYT CYT CYT CYT CYT CYT CYT CYT NUC MIT CYT CYT CYT NUC MIT CYT VAC NUC CYT CYT ME3 ME3 ME2 ME1 ME3 ME3 CYT NUC ME3 ME3 ME3 ME3 NUC NUC POX POX ME3 ME3 ME3 ME3 ME2 NUC ME1 ME1 EXC ME1 NUC NUC ME3 ME3 NUC MIT ME3 ME3 ME3 ME3 ME1 ME2 ME3 ME3 CYT MIT ME3 NUC NUC MIT ME1 ME1 MIT MIT CYT ME2 ME2 ME2 CYT CYT
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//To find radius and MI clc //Given: m=55 //kg l=850/1000, d1=75/1000, d2=100/1000 //m tp1=1.83, tp2=1.68 //seconds //Solution: //Refer Fig. 15.20 //Calculating the length of equivalent simple pendulum when suspended from the top of small end bearing L1=9.81*(tp1/(2*%pi))^2 //m //Calculating the length of equivalent simple pendulum when suspended from the top of big end bearing L2=9.81*(tp2/(2*%pi))^2 //m //Radius of gyration of the rod about an axis passing through the centre of gravity and perpendicular to the plane of oscillation: //Calculating the distances of centre of gravity from the top of small end and big end bearings //We have, h1*(L1-h1) = h2*(L2-h2), or h1^2-h2^2+h2*L2-h1*L1 = 0 .....(i) //Also, h1+h2 = d1/2+l+d2/2, or h1+h2-d1/2-l-d2/2 = 0 .....(ii) function y=f(x) h1=x(1) h2=x(2) y(1)=h1^2-h2^2+h2*L2-h1*L1 y(2)=h1+h2-d1/2-l-d2/2 endfunction z=fsolve([1,1],f) h1=z(1), h2=z(2) //m //Calculating the required radius of gyration of the rod kG=sqrt(h1*(L1-h1)) //m //Calculating the moment of inertia of the rod I=m*(kG)^2 //kg-m^2 //Dynamically equivalent system for the rod: //Calculating the distance of the mass situated at the centre of small end bearing from the centre of gravity l1=h1-d1/2 //m //Calculating the distance of the second mass from the centre of gravity towards big end bearing l2=(kG)^2/l1 //m //Calculating the magnitude of the mass situated at the centre of small end bearing m1=(l2*m)/(l1+l2) //kg //Calculating the magnitude of the second mass m2=(l1*m)/(l1+l2) //kg //Results: printf("\n\n Radius of gyration of the rod about an axis passing through the centre of gravity and perpendicular to the plane of oscillation, kG = %.3f m.\n\n",kG) printf(" Moment of inertia of the rod, I = %.2f kg-m^2.\n\n",I) printf(" Magnitude of the mass situated at the centre of small end bearing, m1 = %.2f kg.\n\n",m1) printf(" Magnitude of the second mass, m2 = %.2f kg.\n\n",m2)
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int tst; void main(){ print(tst); }
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clc clear printf("Example 2.9 | Page number 46 \n\n"); //(a) Compute the torque in the driving shaft and shaft power output of the motor. //(b) Compute the net work for battery and motor. //Given Data d = 0.4 //m //cylinder diameter t = 10 //min //Time taken for stirring L = 0.49 //m //distance moved by the piston p_atm = 1 //bar //atmospheric pressure W_net = -1965 //Nm //net work done n = 750 //rev/min //rotational velocity of electric motor I = 0.9 //A //current V = 24 //V //voltage //Solution //Part(a) printf("Part (a)\n"); W_d = 10^5*p_atm * (%pi/4) * d^2 * L; //Nm //work done by fluid on piston printf("Work done by fluid on the piston = %.1f Nm\n",W_d); W_str = W_net - W_d; //Nm //Work done by stirrer printf("Work done by stirrer on the fluid = %.1f Nm\n",W_str); P_shaft = abs(W_str)/(t*60); //W //shaft power output printf("Shaft power output = %.2f W\n",P_shaft); T = (P_shaft*60)/(2*%pi*n); //Nm //Torque in the driving shaft printf("Torque in the driving shaft = %.3f Nm\n", T); //Part(b) printf("\nPart (b)\n"); W_bat = I*V*t*60; //Nm //work done by battery printf("Work done by battery = %.1f Nm\n",W_bat); W_motor = -1*(W_bat+W_str) //Nm //work done by motor printf("Work done by motor = %.1f Nm",W_motor);
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sigmau=550 sigmay=400 Mmin=-150 Mmax=400 Tmin=-50 Tmax=150 Kfb=1.6 Kfs=1.3 FS=1.5 Kb=1 Ks=0.6 Ksz=0.85 Ksur=0.88 Mm=(Mmax+Mmin)/2 disp(Mm,"Mean bending moment=") Mv=(Mmax-Mmin)/2 disp(Mv,"Variable bending moment=") syms d Z=(%pi/32)*d^3 disp(Z,"Section modulus=") sigmam=(Mm*10^3)/Z disp(sigmam,"Mean bending stress=") sigmav=(Mv*10^3)/Z disp(sigmav,"Variable bending stress=") sigmaeb=sigmau/2 sigmaneb=sigmam+(sigmav*sigmay*Kfb)/(sigmaeb*Ksur*Ksz) Tm=(Tmax+Tmin)/2 taum=(16*Tm*10^3)/(%pi*d^3) disp(taum,"Mean shear stress=") Tv=(Tmax-Tmin)/2 tauv=(16*Tv*10^3)/(%pi*d^3) disp(tauv,"Variable shear stress=") taue=sigmae*Ks disp(taue,"Endurance limit for reversed torsional loading=") tauy=0.5*sigmay disp(tauy,"Yield strength in shear=") //yield stress in shear loading is taken as one half of yield stress in reverse bending taues=taum+((tauv*tauy*Kfs)/(taue*Ksur*Ksz)) d=33.84 disp(d,"Diameter of shaft in mm is=")
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loadmatfile('RBS.mat') testSci = filt(uData,band,channel) disp(testSci) disp(test-testSci)
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clc // Given that A = 0.06// amplitude in meter T = 10 * %pi // time period of s.h.m. in sec // Sample Problem 6 on page no. 7.24 printf("\n # PROBLEM 6 # \n") v = A * (2 * %pi / T) printf("\n Standard formula used \n v = A * (2 * pi / T)") printf("\n Maximum velocity = %e meter/sec",v)
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// Copyright (C) 2015 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Author: Rohit Suri, Rohan Gurve // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in // function[dstImg] = roiPoly(srcImg, col_list, row_list) //This function creates mask by selecting the ROI as a poygon. //This function creates mask by selecting the ROI as a poygon. // // Calling Sequence // I = imimread(image-location) // c = [c1 c2 ..............cn] // r = [r1 r2 ..............rn] // BW = roipoly(I, c, r) // // Parameters // I : Input image // c : a 1xn vector specifying the column indices of the vertices of the n sided polygon // r : a 1xn vector specifying the row indices of the vertices of the n sided polygon // BW: Output mask image for input I // // Description // Returns the ROI specified by the polygon described by vectors c and r, which specify the column // and row indices of each vertex, respectively. c and r must be the same size. // // Examples // I = imread('image_01.jpeg'); // c = [50 50 100 100] //defining the column indices of the vertices of the ROI // r = [100 150 150 100 ] //defining the corresponding row indices of the vertices of the ROI // BW = roipoly(I, c, r) //creating a mask // imshow(BW) //viewing the mask // c=colorChange(I,mask,2.4 ,2.0, 2.2); //using this mask in colorChange function // imshow(c); // // Examples // I = imread('../images/color3.jpg'); // c = [ 150 200 250 300 250 200 ] ; //defining the column indices of the vertices of the ROI // r = [ 135 100 100 135 170 170 ] ; //defining the corresponding row indices of the vertices of the ROI // gray = rgb2gray(I) ; //for a grayscale image // BW = roiPoly(I, c, r); //creating a mask // imshow(BW) //viewing the mask // // Examples // I = imread('/images/color3.jpg'); // c1 = [200 250 300 250 150 200 ] // r1 = [ 170 170 135 100 135 100] //undesired output because changing the order of points // BW = roiPoly(I,c1,r1); // imshow(BW) // // Authors // Vinay Bhat // Rohan Gurve [lhs rhs]=argn(0); if rhs>3 error(msprintf(" Too many input arguments")); elseif rhs<3 error(msprintf(" input arguments missing")); end srcMat = mattolist(srcImg) out = raw_roiPoly(srcMat,row_list,col_list) channels = size(out) for i = 1:channels dstImg(:,:,i) = out(i) end endfunction
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// File name: projects/04/divide/Divide.tst load Divide.asm, output-file DivideTest.out, compare-to DivideTest.cmp, output-list RAM[13]%D2.6.2 RAM[14]%D2.6.2 RAM[15]%D2.6.2 ; set PC 0, set RAM[13] 3000, // Set test arguments set RAM[14] 4, set RAM[15] 1, repeat 750 { ticktock; } output; set PC 0, set RAM[13] 16382, // Set test arguments set RAM[14] 2, set RAM[15] 1, repeat 1100 { ticktock; } output; set PC 0, set RAM[13] 32767, // Set test arguments set RAM[14] 3, set RAM[15] 1, repeat 1200 { ticktock; } output;
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clc// // // //Variable declaration e=1.602*10^-19; //charge of electron(c) epsilon0=8.85*10^-12; //permittivity(C/Nm) r=3*10^-10; //seperation(m) N=6.022*10^20; Ea=502; //ionisation energy of A(kJ/mol) Eb=-335; //electron affinity for B(kJ/mol) //Calculation E=-e^2*N/(4*%pi*epsilon0*r); //electrostatic attraction(kJ/mol) nE=Ea+Eb+E; //net change in energy per mole(kJ/mol) //Result printf("\n net change in energy per mole is %0.0f kJ/mol",nE) printf("\n answer varies due to rounding off errors") printf("\n since the net change in energy is negative, the A+B- molecule will be stable")
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//=========================================================================== //chapter 10 example 20 clc;clear all; //variable declaration V1 = 200; //voltage in V V2 = 126; //voltage in V t = 30; //time in seconds V12 = 200; //voltage in V V22 = 100; //voltage in V //calculations //let CR = a //V2 = V1*e^(t/C*R) a = t/log(V1/V2); //C*R //R1 = (10*R)/(10+R) a1 = t/log(V12/V22); //C*R1 //a1/a =R1/R=x x = a1/a; //since R1 = (10*R)/(10+R) //x*(10+R)*R = 10*R //(x*10)+R*x = 10 R = (10-(x*10))/x; //Resistance in Ω //result mprintf("resistance = %3.2f M Ω",R);
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clc clear //INPUT l=539;//latent heat of water at 100deg.C in cal j=4.2*10^7;//joules constant in ergs/cal t=373;//temperature of water in K v2=1670;//volume of steam formed in cc v1=1;//intial volume in cc g=981;//acceleration due to gravity in cm/sec^2 d=13.6;//specific gravity of hg //CALCULATIONS dp=l*j/(t*(v2-v1)*g*d);//rate of change of saturation pressure in cm of mercury //OUTPUT mprintf('the rate of change of saturation pressure is %3.2f cm of hg',dp)
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clc //Initialization of variables m=1 //lbm T=32+460 //R //calculations disp("From steam tables") hf=0 p=0.08854 //psi vf=0.01602 //ft^3 u = hf- p*vf*144/778.16 //results printf("Internal energy = %.7f Btu/lbm",u)
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function[] =imshow(Image) //retrieving list and creating 3 dimensional matrix out of it dimensions=size(Image) if dimensions==3 then [c d]=size(Image(1)); r=matrix(Image(1),c,d); g=matrix(Image(2),c,d); b=matrix(Image(3),c,d); z(:,:,1)=r; z(:,:,2)=g; z(:,:,3)=b; [NumberOfRows NumberOfColumns NumberOfChannels] = size(z); NumberOfPixels = NumberOfRows * NumberOfColumns; MaxGrayValue = 2 ^ 8 - 1; ColorMap = double(matrix(z, NumberOfPixels, NumberOfChannels)) ... / MaxGrayValue; Img = matrix(1 : NumberOfPixels, NumberOfRows, NumberOfColumns); elseif dimensions==1 then [d c]=size(Image(1)); Img=matrix(Image(1),c,d); MaxUInt8 = 2 ^ 8 - 1; MaximumGrayValue = MaxUInt8; ColorMap = graycolormap(double(MaximumGrayValue + 1)); end; show(Img,ColorMap); endfunction
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//wavelength in coaxial line //given clc V0=3D+8//m/s f=8D+9//hertz epsilon_r=2.25 lem=V0/((sqrt(epsilon_r))*f)//meter disp(lem,'the wave length for the operating frequency of 8GHz in meter:') //error in the form of miscalculation
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//appeler la fonction qui résout le problème modèle cellulaire exec('exo4_modele_cell.sci',-1) //la fonction qui initialise la grille avec des zéros function[res_e,res_r]=initialise_grille(n,e0,r0) res_e=zeros(n*n,1)+e0 res_r=zeros(n*n,1)+r0 endfunction //Afichage en matrice (Mij, j suit x, i suit y) function[M_e,M_r]=affiche_matrice(e,r,n) M_e = matrix(e,n,n) M_r = matrix(r,n,n) endfunction //la fonction principale qui initialise tout function main_initialise(T,t0,dt,e0,r0,n) //-- V_e0, V_r0 sont des vecteurs e0, r0 qui est initialisé [V_e,V_r]=initialise_grille(n,e0,r0) //-- M_e0, M_r0 sont des matrices i,j ; i suit x, j suit y [M_e0,M_r0]=affiche_matrice(V_e,V_r,n) //-- simuler e(t) & r(t) pour chaque cellule for i=1:1:(n*n) main_modele_cell(t0,dt,T,V_e(i,1),V_r(i,1),i) end endfunction //-- L'exemple --// //T=100 //T //t0=0 //Temps initial //dt=0.01 //Pas de temps //e0=1.0 //e initial //r0=0.0 //r initial //n=2 //nxn taille de grille //main_initialise(T,t0,dt,e0,r0,n)
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clc;clear; A= [0 0 1;0 1 1;1 1 1]; disp(A, "The given matrix A is:"); [m,n] = size(A); for k=1:n V(:,k) = A(:,k); for j=1:k-1 R(j,k) = V(:,j)'*A(:,k); V(:,k) = V(:,k)-R(j,k)*V(:,j); end R(k,k) = norm(V(:,k)); V(:,k) = V(:,k)/R(k,k); end disp(V,"Q: ");
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// Case Study:-Chapter 5, Page No:139 // 1.Range of numbers sum1=0; count=0; f=0;value=1; printf("Enter numbers[press enter after each number]:\n input a NEGATIVE number to end\n"); while(value) [value]=scanf("%f"); //Read data if(value<0) then break; end count=count+1; //Calculating height and lowest value if(count==1) then high=value; low=value; elseif(value>high) then high=value; elseif(value<low) then low=value; end //Calculate sum sum1=sum1+value; end average=sum1/count; //Average cost range1=high-low; //Range of values //Print the results printf("Total values: %d\n",count); printf("Highest-values: %f\nLowest-value: %f\n",high,low); printf("Range: %f\n Avarage: %f\n",range1,average);
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Expanding for base=6, level=3, reasons+features=base,same,similiar,evenexp norm Refined variables=x,y [0+1x,0+1y]: unknown -> [1] [0,0] x²-y³+4 ---------------- level 0 expanding queue[0]^-1,meter=[6,6]: x²-y³+4 [2+6x,2+6y]: unknown -> [1] [2,2] 2x+3x²-6y-18y²-18y³ -> solution [2,2],trivial(2) [4+6x,2+6y]: negative-1 [1] by {x=>-x-1} [1+6x,5+6y]: unknown -> [2] [1,5] 2x+6x²-75y-90y²-36y³-20 [5+6x,5+6y]: negative-1 [2] by {x=>-x-1} -> solution [11,5],NONTRIVIAL endexp[0] ---------------- level 1 expanding queue[1]^0,meter=[6,1]: 2x+3x²-6y-18y²-18y³ [2+36x,2+6y]: unknown -> [3] [0,0] 2x+18x²-y-3y²-3y³ -> solution [2,2],trivial(2) endexp[1] expanding queue[2]^0,meter=[6,6]: 2x+6x²-75y-90y²-36y³-20 [7+36x,5+36y]: unknown -> [4] [1,0] 14x+36x²-75y-540y²-1296y³-2 [25+36x,5+36y]: unknown -> [5] [4,0] 50x+36x²-75y-540y²-1296y³+14 [7+36x,17+36y]: unknown -> [6] [1,2] 14x+36x²-867y-1836y²-1296y³-135 [25+36x,17+36y]: unknown -> [7] [4,2] 50x+36x²-867y-1836y²-1296y³-119 [7+36x,29+36y]: unknown -> [8] [1,4] 14x+36x²-2523y-3132y²-1296y³-676 [25+36x,29+36y]: unknown -> [9] [4,4] 50x+36x²-2523y-3132y²-1296y³-660 endexp[2] ---------------- level 2 expanding queue[3]^1,meter=[6,6]: 2x+18x²-y-3y²-3y³ [2+216x,2+36y]: unknown -> [10] [0,0] 2x+108x²-y-18y²-108y³ -> solution [2,2],trivial(2) [110+216x,2+36y]: unknown -> [11] [3,0] 110x+108x²-y-18y²-108y³+28 [38+216x,14+36y]: unknown -> [12] [1,2] 38x+108x²-49y-126y²-108y³-3 [146+216x,14+36y]: unknown -> [13] [4,2] 146x+108x²-49y-126y²-108y³+43 [74+216x,26+36y]: unknown -> [14] [2,4] 74x+108x²-169y-234y²-108y³-28 [182+216x,26+36y]: unknown -> [15] [5,4] 182x+108x²-169y-234y²-108y³+36 endexp[3] expanding queue[4]^2,meter=[6,6]: 14x+36x²-75y-540y²-1296y³-2 [43+216x,5+216y]: unknown -> [16] [1,0] 86x+216x²-75y-3240y²-46656y³+8 [151+216x,5+216y]: unknown -> [17] [4,0] 302x+216x²-75y-3240y²-46656y³+105 [43+216x,77+216y]: unknown -> [18] [1,2] 86x+216x²-17787y-49896y²-46656y³-2105 [151+216x,77+216y]: unknown -> [19] [4,2] 302x+216x²-17787y-49896y²-46656y³-2008 [43+216x,149+216y]: unknown -> [20] [1,4] 86x+216x²-66603y-96552y²-46656y³-15306 [151+216x,149+216y]: unknown -> [21] [4,4] 302x+216x²-66603y-96552y²-46656y³-15209 endexp[4] expanding queue[5]^2,meter=[6,6]: 50x+36x²-75y-540y²-1296y³+14 [97+216x,5+216y]: unknown -> [22] [2,0] 194x+216x²-75y-3240y²-46656y³+43 [205+216x,5+216y]: unknown -> [23] [5,0] 410x+216x²-75y-3240y²-46656y³+194 [97+216x,77+216y]: unknown -> [24] [2,2] 194x+216x²-17787y-49896y²-46656y³-2070 [205+216x,77+216y]: unknown -> [25] [5,2] 410x+216x²-17787y-49896y²-46656y³-1919 [97+216x,149+216y]: unknown -> [26] [2,4] 194x+216x²-66603y-96552y²-46656y³-15271 [205+216x,149+216y]: unknown -> [27] [5,4] 410x+216x²-66603y-96552y²-46656y³-15120 endexp[5] expanding queue[6]^2,meter=[6,6]: 14x+36x²-867y-1836y²-1296y³-135 [7+216x,53+216y]: unknown -> [28] [0,1] 14x+216x²-8427y-34344y²-46656y³-689 [115+216x,53+216y]: unknown -> [29] [3,1] 230x+216x²-8427y-34344y²-46656y³-628 [7+216x,125+216y]: unknown -> [30] [0,3] 14x+216x²-46875y-81000y²-46656y³-9042 [115+216x,125+216y]: unknown -> [31] [3,3] 230x+216x²-46875y-81000y²-46656y³-8981 [7+216x,197+216y]: unknown -> [32] [0,5] 14x+216x²-116427y-127656y²-46656y³-35395 [115+216x,197+216y]: unknown -> [33] [3,5] 230x+216x²-116427y-127656y²-46656y³-35334 endexp[6] expanding queue[7]^2,meter=[6,6]: 50x+36x²-867y-1836y²-1296y³-119 [61+216x,53+216y]: unknown -> [34] [1,1] 122x+216x²-8427y-34344y²-46656y³-672 [169+216x,53+216y]: unknown -> [35] [4,1] 338x+216x²-8427y-34344y²-46656y³-557 [61+216x,125+216y]: unknown -> [36] [1,3] 122x+216x²-46875y-81000y²-46656y³-9025 [169+216x,125+216y]: unknown -> [37] [4,3] 338x+216x²-46875y-81000y²-46656y³-8910 [61+216x,197+216y]: unknown -> [38] [1,5] 122x+216x²-116427y-127656y²-46656y³-35378 [169+216x,197+216y]: unknown -> [39] [4,5] 338x+216x²-116427y-127656y²-46656y³-35263 endexp[7] expanding queue[8]^2,meter=[6,6]: 14x+36x²-2523y-3132y²-1296y³-676 [79+216x,29+216y]: unknown -> [40] [2,0] 158x+216x²-2523y-18792y²-46656y³-84 [187+216x,29+216y]: unknown -> [41] [5,0] 374x+216x²-2523y-18792y²-46656y³+49 [79+216x,101+216y]: unknown -> [42] [2,2] 158x+216x²-30603y-65448y²-46656y³-4741 [187+216x,101+216y]: unknown -> [43] [5,2] 374x+216x²-30603y-65448y²-46656y³-4608 [79+216x,173+216y]: unknown -> [44] [2,4] 158x+216x²-89787y-112104y²-46656y³-23942 [187+216x,173+216y]: unknown -> [45] [5,4] 374x+216x²-89787y-112104y²-46656y³-23809 endexp[8] expanding queue[9]^2,meter=[6,6]: 50x+36x²-2523y-3132y²-1296y³-660 [25+216x,29+216y]: unknown -> [46] [0,0] 50x+216x²-2523y-18792y²-46656y³-110 [133+216x,29+216y]: unknown -> [47] [3,0] 266x+216x²-2523y-18792y²-46656y³-31 [25+216x,101+216y]: unknown -> [48] [0,2] 50x+216x²-30603y-65448y²-46656y³-4767 [133+216x,101+216y]: unknown -> [49] [3,2] 266x+216x²-30603y-65448y²-46656y³-4688 [25+216x,173+216y]: unknown -> [50] [0,4] 50x+216x²-89787y-112104y²-46656y³-23968 [133+216x,173+216y]: unknown -> [51] [3,4] 266x+216x²-89787y-112104y²-46656y³-23889 endexp[9] ---------------- level 3 Maximum level 3 [52] mod 6: x²-y³+4
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function [phi]=pacf(x,n,min,max) // function pacf(x,n,[min,max]) // Partial Autocorrelation function for one-dimensional process // [lhs,rhs]=argn(0) if rhs <= 1 ; n=prod(size(x))/4;end if rhs <= 2 ; min=-1.0;end if rhs <= 3 ; max=1.0;end [cov,mean]=corr(x,n+1); ac=cov'/cov(1); xtitle('Partial Autocorrelation Function '); // Version recursive // phi[k] the k-th partial autocorrelation coefficient is defined // as the k-the element of psi which solves mat(1:k,1:k) psi = ac(2:k+1) // this can be done like this //mat=1/2*diag(ones(1,n)); //for k=1:n-1; mat=mat+ac(k+1)*diag(ones(1,n-k),k);end //mat=mat+mat'; //phi=[];for k=1:n;psi=mat(1:k,1:k)\ac(2:k+1); phi=[phi,psi(k)];end // but we can recursively computes the phi[k] more efficiently phi=0*ones(n,1) phi(1)=ac(2) psi=phi(1); for k=2:n;phi(k)=ac(k+1)- ac(k:-1:2)'*psi;psi=[psi;phi(k)];end plot2d3("onn",(1:n)',phi,[-1],"011"," ",[0,min,n,max]); stde=2*sqrt(1/prod(size(x))); plot2d( [0,0,0;n,n,n],[0,stde,-stde;0,stde,-stde],[-1,-2,-2],"000")
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function scs_m=do_tild(scs_m) // Copyright INRIA while %t [btn,xc,yc,win,Cmenu]=cosclick() if Cmenu<>[] then Cmenu=resume(Cmenu) end k=getblock(scs_m,[xc;yc]) if k<>[] then break,end end if get_connected(scs_m,k)<>[] then message('Connected block can''t be tilded') return end o=scs_m(k) drawobj(o) if pixmap then xset('wshow'),end geom=o(2);geom(3)=~geom(3);o(2)=geom; drawobj(o) scs_m_save=scs_m scs_m(k)=o [scs_m_save,enable_undo,edited]=resume(scs_m_save,%t,%t)
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//EX7.17 V_GS_on=3; V_GS=8.5; //DISPLAYED ON METER V_DS=V_GS; V_DD=15; R_D=4.7*10^3; I_D=(V_DD-V_DS)/R_D; disp(I_D,'Drain current in Amperes')
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//CHAPTER 8- DIRECT CURRENT MACHINES //Example 10 disp("CHAPTER 8"); disp("EXAMPLE 10"); //6 pole DC machine with 400 conductors //VARIABLE INITIALIZATION P=6; //number of poles I=80; //current per conductor in Amperes Z=400; //total number of conductors phi=0.020; //flux per pole in Wb N=1800; //in rpm //SOLUTION //soluion (a): for wave connected disp("(a) For Wave connected"); //(i) A=2; //A=number of parallel paths =2 for wave connected conductors I_a=I*A; disp(sprintf("(i) The total current is %.0f A",I_a)); //(ii) E_a=(phi*Z*N*P)/(60*A); disp(sprintf("(ii) The emf is %.0f V",E_a)); //(iii) p=E_a*I_a; disp(sprintf("(iii) The power developed in armature is %.3f kW",p/1000)); w=(2*%pi*N)/60; T_e=p/w; disp(sprintf("The electromagnetic torque is %.2f N-m",T_e)); //soluion (b): for lap connected disp("(b) For Lap connected"); //(i) A=P; //P=6 is given I_a=I*A; disp(sprintf("(i) The total current is %.0f A",I_a)); //(ii) E_a=(phi*Z*N*P)/(60*A); // induced emf disp(sprintf("(ii) The emf is %.0f V",E_a)); //(iii) p=E_a*I_a; //power developed in armature disp(sprintf("(iii) The power developed in armature is %.1f kW",p/1000)); w=(2*%pi*N)/60; //armature rotation in RPS T_e=p/w; //Torque disp(sprintf("The electromagnetic torque is %.2f N-m",T_e)); //END
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//Exa 4.13 clc; clear; close; //Given Data : format('v',5); d=300;//in cm(spacing) r=1;//in cm epsilon_o=8.854*10^-12;//constnt C=%pi*epsilon_o/log(d/r);//in Farad per meter disp(C*30*1000*10^6,"Capacitance for 30 km line(in uF) :");
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clear// //Variables VCC = 25.0 //Source voltage (in volts) RC = 820.0 //Collector Resistance (in ohm) RB = 180.0 //Base Resistance (in kilo-ohm) beta = 80.0 //Common-Emitter current gain //Calculation IB = VCC / RB //Base current (in milli-Ampere) IC = beta * IB //Collector current (in milli-Ampere) VCE = VCC - IC * RC * 10**-3 //Collector-to-Emitter voltage (in volts) //Result printf("\n The value of base current is %0.2f mA.\nThe value of Collector current is %0.2f mA.\nTHe value of Collector-to-Emitter voltage is %0.2f V.",IB,IC,VCE)
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clear; clc; //Example2.18[Variation of Temperature in a Resistance Heater] //Given:- k=13.55;//[W/m.degree Celcius] ro=0.005;//[m] e_gen=4.3*10^7;//rate of resistance heating[W/m^3] Ts=108;//Surface temperature[degree Celcius] //Solution:- //Integrating we get //T(r)=Ts+((e_gen*(ro^2-r^2)/4k)) T_0=Ts+((e_gen*ro^2)/(4*k)); disp("degree Celcius",round(T_0),"The temperature at the centreline,r=0 is")
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clc // At 10 bar: From steam table for superheated steam h_sup=3051.2; //kJ/kg T_sup=573; //K T_s=452.9; //K v_g=0.194; //m^3/kg v_sup=v_g*T_sup/T_s; p=10; //bar u1=h_sup-p*v_sup*10^2; //kJ/kg disp("Internal energy of superheated steam at 10 bar= ") disp(u1) disp("kJ/kg") // At 1.4 bar: From steam tables p=1.4; //bar h_f=458.4; //kJ/kg h_fg=2231.9; //kJ/kg v_g=1.236; //m^3/kg x=0.8; h=h_f+x*h_fg; u2=h-p*x*v_g*10^2; //kJ du=u2-u1; disp("Change in internal energy=") disp(du) disp("kJ")
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clc;clear; //Example 13.5 //given data T1=220; T2=160; Pm=10; yN=0.79; yO=0.21;//mole fractions of nitrogen and oxygen repesctively //critical properties //for Nitrogen TcrN=126.2; PcrN=3.39; //for Oxygen TcrO=154.8; PcrO=5.08; //constants used Ru=8.314;//in kJ/kg - K //from Tables A-18 & 19 //at T1 h1N=6391; h1O=6404; //for T2 h2N=4648; h2O=4657; //calculations //part - a qouti=yN*(h1N-h2N)+yO*(h1O-h2O); qouti=ceil(qouti); disp(qouti,'the heat transfer during this process using the ideal-gas approximation in kJ/kmol'); //part - b Tcrm=yN*TcrN+yO*TcrO; Pcrm=yN*PcrN+yO*PcrO; Tr1=T1/Tcrm; Tr2=T2/Tcrm; Pr=Pm/Pcrm; //at these values we get Zh1=1; Zh2=2.6; qout=qouti-Ru*Tcrm*(Zh1-Zh2); qout=ceil(qout); disp(qout,'the heat transfer during this process using Kay’s rule in kJ/kmol'); //part - c //for nitrogen TrN1=T1/TcrN; TrN2=T2/TcrN; PrN=Pm/PcrN; //from Fig A-15b Zh1n=0.9; Zh2n=2.4; //for Oxygen TrO1=T1/TcrO; TrO2=T2/TcrO; PcrO=Pm/PcrO; //from Fig A-15b Zh1O=1.3; Zh2O=4.0; //from Eq 12-58 h12N=h1N-h2N-Ru*TcrN*(Zh1n-Zh2n);// h1 - h2 for nitrogen h12O=h1O-h2O-Ru*TcrO*(Zh1O-Zh2O);// h1 - h2 for oxygen qout=yN*h12N+yO*h12O; qout=ceil(qout); disp(qout,'the heat transfer during this process using Amagat’s law in kJ/kmol');
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clc; T2=10+273;//K T1=2000+273;//K eta=1-T2/T1; disp("highest possible efficiency is:"); disp("%",eta*100)
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clc; //Example 14.4 //page no 154 printf("Example 14.4 page no 154\n\n"); //for turbulent fluid flow in across section //(a) for a rectangle w=2//width of a rectangle,in h=10//height of rectangle,in S_a=h*w//cross sectional area P_a=2*h+2*w//perimeter of rectangle D_eq_a=4*S_a/P_a//equivalent diameter printf("\n equivalent diameter D_eq_a=%f in",D_eq_a); //(b) for an annulus d_o=10//outer diameter of annulus d_i=8//inner diameter S_b=%pi*(d_o^2-d_i^2)/4//cross sectional area P_b=%pi*(d_o-d_i)//perimeter D_eq_b=(4*S_b)/(P_b)//eq. diameter printf("\n equivalent diameter D_eq_b=%f cm",D_eq_b); //(c) for an half- full circle d_c=10//diameter of circle S_c=%pi*d_c^2/8// cross sectional area P_c=%pi*d_c/2//perimeter D_eq_c=4*S_c/P_c//eq. diameter printf("\n equivalent diameter D_eq_c=%f cm",D_eq_c);
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//Engineering and Chemical Thermodynamics //Example 9.14 //Page no :466 clear ; clc ; //Given E_0_c = 0.34 ; //[V] E_0_a = -1.23 ; //[V] T = 298 ; // [K] pH = 1 ; z = 2 ; Cu2 = 0.07 ; F = 96485 ; //[C/mol e-] R = 8.314 ; E_0_rxn = E_0_c + E_0_a ; E = E_0_rxn + 2.303 * R * T * 2 * pH / (z * F) + R * T * log(Cu2) / (z * F) ; disp(" Example: 9.14 Page no : 466") ; printf("\n Del_E_0_rxn = %.2f ",E_0_rxn ) ; printf("\n\n We have to apply potential greater than %.2f V",-E) ;
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// Updated(19-7-07) // 13.10 // MacGregor's first control problem A = [1 -1.4 0.45]; dA = 2; C = [1 -0.5]; dC = 1; B = 0.5*[1 -0.9]; dB = 1; k = 1; int1 = 0; u_gmv = []; y_gmv = []; uy_gmv = []; getf gmv.sci; for rho = 0:0.1:10, [S,dS,R,dR] = gmv(A,dA,B,dB,C,dC,k,rho,int1); [Nu,dNu,Du,dDu,Ny,dNy,Dy,dDy,yvar,uvar] = ... cl(A,dA,B,dB,C,dC,k,S,dS,R,dR,int1); u_gmv = [u_gmv uvar]; y_gmv = [y_gmv yvar]; uy_gmv = [uy_gmv; [rho uvar yvar]]; end plot(u_gmv,y_gmv,'b')
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a=input("Please Enter lower Limit"); b=input("Please Enter Upper Limit"); accuracy=input("Please Enter Accuracy"); accuracytemp=b-a; iteration=0; x=a:0.01:b; y=f(x); plot(x,y); while accuracytemp>accuracy iteration=iteration+1; c=(a+b)/2; f1=(a^3)-(a)-2; f2=(b^3)-(b)-2; f3=(c^3)-(c)-2; disp("Itr.no.:"+string(iteration)+"||"+"a ="+ string(a)+"||"+"b ="+string(b)+"||"+"c ="+ string(c)+"||"+"f(c) ="+ string(f3)); plot(c,0,'rx','MarkerSize',10) if f1*f3<0 then b=c; end if f1*f3>0 then a=c; end if (b-a)<0 then accuracytemp=(a-b); end if (b-a)>0 then accuracytemp=(b-a); end end
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//example 4 //determining quality of steam clear clc hi=2850.1 //initial specific heat enthalpy for steam in kJ/kg Vi=50 //initial velocity of steam in m/s Ve=600 //final velocity of steam in m/s he=hi+Vi^2/(2*1000)-Ve^2/(2*1000) //final specific heat enthalpy for steam in kJ/kg hf=467.1 //at final state in kJ/kg hfg=2226.5 //at final state in kJ/kg xe=(he-hf)/hfg //quality of steam in final state printf(" \n hence, the quality is xe=%.3f. \n",xe)
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// example:-6.6,page no.-307. // program to evaluate the worst case percent error in computing magnitude of reflection coefficient. Z1=100;Z2=150;Zl=225; tao_1=(Z2-Z1)/(Z2+Z1); tao_2=(Zl-Z2)/(Zl+Z2); tao_exact=(tao_1+tao_2)/(1+tao_1*tao_2); // this results as angle is taken zero. tao_approx=tao_1+tao_2; // this results as angle is taken zero. eror=abs(((tao_exact-tao_approx)/tao_exact)*100); disp(tao_approx,'approximate value of reflection coefficient is = ') disp(eror,'the error in percent is about = ')
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example14_7pp.sce
clc clear disp('example 14.7') p=100 //MVA of generated f=50 //frequency rpm=3000 //no load rpm lad=25 //load applied to the machiene t=0.5 //time delay h=4.5 //inertia constent ke=h*p //kinetic energy is product of h*p lke=lad*t //loss of ke nf=(((ke-lke)/ke)^t)*f //new frequency ((1-lke/ke)^t)*f fd=(1-(nf/f))*100 //frequency deviation printf("ke at no load %dMW-sec \n loss in k.e due to load %.1fMW-sec \nnew frequency %.1fHz \nfrequency deviation %.1fpercent",ke,lke,nf,fd)
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Ex27_5.sce
//Example 27.5 lambda=550*10^-9;//Wavelength (m) D=2.40;//Diameter (m) theta=1.22*lambda/D;//Smallest angle between two point sources to be just-resolved (rad) printf('a.Angle between the two just-resolved point light sources = %0.2e rad',theta) r=2*10^6;//Distance from the Hubble Space Telescope (ly) s=r*theta;//Distance between the objects (ly) printf('\nb.Closest distance between the objects = %0.2f ly',s) //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest
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// Scilab code Ex2.8: Pg.84 (2008) clc; clear; B_E = 13.6; // Binding energy of H-atom, eV // Since 1 atomic unit, u = 931.5 MeV/c^2, therefore we get u = 931.5e+06; // Mass, eV/c^2 m_l = B_E/u; // Mass lost during formation of Hydrogen atom, u printf("\nThe mass lost during the formation of hydrogen atom = %4.2e u", m_l); // Result // The mass lost during the formation of hydrogen atom = 1.46e-008 u
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example1_1.sce
errcatch(-1,"stop");mode(2);//example 1.1 //page 8 ; funcprot(0); //initialization of variable P=50*144*47.88;//pressure R=8323/29; T=273+20;//temperature rho=P/R/T; disp(rho,"density (kg/m^3)="); exit();
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Example18.sce
clear mode(-1) pwd curr=ans clc printf("Example 18 : Show the method of declaration of subroutines') disp("****************************************************************") disp("Answer : ") disp("INSTRUCTIONS : ") printf("\n1. Here all instructions are preloaded in the form of a demo\n\nInitially the whole perl script is displaying and then \n the result of the same can be seen in the command line interpreter.\n\n2. PLEASE MAKE SURE THAT THE PERLSCRIPT INTERPRETER\nEXISTS IN THE SYSTEM\nOR THE COMMAND WOULD NOT WORK \n\n3. PRESS ENTER AFTER EACH COMMAND to see its RESULT\n\n5. PRESS ENTER AFTER EACH RESULT TO GO TO THE NEXT COMMAND\n") halt('.............Press [ENTER] to continue.....') halt("") clc printf("\tUNIX SHELL SIMULATOR(DEMO VERSION WITH PRELOADED COMMANDS)\n\n\n") printf("\n# Enter the name of the perlscript file whichever you desire \n\n") nam=input('$ cat ','s') halt(' ') clc li(1)='#!/usr/bin/perl ' li(2)='system('+ascii(34)+'cls'+ascii(34)+') ;# Script: '+nam+'.pl - Shows the use of Subroutines ' li(3)="#" li(4)=' system('+ascii(34)+'cls'+ascii(34)+'); #clears the screen' li(5)='$username = &take_input('+ascii(34)+'Oracle user-id: '+ascii(34)+') ;' li(6)='$password = &take_input('+ascii(34)+'Oracle password: '+ascii(34)+', '+ascii(34)+'noecho'+ascii(34)+') ;' li(7)='print '+ascii(34)+'\nThe username and password are $username and $password\n'+ascii(34)+' ;' li(8)=' ' li(9)='sub take_input { ' li(10)=' my ($prompt,$flag) = @_ ; # @_stores arguments of subroutines ' li(11)=' while (1) { # (1) means always true ' li(12)=' print('+ascii(34)+'$prompt'+ascii(34)+') ;' li(13)=' use Term::ReadKey;' li(14)=' ReadMode 2 if (@_==2); #turn ehoing off' li(15)=' chop($name=<STDIN>); ' li(16)=' ReadMode 0 if (@_==2); #turn echoing on back' li(17)=' last if $name =~ /\w/ ; #Quit if $name has atleast one word character' li(18)=' }' li(19)=' $name ; #return $name will also do' li(20)=' }' li(21)='print('+ascii(34)+'\n\nType'+ascii(39)+'exit'+ascii(39)+'to go back to console\n\n'+ascii(34)+')' halt(' ') v=mopen(nam+'.pl','wt') for i=1:20 mfprintf(v,"%s\n",li(i)) if i==13 then printf('\t system(%c stty -echo%c) if (@_==2) ; #Echo off\n',ascii(34),ascii(34)) end if i==16 then printf('\t system(%c stty echo%c) if (@_==2) ; #Echo on\n',ascii(34),ascii(34)) end if i~=20&i~=14&i~=13&i~=16 then printf("%s\n",li(i)) end end mclose(v) if getos()=='Linux' then printf("\n\nPlease open a new terminal window and then go to the directory %s and execute the following instruction\n\nperl %s.pl [Command line parameters if any]\n\nThank You \n\n",curr,nam) halt(' ') exit end printf("\n# type the following command in the command line interpreter as soon as it appears") printf(" \n %c %s.pl %c[ENTER]\n\n",ascii(34),nam,ascii(34)) printf("\n$ %s.pl #to execute the perlscript",nam) halt(' ') dos('start') printf("\n\n\n") halt(' ---------------->Executing PerlScript in Command Line Prompt<-------------- ') printf("\n\n\n$ exit #To exit the current simulation terminal and return to Scilab console\n\n") halt("........# (hit [ENTER] for result)") //clc() printf("\n\n\t\t\tBACK TO SCILAB CONSOLE...\nLoading initial environment') sleep(1000) mdelete(nam+'.pl')
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ex13_3.sce
clc; clear all; de = 9.6e2 ; // Density of sodium in Kg per cubic meter At = 23; // Atomic weight of sodium n = 2;// Number of atoms present in a unit cell av = 6.022e26; // Avagadro constant mass = (n*At)/av; v = (mass/de)^(1/3); // Volume of a unit cell disp('m',v,'The lattice constant osf sodium is')
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jac_flowsheet_residuals.sci
function [At, varargout] = jac_flowsheet_residuals(x, xfull, K_coef, cp1_coef, h_hx_coef, frac ) //****************************************************************************** // Data Reconciliation Benchmark Problems From Literature Review // Author: Edson Cordeiro do Valle // Contact - edsoncv@{gmail.com}{vrtech.com.br} // Skype: edson.cv //****************************************************************************** // Builds a Jacobian matrix of a heat exchanger network problem proposed by Swartz, 1989, // considering the measured and unmeasured flows and temperatures entered by user. // This function is prepared to use the automatic derivatives toolbox of // Scilab. This toolbox can be instaled using the ATOMS installer (package name: diffcode). // The objective of this jacobian is to use it further in variable classification routines // Do not use it for optimization purposes, since it make some costly computational operations // Outputs: // At: The full Jacobian of the system (as if all variables were measured). // Ax: The Jacobian of the system of the measured part. // Au: Jacobian of the system (as if all variables were measured). // varargout(1): unmeasured streams (identified by -1). // varargout(2): fixed streams (identified by -5). // Inputs // // x_full: The measurements. It is a row vector with // the values measured. In the case where a variable is unmeasured, an estimate must be given, eg: // [ 300 200 100] (variable 3 is unmeasured, but ans estimate is given ) // flow: The variable with unmeasured information. It is a row vector with // either the values measured, -1 if the variable is not measured or -5 if the variable is fixed // (fixed variables arrise, for exemple, if we have a flow controler in the process) // It is a matrix with the form: // [ 300 -5 -1] // means variable 1 = 3000 ; variable 2 is fixed and variable 3 unmeasured // the fixed value information comes from x_full input // // K_coef coeficient for calculation of partition coeficient K in the flash // Ki = yi/xi. Since it is not constant, it was adjusted from simulation data // in a range for temperature from -24:-44 oC //cp1_coef coeficient for calculation of Cp in Heat exchanger 1 considering the mixture an ideal gas //h_hx_coef coeficient for calculation of h in the output of the reactor and in the output of second heat // exchanger. It was also adjusted from simulation data //frac split fraction in the splitter //****************************************************************************** A = diffcode_jacobian(list(flowsheet_residuals,K_coef, cp1_coef, h_hx_coef, frac),xfull) //pause At=A'; varargout = list(find(x == -1), find(x == -5)); endfunction
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Ex7_2.sce
clear // // //Initilization of Variables d=25 //mm //Diameter of circular bar F=20*10**3 //N //Axial Force theta=30 //Degree //angle //Calculations //Axial stresses p=F*(%pi*4**-1*d**2)**-1 //N/mm**2 //Normal Stress p_n=p*(cos(30*%pi*180**-1))**2 //Tangential Stress p_t=p*2**-1*sin(2*theta*%pi*180**-1) //Max shear stress occurs on plane where theta2=45 theta2=45 sigma_max=p*2**-1*sin(2*theta2*%pi*180**-1) //Result printf("\n Stresses developed on a plane making 30 degree is: %0.2f N/mm**2",p_n) printf("\n : %0.2f N/mm**2",p_t) printf("\n stress on max shear stress is %0.2f N/mm**2",sigma_max)
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map411 q3,5,6 simulation.sce
//Question 3, 5, et 6 clear; //espace J = 50 ; dx = 1.0/J ; xx = linspace(dx,1,J) ; //pour la graphe //temps T = 1 ; dt = 0.0001; Niter = T/dt ; //La Distribution Initiale // Si on utilise les deux distributions suivants, ne trace pas // la solution exacte et les erreurs (lignes 79-96) //uu0 = ones(1,J).*rand(1,J);//une distribution random //uu0 = ones(1,J); //une distribution uniforme uu0 = (1-cos(2*%pi*xx)) //la distribution initiale de question 4 uu = uu0 ; // Les coefficients alpha = 1; //coefficient de destruction D = 1; //coefficient de diffusion V = 1; //coefficient d'advection disp ("alpha = "); disp (alpha); disp ("D = "); disp (D); disp ("V = "); disp (V); //Les Probabilités pdest = alpha*dt; //de destruction pminus = D*dt/dx/dx; //d'aller à j-1 pplus = V*dt/dx+pminus; //d'aller à j+1 prest = 1-pdest-pplus-pminus; //de rester à j disp ("P(destruction) = "); disp (pdest); disp ("P(j-1) = "); disp (pminus); disp ("P(j+1) = "); disp (pplus); disp ("P(j) = "); disp (prest); if (prest>=0) then //Si la condition CFL est satisfait //Shifters iiL = [2:J 1] ; iiR = [J 1:J-1] ; //chaque pas du temps for n = 1:Niter; uu = prest*uu + pplus*uu(iiR)+pminus*uu(iiL); // Question 4 et 5 : La solution explicite // n*dt=t est un pas du temps sol = (1-cos(2*%pi*(V*n*dt-xx))*exp(-4*%pi^2*D*n*dt))*exp(-alpha*n*dt); erreur=sol-uu; differencelinf(1,n) = norm(erreur,'inf'); differencel2(1,n)=norm(erreur,2); //Question 6: decommenter pour les conditions aux bords //Ensuite, mets en commentaire la solution explicite, //l'erreur et les lignes 79-96 //uu(1,1) = 0; //uu(J) = uu(J-1); //On trace la graphe pour chaque 10eme pas if (modulo(n,10)==0) drawlater() ; clf ; subplot(2,2,1); plot2d(xx,uu,rect=[0,0,1,2]) ; xtitle( 'Simulation', 'Espace', 'Probabilité Densité' ) ; subplot(2,2,2); plot2d(xx,sol,rect=[0,0,1,2],style=5); xtitle( 'Solution', 'Espace', 'Probabilité Densité' ) ; //Trace d'erreur : // En bleu : l'erreur absolu, // En vert: maximum atteint pour la norme subplot(2,2,3); plot2d(xx,erreur,rect=[0,0,1,0.004],style=2); plot2d(xx,ones(1,J)*max(differencelinf),rect=[0,0,1,0.002],style=3); h1=legend(['Erreur Absolu', 'Max(Linf norme)'],1); xtitle( 'Erreur avec Linf borne', 'Espace', 'Probabilité Densité' ) ; subplot(2,2,4); plot2d(xx,erreur,rect=[0,0,1,0.02],style=2); plot2d(xx,ones(1,J)*max(differencel2),rect=[0,0,1,0.01],style=3); h1=legend(['Erreur Absolu', 'Max(L2 norme)'],1); xtitle( 'Erreur avec L2 borne', 'Espace', 'Probabilité Densité' ) ; drawnow(); end end disp ("Max Linf Erreur: ") disp(max(differencelinf)); disp ("Max L2 Erreur: ") disp(max(differencel2)); else disp("Erreur : P(j)<0, condition CFL pas satisfait!") end
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Ex9_2_7.sce
// Scilab Code Ex9.2.7: Page-416 (2008) clc; clear; h = 6.63e-034; // Planck's constant, Js m = 9.11e-031; // Rest mass of an electron, kg c = 3e+008; // Speed of light in vacuum, m/s bita = 3/5; // Boost parameter v = 3/5*c; // Spped of the electron, m/s lambda = h/(m*v)*sqrt(1-bita^2); // de Broglie wavelength of the electron, m printf("\nThe de-Broglie wavelength of the moving electron = %6.4f angstrom", lambda/1e-010); // Result // The de-Broglie wavelength of the moving electron = 0.0323 angstrom
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Ex4_4.sce
// Theory and Problems of Thermodynamics // Chapter 4 // Energy Analysis of Process // Example 4 clear ;clc; //Given data m = 0.1 // mass wet steam in kg X1 = 0.8 // wet steam quality P1 = 0.3 // Pressure in MPa d = 0.8 // distance upto presence of latches in m A = 0.1 // Cross sectionla area of cylinder P1 = P1 * 1e3 // units conversion from MPa to kPa // at 0.3 MPa v_f = 0.001073 // Specific volume of vapor in m^3/kg v_g = 0.6058 // Specific volume of vapor in m^3/kg h_f = 516.47 // Specific enthalpy of vapor in kJ/kg h_fg = 2163.8 // Specific enthalpy of vapor in kJ/kg // Calculations v1 = X1*v_g + (1-X1)*v_f // Specific volume of vapor in m^3/kg V1 = v1* m // Initial Volume of steam in m^3 h1 = h_f + X1*h_fg // specific enthalpy at at 0.3MPa H1 = h1*m // Initial Enthalpy of steam in kJ // State of stem when piston touches the latches P2 = P1 // Pressure of steam when piston touches latch V2 = d*A // Volume of steam when piston touches latch v2 = V2/m // specific volume when piston touches latch W12 = P1*(V2 - V1) // Work done during constant pressure process // From superheated steam tables at P = 0.3 MPa and v3 = 0.8 m^3/kg T2 = 252.3 // Temperature in C h2 = 2972.28 // specific enthalpy obtained from interpolation H2 = h2*m // Enthalpy in kJ // Energy transfer during constant pressure process Q12 = H2 - H1 // Energy transferred in kJ // Constant Volume heating from P2 = 0.3 MPa to P3 = 0.5 MPa P3 = 0.5 // Final Pressure in MPa P3 = P3 * 1e3 // Units conversion from MPa to kPa v3 = v2 // From superheated steam tables at P = 0.3 MPa and v3 = 0.8 m^3/kg T3 = 595.6 // Temperature in C h3 = 3692.1 // specific enthalpy obtained from interpolation W23 = 0; Q23 = m*(h3-h2-v2*(P3-P2)) W = W12 + W23 Q = Q12 + Q23 // Output Results mprintf('Work done by the steam = %6.3f kJ',W) mprintf('\n Energy transferred = %6.2f kJ',Q) mprintf('\n Final Temperature of Steam = %6.1f `C',T3)
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// Exa 3.3 clc; clear; // Given NF = 30; // Noise figure in dB BW = 1; // Bandwidth of 3 dB filter in kHz // Solution printf(' The noise level of the spectrum analyser is related to the noise figure and the IF bandwidth by the following equation - \n MDS = -114 dbm + 10*log(BW/1MHz) + NF \n so, by calculation :- '); MDS = -114 + 10*log10(BW*10^3/10^6)+NF; printf(' MDS = %d dBm \n ' , MDS); // The answer provided in the textbook is wrong
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//Basic Circuit Concepts //pg no.-1.20 //example 1.15 r1=3; r2=2.33; r3=6; v1=18; v2=5.985; mprintf("\nApplying KCL at the node, \n(Va-18)/3+(Va-5.985)/2.33+Va/6 = 0"); Va=((v1*r2*r3)+(v2*r1*r3))/((r2*r3)+(r1*r3)+(r1*r2)); printf("\nSolving the equation,we get, \nVa = %.2f V",Va);
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//Book Name:Fundamentals of Electrical Engineering //Author:Rajendra Prasad //Publisher: PHI Learning Private Limited //Edition:Third ,2014 //Ex1_2.sce. clc; clear; R25=120; //resistance of copper wire at 25 degree celsius T1=25; //temperature1 in degree celsius T2=55; //temperature in degree celsius alphazero=4.2e-3; //temperature coefficient R55=(R25*(1+(T2*alphazero)))/(1+(T1*alphazero)); //resistance of the copper wire at a temperature of 55 degree celsius printf("The resistance value for the resitor(copper wire)=%3.3f ohms",R55)
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clear; clc; printf("\t\t\tExample Number 4.5\n\n\n"); // sudden exposure of semi-infinite solid slab to convection // illustration4.5 // solution alpha = 8.4*10^(-5);// [square meter/s] constant Ts = 200;// [degree celsius] initial temperature of of slab Te = 70;// [degree celsius] environment temperature k = 215;// [W/m degree celsius] heat transfer coefficient of slab h = 525;// [W/square meter degree celsius] heat transfer coefficient x = 0.04;// [m] depth at which temperature is calculated T_x_t = 120;// [degree celsius] temperature at depth 0.04 m // we can use equation (4-15) or figure (4-5) for solution of this problem // by using figure it is easier to calculate it involves iterative method to solve because time appeares in both the variables // h*sqrt(alpha*t)/k and x/(2*sqrt(alpha*t)) K = (T_x_t-Ts)/(Te-Ts); // we seek the values of t such that the above value of K is equal to the value of K which comes out from graph // we therfore try values of t and obtain other readings printf("The iteration are listed below\n"); // at t = 1000s t = 1000;// [s] time A = h*sqrt(alpha*t)/k; B = x/(2*sqrt(alpha*t)); printf(" t\t\th*sqrt(alpha*t)/k \t x/(2*sqrt(alpha*t)) \t (T_x_t-Ts)/(Te-Ts)"); printf("\n %f\t\t %f \t %f \t\t 0.41",t,A,B); t = 3000;// [s] time A = h*sqrt(alpha*t)/k; B = x/(2*sqrt(alpha*t)); printf("\n %f\t\t %f \t %f \t\t 0.61",t,A,B); t = 4000;// [s] time A = h*sqrt(alpha*t)/k; B = x/(2*sqrt(alpha*t)); printf("\n %f\t\t %f \t %f \t\t 0.68",t,A,B); printf("\n consequently the time required is approximately 3000 second");
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// Scilab Code Ex3c.2: Page-184 (2008) clc; clear; I2 = 1; // Assume intensity of light beam from the second source to be unity I1 = 81*I2; // Intensity of light beam from the first source a = sqrt(I1); // Width of the first slit, mm b = sqrt(I2); // Width of the second slit, mm I_max = (1+a/b)^2; // Maximum intensity in the fringe pattern I_min = (1-a/b)^2; // Minimum intensity in the fringe pattern fact = gcd([I_max,I_min]); // Find l.c.m. of I_max and I_min printf("\nThe ratio of maximum to minimum intensity in the fringe system, I_max:I_min = %d:%d", I_max/4, I_min/4); // Result // The ratio of maximum to minimum intensity in the fringe system, I_max:I_min = 25:16
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// https://www.wolframalpha.com/input/?i=x%5E2%3D16 clf // to clear the plot area // x^2 = 16 // prepare data for the plot x=linspace(-10,10) y=x^2 // plot the function (red line) plot(x,y,'r') // plot a point (marker) at x1,y1 // plot(x1, y1, 'o') plot(-4,16, 'ro') plot(4,16, 'ro') // draw line from x1,y1 to x2,y2 // plot([x1,x2], [y1,y2]) plot([-10,10], [16,16], 'b')
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clear ; clc; // Example 13.7 printf('Example 13.7\n\n'); //Page no. 416 // Solution fig E13.7 G = 100 ;// Basis: Pyrolysis Gas-[lb mol] ub_CO = 10/100 ;// fraction of CO left unburnt ex_air = 40/100 ;;// fraction of excess air m_vol = 359 ;// molar volume of gas at std. cond.-[cubic feet] Ts = 492 ;// Standard temperature -[degree Rankine] Ps = 29.92 ;//Standard pressure -[in. Hg] // Analysis of entering gas of entering gas Tf1 = 90 ;// Temperature of gas-[degree F] T_gas = Tf1 + 460 ;//Temperature of gas-[degree Rankine] P_gas = 35 ;//Pressure-[in. Hg] CO2 = 6.4/100 ;// mol fraction of CO2 O2 = 0.1/100 ;// mol fraction of O2 CO = 39/100 ;// mol fraction of CO H2 = 51.8/100 ;// mol fraction of H2 CH4 = 0.6/100 ;// mol fraction of CH4 N2 = 2.1/100 ;// mol fraction of N2 // Analysis of entering air Tf2 = 70 ;// Temperature of air -[degree F] T_air = Tf2 + 460 ;//Temperature of air-[degree Rankine] P_air = 29.4 ;//Pressure of air [in. Hg] f_N2 = 79/100 ;// mol fraction of N2 f_O2 = 21/100 ;// mol fraction of O2 // Get O2 required for combustion of CO,H2 & CH4 according to the following equation // CO + 1/2O2-->CO2 //H2 + 1/2O2-->H20 //CH4 + 2O2--> CO2 + 2H2O O2r_O2 = O2 * G ;// O2 required by O2-[lb mol] O2r_CO = CO * G/2 ;// O2 required by CO-[lb mol] O2r_H2 = H2 * G/2 ;// O2 required by H2-[lb mol] O2r_CH4 = G * CH4 * 2 ;// O2 required by CH4-[lb mol] O2r_total = O2r_O2 + O2r_CO + O2r_H2 + O2r_CH4 ;// Total O2 required-[lb mol] ex_O2 = ex_air * O2r_total ;// Excess O2-[lb mol] total_O2 = ex_O2 + O2r_total ;// Total amt of O2 in air-[lb mol] total_N2 = total_O2 * (f_N2/f_O2);// Total amt of in air-[lb mol] air = total_O2 + total_N2 ;// Total air entering -[lb mol] // Product analysis P_CO = ub_CO * CO * G ;//Unburnt CO in P-[lb mol] //Element balance of 2N P_N2 = N2 * G + total_N2 ;// N2 in P-[lb mol] //Element balance of C P_CO2 = (CO2 + CO + CH4) * G - 1 * P_CO;//CO2 in P-[lb mol] // Element balance of 2H P_H2O = (H2 + 2 * CH4) * G ;// H2 in P-[lb mol] // Element balance of 2O P_O2 = (CO2 + O2 + 0.5 * CO) * G + total_O2 -P_CO2-0.5 * (P_H2O + P_CO);// O2 in P-[lb mol] P = P_CO + P_N2 + P_CO2 + P_H2O + P_O2 ;// Product-[lb mol] Tf3 = 400 ;// Temperature of product-[degree F] T_prod = Tf3 + 460 ;//Temperature of product-[degree Rankine] P_prod = 35 ;// Pressure of product -[in.Hg] V_gas = (G * m_vol * T_gas * Ps)/(Ts * P_gas); V_air = (air * m_vol * T_air * Ps)/(Ts * P_air); V_prod = (P * m_vol * T_prod * Ps)/(Ts * P_prod); air_ft3 = V_air/V_gas ;//Air supplied per ft^3 of gas entered-[cubic feet] P_ft3 = V_prod/V_gas ;//Product gas produced per ft^3 of gas entered-[cubic feet] printf(' Air supplied per ft^3 of gas entered %.2f cubic feet.\n ',air_ft3); printf(' Product gas produced per ft^3 of gas entered %.2f cubic feet.\n',P_ft3);
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// Updated(19-7-07) // 12.6 function [K,KH1,KH2,Tc,dTc,Sc,dSc,R1,dR1] = ... gpc_col(A,dA,B,dB,C,dC,N,k,rho) D=[1 -1]; dD = 0; AD=convol(A,D); dAD=dA+1; zj=1; dzj=0; Nu = N+1; G=zeros(Nu,Nu); H1=zeros(Nu,2*k+N-2+dB); H2 = zeros(Nu,k+N+dA); for j = 1:Nu, zj = convol(zj,[0,1]); dzj = dzj + 1; [Fj,dFj,Ej,dEj] = ... xdync(zj,dzj,AD,dAD,C,dC); [Nj,dNj,Mj,dMj] = ... xdync(zj,dzj,C,dC,1,0); [Gj,dGj] = polmul(Mj,dMj,Ej,dEj); [Gj,dGj] = polmul(Gj,dGj,B,dB); [Pj,dPj] = polmul(Mj,dMj,Fj,dFj); [Pj,dPj] = poladd(Nj,dNj,Pj,dPj); j,Fj,Ej,Mj,Nj,Gj,Pj G(j,1:j) = flip(Gj(1:j)); H1(j,1:dGj-j+1) = Gj(j+1:dGj+1); H2(j,1:dPj+1) = Pj; end K = inv(G'*G+rho*eye(Nu,Nu))*G' // Note: inverse need not be calculated KH1 = K * H1; KH2 = K * H2; R1 = [1 KH1(1,:)]; dR1 = length(R1)-1; Sc = KH2(1,:); dSc = length(Sc)-1; Tc = K(1,:); dTc = length(Tc)-1; endfunction;
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layout 0:30x20+0+5 \ 1:30x20+30+5 \ 3:15x25+60+0 =comment +3------------+ | | | | | | | | +0---------------------------++1---------------------------+| | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | | || || | +----------------------------++----------------------------++-------------+ =end check_horizontal_layout 75x20+0+5 15x5+60+0 check_vertical_layout 15x25+60+0 60x20+0+5 # # window in monitor 0 window 20x10+5+10 RLayoutFindTopBottomEdges 5 24 RLayoutFindLeftRightEdges 0 74 RLayoutFindMonitorBottomEdge 24 RLayoutFindMonitorTopEdge 5 RLayoutFindMonitorLeftEdge 0 RLayoutFindMonitorRightEdge 29 RLayoutFull 75x20+0+5 RLayoutFullHoriz 75x10+0+10 RLayoutFullVert 20x20+5+5 RLayoutFull1 30x20+0+5 RLayoutFullHoriz1 30x10+0+10 RLayoutFullVert1 20x20+5+5 # # window in monitor 1 window 20x10+35+10 RLayoutFindTopBottomEdges 5 24 RLayoutFindLeftRightEdges 0 74 RLayoutFindMonitorBottomEdge 24 RLayoutFindMonitorTopEdge 5 RLayoutFindMonitorLeftEdge 30 RLayoutFindMonitorRightEdge 59 RLayoutFull 75x20+0+5 RLayoutFullHoriz 75x10+0+10 RLayoutFullVert 20x20+35+5 RLayoutFull1 30x20+30+5 RLayoutFullHoriz1 30x10+30+10 RLayoutFullVert1 20x20+35+5
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lya baakalya V;PROG;PL;3;PST lya tulidde V;PL;1;PST+RCT lya okyalya V;PROG;2;PRS lya ndidde V;SG;1;PST+RCT lya baalidde V;PL;3;PST+RCT lya bakyalya V;PROG;PL;3;PRS lya tukyalya V;PROG;PL;1;PRS lya mwalya V;PL;2;PST+RMT lya munaalya V;PL;2;FUT+IMMED lya mukyalya V;PROG;PL;2;PRS lya yaakalya V;PROG;3;PST lya tulya V;PL;1;PRS lya sinnalya V;INTEN;1;FUT lya ndya V;1;PRS lya nkyalya V;PROG;1;PRS lya banaalya V;PL;3;FUT+IMMED lya olidde V;SG;2;PST+RCT lya akyalya V;PROG;3;PRS lya balirya V;PL;3;FUT+RMT lya alya V;3;PRS lya twakalya V;PROG;PL;1;PST lya onoolya V;2;FUT+IMMED lya walidde V;2;PST+RCT lya tonnalya V;INTEN;2;FUT lya mwakalya V;PROG;PL;2;PST lya tannalya V;INTEN;3;FUT lya ndirya V;1;FUT+RMT lya yalya V;3;PST+RMT lya nalidde V;1;PST+RCT lya naalya V;1;FUT+IMMED lya tebannalya V;INTEN;PL;3;FUT lya temunnalya V;INTEN;PL;2;FUT lya tetunnalya V;INTEN;PL;1;FUT lya tunaalya V;PL;1;FUT+IMMED lya olirya V;2;FUT+RMT lya baalya V;PL;3;PST+RMT lya anaalya V;3;FUT+IMMED lya mwalidde V;PL;2;PST+RCT lya alidde V;SG;3;PST+RCT lya naakalya V;PROG;1;PST lya olya V;2;PRS lya lya V;NFIN lya walya V;2;PST+RMT lya twalya V;PL;1;PST+RMT lya waakalya V;PROG;2;PST lya mulya V;PL;2;PRS lya nalya V;1;PST+RMT lya mulidde V;PL;2;PST+RCT lya balya V;PL;3;PRS lya alirya V;3;FUT+RMT lya yalidde V;3;PST+RCT lya tulirya V;PL;1;FUT+RMT lya mulirya V;PL;2;FUT+RMT nywegera mwanywegera V;PL;2;PST+RMT nywegera munywegedde V;PL;2;PST+RCT nywegera tonnanywegera V;INTEN;2;FUT nywegera twakanywegera V;PROG;PL;1;PST nywegera temunnanywegera V;INTEN;PL;2;FUT nywegera onywegera V;2;PRS nywegera nanywegera V;1;PST+RMT nywegera nywegedde V;SG;1;PST+RCT nywegera twanywegera V;PL;1;PST+RMT nywegera okyanywegera V;PROG;2;PRS nywegera waakanywegera V;PROG;2;PST nywegera mukyanywegera V;PROG;PL;2;PRS nywegera balinywegera V;PL;3;FUT+RMT nywegera tebannanywegera V;INTEN;PL;3;FUT nywegera anywegedde V;SG;3;PST+RCT nywegera baanywegera V;PL;3;PST+RMT nywegera yanywegedde V;3;PST+RCT nywegera nkyanywegera V;PROG;1;PRS nywegera baanywegedde V;PL;3;PST+RCT nywegera anywegera V;3;PRS nywegera wanywegera V;2;PST+RMT nywegera munaanywegera V;PL;2;FUT+IMMED nywegera wanywegedde V;2;PST+RCT nywegera yaakanywegera V;PROG;3;PST nywegera baakanywegera V;PROG;PL;3;PST nywegera anaanywegera V;3;FUT+IMMED nywegera sinnanywegera V;INTEN;1;FUT nywegera tunaanywegera V;PL;1;FUT+IMMED nywegera alinywegera V;3;FUT+RMT nywegera naanywegera V;1;FUT+IMMED nywegera twanywegedde V;PL;1;PST+RCT nywegera munywegera V;PL;2;PRS nywegera tunywegera V;PL;1;PRS nywegera yanywegera V;3;PST+RMT nywegera tannanywegera V;INTEN;3;FUT nywegera ndinywegera V;1;FUT+RMT nywegera naakanywegera V;PROG;1;PST nywegera akyanywegera V;PROG;3;PRS nywegera banaanywegera V;PL;3;FUT+IMMED nywegera mulinywegera V;PL;2;FUT+RMT nywegera banywegera V;PL;3;PRS nywegera tukyanywegera V;PROG;PL;1;PRS nywegera nywegera V;1;PRS nywegera tunywegedde V;PL;1;PST+RCT nywegera mwakanywegera V;PROG;PL;2;PST nywegera nywegera V;NFIN nywegera olinywegera V;2;FUT+RMT nywegera bakyanywegera V;PROG;PL;3;PRS nywegera tetunnanywegera V;INTEN;PL;1;FUT nywegera onywegedde V;SG;2;PST+RCT nywegera onoonywegera V;2;FUT+IMMED nywegera tulinywegera V;PL;1;FUT+RMT nywegera nanywegedde V;1;PST+RCT somesa okyasomesa V;PROG;2;PRS somesa naakasomesa V;PROG;1;PST somesa baasomesa V;PL;3;PST+RMT somesa baasomesezza V;PL;3;PST+RCT somesa waakasomesa V;PROG;2;PST somesa yasomesezza V;3;PST+RCT somesa temunnasomesa V;INTEN;PL;2;FUT somesa osomesezza V;SG;2;PST+RCT somesa olisomesa V;2;FUT+RMT somesa yasomesa V;3;PST+RMT somesa anaasomesa V;3;FUT+IMMED somesa bakyasomesa V;PROG;PL;3;PRS somesa baakasomesa V;PROG;PL;3;PST somesa nsomesa V;1;PRS somesa asomesezza V;SG;3;PST+RCT somesa balisomesa V;PL;3;FUT+RMT somesa twasomesa V;PL;1;PST+RMT somesa nasomesa V;1;PST+RMT somesa wasomesa V;2;PST+RMT somesa tonnasomesa V;INTEN;2;FUT somesa tebannasomesa V;INTEN;PL;3;FUT somesa sinnasomesa V;INTEN;1;FUT somesa tetunnasomesa V;INTEN;PL;1;FUT somesa tusomesa V;PL;1;PRS somesa mwakasomesa V;PROG;PL;2;PST somesa tunaasomesa V;PL;1;FUT+IMMED somesa tukyasomesa V;PROG;PL;1;PRS somesa banaasomesa V;PL;3;FUT+IMMED somesa mulisomesa V;PL;2;FUT+RMT somesa tulisomesa V;PL;1;FUT+RMT somesa osomesa V;2;PRS somesa tannasomesa V;INTEN;3;FUT somesa mwasomesezza V;PL;2;PST+RCT somesa twakasomesa V;PROG;PL;1;PST somesa naasomesa V;1;FUT+IMMED somesa nasomesezza V;1;PST+RCT somesa basomesa V;PL;3;PRS somesa somesa V;NFIN somesa ndisomesa V;1;FUT+RMT somesa tusomesezza V;PL;1;PST+RCT somesa wasomesezza V;2;PST+RCT somesa nsomesezza V;SG;1;PST+RCT somesa mwasomesa V;PL;2;PST+RMT somesa twasomesezza V;PL;1;PST+RCT somesa nkyasomesa V;PROG;1;PRS somesa musomesezza V;PL;2;PST+RCT somesa akyasomesa V;PROG;3;PRS somesa yaakasomesa V;PROG;3;PST somesa onoosomesa V;2;FUT+IMMED somesa munaasomesa V;PL;2;FUT+IMMED somesa asomesa V;3;PRS somesa alisomesa V;3;FUT+RMT somesa musomesa V;PL;2;PRS somesa mukyasomesa V;PROG;PL;2;PRS nnyonnyola bannyonnyodde V;PL;3;PST+RCT nnyonnyola munnyonnyola V;PL;2;PRS nnyonnyola mwannyonnyola V;PL;2;PST+RMT nnyonnyola akyannyonnyola V;PROG;3;PRS nnyonnyola waakannyonnyola V;PROG;2;PST nnyonnyola tonnannyonnyola V;INTEN;2;FUT nnyonnyola tunnyonnyola V;PL;1;PRS nnyonnyola olinnyonnyola V;2;FUT+RMT nnyonnyola mulinnyonnyola V;PL;2;FUT+RMT nnyonnyola wannyonnyola V;2;PST+RMT nnyonnyola twannyonnyola V;PL;1;PST+RMT nnyonnyola tebannannyonnyola V;INTEN;PL;3;FUT nnyonnyola nannyonnyola V;1;PST+RMT nnyonnyola ndinnyonnyola V;1;FUT+RMT nnyonnyola tulinnyonnyola V;PL;1;FUT+RMT nnyonnyola okyannyonnyola V;PROG;2;PRS nnyonnyola onnyonnyodde V;SG;2;PST+RCT nnyonnyola baannyonnyola V;PL;3;PST+RMT nnyonnyola bannyonnyola V;PL;3;PRS nnyonnyola naakannyonnyola V;PROG;1;PST nnyonnyola baakannyonnyola V;PROG;PL;3;PST nnyonnyola munaannyonnyola V;PL;2;FUT+IMMED nnyonnyola nannyonnyodde V;1;PST+RCT nnyonnyola twakannyonnyola V;PROG;PL;1;PST nnyonnyola mwannyonnyodde V;PL;2;PST+RCT nnyonnyola naannyonnyola V;1;FUT+IMMED nnyonnyola nyinyonnyodde V;SG;1;PST+RCT nnyonnyola tukyannyonnyola V;PROG;PL;1;PRS nnyonnyola annyonnyola V;3;PRS nnyonnyola tunaannyonnyola V;PL;1;FUT+IMMED nnyonnyola banaannyonnyola V;PL;3;FUT+IMMED nnyonnyola yannyonnyola V;3;PST+RMT nnyonnyola onnyonnyola V;2;PRS nnyonnyola anaannyonnyola V;3;FUT+IMMED nnyonnyola alinnyonnyola V;3;FUT+RMT nnyonnyola nkyannyonnyola V;PROG;1;PRS nnyonnyola yaakannyonnyola V;PROG;3;PST nnyonnyola nnyinyonnyola V;1;PRS nnyonnyola nnyonnyola V;NFIN nnyonnyola bakyannyonnyola V;PROG;PL;3;PRS nnyonnyola mwakannyonnyola V;PROG;PL;2;PST nnyonnyola yannyonnyodde V;3;PST+RCT nnyonnyola temunnannyonnyola V;INTEN;PL;2;FUT nnyonnyola mukyannyonnyola V;PROG;PL;2;PRS nnyonnyola wannyonnyodde V;2;PST+RCT nnyonnyola twannyonnyodde V;PL;1;PST+RCT nnyonnyola tetunnannyonnyola V;INTEN;PL;1;FUT nnyonnyola sinnannyonnyola V;INTEN;1;FUT nnyonnyola balinnyonnyola V;PL;3;FUT+RMT nnyonnyola tannannyonnyola V;INTEN;3;FUT nnyonnyola onoonnyonnyola V;2;FUT+IMMED nnyonnyola annyonnyodde V;SG;3;PST+RCT ba yali V;3;PST+RMT ba aliba V;3;FUT+RMT ba munaaba V;PL;2;FUT+IMMED ba tuli V;PL;1;PRS ba baakaba V;PROG;PL;3;PST ba baali V;PL;3;PST+RMT ba tubadde V;PL;1;PST+RCT ba babadde V;PL;3;PST+RCT ba mukyali V;PROG;PL;2;PRS ba wali V;2;PST+RMT ba anaaba V;3;FUT+IMMED ba twali V;PL;1;PST+RMT ba ba V;NFIN ba ndi V;1;PRS ba temunnaba V;INTEN;PL;2;FUT ba ndiba V;1;FUT+RMT ba nkyali V;PROG;1;PRS ba muli V;PL;2;PRS ba mubadde V;PL;2;PST+RCT ba obadde V;SG;2;PST+RCT ba tannaba V;INTEN;3;FUT ba naaba V;1;FUT+IMMED ba nali V;1;PST+RMT ba sinnaba V;INTEN;1;FUT ba wabadde V;2;PST+RCT ba banaaba V;PL;3;FUT+IMMED ba twakaba V;PROG;PL;1;PST ba yabadde V;3;PST+RCT ba nabadde V;1;PST+RCT ba oliba V;2;FUT+RMT ba waakaba V;PROG;2;PST ba tukyali V;PROG;PL;1;PRS ba naakaba V;PROG;1;PST ba onooba V;2;FUT+IMMED ba mwakaba V;PROG;PL;2;PST ba abadde V;SG;3;PST+RCT ba bakyali V;PROG;PL;3;PRS ba ali V;3;PRS ba yaakaba V;PROG;3;PST ba muliba V;PL;2;FUT+RMT ba okyali V;PROG;2;PRS ba tunaaba V;PL;1;FUT+IMMED ba tuliba V;PL;1;FUT+RMT ba bali V;PL;3;PRS ba akyali V;PROG;3;PRS ba tebannaba V;INTEN;PL;3;FUT ba tonnaba V;INTEN;2;FUT ba twabadde V;PL;1;PST+RCT ba baliba V;PL;3;FUT+RMT ba oli V;2;PRS ba tetunnaba V;INTEN;PL;1;FUT ba mwali V;PL;2;PST+RMT ba baabadde V;PL;3;PST+RCT ba mbadde V;SG;1;PST+RCT nywa tunaanywa V;PL;1;FUT+IMMED nywa twanywa V;PL;1;PST+RMT nywa twakanywa V;PROG;PL;1;PST nywa baakanywa V;PROG;PL;3;PST nywa onywa V;2;PRS nywa balinywa V;PL;3;FUT+RMT nywa okyanywa V;PROG;2;PRS nywa baanywa V;PL;3;PST+RMT nywa tunywedde V;PL;1;PST+RCT nywa mwanywedde V;PL;2;PST+RCT nywa temunnanywa V;INTEN;PL;2;FUT nywa tonnanywa V;INTEN;2;FUT nywa yanywa V;3;PST+RMT nywa alinywa V;3;FUT+RMT nywa nanywa V;1;PST+RMT nywa banywedde V;PL;3;PST+RCT nywa wanywa V;2;PST+RMT nywa onoonywa V;2;FUT+IMMED nywa anywa V;3;PRS nywa tukyanywa V;PROG;PL;1;PRS nywa anywedde V;SG;3;PST+RCT nywa waakanywa V;PROG;2;PST nywa nnywa V;1;PRS nywa sinnanywa V;INTEN;1;FUT nywa bakyanywa V;PROG;PL;3;PRS nywa mukyanywa V;PROG;PL;2;PRS nywa naakanywa V;PROG;1;PST nywa tannanywa V;INTEN;3;FUT nywa olinywa V;2;FUT+RMT nywa ndinywa V;1;FUT+RMT nywa tebannanywa V;INTEN;PL;3;FUT nywa tetunnanywa V;INTEN;PL;1;FUT nywa nnywedde V;SG;1;PST+RCT nywa mwakanywa V;PROG;PL;2;PST nywa onywedde V;SG;2;PST+RCT nywa nkyanywa V;PROG;1;PRS nywa naanywa V;1;FUT+IMMED nywa munaanywa V;PL;2;FUT+IMMED nywa wanywedde V;2;PST+RCT nywa nywa V;NFIN nywa yaakanywa V;PROG;3;PST nywa nanywedde V;1;PST+RCT nywa akyanywa V;PROG;3;PRS nywa banaanywa V;PL;3;FUT+IMMED nywa mwanywa V;PL;2;PST+RMT nywa tunywa V;PL;1;PRS nywa munywa V;PL;2;PRS nywa tulinywa V;PL;1;FUT+RMT nywa anaanywa V;3;FUT+IMMED nywa yanywedde V;3;PST+RCT nywa banywa V;PL;3;PRS nywa mulinywa V;PL;2;FUT+RMT yanjula banaayanjula V;PL;3;FUT+IMMED yanjula ayanjudde V;SG;3;PST+RCT yanjula naakayanjula V;PROG;1;PST yanjula onooyanjula V;2;FUT+IMMED yanjula bakyayanjula V;PROG;PL;3;PRS yanjula tonnayanjula V;INTEN;2;FUT yanjula tunaayanjula V;PL;1;FUT+IMMED yanjula yaakayanjula V;PROG;3;PST yanjula yanjula V;NFIN yanjula twanjula V;PL;1;PRS yanjula twayanjula V;PL;1;PST+RMT yanjula oyanjula V;2;PRS yanjula mwayanjula V;PL;2;PST+RMT yanjula wayanjudde V;2;PST+RCT yanjula yayanjudde V;3;PST+RCT yanjula baakayanjula V;PROG;PL;3;PST yanjula yayanjula V;3;PST+RMT yanjula nayanjula V;1;PST+RMT yanjula bayanjudde V;PL;3;PST+RCT yanjula aliyanjula V;3;FUT+RMT yanjula muliyanjula V;PL;2;FUT+RMT yanjula akyayanjula V;PROG;3;PRS yanjula waakayanjula V;PROG;2;PST yanjula tukyayanjula V;PROG;PL;1;PRS yanjula baayanjula V;PL;3;PST+RMT yanjula baliyanjula V;PL;3;FUT+RMT yanjula temunnayanjula V;INTEN;PL;2;FUT yanjula twayanjudde V;PL;1;PST+RCT yanjula munaayanjula V;PL;2;FUT+IMMED yanjula bayanjula V;PL;3;PRS yanjula nyanjula V;1;PRS yanjula naayanjula V;1;FUT+IMMED yanjula mukyayanjula V;PROG;PL;2;PRS yanjula nayanjudde V;1;PST+RCT yanjula oliyanjula V;2;FUT+RMT yanjula ayanjula V;3;PRS yanjula oyanjudde V;SG;2;PST+RCT yanjula tebannayanjula V;INTEN;PL;3;FUT yanjula twanjudde V;PL;1;PST+RCT yanjula tuliyanjula V;PL;1;FUT+RMT yanjula nkyayanjula V;PROG;1;PRS yanjula mwanjula V;PL;2;PRS yanjula sinnayanjula V;INTEN;1;FUT yanjula twakayanjula V;PROG;PL;1;PST yanjula nyanjudde V;SG;1;PST+RCT yanjula mwakayanjula V;PROG;PL;2;PST yanjula mwanjudde V;PL;2;PST+RCT yanjula okyayanjula V;PROG;2;PRS yanjula tetunnayanjula V;INTEN;PL;1;FUT yanjula anaayanjula V;3;FUT+IMMED yanjula tannayanjula V;INTEN;3;FUT yanjula ndiyanjula V;1;FUT+RMT yanjula baayanjudde V;PL;3;PST+RCT yanjula wayanjula V;2;PST+RMT yongera muliyongera V;PL;2;FUT+RMT yongera oyongedde V;SG;2;PST+RCT yongera yayongedde V;3;PST+RCT yongera nyongera V;1;PRS yongera bayongedde V;PL;3;PST+RCT yongera baliyongera V;PL;3;FUT+RMT yongera tannayongera V;INTEN;3;FUT yongera mwongera V;PL;2;PRS yongera nkyayongera V;PROG;1;PRS yongera munaayongera V;PL;2;FUT+IMMED yongera baakayongera V;PROG;PL;3;PST yongera wayongedde V;2;PST+RCT yongera nayongera V;1;PST+RMT yongera waakayongera V;PROG;2;PST yongera ndiyongera V;1;FUT+RMT yongera sinnayongera V;INTEN;1;FUT yongera bayongera V;PL;3;PRS yongera oliyongera V;2;FUT+RMT yongera twongera V;PL;1;PRS yongera oyongera V;2;PRS yongera naayongera V;1;FUT+IMMED yongera nayongedde V;1;PST+RCT yongera temunnayongera V;INTEN;PL;2;FUT yongera yongera V;NFIN yongera twakayongera V;PROG;PL;1;PST yongera mwayongedde V;PL;2;PST+RCT yongera tukyayongera V;PROG;PL;1;PRS yongera akyayongera V;PROG;3;PRS yongera anaayongera V;3;FUT+IMMED yongera twayongera V;PL;1;PST+RMT yongera tonnayongera V;INTEN;2;FUT yongera tuliyongera V;PL;1;FUT+RMT yongera mwakayongera V;PROG;PL;2;PST yongera tetunnayongera V;INTEN;PL;1;FUT yongera mukyayongera V;PROG;PL;2;PRS yongera aliyongera V;3;FUT+RMT yongera twayongedde V;PL;1;PST+RCT yongera tebannayongera V;INTEN;PL;3;FUT yongera yayongera V;3;PST+RMT yongera yaakayongera V;PROG;3;PST yongera banaayongera V;PL;3;FUT+IMMED yongera okyayongera V;PROG;2;PRS yongera bakyayongera V;PROG;PL;3;PRS yongera wayongera V;2;PST+RMT yongera ayongedde V;SG;3;PST+RCT yongera baayongera V;PL;3;PST+RMT yongera mwayongera V;PL;2;PST+RMT yongera twongedde V;PL;1;PST+RCT yongera naakayongera V;PROG;1;PST yongera nyongedde V;SG;1;PST+RCT yongera onooyongera V;2;FUT+IMMED yongera tunaayongera V;PL;1;FUT+IMMED yongera ayongera V;3;PRS buuza twaakabuuza V;PROG;PL;1;PST buuza yaakabuuza V;PROG;3;PST buuza mukyabuuza V;PROG;PL;2;PRS buuza abuuza V;3;PRS buuza olibuuza V;2;FUT+RMT buuza twabuuza V;PL;1;PST+RMT buuza obuuzizza V;SG;2;PST+RCT buuza tetunnabuuza V;INTEN;PL;1;FUT buuza buuza V;NFIN buuza yabuuza V;3;PST+RMT buuza tulibuuza V;PL;1;FUT+RMT buuza baakabuuza V;PROG;PL;3;PST buuza wabuuzizza V;2;PST+RCT buuza twabuuzizza V;PL;1;PST+RCT buuza baabuuzizza V;PL;3;PST+RCT buuza naabuuza V;1;FUT+IMMED buuza temunnabuuza V;INTEN;PL;2;FUT buuza mbuuza V;1;PRS buuza tukyabuuza V;PROG;PL;1;PRS buuza sinnabuuza V;INTEN;1;FUT buuza naakabuuza V;PROG;1;PST buuza nkyabuuza V;PROG;1;PRS buuza banaabuuza V;PL;3;FUT+IMMED buuza abuuzizza V;SG;3;PST+RCT buuza tebannabuuza V;INTEN;PL;3;FUT buuza waakabuuza V;PROG;2;PST buuza tubuuza V;PL;1;PRS buuza babuuza V;PL;3;PRS buuza mwaakabuuza V;PROG;PL;2;PST buuza mwabuuza V;PL;2;PST+RMT buuza munaabuuza V;PL;2;FUT+IMMED buuza tunaabuuza V;PL;1;FUT+IMMED buuza mubuuza V;PL;2;PRS buuza nabuuza V;1;PST+RMT buuza ndibuuza V;1;FUT+RMT buuza wabuuza V;2;PST+RMT buuza bakyabuuza V;PROG;PL;3;PRS buuza yabuuzizza V;3;PST+RCT buuza mulibuuza V;PL;2;FUT+RMT buuza mwabuuzizza V;PL;2;PST+RCT buuza tubuuzizza V;PL;1;PST+RCT buuza alibuuza V;3;FUT+RMT buuza tonnabuuza V;INTEN;2;FUT buuza onoobuuza V;2;FUT+IMMED buuza baabuuza V;PL;3;PST+RMT buuza anaabuuza V;3;FUT+IMMED buuza akyabuuza V;PROG;3;PRS buuza nabuuzizza V;1;PST+RCT buuza obuuza V;2;PRS buuza balibuuza V;PL;3;FUT+RMT buuza okyabuuza V;PROG;2;PRS buuza tannabuuza V;INTEN;3;FUT buuza mbuuzizza V;SG;1;PST+RCT seka baasese V;PL;3;PST+RCT seka tukyaseka V;PROG;PL;1;PRS seka baaseka V;PL;3;PST+RMT seka tuseka V;PL;1;PRS seka baakaseka V;PROG;PL;3;PST seka aliseka V;3;FUT+RMT seka muliseka V;PL;2;FUT+RMT seka waseka V;2;PST+RMT seka sinnaseka V;INTEN;1;FUT seka banaaseka V;PL;3;FUT+IMMED seka naakaseka V;PROG;1;PST seka tonnaseka V;INTEN;2;FUT seka baliseka V;PL;3;FUT+RMT seka tannaseka V;INTEN;3;FUT seka oliseka V;2;FUT+RMT seka nkyaseka V;PROG;1;PRS seka ndiseka V;1;FUT+RMT seka mwasese V;PL;2;PST+RCT seka tebannaseka V;INTEN;PL;3;FUT seka osese V;SG;2;PST+RCT seka nasese V;1;PST+RCT seka twaseka V;PL;1;PST+RMT seka mwaseka V;PL;2;PST+RMT seka baseka V;PL;3;PRS seka nsese V;SG;1;PST+RCT seka museka V;PL;2;PRS seka oseka V;2;PRS seka tetunnaseka V;INTEN;PL;1;FUT seka asese V;SG;3;PST+RCT seka naaseka V;1;FUT+IMMED seka munaaseka V;PL;2;FUT+IMMED seka twasese V;PL;1;PST+RCT seka tunaaseka V;PL;1;FUT+IMMED seka seka V;NFIN seka waakaseka V;PROG;2;PST seka twakaseka V;PROG;PL;1;PST seka naseka V;1;PST+RMT seka bakyaseka V;PROG;PL;3;PRS seka mukyaseka V;PROG;PL;2;PRS seka yasese V;3;PST+RCT seka nseka V;1;PRS seka anaaseka V;3;FUT+IMMED seka tusese V;PL;1;PST+RCT seka yaseka V;3;PST+RMT seka onooseka V;2;FUT+IMMED seka wasese V;2;PST+RCT seka tuliseka V;PL;1;FUT+RMT seka temunnaseka V;INTEN;PL;2;FUT seka yaakaseka V;PROG;3;PST seka okyaseka V;PROG;2;PRS seka mwakaseka V;PROG;PL;2;PST seka aseka V;3;PRS seka akyaseka V;PROG;3;PRS yaagala oyagala V;2;PRS yaagala mulyagala V;PL;2;FUT+RMT yaagala okyayagala V;PROG;2;PRS yaagala nayagadde V;1;PST+RCT yaagala muyagadde V;PL;2;PST+RCT yaagala wayagadde V;2;PST+RCT yaagala nkyayagala V;PROG;1;PRS yaagala wayagala V;2;PST+RMT yaagala akyayagala V;PROG;3;PRS yaagala mwagala V;PL;2;PRS yaagala tonnayagala V;INTEN;2;FUT yaagala ndyagala V;1;FUT+RMT yaagala naakayagala V;PROG;1;PST yaagala yayagala V;3;PST+RMT yaagala baayagadde V;PL;3;PST+RCT yaagala tunaayagala V;PL;1;FUT+IMMED yaagala ayagadde V;SG;3;PST+RCT yaagala waakayagala V;PROG;2;PST yaagala mwakayagala V;PROG;PL;2;PST yaagala tukyayagala V;PROG;PL;1;PRS yaagala baakayagala V;PROG;PL;3;PST yaagala tebannayagala V;INTEN;PL;3;FUT yaagala yaakayagala V;PROG;3;PST yaagala banaayagala V;PL;3;FUT+IMMED yaagala naayagala V;1;FUT+IMMED yaagala tuyagadde V;PL;1;PST+RCT yaagala mwayagala V;PL;2;PST+RMT yaagala alyagala V;3;FUT+RMT yaagala temunnayagala V;INTEN;PL;2;FUT yaagala tannayagala V;INTEN;3;FUT yaagala anaayagala V;3;FUT+IMMED yaagala munaayagala V;PL;2;FUT+IMMED yaagala oyagadde V;SG;2;PST+RCT yaagala baayagala V;PL;3;PST+RMT yaagala sinnayagala V;INTEN;1;FUT yaagala mukyayagala V;PROG;PL;2;PRS yaagala bayagala V;PL;3;PRS yaagala olyagala V;2;FUT+RMT yaagala nayagala V;1;PST+RMT yaagala tetunnayagala V;INTEN;PL;1;FUT yaagala mwayagadde V;PL;2;PST+RCT yaagala bakyayagala V;PROG;PL;3;PRS yaagala tulyagala V;PL;1;FUT+RMT yaagala onooyagala V;2;FUT+IMMED yaagala njagala V;1;PRS yaagala balyagala V;PL;3;FUT+RMT yaagala twagala V;PL;1;PRS yaagala ayagala V;3;PRS yaagala yaagala V;NFIN yaagala twayagadde V;PL;1;PST+RCT yaagala njagadde V;SG;1;PST+RCT yaagala twayagala V;PL;1;PST+RMT yaagala twakayagala V;PROG;PL;1;PST yaagala yayagadde V;3;PST+RCT soma nsoma V;1;PRS soma mwasoma V;PL;2;PST+RMT soma tebannasoma V;INTEN;PL;3;FUT soma twasoma V;PL;1;PST+RMT soma musoma V;PL;2;PRS soma wasomye V;2;PST+RCT soma yasoma V;3;PST+RMT soma mwasomye V;PL;2;PST+RCT soma waakasoma V;PROG;2;PST soma tusoma V;PL;1;PRS soma akyasoma V;PROG;3;PRS soma twasomye V;PL;1;PST+RCT soma onoosoma V;2;FUT+IMMED soma anaasoma V;3;FUT+IMMED soma nasomye V;1;PST+RCT soma basomye V;PL;3;PST+RCT soma tukyasoma V;PROG;PL;1;PRS soma naasoma V;1;FUT+IMMED soma balisoma V;PL;3;FUT+RMT soma baakasoma V;PROG;PL;3;PST soma nkyasoma V;PROG;1;PRS soma munaasoma V;PL;2;FUT+IMMED soma ndisoma V;1;FUT+RMT soma asomye V;SG;3;PST+RCT soma alisoma V;3;FUT+RMT soma baasoma V;PL;3;PST+RMT soma yaakasoma V;PROG;3;PST soma mukyasoma V;PROG;PL;2;PRS soma temunnasoma V;INTEN;PL;2;FUT soma asoma V;3;PRS soma yasomye V;3;PST+RCT soma nasoma V;1;PST+RMT soma nsomye V;SG;1;PST+RCT soma sinnasoma V;INTEN;1;FUT soma mwakasoma V;PROG;PL;2;PST soma olisoma V;2;FUT+RMT soma twakasoma V;PROG;PL;1;PST soma tonnasoma V;INTEN;2;FUT soma tusomye V;PL;1;PST+RCT soma tetunnasoma V;INTEN;PL;1;FUT soma naakasoma V;PROG;1;PST soma tannasoma V;INTEN;3;FUT soma basoma V;PL;3;PRS soma osomye V;SG;2;PST+RCT soma mulisoma V;PL;2;FUT+RMT soma okyasoma V;PROG;2;PRS soma bakyasoma V;PROG;PL;3;PRS soma banaasoma V;PL;3;FUT+IMMED soma tulisoma V;PL;1;FUT+RMT soma tunaasoma V;PL;1;FUT+IMMED soma musomye V;PL;2;PST+RCT soma wasoma V;2;PST+RMT soma soma V;NFIN soma osoma V;2;PRS tegeera mwategedde V;PL;2;PST+RCT tegeera ategedde V;SG;3;PST+RCT tegeera yategeera V;3;PST+RMT tegeera mukyategeera V;PROG;PL;2;PRS tegeera tetunnategeera V;INTEN;PL;1;FUT tegeera tukyategeera V;PROG;PL;1;PRS tegeera tutegeera V;PL;1;PRS tegeera yategedde V;3;PST+RCT tegeera tutegedde V;PL;1;PST+RCT tegeera anaategeera V;3;FUT+IMMED tegeera wategedde V;2;PST+RCT tegeera baategeera V;PL;3;PST+RMT tegeera tegeera V;NFIN tegeera twakategeera V;PROG;PL;1;PST tegeera alitegeera V;3;FUT+RMT tegeera akyategeera V;PROG;3;PRS tegeera tulitegeera V;PL;1;FUT+RMT tegeera okyategeera V;PROG;2;PRS tegeera baategedde V;PL;3;PST+RCT tegeera tunaategeera V;PL;1;FUT+IMMED tegeera otegeera V;2;PRS tegeera baakategeera V;PROG;PL;3;PST tegeera tannategeera V;INTEN;3;FUT tegeera waakategeera V;PROG;2;PST tegeera naakategeera V;PROG;1;PST tegeera nategeera V;1;PST+RMT tegeera twategeera V;PL;1;PST+RMT tegeera mwategeera V;PL;2;PST+RMT tegeera yaakategeera V;PROG;3;PST tegeera bategeera V;PL;3;PRS tegeera nategedde V;1;PST+RCT tegeera sinnategeera V;INTEN;1;FUT tegeera bakyategeera V;PROG;PL;3;PRS tegeera mutegeera V;PL;2;PRS tegeera wategeera V;2;PST+RMT tegeera tonnategeera V;INTEN;2;FUT tegeera mwakategeera V;PROG;PL;2;PST tegeera mulitegeera V;PL;2;FUT+RMT tegeera tebannategeera V;INTEN;PL;3;FUT tegeera ntegeera V;1;PRS tegeera onootegeera V;2;FUT+IMMED tegeera banaategeera V;PL;3;FUT+IMMED tegeera munaategeera V;PL;2;FUT+IMMED tegeera ntegedde V;SG;1;PST+RCT tegeera naategeera V;1;FUT+IMMED tegeera temunnategeera V;INTEN;PL;2;FUT tegeera ategeera V;3;PRS tegeera olitegeera V;2;FUT+RMT tegeera nkyategeera V;PROG;1;PRS tegeera balitegeera V;PL;3;FUT+RMT tegeera nditegeera V;1;FUT+RMT tegeera otegedde V;SG;2;PST+RCT baawo onoobaawo V;2;FUT+IMMED baawo okyabaawo V;PROG;2;PRS baawo tetunnabaawo V;INTEN;PL;1;FUT baawo tubaddewo V;PL;1;PST+RCT baawo bakyabaawo V;PROG;PL;3;PRS baawo wabaawo V;2;PST+RMT baawo baabaawo V;PL;3;PST+RMT baawo ndibaawo V;1;FUT+RMT baawo mbaawo V;1;PRS baawo mwakabaawo V;PROG;PL;2;PST baawo akyabaawo V;PROG;3;PRS baawo temunnabaawo V;INTEN;PL;2;FUT baawo baabaddewo V;PL;3;PST+RCT baawo wabaddewo V;2;PST+RCT baawo sinnabaawo V;INTEN;1;FUT baawo olibaawo V;2;FUT+RMT baawo babaawo V;PL;3;PRS baawo tukyabaawo V;PROG;PL;1;PRS baawo twakabaawo V;PROG;PL;1;PST baawo balibaawo V;PL;3;FUT+RMT baawo tonnabaawo V;INTEN;2;FUT baawo mulibaawo V;PL;2;FUT+RMT baawo nabaawo V;1;PST+RMT baawo twabaawo V;PL;1;PST+RMT baawo mwabaddewo V;PL;2;PST+RCT baawo naabaawo V;1;FUT+IMMED baawo alibaawo V;3;FUT+RMT baawo naakabaawo V;PROG;1;PST baawo nkyabaawo V;PROG;1;PRS baawo abaddewo V;SG;3;PST+RCT baawo tunaabaawo V;PL;1;FUT+IMMED baawo obaawo V;2;PRS baawo tebannabaawo V;INTEN;PL;3;FUT baawo waakabaawo V;PROG;2;PST baawo mwabaawo V;PL;2;PST+RMT baawo yaakabaawo V;PROG;3;PST baawo munaabaawo V;PL;2;FUT+IMMED baawo mukyabaawo V;PROG;PL;2;PRS baawo tulibaawo V;PL;1;FUT+RMT baawo anaabaawo V;3;FUT+IMMED baawo tubaawo V;PL;1;PRS baawo yabaddewo V;3;PST+RCT baawo abaawo V;3;PRS baawo tannabaawo V;INTEN;3;FUT baawo mubaawo V;PL;2;PRS baawo nabaddewo V;1;PST+RCT baawo banaabaawo V;PL;3;FUT+IMMED baawo obaddewo V;SG;2;PST+RCT baawo yabaawo V;3;PST+RMT baawo mbaddewo V;SG;1;PST+RCT baawo baakabaawo V;PROG;PL;3;PST baawo baawo V;NFIN baawo mubaddewo V;PL;2;PST+RCT tta anatta V;3;FUT+IMMED tta otta V;2;PRS tta tutta V;PL;1;PRS tta nkyatta V;PROG;1;PRS tta mwase V;PL;2;PST+RCT tta olitta V;2;FUT+RMT tta balitta V;PL;3;FUT+RMT tta batta V;PL;3;PST+RMT tta temunnatta V;INTEN;PL;2;FUT tta twakatta V;PROG;PL;1;PST tta okyatta V;PROG;2;PRS tta tannatta V;INTEN;3;FUT tta nzise V;SG;1;PST+RCT tta tuse V;PL;1;PST+RCT tta bakyatta V;PROG;PL;3;PRS tta ase V;SG;3;PST+RCT tta mutta V;PL;2;PRS tta baase V;PL;3;PST+RCT tta yatta V;3;PST+RMT tta mukyatta V;PROG;PL;2;PRS tta akyatta V;PROG;3;PRS tta munatta V;PL;2;FUT+IMMED tta alitta V;3;FUT+RMT tta nditta V;1;FUT+RMT tta naakatta V;PROG;1;PST tta nase V;1;PST+RCT tta twatta V;PL;1;PST+RMT tta baakatta V;PROG;PL;3;PST tta tulitta V;PL;1;FUT+RMT tta nzita V;1;PRS tta tukyatta V;PROG;PL;1;PRS tta mwakatta V;PROG;PL;2;PST tta mulitta V;PL;2;FUT+RMT tta yaakatta V;PROG;3;PST tta tebannatta V;INTEN;PL;3;FUT tta onotta V;2;FUT+IMMED tta mwatta V;PL;2;PST+RMT tta banatta V;PL;3;FUT+IMMED tta tta V;NFIN tta yase V;3;PST+RCT tta watta V;2;PST+RMT tta batta V;PL;3;PRS tta tunatta V;PL;1;FUT+IMMED tta wase V;2;PST+RCT tta base V;PL;3;PST+RCT tta atta V;3;PRS tta sinnatta V;INTEN;1;FUT tta twase V;PL;1;PST+RCT tta natta V;1;FUT+IMMED tta tonnatta V;INTEN;2;FUT tta waakatta V;PROG;2;PST tta ose V;SG;2;PST+RCT tta natta V;1;PST+RMT tta tetunnatta V;INTEN;PL;1;FUT ba ne akyalina V;PROG;3;PRS ba ne tunaaba ne V;PL;1;FUT+IMMED ba ne mubadde ne V;PL;2;PST+RCT ba ne mwakaba ne V;PROG;PL;2;PST ba ne ndiba ne V;1;FUT+RMT ba ne alina V;3;PRS ba ne munaaba ne V;PL;2;FUT+IMMED ba ne olina V;2;PRS ba ne baabadde ne V;PL;3;PST+RCT ba ne mwalina V;PL;2;PST+RMT ba ne tannaba ne V;INTEN;3;FUT ba ne twalina V;PL;1;PST+RMT ba ne okyalina V;PROG;2;PRS ba ne mulina V;PL;2;PRS ba ne obadde ne V;SG;2;PST+RCT ba ne balina V;PL;3;PRS ba ne baalina V;PL;3;PST+RMT ba ne tebannaba ne V;INTEN;PL;3;FUT ba ne nkyalina V;PROG;1;PRS ba ne twakaba ne V;PROG;PL;1;PST ba ne banaaba ne V;PL;3;FUT+IMMED ba ne nalina V;1;PST+RMT ba ne temunnaba ne V;INTEN;PL;2;FUT ba ne wabadde ne V;2;PST+RCT ba ne muliba ne V;PL;2;FUT+RMT ba ne yabadde ne V;3;PST+RCT ba ne tetunnaba ne V;INTEN;PL;1;FUT ba ne sinnaba ne V;INTEN;1;FUT ba ne yalina V;3;PST+RMT ba ne aliba ne V;3;FUT+RMT ba ne nabadde ne V;1;PST+RCT ba ne anaaba ne V;3;FUT+IMMED ba ne tonnaba ne V;INTEN;2;FUT ba ne bakyalina V;PROG;PL;3;PRS ba ne tuliba ne V;PL;1;FUT+RMT ba ne baliba ne V;PL;3;FUT+RMT ba ne tukyalina V;PROG;PL;1;PRS ba ne abadde ne V;SG;3;PST+RCT ba ne onooba ne V;2;FUT+IMMED ba ne nina V;1;PRS ba ne mwabadde ne V;PL;2;PST+RCT ba ne mukyalina V;PROG;PL;2;PRS ba ne waakaba ne V;PROG;2;PST ba ne tubadde ne V;PL;1;PST+RCT ba ne naakaba ne V;PROG;1;PST ba ne ba ne V;NFIN ba ne babadde ne V;PL;3;PST+RCT ba ne walina V;2;PST+RMT ba ne tulina V;PL;1;PRS ba ne twabadde ne V;PL;1;PST+RCT ba ne oliba ne V;2;FUT+RMT ba ne yaakaba ne V;PROG;3;PST ba ne naaba ne V;1;FUT+IMMED ba ne mbadde ne V;SG;1;PST+RCT ba ne baakaba ne V;PROG;PL;3;PST laga walaze V;2;PST+RCT laga twakalaga V;PROG;PL;1;PST laga mwalaze V;PL;2;PST+RCT laga tannalaga V;INTEN;3;FUT laga onoolaga V;2;FUT+IMMED laga ndaga V;1;PRS laga tetunnalaga V;INTEN;PL;1;FUT laga walaga V;2;PST+RMT laga twalaze V;PL;1;PST+RCT laga olaga V;2;PRS laga balaga V;PL;3;PRS laga temunnalaga V;INTEN;PL;2;FUT laga ndaze V;SG;1;PST+RCT laga yalaze V;3;PST+RCT laga akyalaga V;PROG;3;PRS laga alaga V;3;PRS laga nkyalaga V;PROG;1;PRS laga waakalaga V;PROG;2;PST laga munaalaga V;PL;2;FUT+IMMED laga yaakalaga V;PROG;3;PST laga nalaga V;1;PST+RMT laga tukyalaga V;PROG;PL;1;PRS laga mulaga V;PL;2;PRS laga muliraga V;PL;2;FUT+RMT laga baalaze V;PL;3;PST+RCT laga baakalaga V;PROG;PL;3;PST laga yalaga V;3;PST+RMT laga aliraga V;3;FUT+RMT laga okyalaga V;PROG;2;PRS laga baalaga V;PL;3;PST+RMT laga alaze V;SG;3;PST+RCT laga laga V;NFIN laga mwalaga V;PL;2;PST+RMT laga tunaalaga V;PL;1;FUT+IMMED laga tonnalaga V;INTEN;2;FUT laga tulaze V;PL;1;PST+RCT laga twalaga V;PL;1;PST+RMT laga oliraga V;2;FUT+RMT laga ndiraga V;1;FUT+RMT laga tuliraga V;PL;1;FUT+RMT laga banaalaga V;PL;3;FUT+IMMED laga mukyalaga V;PROG;PL;2;PRS laga baliraga V;PL;3;FUT+RMT laga anaalaga V;3;FUT+IMMED laga tebannalaga V;INTEN;PL;3;FUT laga naakalaga V;PROG;1;PST laga tulaga V;PL;1;PRS laga naalaga V;1;FUT+IMMED laga nalaze V;1;PST+RCT laga sinnalaga V;INTEN;1;FUT laga balaze V;PL;3;PST+RCT laga olaze V;SG;2;PST+RCT laga bakyalaga V;PROG;PL;3;PRS laga mwakalaga V;PROG;PL;2;PST wereza mwakaweereza V;PROG;PL;2;PST wereza naaweereza V;1;FUT+IMMED wereza naweereza V;1;PST+RMT wereza tebannaweereza V;INTEN;PL;3;FUT wereza oliweereza V;2;FUT+RMT wereza naakaweereza V;PROG;1;PST wereza okyaweereza V;PROG;2;PRS wereza baliweereza V;PL;3;FUT+RMT wereza wereza V;NFIN wereza nkyaweereza V;PROG;1;PRS wereza mwaaweerezza V;PL;2;PST+RCT wereza ndiweereza V;1;FUT+RMT wereza bakyaweereza V;PROG;PL;3;PRS wereza tannaweereza V;INTEN;3;FUT wereza baweereza V;PL;3;PST+RCT wereza tuliweereza V;PL;1;FUT+RMT wereza oweereza V;2;PRS wereza baweereza V;PL;3;PRS wereza muliweereza V;PL;2;FUT+RMT wereza naweerezza V;1;PST+RCT wereza sinnaweereza V;INTEN;1;FUT wereza yaaweerezza V;3;PST+RCT wereza yaakaweereza V;PROG;3;PST wereza mpeereza V;1;PRS wereza waaweerezza V;2;PST+RCT wereza twakaweereza V;PROG;PL;1;PST wereza mwaweereza V;PL;2;PST+RMT wereza mukyaweereza V;PROG;PL;2;PRS wereza munaaweereza V;PL;2;FUT+IMMED wereza anaaweereza V;3;FUT+IMMED wereza twaweereza V;PL;1;PST+RMT wereza twaaweerezza V;PL;1;PST+RCT wereza tuweereza V;PL;1;PRS wereza muweereza V;PL;2;PRS wereza aliweereza V;3;FUT+RMT wereza yaweereza V;3;PST+RMT wereza tonnaweereza V;INTEN;2;FUT wereza akyaweereza V;PROG;3;PRS wereza banaaweereza V;PL;3;FUT+IMMED wereza tukyaweereza V;PROG;PL;1;PRS wereza tetunnaweereza V;INTEN;PL;1;FUT wereza tunaaweereza V;PL;1;FUT+IMMED wereza waakaweereza V;PROG;2;PST wereza temunnaweereza V;INTEN;PL;2;FUT wereza oweereza V;SG;2;PST+RCT wereza onooweereza V;2;FUT+IMMED wereza aweereza V;SG;3;PST+RCT wereza waweereza V;2;PST+RMT wereza baakaweereza V;PROG;PL;3;PST wereza aweereza V;3;PRS wereza mpeerezza V;SG;1;PST+RCT wereza baaweereza V;PL;3;PST+RMT
92f1996aedd23c532ba081bf5c72169016647943
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clc //ex17.3 V_L=220; V_s=V_L/sqrt(3); //phase voltage I_s=31.87; P_s=400; //total stator copper losses P_r=150; //total rotoe copper losses P_rot=500; //rotational losses PF=0.75; //power factor P_in=3*V_s*I_s*PF; //input power P_ag=P_in-P_s; //air-gap power P_dev=P_in-P_s-P_r; //developed power P_o=P_dev-P_rot; //output power eff=P_o*100/P_in; //efficiency printf(" All the values in the textbook are approximated hence the values in this code differ from those of Textbook") disp(P_ag,'Power crossing the air gap in watts') disp(P_dev,'developed power in watts') disp(P_o,'output power in watts') disp(eff,'effciency percentage') //this value is given wrong in the textbook
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//Example 4.1.7 page 4.8 clc; clear; Iin= 1; lamda= 1550*10^-9; q= 1.602*10^-19; h= 6.625*10^-34; c= 3*10^8; n=0.65; Ip=n*q*lamda*Iin/(h*c); Ip=Ip*1000; //converting in mA for displaying... printf("The average photon current is %d mA",Ip);
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clc clear //Input data T=300 //Temperature in K P=1.01325*10^5 //Absolute pressure in Pa k=1.4 //Adiabatic constant R=287 //Specific gas constant in J/kg-K C_1=60 //Velocity of air in m/s C_2=200 //Velocity of air in m/s C_3=500 //Velocity of air in m/s d_hg=13600 //Density of mercury in kg/m^3 g=9.81 //Acceleration due to gravity in m/s^2 //Calculation a=sqrt(k*R*T) //Sound velocity in m/s M_1=C_1/a //Mach number dP1=(P*C_1^2)/(2*R*T) //Difference in mercury levels in Pa dP1_hg=(dP1/(d_hg*g))*1000 //Difference in mercury levels in mm of Hg M_2=C_2/a //Mach number p1=(1+((k-1)/2)*M_2^2)^(k/(k-1)) //Stagnation to static pressure ratio Po=p1*P //Stagnation pressure in Pa dP2=abs(Po-P) //Difference in mercury levels in Pa dP2_hg=(dP2/(d_hg*g))*1000 //Difference in mercury levels in mm of Hg M_3=C_3/a //Mach number & M_3=Mach number just before shock My=0.723 //Mach number just after shock p1=2.2530 //Ratio of pressure after shock to before shock from gas tables @My Py=p1*P //Pressure after shock in Pa p2=0.706 //Ratio of pressure after shock to Stagnation pressure from gas tables @My Po=Py/p2 //Stagnation pressure in Pa dP3=Po-Py //Difference in mercury levels in Pa dP3_hg=(dP3/(d_hg*g))*1000 //Difference in mercury levels in mm of Hg //Output printf('Difference in mercury levels at velocity equal to:\n (A)%2i m/s is %3.3f mm of Hg\n (B)%3i m/s is %3.1f mm of Hg\n (C)%3i m/s is %3i mm of Hg',C_1,dP1_hg,C_2,dP2_hg,C_3,dP3_hg)
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clc; v=12; //voltage in volt f=60; //frequency in Hz vt=v*sqrt(2); //true voltage vs=vt/10; //sagging voltage disp(vs); av=vt-(vs/2); //calculating average value disp(av,"Average voltage in volt = "); //displaying result
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clc; //Example 3.5 //Page no. 30 printf("Example 3.5 Page no. 30\n\n") //determine potential energy of water // given height,mass of water,g m=1 g=9.8 Z1=0//at ground level Z2=10//at 10 m above from ground level printf("m=%f kg\n g=%f m/s^2\n Z1=%f m\n Z2=%f m\n",m,g,Z1,Z2) PE1=m*g*Z1//potential energy at ground level PE2=m*g*Z2//potential energy at 10m height PE= PE2-PE1 printf("PE1=%fJ\n PE2=%fJ\n PE=%fJ\n",PE1,PE2,PE)
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//Chapter 12 : Solutions to the Exercises //Scilab 6.0.1 //Windows 10 clear; clc; //Solution for 7.1 //(a) A=[1 2;2 -1;-1 0] disp(A) //(b) B=[1 -2;-3 -2;2 3] disp(B)
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clear close clc function [s] = f(x) s = 3*x+2 endfunction fb = 1 fa = 0 n = 4 x = zeros(n+1, 1) y = zeros(n+1, 1) x1 = poly(0, 'x') //CALCULO DO RESULTADO (I) h = (fb-fa)/n x(1,1) = fa for i=2:(n+1) x(i,1) = x(i-1,1)+h end for i=1:(n+1) y(i,1) = f(x(i,1)) end h = x(2,1) - x(1,1) I = h/2*y(1,1) for (i=2:(n)) I = I + h/2*y(i,1)*2 end I = I + h/2*y(n+1,1) disp(I, "Resultado:") //CALCULO DO ERRO (ET) fx = f(x1) fxI = derivat(fx) fxII = derivat(fxI) disp(fx, "Funcao: ") disp(fxI, "Derivada Primeira: ") disp(fxII, "Derivada Segunda: ")
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clc;clear;close; n=3 disp("Enter elements for matrix A") for i=1:n for j=1:n A(i,j)=input("Enter element ") end end lam=poly(0,'lam') lam=lam charMat=A-lam*eye(3,3) disp(charMat,'The charateristic Matrix is') charPoly=poly(A,'lam') disp(charPoly,'The charateristic Polynomial is') lam=spec(A) disp(lam,'The eigen values of A are') function[x,lam]=eigenvectors(A) [n,m]=size(A); lam=spec(A)'; x=[]; for k=1:3 B=A-lam(k)*eye(3,3); C=B(1:n-1,1:n-1); b=-B(1:n-1,n); y=C\b; y=[y;1]; y=y/norm(y); x=[x y]; end endfunction //get f('eigenvectors') [x,lam]=eigenvectors(A) disp(x,'The eigen vectors of A are');
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//Exa:1.9 clc; clear; close; c_mA=7.25;//given c_A=c_mA*1000; printf("%f milliampere current is %f ampere",c_mA,c_A);
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//Example 8.40 clc disp("Excitation table") disp("Present State Next State Flip-flop Inputs") disp(" QC QB A+ B+ J_A K_A J_B K_B") disp(" 0 0 1 1 1 X 1 X") disp(" 0 1 0 0 0 X X 1") disp(" 1 0 0 1 X 1 1 X") disp(" 1 1 1 0 X 0 X 1") disp("") disp("K-map Simplification") disp(" For J_A") disp(" B'' B") disp("A'' 1 0") disp("A X X") disp("J_A = B''") disp("") disp(" For K_A") disp(" B'' B") disp("A'' X X") disp("A 1 0") disp("K_A = B''") disp("") disp(" For J_B") disp(" B'' B") disp("A'' 1 X") disp("A 1 X") disp("J_B = 1") disp("") disp(" For K_B") disp(" B'' B") disp("A'' X 1") disp("A X 1") disp("K_B = 1") disp("")