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clc clear printf('Solve the equation y''+y=3X^2, with boundary points (0,0) and (2, 3.5)') printf('\nCompare computed value form The Galerkin Method vs Analytic result') P=0 X(1,1)=0 for i=1:20 X(1,i+1)=0.1+P P=X(1,i+1) end for i=1:21 A(1,i)=(101/152).*X(1,i).*X(1,i).*X(1,i)-(103/228)*X(1,i).*X(1,i)+(1/228)*X(1,i) B(1,i)=6*cos(X(1,i))+3*(X(1,i).*X(1,i)-2) T=[X(1,i), B(1,i), A(1,i), B(1,i)-A(1,i)] disp(T) end
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//Example_a_16_9 page no:787 clc; Y11=6; Y22=6; Y21=4; Y12=4; Ys=1; driv_pt_admt=((Y22*Ys)+(Y22*Y11)-(Y21*Y12))/(Ys+Y11); disp(driv_pt_admt,"the driving point admittance is (in mho)");
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function []=process_result(filename) M = csvRead(filename, ";") fontS = 4; disp(filename); M1 = M; M1(isnan(M1)) = 60000; disp("total times:"); disp(sum(M1, 1)/1000/60/60); disp(sum(M1)/1000/60/60); f=gcf(); f.figure_size=[1100, 650] f.background=-2; T=5000 N=6000; fact=T/N for j=1:1:size(M,2) x1 = [1:N]; for i=1:1:N x1(i) = sum(M(:,j) < i*fact); end if j == 1 then x = x1; else x = [x; x1]; end end clf; subplot(1,2,1) plot([1:N]/N*60,x); //xtitle(filename, 'čas [s]', 'št. rešenih primerov'); xtitle("", 'čas [s]', 'št. rešenih primerov'); a=gca(); a.font_size = fontS; a.x_label.font_size=fontS; a.y_label.font_size=fontS; a.margins = [0.15, 0.05, 0.125, 0.125] subplot(1,2,2) plot("ln",[1:N]/N*60,x); //xtitle(filename, 'čas [s]', 'št. rešenih primerov'); xtitle("", 'čas [s]', 'št. rešenih primerov'); a=gca(); a.font_size = fontS; a.x_label.font_size=fontS; a.y_label.font_size=fontS; a.margins = [0.15, 0.05, 0.125, 0.125] a.log_flags="ln";// (l=) log scale on y axis legend(['ullmann', 'vf2+subsea', 'vf2'], 4); xs2png(f,strsubst(filename,".txt","")); xs2svg(f,strsubst(filename,".txt","")); xs2pdf(f,strsubst(filename,".txt","")); endfunction figure(1) process_result("diploma/data/results_si2_r001.txt") figure(2) process_result("diploma/data/results_si2_r005.txt") figure(3) process_result("diploma/data/results_si2_r01.txt") figure(4) process_result("diploma/data/results_si4_r001.txt") figure(5) process_result("diploma/data/results_si4_r005.txt") figure(6) process_result("diploma/data/results_si4_r01.txt") figure(7) process_result("diploma/data/results_si6_r001.txt") figure(8) process_result("diploma/data/results_si6_r005.txt") figure(9) process_result("diploma/data/results_si6_r01.txt") //M = csvRead() //subplot(3,3,1);
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//Ex:2.17 clc; clear; close; r_o=40;//resis at 0 degree r_t=44;//at 100 degree t=100;//temperature diff. temp_coeff=(1/t)*((r_t/r_o)-1); printf("Temperature Coefficient = %f per degree centigrade",temp_coeff);
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int main(void) { float x; x++; }
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clc; p1=1.0021; // Initial pressure of the fluid in MPa T1=180; // Initial temperature of the fluid in degree celcius m=0.5; // Mass of the fluid in kg p2=p1; // Constant pressure process // (a).Steam x1=0.8; // Quality of the steam at state 1 // Following are the values taken from steam table vf1=0.001127; vfg1=0.1929; // specific volume of the steam in m^3/kg hf1=763.2; hfg1=2015; // specific enthalpy in kJ/kg sf1=2.1396; sfg1=4.4460; // specific entropy in kJ/kg K v1=vf1+x1*vfg1; // specific volume in m^3/kg h1=hf1+x1*hfg1; // specific enthalpy in kJ/kg s1=sf1+x1*sfg1; // specific entropy in kJ/kg K v2=2*v1; // Final volume of the fluid t2=410.5; // Final temperature of steam in degree celcius (from superheated steam table) h2=3286.4; // specific enthalpy in kJ/kg s2=7.525; // specific entropy in kJ/kg K S21=m*(s2-s1); // Change in entropy W=m*p1*10^3*(v2-v1); // Work done Q=m*(h2-h1); // Heat transferred disp ("kJ",Q,"Heat transferred = ","kJ",W,"Work done = ","kJ/K",S21,"Change in entropy = ","K",t2+273,"Final Temperature = ","(a).Steam"); // (b).Air Cpo=1.0035; // Specific heat at constant pressure in kJ/kg K R=0.287; // characteristic gas constant of air in kJ/kg K V1=m*R*(T1+273)/(p1*10^3); // Initil volume V2=2*V1; // Final volume T2=(T1+273)*V2/V1; // Final temperature S21=m*Cpo*log (V2/V1); // Change in entropy W=p1*10^3*(V2-V1); // Work done Q=m*Cpo*(T2-(T1+273));// Heat transferred disp ("kJ",Q,"Heat transferred = ","kJ",W,"Work done = ","kJ/K",S21,"Change in entropy = ","K",T2,"Final Temperature = ","(b).Air");
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//Chapter-11 example 35 //============================================================================= clc; clear; //input data lamda = 0.03; //wavelength in m RCS = 5; // Radar cross section in m^2 D = 1; // antenna diameter in m F = 5; // noise figure in dB Rmax = 10*10^3 // Radar range BW = 500*10^3; // bandwidth //Calculation F1 = 10^(F/10) // antilog calculation //Rmax = 48*((Pt*D^4*RCS)/(BW*lamda*lamda(F-1)))^0.25 Pt = ((Rmax/48)^4)*((BW*lamda*lamda*(F1-1))/(D^4*RCS)) //Output mprintf('Peak Transmitted Power is %e',Pt); mprintf('\n Note: Antilog Calculation error in textbook at F') //=============================================================================
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y^2 = x^3 + c with x = 24*w + 3, y = 54*v + 5, c = - 2 x -> (2976*w + 31104*w^2 + 165888*w^3 + 331776*w^4 + 129) / (2160*v + 11664*v^2 + 100), y -> ( - 9072*w - 492480*w^2 - 6912000*w^3 - 44789760*w^4 - 143327232*w^5 - 191102976*w^6 + 383) / (32400*v + 349920*v^2 + 1259712*v^3 + 1000)
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//Script to solve dY/dx=F(x,Y), Y(x0)=Y0 function [Z] = F(x, Y) Z(1) = Y(2); Z(2) = (2.5 * sin(.5 * x) - 5 * abs(Y(2)) * Y(2) - 6 * Y(1)) / 2; endfunction; x = [0.0:0.25:15]; x0 = 0; Y0 = [1;0]; Y = ode("rk", Y0, x0, x, F); //solve ODE disp("t Displacement Velocity") disp([x' Y']); y1 = Y(1,:); y2 = Y(2,:); //extract y1, y2C scf(); plot(x, y1, 'b-', x, y2, 'r-'); legend('Disp.', 'Velo.', 1); xtitle('signal plots', 't', 'y'); scf(); plot(y1, y2); xtitle('phase portrait', 'x', 'dx/dt');
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//clc() T1 = 250;//K T = 273.15;//K T2 = 400;//K Cice = 2.037;//kJ/kgK T3 = 373.15;//K Cliq = 75.726;//kJ/kmolK //Cp = 30.475 + 9.652*10^-3*T + 1.189*10^-6*T^2 Hfusion = 6012;//kJ/kmol Hvap = 40608;//kJ/kmol //1 - Heat for raising the temperature of ice, H1 H1 = Cice * (T - T1); //2 - Latent heat of fusion of ice, Hf Hf = Hfusion / 18.016;//kJ //3 - Sensible heat of raising the temperature of water, H2 H2 = Cliq * ( T3 - T)/18.016; //4 - Latent heat of vaporization of water, Hv Hv = Hvap / 18.016; //5 - Sensible heat of raising the temperature of water vapou, H3 H3 = (integrate('30.475 + 9.652*10^-3*T + 1.189*10^-6*T^2','T',T3,T2))/18.016; Q = H1 + H2 + H3 + Hf + Hv; disp("kJ",Q,"Heat required = ")
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l=8; r=400; v=20; disp("Part a"); t=l/r; disp("the time constant (in ms) of the circuit is"); disp(t*10^3); disp("Part b"); i=v/r; disp("final value of the current (in mA) is"); disp(i*10^3); disp("Part c"); rate=v/l; disp("the initial rate of rise of current (in A/s) is"); disp(rate); disp("Part d"); t1=i/rate; disp("time taken (in ms) to reach the final value of current is"); disp(t1*10^3);
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//chapter_no.-6, page_no.-260 //Example_no.6-4-1 clc; //(a) Calculate_the_strong_potential_w(inv)_for_strong_inversion kt=26*(10^-3); Na=3*(10^17); Ni=1.5*(10^10); wsinv=2*kt*log(Na/Ni); disp(wsinv,'the_strong_potential_w(inv)_for_strong_inversion(volts)'); //(b)Calculate_the_insulator_Capacitance eir=4; ei=8.854*(10^-12)*eir; d=.01*(10^-6); Ci=ei/d; Ci=Ci*(1000); disp(Ci,'the_insulator_Capacitance(mF/m^2)='); //(c) Calculate_the_threshold_voltage q=1.6*(10^-19); Na=3*(10^23); er=11.8; e=8.854*er*(10^-12); Vth=wsinv+((2/(Ci*(10^-3)))*((e*q*Na*.437)^(1/2))) disp(Vth,'the_threshold_voltageis ()Volts=');
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// ==================================================================== // Allan CORNET // DIGITEO 2008 - 2010 // ==================================================================== // <-- CLI SHELL MODE --> // ==================================================================== r = xls_NewExcel(); assert_checktrue(r); r = xls_SetVisible(%t); assert_checktrue(r); r = xls_AddWorkbook(); assert_checktrue(r); r = xls_SetWorksheet(1); assert_checktrue(r); for i=1:5 r = xls_ShowGrid(%t); assert_checktrue(r); sleep(200); r = xls_ShowGrid(%f); assert_checktrue(r); sleep(200); end r = xls_SetVisible(%f); assert_checktrue(r); r = xls_SetSave(%t); assert_checktrue(r); r = xls_Close(); assert_checktrue(r); r = xls_Quit(); assert_checktrue(r);
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clear // // //Initilization of Variables L_ED=2 //m //Length of DB & AC L_AC=2 L_DB=2 L_CD=4 //m //Length of CD L_CE=2 //m //Length of CE F_A=40 //KN //Force at C F_B=20 //KN //Force at A E=200*10**6 //KN/mm**2 //Modulus of Elasticity I=50*10**-6 //m**4 //M.I //Calculations //LEt V_C & V_D be the reactions at C & D respectively //V_C+V_D=60 //Taking Moment At D,M_D V_C=-(-F_A*(L_AC+L_CE+L_ED)+F_B*L_DB)*L_CD**-1 V_D=60-V_C //Now Taking Moment at Distance x from A, //M_x=-40*x+50*(x-2)+10*(x-6) //EI*(d**2*y/dx**2)=-40*x+50*(x-2)+10*(x-6) //Now Integrating above Equation we get //EI*(dy/dx)=C1+20*x**2-25*(x-2)+5*(x-6)**2 //Again Integrating above Equation we get //EI*y=C2+C1*x-20*3**-1*x**3+25*3**-1*(x-2)**3+5*3**-1*(x-6)**3 //At x=0 y=0 //C2+2*C1=-53.33 ...............(1) //At x=6 y=0 //C2+6*C1=906.667 ...............(2) //Subtracting Equation 1 from 2 we get C1=853.333*4**-1 C2=53.333-2*C1 x=0 y_A=(C2+C1*x-20*3**-1*x**3+25*3**-1*(x-2)**3+5*3**-1*(x-6)**3)*(E*I)**-1 //Answer For y_A is incorrect in textbook //At Mid-span C1=853.333*4**-1 C2=53.333-2*C1 x=4 y_E=(C2+C1*x-20*3**-1*x**3+25*3**-1*(x-2)**3+5*3**-1*(x-6)**3)*(E*I)**-1 //Answer For y_E is incorrect in textbook //At B C1=853.333*4**-1 C2=53.333-2*C1 x=8 y_B=(C2+C1*x-20*3**-1*x**3+25*3**-1*(x-2)**3+5*3**-1*(x-6)**3)*(E*I)**-1 //Result printf("\n Deflection relative to the level of the supports:at End A %0.4f mm",y_A) printf("\n :at End B %0.4f mm",y_B) printf("\n :at Centre of CD %0.4f mm",y_E)
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//scilab 5.4.1 clear; clc; printf("\t\t\tProblem Number 7.1\n\n\n"); // Chapter 7 : Mixtures Of Ideal Gases // Problem 7.1 (page no. 322) // Solution //As the basis of the calculation,assume that we have 1 lbm of mixture.Also,take the molecular weight of oxygen to be 32.00 and nitrogen to be 28.02.(from table7.1) printf("Solution for (a)\n"); nO2=0.2315/32; //no of moles of oxygen=ratio of mass and molecular weight //0.2315 lb of oxygen per pound printf("The moles of oxygen is %f mole/lbm of mixture\n",nO2); nN2=0.7685/28.02; //no of moles of nitrogen=ratio of mass and molecular weight //0.7685 lb of nitrogen per pound printf("The moles of nitrogen is %f mole/lbm of mixture\n",nN2); nm=nO2+nN2; //Unit:Mole/lbm //number of moles of gas mixture is sum of the moles of its constituent gases printf("The total number of moles is %f mole/lbm\n",nm); xO2=nO2/nm; //mole fraction of oxygen=ratio of no of moles of oxygen and total moles in mixture xN2=nN2/nm; //mole fraction of nitrogen=ratio of no of moles of oxygen and total moles in mixture printf("The mole fraction of oxygen is %f and the mole fraction of nitrogen is %f\n",xO2,xN2); //(Check:xO2+xN2=1) printf("xO2+xN2=%f\n\n",xO2+xN2); printf("Solution for (b)\n"); // the air is at 14.7 psia pO2=xO2*14.7; //the partial pressure of oxygen=pressure of air * the mole fraction of oxygen //psia printf("The partial pressure of oxygen is %f psia\n",pO2); pN2=xN2*14.7; //the partial pressure of nitrogen=pressure of air * the mole fraction of nitrogen //psia printf("The partial pressure of nitrogen is %f psia\n\n",pN2); printf("Solution for (c)\n"); MWm=(xO2*32) + (xN2*28.02); //the molecular weight of air=sum of products of mole fraction of each gas component printf("The molecular weight of air is %f\n\n",MWm); printf("Solution for (d)\n"); Rm=1545/MWm; //the gas constant of air printf("The gas constant of air is %f\n\n",Rm);
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//4.16 clc; Vav=250; V=150; Toff=1*10^-3; Ton=(Vav/V)*Toff-Toff; printf("Period of conduction = %.6f sec", Ton)
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function [num,den]=%p_simp(num,den) // implement complex case // Copyright INRIA
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Ex1_27.sce
//Example 1_27 clc; clear; close; format('v',4); //given data : V1=20;//V V2=4;//V R1=500;//ohm R2=1000;//ohm R3=100;//ohm R4=800;//ohm RL=1000;//ohm //solution VCB=-R2/(R4+R2)*V1;//V //writing KVL equation for the loop I=poly(0,'I'); eqn=V1-R1*I-V2-R3*I;//KVL equation I=roots(eqn);//A VCA=-I*R1;//V //Potential at point B with respect to A VBA=VCB-VCA;//V VOC=VBA;//V Vth=VOC;//V Req=R1*R3/(R1+R3)+R2*R4/(R2+R4);//ohm //Thevenin equivalent current IL=Vth/(Req+RL);//A IL=IL*1000;//mA disp(IL,"Current through 1000 ohm resistor(mA)");
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// [ir,r,cl] = cra(z,M,n) // M: No. of lags // n: Order of pre whitening filter // z is of the form: // z = [y u] // y and u are column matrices function [ir,r,cl] = cra(z,varargin) len = length(varargin); if len==0,M = 20;n = 10; elseif len==1,M = varargin(1);n=10; else M = varargin(1);n = varargin(2); end; [ro,co] = size(z); a1 = armax1(n,-1,0,z(:,2)',zeros(1,ro)); [A,B,D] = arma2p(a1); a11 = coeff(A); z22(1,:) = filt(a11,1,z(:,1)'); z22(2,:) = filt(a11,1,z(:,2)'); Covr = covf(z22',M+1); scir=Covr(4,1); sccf=sqrt(Covr(1,1)*Covr(4,1)); ir = Covr(2,:)'/scir; r(:,1) = -M:M; r(:,2) = [Covr(1,M+1:-1:1) Covr(1,2:M+1)]' r(:,3) = [Covr(4,M+1:-1:1) Covr(4,2:M+1)]' rhoyu = Covr(3,:)'/sccf; rhouy = Covr(2,:)'/sccf; r(:,4) = [rhoyu(M+1:-1:1); rhouy(2:M+1)]; sdreu=2.58*sqrt(r(:,3)'*r(:,2))/scir/sqrt(ro)*ones(2*M+1,1); cl=sdreu(1); timeax=[0:length(ir)-1]; plot(timeax,ir,'bo'); plot2d3(timeax,ir,style = 2); plot(timeax,cl*ones(1,length(ir)),'b-.'); plot(timeax,-cl*ones(1,length(ir)),'b-.'); xtitle('Impulse response estimate','Lags'); xgrid(); endfunction;
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1_3.sce
clc //initialisation of variables p=1.0//metres p0=0.8//metres p100=1.093//metres //CALCULATIONS t=((p-p0)*100/(p100-p0)) //RESULTS printf(' temperature of hot water= % 1f C',t)
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VCAST_TIME_W.tst
-- VectorCAST 6.4d (02/29/16) -- Test Case Script -- -- Environment : VCAST_TIME_W -- Unit(s) Under Test: vcast_time -- -- Script Features TEST.SCRIPT_FEATURE:C_DIRECT_ARRAY_INDEXING TEST.SCRIPT_FEATURE:CPP_CLASS_OBJECT_REVISION TEST.SCRIPT_FEATURE:MULTIPLE_UUT_SUPPORT TEST.SCRIPT_FEATURE:MIXED_CASE_NAMES TEST.SCRIPT_FEATURE:STANDARD_SPACING_R2 TEST.SCRIPT_FEATURE:OVERLOADED_CONST_SUPPORT TEST.SCRIPT_FEATURE:UNDERSCORE_NULLPTR TEST.SCRIPT_FEATURE:FULL_PARAMETER_TYPES TEST.SCRIPT_FEATURE:STATIC_HEADER_FUNCS_IN_UUTS -- -- Test Case: time_add_seconds.001 TEST.UNIT:vcast_time TEST.SUBPROGRAM:time_add_seconds TEST.NEW TEST.NAME:time_add_seconds.001 TEST.NOTES: Author: Date: Version: Requirement: TEST.END_NOTES: TEST.VALUE:vcast_time.time_add_seconds.start.mins:(2)59 TEST.VALUE:vcast_time.time_add_seconds.start.secs:(2)59 TEST.VALUE:vcast_time.time_add_seconds.seconds:1,61 TEST.EXPECTED:vcast_time.time_add_seconds.return.mins:(2)60 TEST.EXPECTED:vcast_time.time_add_seconds.return.secs:0,60 TEST.END -- Test Case: time_add_seconds.002 TEST.UNIT:vcast_time TEST.SUBPROGRAM:time_add_seconds TEST.NEW TEST.NAME:time_add_seconds.002 TEST.NOTES: Author: Date: Version: Requirement: TEST.END_NOTES: TEST.VALUE:vcast_time.time_add_seconds.seconds:1 TEST.VALUE_USER_CODE:vcast_time.time_add_seconds.start <<vcast_time.time_add_seconds.start>>.mins = 59; <<vcast_time.time_add_seconds.start>>.secs = 59; TEST.END_VALUE_USER_CODE: TEST.EXPECTED_USER_CODE:vcast_time.time_add_seconds.return {{ <<vcast_time.time_add_seconds.return>>.mins == 60 }} {{ <<vcast_time.time_add_seconds.return>>.secs == 0 }} TEST.END_EXPECTED_USER_CODE: TEST.END
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пуғдай пуғдайзар N;ALL;SG кӱскӱ кӱскӱнің N;GEN;SG алтын алтын N;NOM;SG чайғы чайғылар N;NOM;PL хар харның N;GEN;SG ағас ағастар N;NOM;PL хуча хучаларнаң N;INS;PL кӱскӱ кӱскӱлерзер N;ALL;PL хара хурт хара хурт N;NOM;SG тарбаған тарбағаннарда N;AT;PL иир иирзер N;ALL;SG алтынзарых алтынзарыхтарзар N;ALL;PL інек інектерні N;ACC;PL хысхы хысхыларның N;GEN;PL аба абаларнаң N;INS;PL тигір тигірлерні N;ACC;PL кӱзен кӱзеннер N;NOM;PL хысхы хысхы N;NOM;SG тағ тағның N;GEN;SG пулут пулуттардаң N;ABL;PL хымысха хымысханың N;GEN;SG тиин тииннің N;GEN;SG алтынзарых алтынзарыхтарнаң N;INS;PL часхы часхыларнаң N;INS;PL чылтыс чылтыстарнаң N;INS;PL кӧл кӧллердең N;ABL;PL хамнос хамностарға N;DAT;PL хозан хозаннар N;NOM;PL хамнос хамностар N;NOM;PL пӧрік пӧрік N;NOM;SG ӱстінзарых ӱстінзарыхтарны N;ACC;PL чар чарларзар N;ALL;PL хозан хозанны N;ACC;SG тирек тирек N;NOM;SG ӧрке ӧркелерге N;DAT;PL сабын сабыннарда N;AT;PL суғ суғны N;ACC;SG киндір киндірні N;ACC;SG кӱскӱ кӱскӱлернең N;INS;PL пуғдай пуғдайны N;ACC;SG чар чарзар N;ALL;SG тағ таға N;DAT;SG пуға пуғазар N;ALL;SG тиин тииннер N;NOM;PL пус пуснаң N;INS;SG пуға пуғалар N;NOM;PL іскер іскердең N;ABL;SG часхы часхыларны N;ACC;PL порсых порсых N;NOM;SG тас тассар N;ALL;SG кӱн кӱннернең N;INS;PL палых палыхтарнаң N;INS;PL кӧрік кӧріктернең N;INS;PL іскер іскерге N;DAT;SG тағ тағнаң N;INS;SG пуға пуғаларда N;AT;PL пулут пулуттарның N;GEN;PL тимір тимірнің N;GEN;SG тарбаған тарбағанның N;GEN;SG тас тастаң N;ABL;SG часхы часхыда N;AT;SG інек інектернің N;GEN;PL мылтых мылтыхтаң N;ABL;SG парыс парыстың N;GEN;SG хысхы хысхылар N;NOM;PL кӱн кӱннең N;ABL;SG мылтых мылтыхтар N;NOM;PL азах азах N;NOM;SG палых палыхтардаң N;ABL;PL тіл тілде N;AT;SG аба абаларны N;ACC;PL тайға тайғаларнаң N;INS;PL кӱскӱ кӱскӱзер N;ALL;SG хозан хозаннарнаң N;INS;PL порсых порсыхтарға N;DAT;PL оо ооларнаң N;INS;PL суғ суғларзар N;ALL;PL тайға тайға N;NOM;SG пуға пуғалардаң N;ABL;PL сабын сабыннарның N;GEN;PL кӧл кӧллерде N;AT;PL пӧрік пӧріктерні N;ACC;PL чис чиске N;DAT;SG кӱскӱ кӱскӱлерде N;AT;PL парыс парыстарда N;AT;PL хоосха хоосханаң N;INS;SG тиин тиинзер N;ALL;SG алабарыс алабарыстарны N;ACC;PL чылан чыланнар N;NOM;PL тиин тииннернең N;INS;PL кӧл кӧллернең N;INS;PL хымысха хымысхадаң N;ABL;SG хоосха хоосхаларнаң N;INS;PL тӱлгӱ тӱлгӱзер N;ALL;SG порсых порсыхтарның N;GEN;PL чылтыс чылтыстың N;GEN;SG часхы часхынаң N;INS;SG ағас ағастарның N;GEN;PL азах азахтардаң N;ABL;PL сыын сыыннарда N;AT;PL кӧл кӧллерзер N;ALL;PL порсых порсыхнаң N;INS;SG чис чистердең N;ABL;PL кӱмӱс кӱмӱстернің N;GEN;PL молат молатнаң N;INS;SG ағас ағастарны N;ACC;PL пӧрік пӧріктең N;ABL;SG адай адайның N;GEN;SG чазы чазылардаң N;ABL;PL харағай харағайның N;GEN;SG кӱмӱс кӱмӱстерге N;DAT;PL кидер кидернең N;INS;SG кӧрік кӧріктең N;ABL;SG чылан чылан N;NOM;SG адай адайға N;DAT;SG азах азахха N;DAT;SG чил чиллер N;NOM;PL пулут пулуттарзар N;ALL;PL пуға пуғадаң N;ABL;SG тамыр тамыр N;NOM;SG чылан чыланнаң N;ABL;SG тибе тибелерзер N;ALL;PL адай адайларны N;ACC;PL тирек тиректерге N;DAT;PL тайға тайғазар N;ALL;SG хысхы хысхыларны N;ACC;PL тамыр тамырларзар N;ALL;PL алабарыс алабарыстарға N;DAT;PL тіл тілге N;DAT;SG киндір киндірлерзер N;ALL;PL ағас ағасты N;ACC;SG хоосха хоосхаларның N;GEN;PL парыс парыста N;AT;SG хозан хозаннарда N;AT;PL кӱн кӱннерге N;DAT;PL кидер кидерлер N;NOM;PL хамнос хамностарнаң N;INS;PL кӱскӱ кӱскӱлернің N;GEN;PL інек інексер N;ALL;SG тигір тигірлерде N;AT;PL сыын сыынға N;DAT;SG тибе тибезер N;ALL;SG алтынзарых алтынзарыхтарның N;GEN;PL хозан хозанда N;AT;SG ӱстінзарых ӱстінзарыхтарзар N;ALL;PL чон чонны N;ACC;SG тимір тимірлернің N;GEN;PL сосха сосхазар N;ALL;SG тас тастарнаң N;INS;PL часхы часхы N;NOM;SG тас тастарзар N;ALL;PL чазы чазызар N;ALL;SG хуча хучаларға N;DAT;PL хузурух хузурухтың N;GEN;SG наңмыр наңмырзар N;ALL;SG тӱн тӱнзер N;ALL;SG пуғдай пуғдайларда N;AT;PL талай талайларны N;ACC;PL чар чарның N;GEN;SG іскер іскерлернең N;INS;PL хуча хучалар N;NOM;PL чар чарларны N;ACC;PL хысхы хысхының N;GEN;SG харағай харағайзар N;ALL;SG ағас ағастарда N;AT;PL сыын сыынның N;GEN;SG тирек тирекнең N;INS;SG тигір тигірзер N;ALL;SG кӱзен кӱзеннернең N;INS;PL кӱзен кӱзеннең N;ABL;SG оо ооның N;GEN;SG тас таста N;AT;SG пуғдай пуғдайнаң N;INS;SG тибе тибенең N;INS;SG сосха сосхалардаң N;ABL;PL тағ тағда N;AT;SG тибе тибені N;ACC;SG чон чонның N;GEN;SG тамыр тамырға N;DAT;SG хум хумнар N;NOM;PL тарбаған тарбағаннар N;NOM;PL хамнос хамностаң N;ABL;SG тарбаған тарбағаннаң N;ABL;SG иир иирлерні N;ACC;PL чил чиллерні N;ACC;PL тайға тайғадаң N;ABL;SG парыс парыстарзар N;ALL;PL алтынзарых алтынзарыхтарны N;ACC;PL суғ суғларнаң N;INS;PL хул хулда N;AT;SG чылан чыланнардаң N;ABL;PL молат молаттарнаң N;INS;PL тас тас N;NOM;SG кӱзен кӱзеннерні N;ACC;PL чазы чазыны N;ACC;SG порсых порсыхха N;DAT;SG молат молаттарның N;GEN;PL чазы чазыларны N;ACC;PL табах табахтарны N;ACC;PL аба абаларға N;DAT;PL тӱлгӱ тӱлгее N;DAT;SG хуча хуча N;NOM;SG пӧрік пӧріктерзер N;ALL;PL хара хурт хара хурттарда N;AT;PL адай 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// ******************************************************************* // Lagrange Interpolation for the given data: **** // (x1, f1), (x2, f2), (x3, f3), ......(xn, fn) **** // NPDE-TCA UG-Level workshop at IMA Bhubaneshwar **** // By Manas,FOSSEE,IITB **** //******************************************************************** function y = Lagrange(x0, x,f, n) m = n + 1; N = ones(1,m); D = N; C = N; y = 0.0; for j = 1:m for k = 1:m if (k<>j) then N(j) = N(j)*(x0 - x(k)) D(j) = D(j)*(x(j) - x(k)) end end L(j) = N(j)/D(j); y = y + L(j)*f(j); end disp(L','L') disp(f,'f(x)') endfunction
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//Exa 1.12 clc; clear; close; //Given data format('v',6); C1=21;//in pF V1=4;//in volt V2=9;//in volt disp("C is proportional to 1/sqrt(V)"); disp("So, C2/C1=sqrt(V1/V2)"); C2=sqrt(V1/V2)*C1;//in pF disp(C2,"At reverse bias 9V, Diode capacitance in pF : ");
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function [fx] = FungsiD(x) M = sum(x); [m, n] = size(x); for i = 1 : n fx(i) = (x(i)) / M end endfunction
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//Bilinear transformation //To convert twin-T notch analog filter to digital filter s=%s; z=%z; HS=(s^2+1)/(s^2+4*s+1); Wo=1; S=240;f=60;//sampling and analog frequencies W=0.5*%pi;//digital frequency C=Wo/tan(0.5*W) HZ=horner(HS,C*(z-1)/(z+1)) f=0:120; HZ1=abs(horner(HZ,exp(-%i*%pi*f'/120))); HS1=abs(horner(HS,(%i*f'/60))); a=gca(); a.x_location="origin"; plot2d(f,HZ1); plot2d(f,HS1); xlabel('Analog Frequency f[kHZ]'); ylabel('Magnitude'); xtitle('Notch filter H(S) and digital filter H(z)');
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// Example 8_2 clc;funcprot(0); // Given data Q_solar=100*10^3;// Btu/h T_river=40+459.67;// R T_collector=200+459.67;// R // Calculation W_e_rev=(Q_solar*(1-(T_river/T_collector)))/3412;// kW printf("\nThe maximum steady state electrical power (in kW) that can be produced by this power plant,(W_electrical)_rev=%1.2f kW",W_e_rev);
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function [x_q, s_q] = delta_mod(sinal,delta) e(1) = 0; e_q(1) = delta*sign(e(1)); x_q(1) = 0; for k=1:length(sinal) e(k+1) = sinal(k) - x_q(k); e_q(k+1) = delta*sign(e(k)); x_q(k+1) = x_q(k) + e_q(k); end s_q = e_q./delta; endfunction
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clc; funcprot(0); //Example 24.1 //Initializing the variables H_at = 10.3; Hs = 1.5; Hd = 4.5; Ls = 2; Ld = 15; g = 9.81; Ds = 0.4; // Diameter of stroke Db = 0.15; // Diameter of bore Dd = 0.05; // Diameter of discharge and suction pipe nu = 0.2; f = 0.01; abs_pump_pressure = 2.4; //Calculations A = %pi*(Db)^2/4; a = %pi*(Dd)^2/4; r = Ds/2; W = 2*%pi*nu; Hsf = 0; function[y] = H_suck(n) // n for checking the sign of Hsi = 4fl/2dg *(vA/a)^2 y = H_at - Hs +(-1)^n*(L/g)*(A/a)*W^2*r; endfunction function[y] = H(n,DischargeOrSuction)// n for checking the sign of Hsi = 4fl/2dg *(vA/a)^2, for suction 1 and for discharge2 if(DischargeOrSuction == 1) then y = H_at - Hs +(-1)^n*(Ls/g)*(A/a)*W^2*r; elseif(DischargeOrSuction == 2) then y = H_at + Hd +(-1)^n*(Ld/g)*(A/a)*W^2*r; else disp("There is something wrong :") end endfunction function[y] = H_mid(DischargeOrSuction,uA)// n for checking the sign of Hsi = 4fl/2dg *(vA/a)^2, for discharge 1 and for suction 2 if(DischargeOrSuction == 1) then Hsf = 4*f*Ls/(2*Dd*g)*(uA/a)^2; y = H_at - Hs - Hsf; elseif(DischargeOrSuction == 2) then Hsf = 4*f*Ld/(2*Dd*g)*(uA/a)^2; y = H_at + Hd + Hsf; else disp("There is something wrong :") end endfunction Hs_start = H(1,1); // Inertia head negative hence n = 1 Hs_end = H(2,1); // Inertia head positive hence n = 2 Hd_start = H(1,2); Hd_end = H(2,2); u = W*r; Hs_mid = H_mid(1,u*A); slip = 0.04; Hd_mid = H_mid(2,u*A); suction = [Hs_start Hs_end Hs_mid]; discharge = [Hd_start Hd_end Hd_mid]; header = [" Start(m)"," End(m)"," Mid(m)"]; W_max = sqrt((abs_pump_pressure - H_at + Hs)*(g/Ls)*(a/A)*(1/r)); W_max_rev = W_max/(2*%pi)*60; // maximum rotation speed in rev/min disp(W_max_rev,"Drive speed for s eperation (rev/min) :","!----Part(c)----1",discharge,header,"!----Part(b)----! Head at",suction,header,"!----Part(a)----! Head at");
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//chapter 21 Ex 1 clc; clear; close; p=68000; r=50/3; t=9/12; sInterest=(p*r*t)/100; printf("The simple interest is Rs. %d",sInterest);
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//chapter6,Example6_19,pg 148 Ie=1*10^-3 Ib=0.04*10^-3 Ic=Ie-Ib alpha=Ic/Ie printf("current gain\n") printf("alpha=%.2f",alpha)
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// Exa 2.16.5 clc; clear; close; format('e',8) // Given data At = 63.5;// atomic weight d = 8.96;// in gm/cc Miu_e = 43.28;// in cm^2/V.sec N_A = 6.02*10^23;// in /gm mole e = 1.6*10^-19;// in C n = (N_A/At)*d;// in /cc Rho = 1/(n*e*Miu_e);// in ohm-cm disp(Rho,"The resistivity in ohm-cm is");
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// ELECTRICAL MACHINES // R.K.Srivastava // First Impression 2011 // CENGAGE LEARNING INDIA PVT. LTD // CHAPTER : 6 : SYNCHRONOUS MACHINES // EXAMPLE : 6.28 clear ; clc ; close ; // Clear the work space and console // GIVEN DATA V = 400; // Operating voltage of the Synchronous generator in Volts f = 50; // Operating Frequency of the Synchronous generator in Hertz xd = 12; // Direct axis reactances in Ohms xq = 5; // Quadrature axis reactances in Ohms delta = 15; // Power(Torque) angle in degree p = 2; // Number of the poles m = 3; // Number of the phase // CALCULATIONS v = V/sqrt(3); // Rated Phase Votage in Volts Ns = (120*f)/p; // Operating speed in RPM Ws = (2*%pi*f)/(p/2); // Synchronous speed in radians/s T = (3*v^2*sind(2*delta)/(2*Ws))*((1/xq)-(1/xd)); // Developed Torque in Newton-meter // DISPLAY RESULTS disp("EXAMPLE : 6.28: SOLUTION :-"); printf("\n (a) Operating speed, Ns = %.f RPM \n",Ns) printf("\n (b) Developed Torque , T = %.2f N-m \n",T)
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clc; bore=5;//cm stroke=7.5;//cm V=(%pi/4)*5^2*7.5 V0=21.3; tV=V+V0; rv=tV/V0; y=1.4; eta=1-[rv^(1-y)]; disp("efficiency is:"); disp("%",eta*100)
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FOSSEE/Scilab-TBC-Uploads
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refs/heads/master
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//Variable declaration theta=90; //angle(degrees) lamda=1.5; //wavelength(angstrom) d=1.6; //spacing(angstrom) //Calculation theta=theta*%pi/180; //angle(radian) n=2*d*sin(theta)/lamda; //order of diffraction //Result printf('order of diffraction is %0.3f \n',int(n))
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/DSP Functions/allpasslp2bs/allpasslp2bs.sci
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shreniknambiar/FOSSEE-DSP-Toolbox
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refs/heads/master
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allpasslp2bs.sci
function [AllpassNum,AllpassDen]= allpasslp2bs (Wo,Wt) // Allpass filter for lowpass to bandstop transformation // //Calling Sequence: //[AllpassNum,AllpassDen] = allpasslp2bs(Wo,Wt): returns the numerator, AllpassNum, and the denominator, AllpassDen, of the second-order allpass mapping filter for performing a real lowpass to real bandstop frequency transformation. This transformation effectively places one feature of an original filter, located at frequency -Wo, at the required target frequency location, Wt1, and the second feature, originally at +Wo, at the new location, Wt2. It is assumed that Wt2 is greater than Wt1. This transformation implements the "Nyquist Mobility," which means that the DC feature stays at DC, but the Nyquist feature moves to a location dependent on the selection of Wo and Wt. // //Input Parameters: // Wo: Frequency value of the prototype filter // Wt: Desired Frequencies for the target filter // //Output Parameters: // AllpassNum: Numerator of mapping filer // AllpassDen: Denominator of mapping filter //Example: Design the allpass mapping filter changing the lowpass filter with cutoff frequency at Wo=0.65 to the real–valued bandstop filter with cutoff frequencies at Wt1=0.23 and Wt2=0.45. // // Wo = 0.65; Wt = [0.23 0.45]; // [AllpassNum, AllpassDen] = allpasslp2bs(Wo, Wt); // [h, f] = freqz(AllpassNum, AllpassDen); // plot(f/%pi,-angle(h)/%pi); // //Author: Shrenik Nambiar // //References: 1. Constantinides, A.G., "Spectral transformations for digital filters," IEEE® Proceedings, vol. 117, no. 8, pp. 1585-1590, August 1970. // 2. Constantinides, A.G., "Design of bandpass digital filters," IEEE Proceedings, vol. 1, pp. 1129-1231, June 1969. // // Input Validation Statements if argn(2) ~=2 then error("Number of input arguments should be 2"); end if argn(1)<1| argn(1)>2 then error("Number of output arguments should be either 1 or 2"); end if ~isscalar(Wo) | ~isreal(Wo) then error("Wo must be real ,numeric and scalar"); end if Wo<=0 | Wo>=1 then error("Wo must lie between 0 and 1"); end if length(Wt)~=2 | ~isreal(Wt) then error("Wt must be real and numeric and must contain only 2 elements"); end if Wt(1)<=0 | Wt(1)>=1 | Wt(2)<=0 | Wt(2)>=1 then error("Wt must lie between 0 and 1"); end //Calculating the numerator and denominator for the mapping filter Wc = sum(Wt) / 2; bw = max(Wt) - min(Wt); al = cos(%pi*(Wo+bw)/2) / cos(%pi*(Wo-bw)/2); be = cos(%pi*Wc) / cos(%pi*bw/2); AllpassDen = [1 -be*(1+al) al]; AllpassNum = flipdim(AllpassDen,2); endfunction
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FOSSEE/xcos_on_cloud
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2023-05-02T00:18:57
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CURVE_c.sci
// Scicos // // Copyright (C) INRIA - Masoud Najafi <masoud.najafi@inria.fr> // Serge Steer <serge.steer@inria.fr> 1993 // Habib Jreij 1993 // // This program is free software; you can redistribute it and/or modify // it under the terms of the GNU General Public License as published by // the Free Software Foundation; either version 2 of the License, or // (at your option) any later version. // // This program is distributed in the hope that it will be useful, // but WITHOUT ANY WARRANTY; without even the implied warranty of // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the // GNU General Public License for more details. // // You should have received a copy of the GNU General Public License // along with this program; if not, write to the Free Software // Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA. // // See the file ../license.txt // function [x,y,typ]=CURVE_c(job,arg1,arg2) //** 07/01/2008 : Adapted fot Scilab 5.0 by Simone Mannori x=[]; y=[]; typ=[]; select job case "set" then x = arg1; model = arg1.model; graphics = arg1.graphics; exprs = graphics.exprs; ok = %f; SaveExit = %f; while %t do Ask_again = %f; [ok,Method,xx,yy,PeriodicOption,graf,exprs] = scicos_getvalue("Spline data",["Spline"+... " Method (0..7)";"x";"y";"Periodic signal(y/n)?";"Launch"+... " graphic window(y/n)?"],list("vec",1,"vec",-1, ... "vec",-1,"str",1,"str",1),exprs) if ~ok then break; end if PeriodicOption=="y" | PeriodicOption=="Y" then PO=1; else exprs(4)="n"; PO=0; end mtd=int(Method); if mtd<0 then mtd=0 end; if mtd>7 then mtd=7; end METHOD = getmethod(mtd); if ~Ask_again then xx=xx(:); yy=yy(:); [nx,mx] = size(xx); [ny,my]=size(yy); if ~((nx==ny)&(mx==my)) then messagebox("Incompatible size of [x] and [y]","modal","error"); Ask_again = %t; end end if ~Ask_again then //+++++++++++++++++++++++++++++++++++++++ xy = [xx,yy]; [xy] = cleandata(xy); // just for sorting to be able to compare data before and after poke_point(.) N= size(xy,"r"); exprs(5)="n";// exprs.graf='n' if graf=="y" | graf=="Y" then //_______Graphic editor___________ ipar=[N;mtd;PO]; rpar=[]; if (winsid() == []) then curwin = 0; else curwin = max(winsid())+1; //** prepare a brand new win end //** see below in this file; "poke_point" is very similar to "edit_curv" [orpar,oipar,ok] = poke_point(xy,ipar,rpar); //** HERE WE ARE +++++++++++++++++++++++++++++++++++ if ~ok then break; end;// exit without save // verifying the data change N2=oipar(1); xy2=[orpar(1:N2),orpar(N2+1:2*N2)]; New_methhod=oipar(2); DChange=%f; METHOD=getmethod(New_methhod); if or(xy(:,1)<>xy2(:,1)) then, DChange=%t; end if or(xy(1:N-1,2)<>xy2(1:N2-1,2)) then, DChange=%t; end if (xy(N,2)<>xy2(N2,2) & (METHOD<>"periodic")) then, DChange=%t; end if DChange then exprs(2)=strcat(sci2exp(xy2(:,1))) exprs(3)=strcat(sci2exp(xy2(:,2))) end exprs(1)=sci2exp(New_methhod); if oipar(3)==1 then, perop="y"; else, perop="n"; end exprs(4)=perop; SaveExit=%t else//_____________________No graphics__________________________ [Xdummy,Ydummy,orpar]=Do_Spline(N,mtd,xy(:,1),xy(:,2)); if (METHOD=="periodic") then // periodic spline xy(N,2)=xy(1,2); end if (METHOD=="order 2" | METHOD=="not_a_knot"|METHOD=="periodic" | METHOD=="monotone"| METHOD=="fast" | METHOD=="clamped") then orpar=[xy(:,1);xy(:,2);orpar]; else if (METHOD=="zero order"|METHOD=="linear") orpar=[xy(:,1);xy(:,2);] end end exprs(1)=sci2exp(mtd);// pour le cas methode>7 | method<0 oipar=[N;mtd;PO] SaveExit=%t end //___________________________________________________________ end //++++++++++++++++++++++++++++++++++++++++++++++++++++++ if (SaveExit) then xp=find(orpar(1:oipar(1))>=0); if (xp<>[]) then model.firing=orpar(xp(1)); //first positive event else model.firing=-1; end model.rpar=orpar model.ipar=oipar graphics.exprs=exprs; x.model=model x.graphics=graphics break end end case "define" then model=scicos_model() xx=[0, 1, 2]; yy=[10, 20, -30]; N=3; Method=3; PeriodicOption="y"; Graf="n" model.sim=list("curve_c",4) model.in=[] model.out=1 model.rpar=[xx(:);yy(:)] model.ipar=[N;Method;1] model.blocktype="c" model.dep_ut=[%f %t] model.evtin=1 model.evtout=1 model.firing=0 exprs=[sci2exp(Method);sci2exp(xx);sci2exp(yy);PeriodicOption;Graf] gr_i=[] x=standard_define([2 2],model,exprs,gr_i) end endfunction function [rpar,ipar,ok] = poke_point(ixy,iparin,rparin) [lhs,rhs]=argn(0) //** get_click is already defined in "editi_curv" //in line definition of get_click deff("[btn,xc,yc,win,Cmenu]=get_click(flag)",[ "if ~or(winsid() == curwin) then Cmenu = ''Quit'';return,end,"; "if argn(2) == 1 then"; " [btn, xc, yc, win, str] = xclick(flag);"; "else"; " [btn, xc, yc, win, str] = xclick();"; "end;"; "if btn == -1000 then"; " if win == curwin then"; " Cmenu = ''Quit'';"; " else"; " Cmenu = ''Open/Set'';"; " end,"; " return,"; "end"; "if btn == -2 then"; " xc = 0;yc = 0;"; " try " // added to handle unwanted menu actions in french version " execstr(''Cmenu='' + part(str, 9:length(str) - 1));"; " execstr(''Cmenu='' + Cmenu);"; " catch" " Cmenu=[]" " end " " return,"; "end"; "Cmenu=[]"]) ok = %f if rhs==0 then ixy=[]; end; if size(xy,"c")<2 then xinfo(" No [y] is provided"); return end [xy] = cleandata(ixy) N = size(xy,"r"); if rhs<=1 then NOrder = 1; PeridicOption = 0; ipar = [N;NOrder;PeridicOption] rpar = [] else if rhs==2 then NOrder = iparin(2); PeridicOption = iparin(3); ipar = iparin; rpar = []; else if rhs==3 then NOrder = iparin(2); PeridicOption = iparin(3); ipar = iparin; rpar = rparin end end //** ??? end //** ??? Amp=[]; wp=[]; phase=[]; offset=[]; np1=[]; Sin_exprs = list(string(Amp),string(wp), string(phase),string(offset),string(np1)); sAmp=[]; sTp=[]; sdelay=[]; Sawt1_exprs = list(string(sAmp),string(sTp),string(sdelay)); sAmp2=[]; sTp2 = []; Sawt2_exprs = list(string(sAmp2),string(sTp2)); Amp3=[]; Tp3=[]; Pw3=[]; Pd3=[]; Bias3=[]; Pulse_exprs=list(string(Amp3), string(Tp3),string(Pw3),string(Pd3),string(Bias3)) mean4=[]; var4=[]; seed4=[]; sample4=[]; np4=[]; random_n_exprs=list(string(mean4),string(var4), string(seed4),string(sample4),string(np4)) min5=[]; max5=[]; seed5=[]; sample5=[]; np5=[]; random_u_exprs=list(string(min5), string(max5), string(seed5),string(sample5),string(np5)) // bornes initiales du graphique xmx = max(xy(:,1)); xmn=min(xy(:,1)), xmn=max(xmn,0); ymx = max(xy(:,2)); ymn=min(xy(:,2)); dx = xmx-xmn; dy = ymx-ymn if dx==0 then dx=max(xmx/2,1), end; xmx = xmx+dx/50; if dy==0 then dy=max(ymx/2,1), end; ymn = ymn-dy/50; ymx = ymx+dy/50; rect = [xmn,ymn;xmx,ymx]; // initial draw f = scf(curwin); menu_r = []; menu_s = []; menu_o = ["zero order","linear","order 2","not_a_knot","periodic","monotone","fast","clamped"] menu_d = ["Clear","Data Bounds","Load from text file","Save to text file","Load from Excel","Periodic signal"] menu_t=["sine","sawtooth1","sawtooth2","pulse","random normal","random uniform"] menu_e=["Help","Exit without save","Save/Exit"] MENU=["Autoscale","Spline","Data","Standards","Exit"]; menus = list(MENU,menu_s,menu_o,menu_d,menu_t,menu_e); scam="menus(1)(1)" w="menus(3)("; r=")"; Orderm=w(ones(menu_o))+string(1:size(menu_o,"*"))+r(ones(menu_o)) w="menus(4)("; r=")"; Datam=w(ones(menu_d))+string(1:size(menu_d,"*"))+r(ones(menu_d)) w="menus(5)("; r=")"; Standm=w(ones(menu_t))+string(1:size(menu_t,"*"))+r(ones(menu_t)) w="menus(6)("; r=")"; Exitm=w(ones(menu_e))+string(1:size(menu_e,"*"))+r(ones(menu_e)) execstr("Autoscale_"+string(curwin)+"=scam") execstr("Spline_"+string(curwin)+"=Orderm") execstr("Data_"+string(curwin)+"=Datam") execstr("Standards_"+string(curwin)+"=Standm") execstr("Exit_"+string(curwin)+"=Exitm") addmenu(curwin,MENU(1)) addmenu(curwin,MENU(2),menu_o) addmenu(curwin,MENU(3),menu_d) addmenu(curwin,MENU(4),menu_t) addmenu(curwin,MENU(5),menu_e) //=================================================================== drawlater(); a = gca(); a.data_bounds = rect; a.axes_visible = "on"; a.clip_state = "on"; xtitle( "", "time", "Output" ) ; a.title.font_size=2; a.title.font_style=4; a.title.foreground=2; a.grid=[2 2]; xpolys(xy(:,1),xy(:,2),[-1]); //children(2) xpolys(xy(:,1),xy(:,2),[5]); //children(1) splines = a.children(1).children points = a.children(2).children //--------------------------------------- [rpar,ipar]=AutoScale(a,xy,ipar,rpar) drawnow(); // -- boucle principale lines(0); while %t then //================================================= N = size(xy,"r"); [btn,xc,yc,win,Cmenu] = get_click(); //** see if ((win>0) & (win<>curwin)) then Cmenu="Mouse click is Offside!"; end if Cmenu==[] then Cmenu="edit", end if (Cmenu=="Exit") |(Cmenu=="Quit" ) then, ipar=[]; rpar=[]; ok=%f; return; end //------------------------------------------------------------------- if ((Cmenu=="zero order") | (Cmenu=="linear") | (Cmenu=="order 2")| ... (Cmenu=="not_a_knot")| (Cmenu=="periodic")| (Cmenu=="monotone")| ... (Cmenu=="fast")| (Cmenu=="clamped")) then select Cmenu case "zero order" then NOrder=0; case "linear" then NOrder=1; case "order 2" then NOrder=2; case "not_a_knot" then NOrder=3; case "periodic" then NOrder=4; case "monotone" then NOrder=5; case "fast" then NOrder=6; case "clamped" then NOrder=7; end ipar(2)=NOrder; [rpar,ipar]=AutoScale(a,xy,ipar,rpar) end //------------------------------------------------------------------- select Cmenu case "Data Bounds" then rectx=findrect(a); [mok, xmn1, xmx1, ymn1, ymx1] = scicos_getvalue("Enter new bounds",["xmin";"xmax"; "ymin";"ymax"], .. list("vec", 1,"vec", 1,"vec", 1,"vec", 1), string(rectx(:))) //drawlater(); if mok then if (xmn1 > xmx1 | ymn1 > ymx1) then xinfo("Incorrect bounds") mok=%f; end if xmn1<0 then xinfo("X should be positive") mok=%f; end if mok then a.data_bounds=[xmn1, ymn1; xmx1, ymx1]; end end //drawnow(); //------------------------------------------------------------------- case "Autoscale" then [rpar,ipar]=AutoScale(a,xy,ipar,rpar) //------------------------------------------------------------------- case "Periodic signal" then if PeridicOption==1 then, ans0="y", else, ans0="n", end; [mok,myans]=scicos_getvalue("Generating periodic signal",["y/n"],list("str",1),list(ans0)); if ((myans=="y")|(myans=="Y")) then, PeridicOption=1, else, PeridicOption=0; end; ipar(3)=PeridicOption; [rpar,ipar]=AutoScale(a,xy,ipar,rpar) //------------------------------------------------------------------- case "sine" then [mok,Amp,wp,phase,offset,np1,Sin_exprs2]=scicos_getvalue(" Sine parameters", ... ["Amplitude";"Frequency(rad/sec)"; ... "Phase(rad)";"Bias";"number of points"],list("vec",1,"vec",1,"vec",1, ... "vec",1,"vec",1),Sin_exprs) if np1< 2 then np1=2; end if mok & wp>0 then NOrder=3; ipar(2)=NOrder; phase=atan(tan(phase)); xt=linspace(0,%pi*2/wp,np1)'; yt=Amp*sin(wp*xt+phase)+offset; xy=[xt,yt]; [rpar,ipar]=AutoScale(a,xy,ipar,rpar) Sin_exprs=Sin_exprs2 end //------------------------------------------------------------------- case "sawtooth1" then [mok,sAmp,sTp,sdelay,Sawt1_exprs2]=scicos_getvalue("Sawtooth signal parameters", ... ["Amplitude";"Period";"delay"], ... list("vec",1,"vec",1,"vec",1),Sawt1_exprs) if mok & sTp>0 then NOrder=1; ipar(2)=NOrder; if sdelay<sTp then xt=[0;sdelay;sTp]; yt=[0;0;sAmp]; else xt=[0]; yt=[0]; end xy=[xt,yt]; [rpar,ipar]=AutoScale(a,xy,ipar,rpar); Sawt1_exprs=Sawt1_exprs2 end //------------------------------------------------------------------- case "sawtooth2" then [mok,sAmp2,sTp2,Sawt2_exprs2]=scicos_getvalue("Sawtooth signal parameters", ... ["Amplitude";"Period"],list("vec",1,"vec",1),Sawt2_exprs) if mok & sTp2>0 then NOrder=1; ipar(2)=NOrder; xt=[0;sTp2]; yt=[sAmp2;-sAmp2]; xy=[xt,yt]; [rpar,ipar]=AutoScale(a,xy,ipar,rpar); Sawt2_exprs=Sawt2_exprs2 end //------------------------------------------------------------------- case "pulse" then [mok,Amp3,Tp3,Pw3,Pd3,Bias3,Pulse_exprs2] = scicos_getvalue("Square wave pulse signal", ... ["Amplitude";"Period (sec)";"Pulse width(% o"+... "f period)";"Phase delay (sec)";"Bias"],list("vec",1, ... "vec",1,"vec",1,"vec",1,"vec",1),Pulse_exprs); if mok & Tp3>0 then NOrder=0; ipar(2)=NOrder; if (Pd3>0) then xt=0; yt=Bias3; else xt=[]; yt=[]; end //otherwise there would be double points at 0 if Pd3<Tp3 then if Pw3>0 then xt=[xt;Pd3; Pw3*Tp3/100+Pd3;Tp3]; yt=[yt;Amp3+Bias3;Bias3;Bias3]; else xt=[0;Tp3];yt=[Bias3;Bias3]; end else xt=[0;Tp3];yt=[Bias3;Bias3]; end xy=[xt,yt]; [rpar,ipar]=AutoScale(a,xy,ipar,rpar); Pulse_exprs=Pulse_exprs2; end //------------------------------------------------------------------- case "random normal" then [mok,mean4,var4,seed4,sample4,np4,random_n_exprs2]=scicos_getvalue("Normal (Gaussian) random signal", ... ["Mean";"Variance";"Initial seed";"Sample time";"Number of points"],list("vec",1, ... "vec",1,"vec",1,"vec", ... 1,"vec",1),random_n_exprs) if mok & sample4>0 then NOrder=0; ipar(2)=NOrder; rand("normal"); rand("seed",seed4); xt=0:sample4:sample4*(np4-1); xt=xt(:); yt=mean4+sqrt(var4)*rand(np4,1); xy=[xt,yt]; [rpar,ipar]=AutoScale(a,xy,ipar,rpar); random_n_exprs2=random_n_exprs; end //------------------------------------------------------------------- case "random uniform" then [mok,min5,max5,seed5,sample5,np5,random_u_exprs2]=scicos_getvalue("Uniform random signal", ... ["Minimum";"Maximum";"Initial seed";"Sample time";"Number of points"],list("vec",1, ... "vec",1,"vec",1,"vec", ... 1,"vec",1),random_u_exprs) if mok & sample5>0 then NOrder=0; ipar(2)=NOrder; rand("uniform"); rand("seed",seed5); xt=0:sample5:sample5*(np5-1); xt=xt(:); yt=min5+(max5-min5)*rand(np5,1); xy=[xt,yt]; [rpar,ipar]=AutoScale(a,xy,ipar,rpar); random_u_exprs2=random_u_exprs; end //------------------------------------------------------------------- case "Save/Exit" then NOrder=ipar(2); PeridicOption=ipar(3); METHOD=getmethod(NOrder); if (METHOD=="periodic") then // periodic spline xy(N,2)=xy(1,2); end if (METHOD=="order 2" | METHOD=="not_a_knot"|METHOD=="periodic" | METHOD=="monotone"| METHOD=="fast" | METHOD=="clamped") then rpar=[xy(:,1);xy(:,2);rpar]; else if (METHOD=="zero order"|METHOD=="linear") rpar=[xy(:,1);xy(:,2);] end end ok=%t delete(f); return //------------------------------------------------------------------- case "Exit without save" then ipar=[]; rpar=[]; ok=%f delete(f); return //------------------------------------------------------------------- case "Clear" then xy=[0,0]; NOrder=0; ipar(2)=NOrder; [rpar,ipar]=AutoScale(a,xy,ipar,rpar) //---------------------------------------------------------------- case "Edit text data NOT IN USE" then // editvar xy; [mok,xt,yt]=scicos_getvalue("Enter x and y data",["x";"y"],list("vec",-1,"vec",-1),list(strcat(sci2exp(xy(:,1))),strcat(sci2exp(xy(:,2))))); if mok then, xy=[xt,yt]; [xy]=cleandata(xy), [rpar,ipar]=AutoScale(a,xy,ipar,rpar) end //--------------------------------------------------------------- case "Help" then t1="Mouse-left click: adding a new point" t2="Mouse-right click: remove a point" t3="Mouse-left double click: edit a point''s coordinates" t4="Mouse-left button press/drag/release: move a point" t5="Change the window size: ''Data'' menu -> ''Databounds''" messagebox([t1;t2;t3;t4;t5],"modal","info"); //--------------------------------------------------------------- case "Load from Excel" then [tok,xytt]=ReadExcel() if tok then xy=xytt; NOrder=1 ipar(2)=NOrder; [rpar,ipar]=AutoScale(a,xy,ipar,rpar) end //--------------------------------------------------------------- case "Load from text file" then [tok,xytt]=ReadFromFile() if tok then xy=xytt; NOrder=1 ipar(2)=NOrder; [rpar,ipar]=AutoScale(a,xy,ipar,rpar) end //--------------------------------------------------------------- case "Save to text file" then [sok]=SaveToFile(xy) //--------------------------------------------------------------- case "Replot" then if xy<>[] then drawlater(); points.data=xy; [rpar,ipar]=drawSplin(a,xy,ipar,rpar); drawnow() end //---------------------------------------------------------- case "edit" then HIT=%f if N<>0 then xt=xy(:,1); yt=xy(:,2); dist=((xt-ones(N,1)*xc))^2+((yt-ones(N,1)*yc))^2 [dca,k]=min(dist); rectx=a.data_bounds; ex=abs(rectx(2,1)-rectx(1,1))/80; ey=abs(rectx(2,2)-rectx(1,2))/80; if (abs(xc-xt(k))<ex & abs(yc-yt(k))<ey) then HIT=%t end end //_________________________ // if ~((NOrder==-1|NOrder==-2|NOrder==-3|NOrder==-4)) then if (~HIT)&(btn==0 | btn==3) then // add point if (xc>=0) then if (xc==0) then zz=find(x==0); xy(zz,:)=[]; end xy=[xy;xc,yc]; [xtt,k2]=gsort(xy(:,1),"r","i");xy=xy(k2,:) drawlater(); points.data=xy; [rpar,ipar]=drawSplin(a,xy,ipar,rpar); drawnow(); end end if (HIT)&(btn==2 | btn==5) then // remove point if (xy(k,1)>0) |( xy(k,1)==0 & (size(find(xy(:,1)==0),"*")>1)) then xy(k,:)=[]; end drawlater(); points.data = xy; [rpar,ipar] = drawSplin(a,xy,ipar,rpar); drawnow(); end if (HIT)&(btn==0) then // move point [xy,rpar,ipar] = movept(a,xy,ipar,rpar,k) end if (HIT)&(btn==10) then // change data:: double click [mok,xt,yt]=scicos_getvalue("Enter new x and y",["x";"y"],... list("vec",1,"vec",1),list(sci2exp(xy(k,1)),sci2exp(xy(k,2)))); if mok then xy(k,:) = [xt,yt]; [xy] = cleandata(xy) drawlater(); points.data=xy; [rpar,ipar]=AutoScale(a,xy,ipar,rpar) drawnow() end end // end //_________________________________ end //---------------------------------------------------------- end endfunction //======================================================================== function [orpar,oipar] = drawSplin(a,xy,iipar,irpar) N=size(xy,"r");// new size of xy x=xy(:,1); y=xy(:,2); points=a.children(2).children splines=a.children(1).children order=iipar(2); periodicoption=iipar(3); orpar=irpar; METHOD=getmethod(order); if periodicoption==1 then PERIODIC="periodic, T="+string(x(N)-x(1)); else PERIODIC="aperiodic"; end a.title.text=[string(N)+" points, "+"Method: "+METHOD+", "+PERIODIC]; if (N==0) then, return; end if (N==1) then, order=0; end // NP=50;// number of intermediate points between two data points [X,Y,orpar]=Do_Spline(N,order,x,y); if (periodicoption==1) then X=[X;X($)]; Y=[Y;Y(1)]; else xmx=max(points.data(:,1)); xmn=min(points.data(:,1)); XMX=max(0,xmx); XMN=max(0,xmn); xmx1=max(a.x_ticks.locations) XMX=max(XMX,xmx1); X=[X;XMX]; Y=[Y;Y($)]; end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! splines.data=[X,Y]; oipar=[N;iipar(2);periodicoption] endfunction //============================================================= function [xyt,orpar,oipar]=movept(a,xy,iipar,irpar,k) //on bouge un point existant points=a.children(2).children splines=a.children(1).children oipar=iipar orpar=irpar order=iipar(2); x=xy(:,1); y=xy(:,2); if (x(k)==0) then zz=find(x==0); x(zz)=[]; y(zz)=[]; ZERO_POINT=%t else x(k)=[]; y(k)=[]; ZERO_POINT=%f end btn=-1 while ~(btn==3 | btn==0| btn==10| btn==-5) rep=xgetmouse([%t %t]); xc=rep(1);yc=rep(2);btn=rep(3); if (ZERO_POINT) then xc=0; else if (xc<=0) then zz=find(x==0); x(zz)=[]; y(zz)=[]; ZERO_POINT=%t; xc=0; end end xt=[x;xc]; yt=[y;yc]; [xt,k2]=gsort(xt,"r","i");yt=yt(k2) xyt=[xt,yt]; drawlater(); points.data=xyt; [orpar,oipar]=drawSplin(a,xyt,oipar,orpar); drawnow() end endfunction //========================================================== function rectx = findrect(a) splines=a.children(1).children points=a.children(2).children if (points.data==[]) then rectx=a.data_bounds; return; end ymx1=max(splines.data(:,2)); ymn1=min(splines.data(:,2)) xmx=max(points.data(:,1)); xmn=min(points.data(:,1)); ymx=max(points.data(:,2)); ymn=min(points.data(:,2)); XMX=max(0,xmx); XMN=max(0,xmn); YMX=max(ymx,ymx1); YMN=min(ymn,ymn1); dx=XMX-XMN; dy=YMX-YMN if dx==0 then dx=max(XMX/2,1), end; XMX=XMX+dx/50 if dy==0 then dy=max(YMX/2,1), end; YMN=YMN-dy/50; YMX=YMX+dy/50; rectx=[XMN,YMN;XMX,YMX]; endfunction //============================================================ function [tok,xyo]=ReadExcel() TA=["A";"B";"C";"D";"E";"F";"G";"H";"I";"J";"K";"L";"M";"N";"O";"P"; ... "Q";"R";"S";"T";"U";"V";"W";"X";"Y";"Z";"a";"b";"c";"d";"e";"f"; ... "g";"h";"i";"j";"k";"l";"m";"n";"o";"p";"q";"r";"s";"t";"u";"v"; ... "w";"x";"y";"z"]; TN=["0","1","2","3","4","5","6","7","8","9"]; xyo=[]; tok=%f; while %t [zok,filen,sheetN,xa,ya]=scicos_getvalue("Excel data file ",["Filename";"Sheet #"+... " ";"X[start:Stop]";"Y[start:stop]"],list("str",1, ... "vec",1,"str",1, ... "str",1), ... list(["Classeur1.xls"],["1"],["C5:C25"],["D5:D25"])); if ~zok then break, end try [fd,SST,Sheetnames,Sheetpos] = xls_open(filen); catch xinfo("Scicos cannot find the excel file:"+filen); break; end try N=size(Sheetnames,"*"); if ((sheetN<=N) &(sheetN>0)) then [Value,TextInd] = xls_read(fd,Sheetpos(sheetN)) mclose(fd) end xa=strsubst(xa," ",""); px=strindex(xa,":"); ya=strsubst(ya," ",""); py=strindex(ya,":"); x1=part(xa,1:px-1); x2=part(xa,px+1:length(xa)); y1=part(ya,1:py-1); y2=part(ya,py+1:length(ya)); x1p=min(strindex(x1,TN)); if x1p==[] then, xinfo("Bad address in X:"+x1); break, end x11=part(x1,1:x1p-1); x12=part(x1,x1p:length(x1)); x2p=min(strindex(x2,TN)); if x2p==[] then, xinfo("Bad address in X:"+x2); break, end x21=par t(x2,1:x2p-1); x22=part(x2,x2p:length(x2)); y1p=min(strindex(y1,TN)); if y1p==[] then, xinfo("Bad address in Y:"+y1); break, end y11=part(y1,1:y1p-1); y12=part(y1,y1p:length(y1)); y2p=min(strindex(y2,TN)); if y2p==[] then, xinfo("Bad address in Y:"+y2); break, end y21=part(y2,1:y2p-1); y22=part(y2,y2p:length(y2)); // x11 x12: x21 x22 lx11=length(x11); lx21=length(x21); ly11=length(y11); ly21=length(y21) xstC=0; for i=1:lx11, xstC=xstC+modulo(find(TA==part(x11,lx11-i+1)),26)*26^(i-1); end xenC=0; for i=1:lx21, xenC=xenC+modulo(find(TA==part(x21,lx21-i+1)),26)*26^(i-1); end ystC=0; for i=1:ly11, ystC=ystC+modulo(find(TA==part(y11,ly11-i+1)),26)*26^(i-1); end yenC=0; for i=1:ly11, yenC=yenC+modulo(find(TA==part(y21,ly21-i+1)),26)*26^(i-1); end xstR=evstr(x12); xenR=evstr(x22); ystR=evstr(y12); yenR=evstr(y22); [mv,nv]=size(Value) if ~(xstR<=mv & xstR>0 & xenR<=mv & xenR>0&ystR<=mv & ystR>0&yenR<=mv&yenR>0 ) then xinfo("error in Row data addresses"); break end if ~(xstC<=nv & xstC>0 & xenC<=nv & xenC>0&ystC<=nv & ystC>0&yenC<=nv&yenC>0 ) then xinfo("error in Column data addresses"); break end xo=Value(min(xstR,xenR):max(xstR,xenR),min(xstC,xenC):max(xstC,xenC)); yo=Value(min(ystR,yenR):max(ystR,yenR),min(ystC,yenC):max(ystC,yenC)); [nx,mx]=size(xo);// adjusting the x and y size [ny,my]=size(yo); N=min(nx,ny); xo=xo(1:N,:); yo=yo(1:N,:); xyo=[xo,yo]; [xyo]=cleandata(xyo) tok=%t; break, catch xinfo(" Scicos cannot read your Excel file, please verify"+... " the parameters "); break end end endfunction //--------------------------------------------------------------- function [xyo]=cleandata(xye) xe=xye(:,1) ye=xye(:,2) [nx,mx]=size(xe);// adjusting the x and y size [ny,my]=size(ye); N=min(nx,ny); xe=xe(1:N,:); ye=ye(1:N,:); // checking for NULL data for i=1:N if (xe(i)<>xe(i)) then xinfo("x contains no data:x("+string(i)+")"); return; end if (ye(i)<>ye(i)) then xinfo("Y contains no data:y("+string(i)+")"); return; end end zz=find(xe<0); xe(zz)=[]; ye(zz)=[] if (find(xe==0)==[]) then // add zero point xe($+1)=0; ye($+1)=0; end [xo,k2]=gsort(xe,"r","i"); yo=ye(k2) xyo=[xo,yo]; endfunction //--------------------------------------------------------------- function [orpar,oipar] = AutoScale(a,xy,inipar,inrpar) drawlater(); oipar = inipar orpar = inrpar points = a.children(2).children splines = a.children(1).children points.data = xy; splines.data = xy; [orpar,oipar] = drawSplin(a,xy,oipar,orpar); rectx=findrect(a); a.data_bounds = rectx; drawnow() endfunction //============================ function METHOD = getmethod(order) select order case 0 then, METHOD="zero order" case 1 then, METHOD="linear" case 2 then, METHOD="order 2" case 3 then, METHOD="not_a_knot" case 4 then, METHOD="periodic" case 5 then, METHOD="monotone" case 6 then, METHOD="fast" case 7 then, METHOD="clamped" end endfunction //======================================= function [sok,xye] = ReadFromFile() xye=[];sok=%f; while %t [sok,filen,Cformat,Cx,Cy]=scicos_getvalue("Text data file ",["Filename";"Reading [C] f"+... "ormat";"Abscissa column";"Output"+... " column"],list("str",1,"str",1,"vec",1,"vec",1), ... list(["mydatafile.dat"],["%g %g"],["1"],["2"])); if ~sok then break, end px=strindex(Cformat,"%"); NC=size(px,"*"); if NC==[] then, xinfo("Bad format in reading data file"); sok=%f; break; end Lx=[]; try fd=mopen(filen,"r"); Lx=mfscanf(-1,fd,Cformat); mclose(fd); catch xinfo("Scicos cannot open the data file: " + filen); break; end [nD,mD] = size(Lx); if ((mD==0) | (nD==0)) then, xinfo("No data read"); sok=%f; break; end if (mD<>NC) then, xinfo("Bad format"); sok=%f; break; end xe=Lx(:,Cx); ye=Lx(:,Cy); xye=[xe,ye]; [xye]=cleandata(xye) sok=%t; break, end endfunction //======================================= function [sok]=SaveToFile(xye) xe=xye(:,1) ye=xye(:,2) sok=%f; while %t [sok,filen,Cformat]=scicos_getvalue("Text data file ",["Filename";"Writing [C] f"+... "ormat"],list("str",1,"str",1), ... list(["mydatafile.dat"],["%g %g"])); if ~sok then break, end px=strindex(Cformat,"%"); NC=size(px,"*"); if NC<>2 then, xinfo("Bad format in writing data file"); sok=%f; break; end Cformat=Cformat+"\n"; try fd=mopen(filen,"w"); mfprintf(fd,Cformat,xe,ye); mclose(fd); catch xinfo("Scicos cannot open the data file:"+filen); break; end sok=%t; break, end endfunction //========================================================= function [X,Y,orpar]=Do_Spline(N,order,x,y) X=[]; Y=[]; orpar=[]; METHOD=getmethod(order); if (METHOD=="zero order") then X=x(1); Y=y(1); for i=1:N-1 X=[X;x(i);x(i+1);x(i+1)]; Y=[Y;y(i);y(i);y(i+1)]; end return end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! if (METHOD=="linear") then X=[]; for i=1:N X=[X;x(i)]; Y=[Y;y(i)]; end return end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! if (N<25) then NP=10; else if (N<50) then NP=5; else if (N<100) then NP=2; else if (N<200) then NP=1; else NP=0; end; end; end; end for i=1:N-1 X=[X;linspace(x(i),x(i+1),NP+2)']; // pour tous sauf "linear" et "zero order" end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! if (N>2) & (METHOD=="order 2") then Z=ORDER2(x,y); A=Z(1:N-1); B=Z(N:2*N-2); C=Z(2*N-1:3*N-3); for j=1:size(X,"*") for i=N-1:-1:1 if X(j)>=x(i) then, break; end end Y(j)=A(i)*(X(j)-x(i))^2+B(i)*(X(j)-x(i))+C(i); end orpar=matrix(Z,-1,1) end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! if (METHOD=="not_a_knot") then try d = splin(x, y, METHOD); Y = interp(X, x, y, d); orpar=d(:); catch xinfo("ERROR in SPLINE: "+METHOD) end end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! if (METHOD=="periodic") then if y(1)<>y(N) then y(N)=y(1) end try d = splin(x, y,METHOD); Y = interp(X, x, y, d); orpar=d(:); catch xinfo("ERROR in SPLINE: "+METHOD) end end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! if (METHOD=="monotone" ) then try d = splin(x, y, METHOD); Y = interp(X, x, y, d); orpar=d(:); catch xinfo("ERROR in SPLINE: "+METHOD) end end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! if (METHOD=="fast") then try d = splin(x, y, METHOD); Y = interp(X, x, y, d); orpar=d(:); catch xinfo("ERROR in SPLINE: "+METHOD) end end //!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! if (METHOD=="clamped") then try d = splin(x, y, METHOD,[0;0]); Y = interp(X, x, y, d); orpar=d(:); catch xinfo("ERROR in SPLINE: "+METHOD) end end endfunction //================================================= function [Z]=ORDER2(x,y) N=size(x,"*")-1; A=zeros(3*N-1,N*3); B=zeros(3*N-1,1); for i=1:N j=3*(i-1)+1; A(j,i+2*N)=1; B(j)=y(i); A(j+1,i)=(x(i+1)-x(i))^2; A(j+1,i+N)=x(i+1)-x(i); A(j+1,i+2*N)=1; B(j+1)=y(i+1); end for i=1:N-1 j=3*(i-1)+1; A(j+2,i)=2*(x(i+1)-x(i)); A(j+2,i+N)=1; A(j+2,i+N+1)=-1; end Q=zeros(3*N,3*N); for i=1:N Q(i,i)=4*(x(i+1)-x(i))^2 Q(i,i+N)=2*(x(i+1)-x(i)) Q(i+N,i)=2*(x(i+1)-x(i)) Q(i+N,i+N)=1; end At=[Q,A';A,zeros(3*N-1,3*N-1)] Bt=[zeros(3*N,1);B] Zt=At\Bt; Z=Zt(1:3*N,1) endfunction //===================================================
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i=0.2; v1=120; f=60; v2=95; disp("Part a"); z1=v1/i; x_l=sqrt(z1^2-r^2); z2=v2/i; x_c=x_l-sqrt(z2^2-r^2); c=1/(2*%pi*f*x_c); disp("the size of capacitance (in μF) needed is"); disp(c*10^6); disp("Part b"); vc=i*x_c; disp("voltage (in V) across capacitor is");disp(vc); disp("Part c"); v=i*z1; disp("voltage (in V) across solenoid is"); disp(v);
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// Exa 5.10 clc; clear; close; // Given data Vin= 10;// in volt R=2.2;// in k ohm R=R*10^3;//in ohm Ad=10^5;// voltage gain T= 1;// in ms T=T*10^-3;// in second C=1;// in micro F C=C*10^-6;// in F I= Vin/R;// in volt V= I*T/C;// in V disp(V,"The output voltage at the end of the pulse in volt"); RC_desh= R*C*Ad; disp(RC_desh,"The closed-loop time constant in second is");
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clc //initialization of varaibles disp("From psychrometric charts,") e=0.7 phi=0.5 g1=0.0131 //lb water/lb dry air h1=32.36 //B/lb of dry air g3=0.0073 h3=24.26 pg=0.3390 T3=528 //R V3=1000 Rw=85.8 //calculations pw3=phi*pg ww3=pw3*144*V3/(Rw*T3) wa3=ww3/g3 wa1=phi*wa3 wa2=phi*wa3 ww1=g1*wa1 ww2=ww3-ww1 g2=ww2/wa2 h2=(wa3*h3-wa1*h1)/wa2 tdb=61 //F //results printf("Air supplied = %.3f lb/min",ww2) printf("\n temperature = %d F",tdb) printf("\n Humidity = %.5f lb water/lb dry air",g2)
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// Scilab code Exa4.5.8: To determine the threshold energy for given reaction : P.no. 185 (2011) // Na(11,23)+ n > F(9,20)+ He(2,4) is the reaction M_Na_23 = 22.99097; // Mass of Na-23, amu M_n_1 =1.00866 ; // Mass of n-1, amu Q = -5.4; // Q-value, MeV E_th = -Q*(M_Na_23+M_n_1)/M_Na_23; // Threshold energy, MeV printf("\nThe threshold energy for the reaction : %4.2f MeV ", E_th) // Result // The threshold energy for the reaction : 5.64 MeV
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//example 14.34 //calculate concentration at point 10 cm above the bed clc;funcprot(0); //given D=2.8; //depth of flow c_=700; //concentration at 30 cm below water surface y=0.1; a=D-0.3; e=0.4; //exponent in rouse equation; c=c_*(a*(D-y)/(y*(D-a)))^e; mprintf("concentration at point 10 cm above the bed=%i ppm.",c);
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function y=f(x) y=-sin(x^2)/x endfunction x=[0.001:0.02:2*%pi]; clf; plot(x,f,"r")
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function demo_scatterly_sin() x=[0:0.1:2*%pi]; y=2*sin(x); scatterly(x,y) endfunction demo_scatterly_sin(); clear demo_scatterly_sin;
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clc; g1=1.5; // gain factor of amplifier g2=80; // gain factor of generator vo=250; // output voltage at no load s=0.2; // feedback potentiometer setting // for generated voltage= 80V field current is 1 A ifl=vo/g2; // field current for generated voltage= 250V vi=ifl/g1; // amplifier input voltage for field current corresponding to generated voltage= 250V vfb=s*vo; // feedback voltage vr=vfb+vi; printf('Reference voltage for given potentiometer setting is %f V\n',vr); printf('When feedback setting is zero, reference voltage is %f V',vi);
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// Calculate the value of resistance after 15s clc; R0=29.44; Rs=100; t=15; tc=5.5; R_15=Rs+R0*[1-exp(-t/tc)]; disp(R_15,'value of resistance after 15s(ohm)')
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clc //initialisation of variables clear p1= 10 //atm p2= 1 //atm T1= 25 //C n= 2/5 //CALCULATIONS T2= (p1/p2)^n*(273+T1)-273 //RESULTS printf ('Final temperature = %.f C',T2)
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syms I R C s V1=I*(R+1/(s*C)) V2=I*(1/(s*C)) disp(V2/V1,"V2/V1 = ")
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//scilab 5.4.1 clear; clc; printf("\t\t\tProblem Number 11.26\n\n\n"); // Chapter 11 : Heat Transfer // Problem 11.26 (page no. 603) // Solution //From the table 11.7, //For the oil side,a resistance(fouling factor) of 0.005 (hr*F*ft^2)/Btu can be used //and for the water side,a fouling factor of 0.001 (hr*F*ft^2)/Btu can be used //From problem 11.25, U=40;//The coefficient of heat transfer of the unit //Unit:Btu/(hr*ft^2*F) //therefore, Roil=0.005; //unit:(hr*ft^2*F)/Btu //resistance at oil side Rwater=0.001; //unit:(hr*ft^2*F)/Btu //resistance for water side Rcleanunit=inv(U); //unit:(hr*ft^2*F)/Btu //resistance at clean unit Roverall=Roil+Rwater+Rcleanunit; //unit:(hr*ft^2*F)/Btu //overall resistance Uoverall=inv(Roverall); //Unit:Btu/(hr*ft^2*F) //The overall coefficient of heat transfer of the unit //Because all the parameters are the same,the surface area required will vary inversely as U A=569*(U/Uoverall); //A=569 ft^2 in the problem 11.25 //unit:ft^2 //The outside surface area printf("The outside surface area required is %f ft^2",A);
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Expanding for base=2, level=6, reasons+features=base,same,similiar invall,norm Refined variables=x,y [0+1x,0+1y]: unknown -> [1] [0,0] x²-y³+3 ---------------- level 0 expanding queue[0]^-1,meter=[2,2]: x²-y³+3 [1+2x,0+2y]: unknown -> [1] [1,0] x+x²-2y³+1 [0+2x,1+2y]: unknown -> [2] [0,1] 2x²-3y-6y²-4y³+1 endexp[0] ---------------- level 1 expanding queue[1]^0,meter=[2,2]: x+x²-2y³+1 endexp[1] expanding queue[2]^0,meter=[2,2]: 2x²-3y-6y²-4y³+1 [0+4x,3+4y]: unknown -> [3] [0,1] 4x²-27y-36y²-16y³-6 [2+4x,3+4y]: unknown -> [4] [1,1] 4x+4x²-27y-36y²-16y³-5 endexp[2] ---------------- level 2 expanding queue[3]^2,meter=[2,2]: 4x²-27y-36y²-16y³-6 [0+8x,3+8y]: unknown -> [5] [0,0] 8x²-27y-72y²-64y³-3 [4+8x,3+8y]: unknown -> [6] [1,0] 8x+8x²-27y-72y²-64y³-1 endexp[3] expanding queue[4]^2,meter=[2,2]: 4x+4x²-27y-36y²-16y³-5 [2+8x,7+8y]: unknown -> [7] [0,1] 4x+8x²-147y-168y²-64y³-42 [6+8x,7+8y]: unknown -> [8] [1,1] 12x+8x²-147y-168y²-64y³-38 endexp[4] ---------------- level 3 expanding queue[5]^3,meter=[2,2]: 8x²-27y-72y²-64y³-3 [0+16x,11+16y]: unknown -> [9] [0,1] 16x²-363y-528y²-256y³-83 [8+16x,11+16y]: unknown -> [10] [1,1] 16x+16x²-363y-528y²-256y³-79 endexp[5] expanding queue[6]^3,meter=[2,2]: 8x+8x²-27y-72y²-64y³-1 [4+16x,11+16y]: unknown -> [11] [0,1] 8x+16x²-363y-528y²-256y³-82 [12+16x,11+16y]: unknown -> [12] [1,1] 24x+16x²-363y-528y²-256y³-74 endexp[6] expanding queue[7]^4,meter=[2,2]: 4x+8x²-147y-168y²-64y³-42 [2+16x,7+16y]: unknown -> [13] [0,0] 4x+16x²-147y-336y²-256y³-21 [10+16x,7+16y]: unknown -> [14] [1,0] 20x+16x²-147y-336y²-256y³-15 endexp[7] expanding queue[8]^4,meter=[2,2]: 12x+8x²-147y-168y²-64y³-38 [6+16x,7+16y]: unknown -> [15] [0,0] 12x+16x²-147y-336y²-256y³-19 [14+16x,7+16y]: unknown -> [16] [1,0] 28x+16x²-147y-336y²-256y³-9 endexp[8] ---------------- level 4 expanding queue[9]^5,meter=[2,2]: 16x²-363y-528y²-256y³-83 [0+32x,27+32y]: unknown -> [17] [0,1] 32x²-2187y-2592y²-1024y³-615 [16+32x,27+32y]: unknown -> [18] [1,1] 32x+32x²-2187y-2592y²-1024y³-607 endexp[9] expanding queue[10]^5,meter=[2,2]: 16x+16x²-363y-528y²-256y³-79 [8+32x,27+32y]: unknown -> [19] [0,1] 16x+32x²-2187y-2592y²-1024y³-613 [24+32x,27+32y]: unknown -> [20] [1,1] 48x+32x²-2187y-2592y²-1024y³-597 endexp[10] expanding queue[11]^6,meter=[2,2]: 8x+16x²-363y-528y²-256y³-82 [4+32x,11+32y]: unknown -> [21] [0,0] 8x+32x²-363y-1056y²-1024y³-41 [20+32x,11+32y]: unknown -> [22] [1,0] 40x+32x²-363y-1056y²-1024y³-29 endexp[11] expanding queue[12]^6,meter=[2,2]: 24x+16x²-363y-528y²-256y³-74 [12+32x,11+32y]: unknown -> [23] [0,0] 24x+32x²-363y-1056y²-1024y³-37 [28+32x,11+32y]: unknown -> [24] [1,0] 56x+32x²-363y-1056y²-1024y³-17 endexp[12] expanding queue[13]^7,meter=[2,2]: 4x+16x²-147y-336y²-256y³-21 [2+32x,23+32y]: unknown -> [25] [0,1] 4x+32x²-1587y-2208y²-1024y³-380 [18+32x,23+32y]: unknown -> [26] [1,1] 36x+32x²-1587y-2208y²-1024y³-370 endexp[13] expanding queue[14]^7,meter=[2,2]: 20x+16x²-147y-336y²-256y³-15 [10+32x,23+32y]: unknown -> [27] [0,1] 20x+32x²-1587y-2208y²-1024y³-377 [26+32x,23+32y]: unknown -> [28] [1,1] 52x+32x²-1587y-2208y²-1024y³-359 endexp[14] expanding queue[15]^8,meter=[2,2]: 12x+16x²-147y-336y²-256y³-19 [6+32x,23+32y]: unknown -> [29] [0,1] 12x+32x²-1587y-2208y²-1024y³-379 [22+32x,23+32y]: unknown -> [30] [1,1] 44x+32x²-1587y-2208y²-1024y³-365 endexp[15] expanding queue[16]^8,meter=[2,2]: 28x+16x²-147y-336y²-256y³-9 [14+32x,23+32y]: unknown -> [31] [0,1] 28x+32x²-1587y-2208y²-1024y³-374 [30+32x,23+32y]: unknown -> [32] [1,1] 60x+32x²-1587y-2208y²-1024y³-352 endexp[16] ---------------- level 5 expanding queue[17]^9,meter=[2,2]: 32x²-2187y-2592y²-1024y³-615 [0+64x,59+64y]: unknown -> [33] [0,1] 64x²-10443y-11328y²-4096y³-3209 [32+64x,59+64y]: unknown -> [34] [1,1] 64x+64x²-10443y-11328y²-4096y³-3193 endexp[17] expanding queue[18]^9,meter=[2,2]: 32x+32x²-2187y-2592y²-1024y³-607 [16+64x,59+64y]: unknown -> [35] [0,1] 32x+64x²-10443y-11328y²-4096y³-3205 [48+64x,59+64y]: unknown -> [36] [1,1] 96x+64x²-10443y-11328y²-4096y³-3173 endexp[18] expanding queue[19]^10,meter=[2,2]: 16x+32x²-2187y-2592y²-1024y³-613 [8+64x,59+64y]: unknown -> [37] [0,1] 16x+64x²-10443y-11328y²-4096y³-3208 [40+64x,59+64y]: unknown -> [38] [1,1] 80x+64x²-10443y-11328y²-4096y³-3184 endexp[19] expanding queue[20]^10,meter=[2,2]: 48x+32x²-2187y-2592y²-1024y³-597 [24+64x,59+64y]: unknown -> [39] [0,1] 48x+64x²-10443y-11328y²-4096y³-3200 [56+64x,59+64y]: unknown -> [40] [1,1] 112x+64x²-10443y-11328y²-4096y³-3160 endexp[20] expanding queue[21]^11,meter=[2,2]: 8x+32x²-363y-1056y²-1024y³-41 [4+64x,43+64y]: unknown -> [41] [0,1] 8x+64x²-5547y-8256y²-4096y³-1242 [36+64x,43+64y]: unknown -> [42] [1,1] 72x+64x²-5547y-8256y²-4096y³-1222 endexp[21] expanding queue[22]^11,meter=[2,2]: 40x+32x²-363y-1056y²-1024y³-29 [20+64x,43+64y]: unknown -> [43] [0,1] 40x+64x²-5547y-8256y²-4096y³-1236 [52+64x,43+64y]: unknown -> [44] [1,1] 104x+64x²-5547y-8256y²-4096y³-1200 endexp[22] expanding queue[23]^12,meter=[2,2]: 24x+32x²-363y-1056y²-1024y³-37 [12+64x,43+64y]: unknown -> [45] [0,1] 24x+64x²-5547y-8256y²-4096y³-1240 [44+64x,43+64y]: unknown -> [46] [1,1] 88x+64x²-5547y-8256y²-4096y³-1212 endexp[23] expanding queue[24]^12,meter=[2,2]: 56x+32x²-363y-1056y²-1024y³-17 [28+64x,43+64y]: unknown -> [47] [0,1] 56x+64x²-5547y-8256y²-4096y³-1230 [60+64x,43+64y]: unknown -> [48] [1,1] 120x+64x²-5547y-8256y²-4096y³-1186 endexp[24] expanding queue[25]^13,meter=[2,2]: 4x+32x²-1587y-2208y²-1024y³-380 [2+64x,23+64y]: unknown -> [49] [0,0] 4x+64x²-1587y-4416y²-4096y³-190 [34+64x,23+64y]: unknown -> [50] [1,0] 68x+64x²-1587y-4416y²-4096y³-172 endexp[25] expanding queue[26]^13,meter=[2,2]: 36x+32x²-1587y-2208y²-1024y³-370 [18+64x,23+64y]: unknown -> [51] [0,0] 36x+64x²-1587y-4416y²-4096y³-185 [50+64x,23+64y]: unknown -> [52] [1,0] 100x+64x²-1587y-4416y²-4096y³-151 endexp[26] expanding queue[27]^14,meter=[2,2]: 20x+32x²-1587y-2208y²-1024y³-377 [10+64x,55+64y]: unknown -> [53] [0,1] 20x+64x²-9075y-10560y²-4096y³-2598 [42+64x,55+64y]: unknown -> [54] [1,1] 84x+64x²-9075y-10560y²-4096y³-2572 endexp[27] expanding queue[28]^14,meter=[2,2]: 52x+32x²-1587y-2208y²-1024y³-359 [26+64x,55+64y]: unknown -> [55] [0,1] 52x+64x²-9075y-10560y²-4096y³-2589 [58+64x,55+64y]: unknown -> [56] [1,1] 116x+64x²-9075y-10560y²-4096y³-2547 endexp[28] expanding queue[29]^15,meter=[2,2]: 12x+32x²-1587y-2208y²-1024y³-379 [6+64x,55+64y]: unknown -> [57] [0,1] 12x+64x²-9075y-10560y²-4096y³-2599 [38+64x,55+64y]: unknown -> [58] [1,1] 76x+64x²-9075y-10560y²-4096y³-2577 endexp[29] expanding queue[30]^15,meter=[2,2]: 44x+32x²-1587y-2208y²-1024y³-365 [22+64x,55+64y]: unknown -> [59] [0,1] 44x+64x²-9075y-10560y²-4096y³-2592 [54+64x,55+64y]: unknown -> [60] [1,1] 108x+64x²-9075y-10560y²-4096y³-2554 endexp[30] expanding queue[31]^16,meter=[2,2]: 28x+32x²-1587y-2208y²-1024y³-374 [14+64x,23+64y]: unknown -> [61] [0,0] 28x+64x²-1587y-4416y²-4096y³-187 [46+64x,23+64y]: unknown -> [62] [1,0] 92x+64x²-1587y-4416y²-4096y³-157 endexp[31] expanding queue[32]^16,meter=[2,2]: 60x+32x²-1587y-2208y²-1024y³-352 [30+64x,23+64y]: unknown -> [63] [0,0] 60x+64x²-1587y-4416y²-4096y³-176 [62+64x,23+64y]: unknown -> [64] [1,0] 124x+64x²-1587y-4416y²-4096y³-130 endexp[32] ---------------- level 6 Maximum level 6 [65] mod 2: x²-y³+3
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1*a^1 + 1*b^1 > 0; 1*a^1 - 1*b^1 > 0; 1*a^1 > 0 evaluate: failure biased
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Ex4_2.sce
clear // //The composite figure is divided into three simple figures and taking A as origin coordinates of their centroids //variable declaration L1=400.0 //length of wire AB,mm L2=150.0*%pi //length of wire BC,mm L3=250.0 //length of wire CD,mm theta=30*%pi/180 //The wire is divided into three segments AB, BC and CD. Taking A as origin the coordinates of the centroids of AB, BC and CD are (X1,Y1),(X2,Y2),(X3,Y3) X1=200.0 X2=475.0 X3=400+300.0+250*cos(theta)/2 Y1=0 Y2=2*150/%pi Y3=125*sin(theta) L=L1+L2+L3 //Total length,mm xc=(L1*X1+L2*X2+L3*X3)/L printf("\n xc= %0.2f mm",xc) yc=(L1*Y1+L2*Y2+L3*Y3)/L printf("\n yc= %0.2f mm",yc)
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[[-1,2,-1,0,0],[1,2,-1,1,0],[2,-2,1,-1,0],[2,-1,2,0,0]] [0,1,0,1]*3 [-2,15,9,16]*2 [-12,43,38,51]*3 [-12,31,33,40]*12 [-80,171,204,235]*5 [-150,283,365,408]*6 [-84,145,198,217]*21 [[-1,2,1,1,0],[1,2,1,0,0],[2,1,2,0,0],[2,2,1,1,0]] [3,4,5,6] [1,6,8,9]*6 [-5,48,69,76]*3 [-27,100,152,165]*4 [-23,60,95,102]*15 [-137,294,480,511]*6 [-237,448,749,792]*7 [[0,-1,2,-1,0],[0,1,2,-1,1],[0,2,-2,1,-1],[0,2,-1,2,0]] [0,1,0,1]*3 [-2,15,9,16] [-12,43,38,51] [-12,31,33,40]*3 [-80,171,204,235] [-150,283,365,408] [-84,145,198,217]*3 [[0,-1,2,1,1],[0,1,2,1,0],[0,2,1,2,0],[0,2,2,1,1]] [3,4,5,6] [1,6,8,9]*3 [-5,48,69,76] [-27,100,152,165] [-23,60,95,102]*3 [-137,294,480,511] [-237,448,749,792] [[0,0,1,-2,1],[0,0,2,-1,2],[0,1,-1,2,-2],[0,1,-1,2,1]] [0,1,0,1]*3 [1,8,6,9] [4,17,22,25] [3,10,18,19]*3 [16,47,108,111] [25,68,190,193] [12,31,102,103]*3 [[0,0,1,2,1],[0,0,2,1,2],[0,1,1,2,-1],[0,1,1,2,2]] [4,5,3,6] [3,4,5,6]*3 [16,23,41,44] [25,38,87,90] [12,19,53,54]*3 [49,80,263,266] [64,107,405,408] [[0,1,-2,-1,-1],[0,2,2,1,1],[1,1,2,-1,0],[1,1,2,2,0]] [-1,2,1,2]*3 [-1,9,10,12]*3 [5,76,123,132] [9,55,116,120]*3 [23,102,265,270]*3 [137,511,1578,1596] [79,264,945,952]*3 [[0,1,0,0,-1],[0,2,0,0,1],[1,0,0,-1,0],[1,0,0,2,0]] [0,1,0,1]*3 [7,17,14,20] [26,55,78,87] [21,43,84,88]*3 [124,251,620,635] [215,433,1290,1308] [114,229,798,805]*3 [[0,1,-2,1,0],[0,2,-1,2,0],[1,-1,2,-2,0],[1,-1,2,1,0]] [0,1,0,1]*3 [1,8,6,9]*2 [4,17,22,25]*3 [3,10,18,19]*12 [16,47,108,111]*5 [25,68,190,193]*6 [12,31,102,103]*21 [[0,1,2,1,0],[0,2,1,2,0],[1,1,2,-1,0],[1,1,2,2,0]] [4,5,3,6] [3,4,5,6]*6 [16,23,41,44]*3 [25,38,87,90]*4 [12,19,53,54]*15 [49,80,263,266]*6 [64,107,405,408]*7 [[0,1,2,-1,1],[0,2,-2,1,-1],[1,-1,2,-2,0],[1,-1,2,1,0]] [1,0,0,1]*3 [5,3,4,6]*3 [43,38,66,75] [31,33,72,76]*3 [57,68,180,185]*3 [283,365,1140,1158] [145,198,714,721]*3 [[0,1,0,0,1],[0,2,0,0,-1],[1,0,0,-2,0],[1,0,0,1,0]] [2,1,-1,2] [3,5,4,6]*3 [28,53,75,84] [65,127,248,260] [42,83,205,210]*3 [217,431,1284,1302] [344,685,2387,2408] #---> reslines=12
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// chapter 7 example 5 //----------------------------------------------------------------------------- clc; clear; // given data Ptot = 100; // certain antenna radiating power Ptot_iso = 10*10^3; // isotropic antenna radiating power // Calculations D = 10*log10(Ptot_iso/Ptot); // Directivity of antenna // Output mprintf('Directivity of antenna = %d dB',D); //------------------------------------------------------------------------------
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Ex9_27.sce
clear //Given A=10**-3 //m** n=10 I=2 //A B=0.1 //T //Calculation // t=n*I*A*B*cos(0) t1=n*I*A*B*cos(60*3.14/180.0) //Result printf("\n (i) Torque when magnetic field is parallel to the field %0.0f *10**-3 Nm",t*10**3) printf("\n (ii) Torque when magnetic field is perpendicular to the field is zero") printf("\n (iii) Torque when magnetic field is 60 degree to the field is %0.1f *10**-3 Nm",t1*10**3)
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clear; clc; close; w=0.4;//in micrometer l=100;//in nanometer Cg=1.6;//in fF/micrometer Ct=Cg*w; Cgs1=0;Cgd1=0;Cgb1=Ct/2;//cutoff Cgs2=Ct/2;Cgd2=Ct/2;Cgb2=0;//linear Cgs3=(2*Ct)/3;Cgb3=0;Cgd3=0;//saturation disp(Cgs1,'Cgs for cutoff region');//units in fF disp(Cgd1,'Cgd for cutoff region'); disp(Cgb1,'Cgb for cutoff region'); disp(Cgs2,'Cgs for linear region'); disp(Cgd2,'Cgd for linear region'); disp(Cgb2,'Cgb for linear region'); disp(Cgs3,'Cgs for saturation region'); disp(Cgd3,'Cgs for saturation region'); disp(Cgb3,'Cgs for saturation region');
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clc // Given that E = 5e-19 // energy of photon in J h = 6.62e-34 // Planck constant in J-sec c = 3e8 // speed of light in m/sec e = 1.6e-19 // charge on an electron in C // Sample Problem 5 on page no. 14.21 printf("\n # PROBLEM 5 # \n") printf("Standard formula used \n") printf(" E = h*c/lambda \n") lambda = c * h / E printf("\n Wavelength is %f Angstrom.",lambda * 10^10)
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clear clc disp("example 8.6") mh=205//mean height a=1000*10^6//in miters r=1.25//annual rain fall er=0.8//efficiency lf=0.75//load factor hl=5//head loss et=0.9//efficiency of turbine eg=0.95//efficiency of generator wu=a*r*er/(365*24*3600) printf("\nwater used is \t\t%fm^3/sec",wu) eh=mh-hl printf("\neffective head is \t%dm",eh) p=(735.5/75)*(wu*eh*et*eg) printf("\npower generated is \t%fkW =\t%fMW",p,p/1000) pl=p/lf printf("\npeak load is \t\t%fMw \ntherefore the MW rating of station is \t%fMW",pl/1000,pl/1000) if eh<=200 then printf("\nfor a head above 200m pelton turbine is suitable,\nfrancis turbine is suitable in the range of 30m-200m.,\nhowever pelton is most suitable") else printf("only pelton turbine is most suitable") end
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V=32 I=1 R1=20 R2=8 R3=2 Voc1=V/(R1+R2+R3)*(R2+R3) ///a,b open Isc1=V/R1 ///a,b short Voc2=I*R2/(R1+R2+R3)*R1 Isc2=I*R2/(R2+R3) ////by superposition Voc=Voc1+Voc2 Isc=Isc1+Isc2 disp(Voc) disp(Isc)
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clc; clear all; //page no 157 //prob no. 5.6 fLO=110; //MHz //for V2(f) f=[0:.01:231+.01]; //x axis function V=pulse() V=[] for i=1:.005:1.5 V=[V i] end endfunction V2=[zeros(0:.01:120-fLO-.01) pulse() zeros(121-fLO+.01:.01:120+fLO-.01) pulse() 0]; //y axis clf; subplot(211); plot2d(f,V2,[5],rect=[0,0,240,2]) xtitle('Spectral diagram','f,MHz','V2(f)'); //for V3(f) f=[0:.01:11+.01]; //x axis V3=[zeros(0:.01:120-fLO-.01) pulse() 0]; //y axis subplot(212); plot2d(f,V3,[5],rect=[0,0,20,2]) xtitle('Spectral Diagram','f,MHz','V3(f)');
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function[e,xn,a,b,c]=newton(x) a=(x^3)-(0.165*(x^2))+(3.993*(10^-4)); b=(3*x^2)-(0.33*x); xn=x-(a/b); e=abs((xn-x)/xn)*100; if(e>0) then newton(xn); else disp(xn); disp(e); end endfunction
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//Example 5// Ch 12 clc; clear; close; // given data C2 = 0.75/3;//capacitance between 3 core bunched together and lead sheath in uF/km C3=0.56//in uf/km V=33*10^3; f=50;//in Hz C4=0.5*(C2+C3)*10;//capacitance per km b/w any two cores printf("capacitance per km b/w any two cores %f uF",C4) ChargKVAr=V^2*2*%pi*f*C4/10^9; printf("Charging KVAr %f KVAr",ChargKVAr) //given ans in book is wrong the capacitance of 10km b/w 2 cores is 4.05uF
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// for open loop system // given speed=60km/hr syms R K1 K; (R*K1*K)=60 K1=50; K=1.5; R=60/(K1*K) disp(R,"Input open=") // for closed loop R=60(1+(K1*K))/(K1*K) disp(R,"Input closed=")
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//Chapter 26 clc //Example4 //given c=3*10^8 //velocity of light in m/sec //when the spaceship is at rest x=52 // diatance in x direction in meters y=25 //measurement in y direction v=0.95*c //when the spaceship moves to an observer at rest only x dimension looks contracted gamma=1/sqrt(1-(v^2/c^2)) L=x/gamma disp(L,"The observer sees the horizontal dimension of the spaceship gets contracted to a length in meters of")
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//example 5.7 //calculate discharge and percent increase in discharge clc; //given k=0.005; //coefficient of permeability r=0.1; //well radius s=4; //drawdown b=10; //thickness R=300; //radius of circle of influence //Part(a) Q1=2.72*b*k*s/log10(R/r); Q1=round(Q1*10000)/10000; mprintf("Discharge=%f cumec",Q1); //Part (b) r=0.2; Q2=2.72*b*k*s/log10(R/r); I=(Q2-Q1)*100/Q1; I=round(I*10)/10; mprintf("\npercent increase in discharge=%f percent.",I);
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clear; clc; disp('Example 4.2'); // aim : To determine // saturation temperature and enthalpy // Given values P = 2.04;// pressure, [MN/m^2] // solution // since in the steam table values of enthalpy and saturation temperature at 2 and 2.1 MN?m^2 are given, so for knowing required values at given pressure,there is need to do interpolation // calculation of saturation temperature // from steam table Table_P_tf = [[2.1,2.0];[214.9,212.4]]; // P in [MN/m^2] and tf in [C] // using interpolation tf = interpln(Table_P_tf,2.04);// saturation temperature at given condition mprintf('\n The Saturation temperature is = %f C \n',tf); // calculation of specific liquid enthalpy // from steam table Table_P_hf = [[2.1,2.0];[920.0,908.6]];// P in [MN/m^2] and hf in [kJ/kg] // using interpolation hf = interpln(Table_P_hf,2.04); // enthalpy at given condition, [kJ/kg] mprintf('\n The Specific liquid enthalpy is = %f kJ/kg \n',hf); // calculation of specific enthalpy of evaporation // from steam table Table_P_hfg = [[2.1,2.0];[1878.2,1888.6]];// P in [MN/m^2] and hfg in [kJ/kg] // using interpolation hfg = interpln(Table_P_hfg,2.04); // enthalpy at given condition, [kJ/kg] mprintf('\n The Specific enthalpy of evaporation is = %f kJ/kg \n',hfg); // calculation of specific enthalpy of dry saturated steam // from steam table Table_P_hg = [[2.1,2.0];[2798.2,2797.2]];//P in [MN/m^2] and hg in [kJ/kg] // using interpolation hg = interpln(Table_P_hg,2.04); // enthalpy at given condition, [kJ/kg] mprintf('\n The Specific enthalpy of dry saturated steam is = %f kJ/kg \n',hg); // End
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clc D = 12.7 // diameter in mm d = 50 // depth in mm v = 75 // cutting speed in m/min. f = 0.175 // feed in mm/rev l = d + 2*0.29*D // lemgth of drill travel in mm N = (1000*v)/(%pi*D) // r.p.m. tm = l/(f*N) // min printf("\n Time taken to drill hole = %0.3f min." , tm)
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//Tested on Windows 7 Ultimate 32-bit //Chapter 10 Feedback in Amplifiers Pg no. 330 and 331 clear; clc; //Given A=500;//open loop gain B=0.1;//feedback factor beta dA_to_A=10/100;//variation in open loop gain //Solution dAfb_to_Afb=dA_to_A*1/(A*B);//variation in closed loop gain printf("Percentage variation in closed loop gain = %.1f %%",dAfb_to_Afb*100);
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//CHAPTER 2- STEADY-STATE ANALYSIS OF SINGLE-PHASE A.C. CIRCUIT //Example 51 clc; disp("CHAPTER 2"); disp("EXAMPLE 51"); //VARIABLE INITIALIZATION Y1=0.4+(%i*0.6); //admittance of 1st branch in Siemens Y2=0.1+(%i*0.4); //admittance of 2nd branch in Siemens Y3=0.06+(%i*0.23); //admittance of 3rd branch in Siemens //SOLUTION Y=Y1+Y2+Y3; //function to convert from rectangular form to polar form function [Y,angle]=rect2pol(x,y); Y=sqrt((x^2)+(y^2)); angle=atan(y/x)*(180/%pi); //to convert the angle from radians to degrees endfunction; [Y1,angle]=rect2pol(real(Y),imag(Y)); disp(sprintf("The total admittance of the circuit is %f S, %f degrees",Y1,angle)); z=1/Y1; disp(sprintf("The impedance of the circuit is %f Ω, %f degrees",z,-angle)); //END
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("16*x^4 - 16*y^4 - z^2").isMappableTo("x^4 - y^4 - z^2") = {x=>2*x,y=>2*y,z=>z}
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//chapter 9 example 4a// clc clear //angular velocity=A,llength at which rotating mirror from the photo detector=L,shadow pulse of width=We,shadow velocity=V,outer diametetr=do// L=0.1;//in mts// A=4;//in rad sec-1// V=L*A;//in mts/sec// printf("\n shadow velocity=%f m/sec\n",V) We=250;//in micro seconds// do=We*V;//outer diameter of the fibre// printf("\n outer diamter of the fibre=%f micro meter\n",do)
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Ex7_5.sce
//Example number 7.5, Page number 147 clc;clear; close; //Variable declaration A=650*10**-4; //area(m**2) epsilon0=8.85*10**-12; d=4*10**-2; //seperation(m) Q=2*10**-10; //charge(C) epsilonr=3.5; //dielectric constant //Calculation C=A*epsilon0/d; V=Q/C; //voltage(V) //Result printf("voltage is %.1f V",V)
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clc //Example 8.7 //Calculate the cross sectional area, pressure, temperature and mach number at a pt in duct where air velocity is 1400ft/s P1=30//psia T1=660//R (Rankine temperature scale) ratio_T=0.83333//dimentionless m=10//lbm/s mass flow rate v1=1400//ft/s R=4.98*10^4//(ft^2/s^2)*(lbm/lbmol.R)^0.5 k=1.4//dimentionless M=29//lbm/lbmol T2=T1*ratio_T//R (Rankine temperature scale) printf("The temperature at the pt in the duct where air velocity is 1400 ft/s is %f R\n",T2); c=223*(k*T2/M)^0.5//ft/s Ma=v1/c//dimentionless (Mach number) printf("The mach number at the pt in the duct where air velocity is 1400 ft/s is %f\n",Ma); ratio_t=0.7528//dimentionless ratio_P=0.3701//dimentionless ratio_A=1.0587//dimentionless T=T1*ratio_t//R (Rankine temperature scale) printf("T=%f\n",T); P=P1*ratio_P//psia printf("P=%f",P);
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//Example 3.15.2: shunt resistance clc; clear; close; //given data : Im=1;// in mA Rm=100;// in ohm I=100;// in mA Rsh=(Im*10^-3*Rm)/((I-Im)*10^-3); disp(Rsh,"shunt resistance,Rsh(ohm) = ")
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// Example 5.4 //slope efficiency clc; clear; close; eg=1242;// e=1300;//in nm n=0.1;//efficiency s=((eg/e)*n);// disp(s,"slope efficiency is")
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clc // Given that l = 3e-10 // width of box in m e = 1.6e-19 // charge on an electron in C m = 9.1e-31 // mass of electron in kg c = 3e8 // speed of light in m/sec h = 6.62e-34 // Planck constant in J-sec // Sample Problem 16 on page no. 15.30 printf("\n # PROBLEM 16 # \n") printf("Standard Formula used \n") printf(" E = (n^2 * h^2) / (8 * m * L^2)) \n") n = 1 // For n=1 E = (n^2 * h^2) / (8 * m * l^2) n = 2 // For n=2 E_ = (n^2 * h^2) / (8 * m * l^2) n = 3 // For n=3 E__ = (n^2 * h^2) / (8 * m * l^2) printf("\n Energy of electron -\n For (n=1) is %e J.\n For (n=2) is %e J.\n For (n=3) is %e J.",E,E_,E__)
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//Ex:67 clc; clear; close; R_e=6378;// in km H=35786;// in km E_min=5;// min elevation angle in degree x=cos(E_min*3.14/180); R=R_e/(R_e+H); P=2*asin(R*x);// in radian a_max=(P)*180/3.14;// in degree printf("The max coverage angle=%f degree", a_max);
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// This file is part of the materials accompanying the book // "The Elements of Computing Systems" by Nisan and Schocken, // MIT Press. Book site: www.idc.ac.il/tecs // File name: projects/07/MemoryAccess/BasicTest/BasicTestVME.tst load BasicTest.vm, output-file BasicTest.out, compare-to BasicTest.cmp, output-list RAM[256]%D1.6.1 RAM[300]%D1.6.1 RAM[401]%D1.6.1 RAM[402]%D1.6.1 RAM[3006]%D1.6.1 RAM[3012]%D1.6.1 RAM[3015]%D1.6.1 RAM[11]%D1.6.1; set sp 256, set local 300, set argument 400, set this 3000, set that 3010, repeat 25 { vmstep; } output;
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clc //Initialization of variables H=-169182 //Btu/mole s1=1.3609 //Btu/mole R s2=49.003 //Btu/mole R s3=51.061 //Btu/mole R T=537 //R //calculations dG=H-T*(s3-s2-s1) //results printf("Change in Gibbs energy = %d Btu/mole carbon",dG)
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clear; clc; funcprot(0); //Example - 15.16 //Page number - 534 printf("Example - 15.16 and Page number - 534\n\n"); //Given T = 78.15;//[C] P_1_sat = 755;//[mm Hg] P_2_sat = 329;//[mm Hg] z_1 = 0.3; V = 0.5; // log(Y1) = 0.845/(1 + 0.845*(x_1/x_2))^(2) // log(Y2) = 1/(1 + 1.183*(x_2/x_1))^(2) // A value of x_1 is to determined for which V = 0.5 // Let us assume a value of x_1, say x_1 = 0.150 x_1 = 0.150; error = 10; while(error>0.001) x_2 = 1 - x_1; Y1 = exp(0.845/(1 + 0.845*(x_1/x_2))^(2)); Y2 = exp(1/(1 + 1.183*(x_2/x_1))^(2)); P = x_1*Y1*P_1_sat + x_2*Y2*P_2_sat; y_1 = (x_1*Y1*P_1_sat)/P; V_prime = (z_1 - x_1)/(y_1 - x_1); error=abs(V_prime - V); x_1 = x_1 + 0.00001; end P_prime = x_1*Y1*P_1_sat + x_2*Y2*P_2_sat;//[mm hg] // At x_1 , V = 0.5, // Therefore when the mixture is 50 % vaporized at 78.15 C the mole fraction of component 1 in the liquid phase is x_1 and the system pressure is P_prime printf(" The required pressure is %f mm Hg\n\n",P_prime); printf(" and the mole fraction of component 1 in the liquid phase for this pressure is x_1 = %f\n\n",x_1);
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clear; clc; close; yos = 50*10^(-6); Idss = 10*10^(-3); Vp = -4; Vgsq = -2.2; Idq = 2.03*10^(-3); Rd = 3.6*10^(3); Rs = 1.1*10^(3); Vi = 40*10^(-3); gmo = 2*Idss/abs(Vp); gm = gmo*(1-(Vgsq/Vp)); rd = 1/yos; Zi = Rs*((rd+Rd)/(1+gm*rd))/(Rs+((rd+Rd)/(1+gm*rd))); Zi2 = Rs*gm^(-1)/(Rs+gm^(-1)); Zo = Rd*rd/(Rd+rd); Zo2 = Rd; Av = (gm*Rd+(Rd/rd))/(1+Rd/rd); Vo = Av*Vi; Av2 = gm*Rd; Vo2 = Av2*Vi; disp(gm,'gm(S) = '); disp(rd,'rd(ohms) = '); disp(Zi,'Zi(ohms) = '); disp(Zi2,'Zi(ohms) without rd = '); disp(Zo,'Zo(ohms) = '); disp(Zo2,'Zo(ohms) without rd = ') disp(Av,'Voltage gain Av = '); disp(Vo,'Vo = '); disp(Av2,'Volatge gain Av(ignoring rd) = '); disp(Vo2,'Vo2 witout rd = ');
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function[x]= descente(A,b) n=size(A) i=1:n j=1:n A=A(i,j) x(1)=b(1)/A(1,1) for k=2:n s=0 for j=1:k-1 s=s+A(k,j)*x(j) end x(k)=(b(k)-s)/A(k,k) end endfunction
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// HW_7 Problem 1 // clear and close everything!!! clear; clc; close; close; close; close; // Independent Parameters ------------------------------------------------ gamma_a = 1.4; gamma_e = 1.3; R = 287; // (j/(kg*K)) M = 1.8; P_a = 12112; // (Pa) T_a = 216.650; // (K) T_max = 1500; // (K) h_c = 43124000; // (j/kg) FA_st = 0.06; P_e = P_a; // (Pa) eff_dif = 0.9; eff_comp = 0.9; eff_burn = 0.98; eff_turb = 0.92; eff_nozz = 0.98; r_b = 0.97; r_c = [2:2:60]; // Dependent Parameters -------------------------------------------------- Po_3 = zeros(1,30); // (Pa) To_3_i = zeros(1,30); // (K) To_3_r = zeros(1,30); // (K) W_c_in = zeros(1,30); //(W) FA = zeros(1,30); eq_ratio = zeros(1,30); W_t_out = zeros(1,30); // (W) Po_4 = zeros(1,30); // (Pa) To_5_i = zeros(1,30); // (K) To_5_r = zeros(1,30); // (K) Po_5 = zeros(1,30); // (Pa) To_7_r = zeros(1,30); // (K) T_7_i = zeros(1,30); // (K) T_7_r = zeros(1,30); // (K) u_e = zeros(1,30); // (m/s) M_e = zeros(1,30); A_ratio = zeros(1,30); TSFC = zeros(1,30); // (kg/(N*s)) I = zeros(1,30); // (N*s/kg) eff_therm = zeros(1,30); eff_propul = zeros(1,30); eff_overall = zeros(1,30); // Calculate specific heat at constant pressure--------------------------- cp_a = (gamma_a/(gamma_a-1))*R; cp_e = (gamma_e/(gamma_e-1))*R; // Ambient conditions----------------------------------------------------- Po_a = P_a*(1+(gamma_a-1)/2*M^2)^(gamma_a/(gamma_a-1)); To_a = T_a*(1+(gamma_a-1)/2*M^2); u = M*sqrt(gamma_a*R*T_a); // Diffuser Stage (a-2)--------------------------------------------------- To_2_r = To_a; To_2_i = eff_dif*(To_2_r-T_a)+T_a; Po_2 = P_a*(To_2_i/T_a)^(gamma_a/(gamma_a-1)); // Compressor Stage-(2-3)------------------------------------------------- Po_3 = r_c.*Po_2; To_3_i = r_c.^((gamma_a-1)/gamma_a).*To_2_r; To_3_r = ((To_3_i-To_2_r)./eff_comp)+To_2_r; W_c_in = cp_a.*(To_3_r-To_2_r); // Burner Stage-(3-4)----------------------------------------------------- // Verify that FA <= FA_st FA = ((T_max./To_3_r)-1)./(((eff_burn.*h_c)./(cp_e.*To_3_r))-(T_max./To_3_r)); eq_ratio = FA./FA_st; for i = 1:30, if eq_ratio <= 1 then To_4_r = T_max; else To_4_r(i) = 1.0./(1+FA_st).*((eff_burn.*h_c./cp_e)+To_3_r(i)); end, end Po_4 = r_b.*Po_3; // Turbine Stage-(4-5)---------------------------------------------------- W_t_out = W_c_in; To_5_r = To_4_r-(W_t_out./((1+FA).*cp_e)); To_5_i = To_4_r-((To_4_r-To_5_r)./eff_turb); Po_5 = Po_4.*(To_5_i/To_4_r).^(gamma_e./(gamma_e-1)); // Nozzle Stage -(5-7)---------------------------------------------------- To_7_r = To_5_r; Po_7 = Po_5; P_7 = P_e; T_7_i = To_5_r.*(P_7./Po_5).^((gamma_e-1)./gamma_e); T_7_r = To_5_r-(eff_nozz.*(To_5_r-T_7_i)); u_e = sqrt(2.*eff_nozz.*(gamma_e./(gamma_e-1)).*R.*To_5_r.*(1-(P_a./Po_5).^((gamma_e-1)./gamma_e))); M_e = u_e./sqrt(gamma_e.*R.*T_7_r); A_ratio = 1.0./M_e.*((2/(gamma_e+1)).*(1+((gamma_e-1)./2.0).*M_e.^2)).^((gamma_e+1)./(2.0.*(gamma_e-1))); // Calculate Specific Thrust; TSFC; and Efficiencies;--------------------- I = ((1+FA).*u_e-u); TSFC = FA./I; eff_therm = ((1+FA).*u_e.^2-u.^2)./(2.0.*FA.*h_c); eff_propul = (I.*u)./((1+FA).*(u_e.^2.0./2)-(u.^2.0./2)); eff_overall = eff_therm.*eff_propul; // Plot Graphs------------------------------------------------------------ f0 = scf(0); //creates figure with id==0 and make it the current one f1 = scf(1); //creates figure with id==1 and make it the current one f2 = scf(2); f3 = scf(3); f4 = scf(4); // Plot Specific Thrust--------------------------------------------------- scf(f0); subplot(311); plot(r_c,I, 'r'); xtitle("Specific Thurst VS Compressor Pressure Ratio","r_c","Specific Thurst(N*s/Kg)"); //a=get("current_axes") //a.data_bounds=[1,500;6,1220]; // plot TSFC-------------------------------------------------------------- subplot(312); plot(r_c,TSFC, 'g'); xtitle("TSFC VS Compressor Pressure Ratio","r_c","TSFC(Kg/N*s)"); // plot area ratio subplot(313); plot(r_c,A_ratio, 'r'); xtitle("Area Ratio VS Compressor Pressure Ratio","r_c","Area Ratio"); // Plot Temperature Across TurboJet--------------------------------------- scf(f1); subplot(111); plot(r_c,To_3_r, 'b'); plot(r_c,To_5_r, 'c'); plot(r_c,T_7_r, 'm'); xtitle("Stagnation Temperature VS Compressor Pressure Ratio","r_c","Temperature (K)"); leg=legend(['To_3_r';'To_5_r';'T_7_r'],[4]); //a=get("current_axes") //a.data_bounds=[1,2300;6,2800]; // Plot Temperature Across TurboJet--------------------------------------- scf(f2); subplot(111); plot(r_c,Po_3, 'b'); plot(r_c,Po_4, 'c'); plot(r_c,Po_5, 'm'); xtitle("Stagnation Pressure VS Compressor Pressure Ratio","r_c","Pressure (Pa)"); leg=legend(['Po_3';'Po_4';'Po_5'],[4]); //a=get("current_axes") //a.data_bounds=[1,2300;6,2800]; // plot efficiencies------------------------------------------------------ scf(f3); subplot(111); plot(r_c,eff_therm, 'r'); plot(r_c,eff_propul, 'b'); plot(r_c,eff_overall, 'g'); xtitle("Efficiencies VS Compressor Pressure Ratio","r_c","Effeciency"); leg=legend(['Thermal Efficiency';'Propulsive Efficiency';'Overall Efficiency'],[4]); // Plot Exit Mach Number-------------------------------------------------- scf(f4); subplot(111); plot(r_c,M_e, 'r'); xtitle("Exit Mach Number VS Compressor Pressure Ratio","r_c","M");
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disp('To find:number of mathematics students taking atleast one of the languages French(F),German(G) and Russian(R)') F=65; //number of students studying French G=45; // number of students studying German R=42; //number of students studying Russian FandG=20; //number of students studying French and German FandR=25; //number of students studying French and Russian GandR=15; //number of students studying German and Russian FandGandR=8; //number of students studying French,German and Russian //By inclusion-exclusion principle ForGorR=F+G+R-FandG-FandR-GandR+FandGandR; disp(ForGorR,'the number of students studying atleast one of the languages :')
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//CHAPTER 2- STEADY-STATE ANALYSIS OF SINGLE-PHASE A.C. CIRCUIT //Example 45 disp("CHAPTER 2"); disp("EXAMPLE 45"); //VARIABLE INITIALIZATION L=1.405; //inductance in Henry r=40; //resistance in Ohms C=20/(10^6); //capacitance in Farad v=100; //voltage in Volts //SOLUTION //resonant frequency f=1/2.pi.sqrt (L.C) f0=1/(2*%pi*sqrt(L*C)); disp(sprintf("The frequency at which the circuit resonates is %d Hz",f0)); I0=v/r; disp(sprintf("The current drawn from the supply is %.1f A",I0)); xl0=2*%pi*f0*L; z0=sqrt((r^2)+(xl0^2)); vl0=I0*z0; disp(sprintf("The voltage across the coil is %.1f V",vl0)); xc0=1/(2*%pi*f0*C); disp(sprintf("The capcitative reactance is %.1f Ω",xc0)); Q0=(2*%pi*f0*L)/r; disp(sprintf("The quality factor is %.3f", Q0)); bw=r/L; disp(sprintf("The bandwidth is %.3f Hz",bw)); //END
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clc clear //Initialization of variables d=8 //in V=3.65 //ft/s u1=4.75 //ft/s r0=4 //in //calculations f=0.0449 Q=V*%pi/4 *(d/12)^2 Vs=(u1-V)/3.75 r0e=10^((u1/Vs - 8.5)/5.75) e=r0/r0e //results printf("Flow rate = %.2f ft^3/s",Q) printf("\n roughness factor = %.3f in",e)
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//Variable declaration N=1.6*10**20; //number of molecules(/m**3) T=300; //temperature(K) E=5*10**5; //electric field(V/m) x=0.25*10**-9; //separation(m) Kb=1.381*10**-23; //boltzmann constant e=1.6*10**-19; //Calculation Pd=N*e**2*x**2*E/(3*Kb*T); //orientational polarization //Result printf('orientational polarization is %0.3f *10**-11 C m \n',(Pd*10**11))
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<?xml version="1.0" encoding="utf-8"?> <test> <description>3D Tet Kovasnay solution using DG SVV Kerneal and dealiasing</description> <executable>IncNavierStokesSolver</executable> <parameters>Tet_Kovasnay_SVV_DGKer.xml</parameters> <files> <file description="Session File">Tet_Kovasnay_SVV_DGKer.xml</file> </files> <metrics> <metric type="L2" id="1"> <value variable="u" tolerance="1e-6">0.00476409</value> <value variable="v" tolerance="1e-6">0.000908482</value> <value variable="w" tolerance="1e-6">0.000616045</value> <value variable="p" tolerance="1e-6">0.00422569</value> </metric> <metric type="Linf" id="2"> <value variable="u" tolerance="1e-6">0.0418501</value> <value variable="v" tolerance="1e-6">0.00387299</value> <value variable="w" tolerance="1e-6">0.00349122</value> <value variable="p" tolerance="1e-6">0.0254931</value> </metric> </metrics> </test>
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// Scilab code Exa3.7: : Page 125(2011) clc; clear; Z = 82; // Atomic number E = 1; // Energy of the beta paricle, MeV I_l = 800; // Ionisation loss, MeV R = Z*E/I_l; // Ratio of radiation loss to ionisation loss E_1 = I_l/Z; // Energy of the beta particle when radiation radiation loss is equal to ionisation loss, MeV printf("\nThe ratio of radiation loss to ionisation loss = %5.3e \nThe energy of the beta particle = %4.2f MeV ", R, E_1); // Result // The ratio of radiation loss to ionisation loss = 1.025e-01 // The energy of the beta particle = 9.76 MeV
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clear; clc; disp('Example 4.19'); // aim : To determine the condition of the steam after // (a) isothermal compression to half its initial volume,heat rejected // (b) hyperbolic compression to half its initial volume // Given values V1 = .3951;// initial volume,[m^3] P1 = 1.5;// initial pressure,[MN/m^2] // solution // (a) // from steam table, at 1.5 MN/m^2 hf1 = 844.7;// [kJ/kg] hfg1 = 1945.2;// [kJ/kg] hg1 = 2789.9;// [kJ/kg] vg1 = .1317;// [m^3/kg] // calculation m = V1/vg1;// mass of steam,[kg] vg2b = vg1/2;// given,[m^3/kg](vg2b is actual specific volume before compression) x1 = vg2b/vg1;// dryness fraction h1 = m*(hf1+x1*hfg1);// [kJ] Q = m*x1*hfg1;// heat loss,[kJ] mprintf('\n (a) The Quantity of steam present is = %f kg \n',m); mprintf('\n Dryness fraction is = %f \n',x1); mprintf('\n The enthalpy is = %f kJ \n',h1); mprintf('\n The heat loss is = %f kJ \n',Q); // (b) V2 = V1/2; // Given compression is according to the law PV=Constant,so P2 = P1*V1/V2;// [MN/m^2] // from steam table at P2 hf2 = 1008.4;// [kJ/kg] hfg2 = 1793.9;// [kJ/kg] hg2 = 2802.3;// [kJ/kg] vg2 = .0666;// [m^3/kg] // calculation x2 = vg2b/vg2;// dryness fraction h2 = m*(hf2+x2*hfg2);// [kJ] mprintf('\n (b) The dryness fraction is = %f \n',x2); mprintf('\n The enthalpy is = %f kJ\n',h2); // End
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clc; //e.g 28.10 C1=0.1*10**-6; C2=1*10**-6; L=470*10**-6; C=(C1*C2)/(C1+C2) fo=1/(2*%pi*sqrt(L*C)); disp('kHZ',fo*10**-3,"fo=");
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clc //Chapter15 //Example15.1, page no 533 //Given P_A=0.5// probability of producing symbol 'A' P_B=0.25// probability of producing symbol 'B' P_C=0.25// probability of producing symbol 'C' H=P_A*log2(1/P_A)+P_B*log2(1/P_B)+P_C*log2(1/P_C)// the source entropy mprintf('The source entropy is: %f bits/symbol',H)
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//Fluid system - By - Shiv Kumar //Chapter 2 - Impact of Jet //Example 2.6 clc clear //Given Data:- M=13.5; //Mass of plate, kg d=16; //Diameter of the Jet, mm V=20; //Velocity of the Jet, m/s L=300; //Length of Edge of plate, mm //Data Used:- rho=1000; //Density of water, kg/m^3 g=9.81; //Acceleration due to gravity, m/s^2 //Computations:- d=d/1000; //m L=L/1000; //m W=M*g; //Weight of Plate, N a=(%pi/4)*d^2; //cross sectional area of Jet, m^2 //(a) Fx=rho*a*V^2; //Force exerted by Jet normal to plate, N //Taking Moment at 'A', P=Fx*(L/2)/L; //N //(b) theta=asind(rho*a*V^2/W); //Angle of Swing, degrees //Results:- printf("(a)Horizontal force applied at Lower edge of plate to keep it vertical, P=%.3f N \n", P) //The answer vary due to round off error printf("(b)Angle of swing, theta=%.2f degrees", theta) //The answer vary due to round off error
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// Copyright (C) INRIA 1999-2005 // // This program is free software; you can redistribute it and/or modify it // under the terms of the GNU General Public License version 2 as published // by the Free Software Foundation. // // This program is distributed in the hope that it will be useful, but // WITHOUT ANY WARRANTY; without even the implied warranty of // MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General // Public License for more details. // // You should have received a copy of the GNU General Public License along // with this program; if not, write to the Free Software Foundation, Inc., // 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA. //% // @file LagrangianDynamics/Complete/Visu.scilab // @author Pierre-Brice Wieber // // Affiliation(s): INRIA, team BIPOP // // Email(s): Pierre-Brice.Wieber@inria.fr // // @brief Draw the visualisation 3D // // Description: // // Modifications: // $Log$ // Revision 1.6 2005/10/28 08:14:14 billet // Moving from old to new graphic style and removing of windows scilab visualization bug // // Revision 1.5 2005/05/04 13:13:15 billet // Correction and changes for doxygen documentation // // Revision 1.4 2005/05/03 11:45:17 billet // Comments for doxygen documentation // // Revision 1.3 2005/05/02 12:03:13 wieber // Added the possibility to print a Message above the figure and prepared the new figure_style mode, still not active because buggy in Scilab 3.0. // // Revision 1.2 2005/04/07 15:37:29 wieber // Drawing contact forces on different solids through the use of the variable ContactSolids. // // Revision 1.1.1.1 2005/02/08 13:08:22 rpissard // version start HuMAnS // // function [] = VisuPlay(flag, gwin) /////////////////////////////////////////// // Draws a 3D stick figure of the system following the trajectory Q1. // If LAMBDA is available, also draws the contact forces with a // ratio of 1000N for 1m. /////////////////////////////////////////// global QVISU; global LAMBDAVISU; /////////////////////////////////////////// // Compute the bounding box. /////////////////////////////////////////// mmin = [%inf, %inf, %inf]; mmax = -mmin; for k = 1:size(QVISU, 2), tag = Tags(QVISU(:, k)); mmin = min([mmin; tag], 'r'); mmax = max([mmax; tag], 'r'); end; mmin(2) = 0; delta_iso = max(mmax-mmin); mmin = (mmin+mmax)/2-0.55*delta_iso; mmin(2) = 0; mmax = mmin+1.1*delta_iso; f = scf(gwin); f.figure_name = "3D Stick Figure (HuMAnS)"; ha = f.children; ha.axes_visible = "on"; ha.box = "on"; ha.view = "3d"; f.pixmap = "on"; ha.data_bounds = [mmin(3), mmin(1), mmin(2); mmax(3), mmax(1), mmax(2)]; if flag~=0 then delete(ha.children); else f.figure_size=[600,600]; ha.rotation_angles = [80, 30]; end; for k = 1:size(QVISU, 2), tag = Tags(QVISU(:, k)); if k>1 then delete(ha.children); end; /////////////////////////////////////////// // Draw the center of mass of the system, /////////////////////////////////////////// param3d1([tag($,3)-0.02;tag($,3)+0.02;tag($,3)+0.02;tag($,3)-0.02;tag($,3)-0.02],... [tag($,1)-0.02;tag($,1)+0.02;tag($,1)-0.02;tag($,1)+0.02;tag($,1)-0.02],... list([tag($,2);tag($,2);tag($,2);tag($,2);tag($,2)],21), ... ha.rotation_angles(2), ha.rotation_angles(1),"Z@X@Y", [1,4]); if exists('LAMBDAVISU', 'all')&(size(LAMBDAVISU, 2)==size(QVISU, 2)) then contact = Contact(QVISU(:, k)); contact = [contact(1:$/3), contact($/3+1:2*$/3), contact(2*$/3+1:$)]; lambda = [LAMBDAVISU(1:$/3, k), LAMBDAVISU($/3+1:2*$/3, k), LAMBDAVISU(2*$/3+1:$, k)]; ///////////////////////////////////////////// // draw the sum of the contact forces acting on each contacting solid // at the corresponding center of pressure, ///////////////////////////////////////////// for i = 1:size(ContactSolids, 1), ContactPoints = ContactSolids(i, 1):ContactSolids(i, 2); Force = lambda(ContactPoints, :); if sum(Force(:, 2))>sqrt(%eps) then COP = sum(diag(Force(:, 2))*contact(ContactPoints, :), 'r')/sum(Force(:, 2)); Force = COP+sum(Force/1000, 'r'); param3d1([COP(3)-0.02;COP(3)+0.02;COP(3)+0.02;COP(3)-0.02;COP(3)-0.02;COP(3);Force(3)],... [COP(1)-0.02;COP(1)+0.02;COP(1)-0.02;COP(1)+0.02;COP(1)-0.02;COP(1);Force(1)],... list([COP(2);COP(2);COP(2);COP(2);COP(2);COP(2);Force(2)],24),... ha.rotation_angles(2), ha.rotation_angles(1), "Z@X@Y", [0,0]); end; end; /////////////////////////////////////////// // draw the sum of all the contact forces acting on the system at the // global center of pressure on the ground (aka the zero moment point), /////////////////////////////////////////// if sum(lambda(:, 2))>sqrt(%eps) then contact = contact(lambda(:, 2)>sqrt(%eps), :); lambda = lambda(lambda(:, 2)>sqrt(%eps), :); contact = contact-diag(contact(:, 2)./lambda(:, 2))*lambda; COP = sum(diag(lambda(:, 2))*contact, 'r')/sum(lambda(:, 2)); lambda = COP+sum(lambda/1000, 'r'); param3d1([COP(3)-0.02;COP(3)+0.02;COP(3)+0.02;COP(3)-0.02;COP(3)-0.02;COP(3);lambda(3)],... [COP(1)-0.02;COP(1)+0.02;COP(1)-0.02;COP(1)+0.02;COP(1)-0.02;COP(1);lambda(1)],... list([COP(2);COP(2);COP(2);COP(2);COP(2);COP(2);lambda(2)],11),... ha.rotation_angles(2), ha.rotation_angles(1), "Z@X@Y", [0,0]); end; end; /////////////////////////////////////////// // and finally draw the 3D stick figure of the system. /////////////////////////////////////////// param3d1([tag(StickFigure(:,1),3)'; tag(StickFigure(:,2),3)'], ... [tag(StickFigure(:,1),1)'; tag(StickFigure(:,2),1)'], ... [tag(StickFigure(:,1),2)'; tag(StickFigure(:,2),2)'], ... ha.rotation_angles(2), ha.rotation_angles(1), "Z@X@Y", [0,0]); if exists('Message') then xtitle(Message); end; show_pixmap(); end; endfunction //% // Draw the visualisation 3D of a position or a trajectory with contact // forces if they exist. // @param Q (float matrix, size = NDOF x NSAMPLES) trajectory or position // @param LAMBDA (float matrix) contact forces // @param Message (string, optionnal) Message to print above the figure // @param DuringSimulationFlag (boolean, optionnal) Flag to know if we draw // the figure during the simulation or not. // function [] = Visu(Q, LAMBDA, Message, DuringSimulationFlag) global QVISU; global LAMBDAVISU; QVISU = Q; if exists('LAMBDA', 'local')|(~exists('LAMBDA', 'local')&exists('LAMBDA', 'all')) then LAMBDAVISU = LAMBDA; end; if ~exists('DuringSimulationFlag', 'local') then DuringSimulationFlag = %F; end; if DuringSimulationFlag then scf(2005); clf(); end VisuPlay(0, 2005); if (~DuringSimulationFlag) then addmenu(2005, "Replay", list(2, 'VisuPlay')); end; endfunction
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function ldot = f(t,l) ldot = [sigma*(l(2,1)-l(1,1)); (r-l(3,1))*l(1,1)-l(2,1); l(1,1)*l(2,1)-b*l(3,1)]; endfunction /*x = l(1,1); y = l(2,1); z = l(3,1);*/ sigma = 10; r = 28; b = 2.66; t = [0:0.01:90]; t0 = 0; l0 = [0;1;1]; ls = ode(l0,t0,t,f); title('Auto correlation for lorenz attractor') [c, ind] = xcorr(ls(2,:), "coeff"); plot(ind, c) a=get("current_axes")//get the handle of the newly created axes a.axes_visible="on"; // makes the axes visible a.font_size=3; //set the tics label font size //a.x_location="top"; //set the x axis position a.data_bounds=[0,0,-1;400,1,1]; //set the boundary values for the x, y and z coordinates. a.sub_tics=[5,0]; a.labels_font_color=5; //a.grid=[2,2]; a.box="off";
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//mass of an element in a given compound clear; clc; printf("\t Example 3.10\n"); massCuFeS2=3.71*10^3;//given mass of CuFeS2, kg CuFeS2=183.5;//mol. mass of CuFeS2, g Cu=63.55;//mol. mass of Cu, g percentCu=Cu/CuFeS2*100;//percent Cu in CuFeS2 massCu=percentCu*massCuFeS2/100;//mass of Cu in given CuFeS2, kg printf("\t the mass of Cu in CuFeS2 is : %1.2f*10^3 kg\n",massCu*10^-3); //End
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//Example 14.10 //Spline Integration Method //Page no. 478 clc;close;clear; deff('y=f(x)','y=sind(%pi*x)') deff('y=f1(x,h)','y=(f(x+h)-f(x))/h') h=0.01; n=2;h=0.5;a=0;b=1; disp(integrate('f(x)','x',0,1),'I = ')
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clc //initialisation of variables clear v= 1 //lit p= 1 //atm h= 76 //cm d= 13.595 //kg/cm^3 g= 980.66 //dunes cm^-2 j= 4.18 //joules //CALCULATIONS W= v*p W1= h*d*g W2= W1*10^-4 W3= W2/j //RESULTS printf ('Work done in lit-atm = %.f lit-atm',W) printf ('\n Work done in dynes = %.2e dynes cm^-2',W1) printf ('\n Work done in ergs = %.2e ergs',W2) printf ('\n Work done in calories = %.2f calories',W3)
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example_10_16.sce
clear; clc; disp("--------------Example 10.16---------------"); x=poly(0,"x"); // a) x+1 g=x^1+1; t=0; // compute t while(%T) q=(x^t+1)/g; if(q == 1) break; end t=t+1; end printf("a. t = %d . This is a very poor choice for a generator. Any two errors next to each other cannot be detected.\n\n",t); // display result // b) x^4+1 g=x^4+1; t=0; // compute t while(%T) q=(x^t+1)/g; if(q == 1) break; end t=t+1; end printf("b. t = %d .This generator cannot detect two errors that are four positions apart. The two errors can be anywhere, but if their\ndistance is %d, they remain undetected.\n\n",t,t); // display result // c) x^7+x^6+1 g=x^7+x^6+1; printf("c. This is a good choice for this purpose.\n\n"); // display result // d) x^15+x^14+1 t=32768; // very large to compute printf("d. This polynomial cannot divide any error of type x^t + 1 if t is less than %d. This means that a codeword with two isolated\nerrors that are next to each other or up to %d bits apart can be detected by this generator.",t,t); // display result