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//Example 6.9// speed clc; clear; close; format('v',6) i1=50;//primary current in amperes i2=i1/(sqrt(2));//secondary current in amperes r1=0.2;//primary resistance in ohms v1=220;//primary voltage in volts eb1=((v1-(i1*r1)));//primary emf in volts eb2=((v1-(i2*r1)));//secondary emf in volts n1=1000//primary speed in rpm n2=(n1*(eb2/eb1)*(i1/i2));//seconadry speed in rpm disp(n2,"speed is,(rpm)=")
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## Tag create test read <sample1.fi set echo tag newtag create :15 write -
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//Chapter 5, Problem 6, Figure 5.13 clc; //Potential difference across R1 is the same as the supply voltage V R1=5; R3=20; I=11; I1=8; //Hence supply voltage is V=R1*I1; I3=V/R3; //Reading on ammeter, printf("Reading on ammeter = %f A\n\n\n",I3); I2=I-I1-I3; R2=V/I2; //Current flowing through R2 printf("Resistance R2 = %f ohm\n\n\n",R2);
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clc; // Chapter 2 Switched communication systems //Example 2.5,page no 127 //given N=1000//no of turns L1=5e-8//inductance per turn L=N^2*L1//total inductance mprintf('total inductance is %f H \n',L) R=100//resistance of winding in ohm MMF=5//operating MMF in amp. turn V=1//voltage of received signal in volts Im=V/R//maximum current mprintf('maximum current is %f mA \n',Im*1e3) Io=MMF/N//operating current mprintf('operating current is %f mA \n',Io*1e3) to=(L/R)*log(1/(1-(Io/Im)))//operate lag mprintf('operate lag is %f msec \n',to*1e3)
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//Chapter-5,Example 5_11,Page 5-29 clc() //Given Values: m1=50*10^-9 //mass of particle in kg m2=9.1*10^-31 //mass of electron in kg h=6.625*10^-34 //Planck's constant v1=1 //velocity of particle v2=3*10^6 //velocity of electron //Calculations: lam1=h/(m1*v1)*10^10 //de Broglie wavelength printf('de Broglie wavelength associated with particle is =%.20f Angstrom \n \n',lam1) lam2=h/(m2*v2)*10^10 //de Broglie wavelength printf(' de Broglie wavelength associated with electron is =%.3f Angstrom \n \n',lam2) printf(' Wavelength of electron is measurable.')
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function neighbors = kNN(kdtree,k,point) //Author : Maxens ACHIEPI //Space Robotics Laboratory - Tohoku Univeristy //Description: //Outputs the k-nearest neighbors of an input point. Uses a k-d tree structure as input. ///2018/08/01 : Doesn't output the actual nearest neighbors, nut more of an approximation //INPUT: //kdtree : the k-d tree structure. It is a cell array. //k : the numbers of neighbors we want //point : the point from which we want neighbors //OUTPUT: //neighbors: a (k x 3) matrix containing the coordinates of the k nearest neighbors //TODO: Debug; Probably due to not unwraping new explorations of the tree when recursing up the tree. // Should probably change the way we check for intersection. //----------------------------------------------------------------------------// // distance field distance = zeros(k,1); //init neighbors with root point for i=1:k neighbors(i,:) = kdtree(1).entries.point; // distance(i) = normNoSqrt(point-kdtree(1).entries.point); distance(i) = 1000000000000; end //init current node curNode = kdtree(1).entries; //init stack stack = list(); // stack = stackInsert(stack,curNode); //first exploration of the tree //[stackOut,neighborsOut,distanceOut] = tree_expl(kdtree,root,point,neighborsIn,stackIn,distanceIn) [stack,neighbors,distance] = tree_expl(kdtree,curNode,point,neighbors,stack,distance); disp("Done with first exploration"); // [curNode,stack] = stackPop(stack); //pop the leaf node, throw it away //reverse exploration of tree //[stackOut,distanceOut,neighborsOut] = tree_rev_expl(kdtree,stackIn,point,distanceIn,neighborsIn) [stack,distance,neighbors] = tree_rev_expl(kdtree,stack,point,distance,neighbors); disp("Done with reverse exploration"); endfunction
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function [ar, sigma2,rc] = levin(r); // //[ar,sigma2,rc]=lev(r) // //Resolve the Yule-Walker equations: // // // // |r(0) r(1) ... r(N-1)|| a(1) | |sigma2| // // |r(1) r(0) ... r(n-1)|| a(2) | | 0 | // // | : : ... : || : |=| 0 | // // | : : ... : || : | | 0 | // // |r(N-1) r(N-2) ... r(0) ||a(N-1)| | 0 | // // // //using Levinson's algorithm. // // r :Correlation coefficients // // ar :Auto-Regressive model parameters // // sigma2 :Scale constant // // rc :Reflection coefficients <<<<<<< HEAD // Example : ======= >>>>>>> 6bbb00d0f0128381ee95194cf7d008fb6504de7d if length(r)==1 then ar=1; sigma2=r; rc=[]; else ar = 0; aj(1) = 1; ej = r(1); rc = []; p=length(r)-1 for j=1:p, aj1 = zeros(j+1, 1); aj1(1) = 1; gammaj = r(j+1); for i=2:j, gammaj = gammaj + aj(i)*r(j-i+2); end if ej==0 then lambdaj1=%nan else lambdaj1 = -gammaj/ej; end rc=[rc; lambdaj1]; for i=2:j, aj1(i) = aj(i)+lambdaj1*(aj(j-i+2)'); end aj1(j+1) = lambdaj1; ej1 = ej*(1-abs(lambdaj1)^2); aj = aj1; ar = aj1; ej = ej1; end sigma2 = sqrt(ej1); end endfunction
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//---- perceptron trenowanie //---- okreslenie par wektorow trenujacych //---- dla funktora AND A = ones(4,4); A(1,2) = -1; A(1,3) = -1; A(1,4) = -1; A(2,2) = -1; A(3,3) = -1; //---- wykreslenie obszaru klasyfikacji mtlb_hold on; for i=1:4 if A(i,4)==1 plot(A(i,2),A(i,3),'ko:'); else plot(A(i,2),A(i,3),'r+:'); end end mtlb_axis([-2 2 -2 2]); //---- ustalenie poczatkowych wartosci wag W=[0 0 0]; //---- proces trenowania disp(W); disp('----------------'); BrakZmiany=0; Nr_Wektora=1; while (BrakZmiany<4) //--- kolejno pobiera wektory trenujace S=A(Nr_Wektora,1)*W(1)+A(Nr_Wektora,2)*W(2)+A(Nr_Wektora,3)*W(3); Sig=0; if S>0 Sig=1; end if S<0 Sig=-1; end if ((Sig>0) & (A(Nr_Wektora,4)==1)) | ((Sig<0) & (A(Nr_Wektora,4)==-1)) W=W; BrakZmiany=BrakZmiany+1; else BrakZmiany=0; if S~=0 for j=1:3 W(j)=W(j)+0.5*(A(Nr_Wektora,4)-Sig)*A(Nr_Wektora,j); end else for j=1:3 W(j)=W(j)+A(Nr_Wektora,4)*A(Nr_Wektora,j); end end end disp(W); Nr_Wektora=Nr_Wektora+1; if Nr_Wektora>4 Nr_Wektora=1; end end u1 = input('Podaj u1: '); u2 = input('Podaj u2: '); S = 1 * W(1) + u1 * W(2) + u2 * W(3); Sig = 0; if S > 0 then Sig = 1; end if S < 0 then Sig = -1; end disp(Sig,'Sig = '); //---- wykreslenie otrzymanej linii podzialu k=0; for i=-2:0.01:2 k=k+1; XX(k)=i; YY(k)=-((W(2)/W(3))*i)-(W(1)*1)/W(3); end plot(XX,YY); mtlb_axis([-2 2 -2 2]);
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errcatch(-1,"stop");mode(2);// Example 4.4:core diameter ; ; format('v',4) d=0.02;//difference n1=1.5;//core refrative index m=1000;// number of modes h= 1.3;// Wavelenght in micrometers a=((h/(%pi*n1))*(m/d)^(1/2));//core diamter in micro meter disp(a,"core diameter in micro meter") exit();
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//Working loop mean effective pressure(in bar) wlep=6; //Pumping loop mean effective pressure(in bar) plep=0.4; //Speed of the engine(in rpm) N=400; //Working cycle per minue in no load conditioons(in rpm) Wc=50; //Mean effective pressure(in bar) pfm=0.6; //Diameter of he engine(in m) D=0.18; //Stroke of the engine(in m) L=0.33;
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//chapter 6 Ex 3 clc; clear; close; a=[]; for i=1:20 a(i)=7*i; end Sum=sum(a); Average=Sum/size(a,"r"); printf("The average of first 20 multiples of 7 is %3.2f",Average);
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clc //initialization of varaibles P=15 //psia T2=70+460 //R T1=55+460 //R //calculations pw=0.2141 pA=P-pw mratio=pA*29/(pw*18) mAbym=mratio/(1+mratio) mwbym=1/(1+mratio) pg=0.3631 //psia phi=pw/pg gamma=1/mratio //results printf("Partial pressure of water vapor = %.2f psia",pA) printf("\n Specific humidity = %.4f lb vapor/lb air",gamma)
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clc clear //Page number 497 //Input data L=80;//The latent heat of fusion of ice in cal/gm Li=3.3*10^5;//Specific latent heat of ice fusion in Jkg^-1 dp=1;//The increase in pressure in atmospheres t=0;//The given temperature in degree centigrade v=-0.1;//The change in specific volume in cm^3/gm //Calculations dP=0.76*13.6*10^3*9.8;//The increase in pressure in N/m^2 V=v*10^-3;//The change in specific volume in m^3/kg T=t+273;//The given temperature in K dT=-(dP*T*(V))/Li;//The decrease in the melting point of ice with increase in the pressure of one atmosphere in K //Output printf('The decrease in melting point of ice is %3.4f K (or) %3.4f degree centigrade ',dT,dT)
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//Wired Digital Communications : example 9-5 : (pg 411) Tb=1/(8*10^3);//bit frequency BWmin=1/(2*Tb);//minimum bandwidth printf("\nTb = %.8f s",Tb); printf("\nBWmin = 1/2.Tb = %.f Hz",BWmin);
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//chapter 18 //example 18.2 //page 762 printf("\n") printf("given") Vo=12;Il=40*10^-3;Vs=20;Vbe=.7; Vz=.75*Vo disp("for minimum D1 current select") Ir2=10*10^-3; R2=(Vo-Vz)/Ir2 Ie1=Il+Ir2 disp("specification for Q") Vce1=20;Vs=Vce1; Ic1=50*10^-3; Pd=(Vs-Vo)*Ie1 hfe=50; Ib1=Ie1/hfe Ic2=5*10^-3; R1=(Vs-(Vo+.7))/(Ic2+Ib1) Iz=Ie2+Ir2 I4=1*10^-3; R4=(Vz+Vbe)/I4 R3=(Vo-(Vz+Vbe))/I4
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//Example 31.4 t_half=5730;//Half-life of Carbon-14 (y) lambda=0.693/t_half;//Decay constant (1/y) t=-log(0.92)/lambda;//Calculated age (y) //Above formula is obtained after mathematical simplification of Equation 31.38 printf('The age of the Shroud of Turin = %0.1f years',t) //The answer varies due to round off error //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest
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//Problem 43.03: Two coils have self inductances of 250 mH and 400 mH respectively. Determine the magnetic coupling coefficient of the pair of coils if their mutual inductance is 80 mH. //initializing the variables: La = 250E-3; // in Henry Lb = 400E-3; // in Henry M = 80E-3; // in Henry //calculation: //coupling coefficient, k = M/(La*Lb)^0.5 printf("\n\n Result \n\n") printf("\n coupling coefficient, is %.3f",k)
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decorrstretch.sci
function new_image = decorrstretch(image) image_list = mattolist(image) out = opencv_decorrstretch(image_list) sz = size(out) for i=1:sz new_image(:, :, i) = out(i) end endfunction
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4_4.sce
clear; clc; v3=20; v2=15; //putting v1=15/(1+k) s=poly([-1 5 3],"x","coeff"); K=roots(s); k=K(2) v1=15/(1+k); //disp(v1) x=v1(1); //disp(x); vnew=x+v3+v2; xl=sqrt(3)*vnew; n=vnew/(3*v3); mprintf("capacitance ratio= %.2f \nthe line to neutral voltage= %.1fkV \n string efficiency=%.1fpercent",k,xl,n*100);
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// Scilab Code Ex9.5 Change in voltage across a G.M. tube: Pg:202 (2008) e= 1.6e-019; // Charge on an electron, coulomb W = 25; // Ionization potential of gas (Ar/N2), eV E = 5e+06; // Energy of incident alpha particles, eV C = 1e-010; // Capacity of the system, farad N = E/W; // Number of ions produced delta_V = N*e/C; // Change in voltage across the G.M. tube, volt printf("\nThe change in voltage across the G.M. tube = %3.1e volt", delta_V); // Result // The change in voltage across the G.M. tube = 3.2e-004 volt
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mdaqAIScanInit.sci
function mdaqAIScanInit(arg1, arg2, arg3, arg4, arg5, arg6) link_id = -1; if argn(2) == 5 then channels = arg1; aiRange = arg2; aiMode = arg3; scan_freq = arg4; scan_time = arg5; end if argn(2) == 6 then link_id = arg1; channels = arg2; aiRange = arg3; aiMode = arg4; scan_freq = arg5; scan_time = arg6; if link_id < 0 then error("Invalid connection ID!") return; end end global %microdaq; if %microdaq.private.mdaq_hwid <> [] then adc_info = get_adc_info(%microdaq.private.mdaq_hwid); if argn(2) > 6 | argn(2) < 5 then mprintf("Description:\n"); mprintf("\tInitiates AI scanning session\n"); mprintf("Usage:\n"); mprintf("\tmdaqAIScanInit(linkID, channels, range, isDifferential, rate, duration)\n"); mprintf("\tlinkID - connection id returned by mdaqOpen() (OPTIONAL)\n"); mprintf("\tchannels - analog input channels to read\n"); mprintf("\trange - analog input range matrix e.g.\n"); mprintf("\t [-10,10] - single range argument applied for all used channels\n"); mprintf("\t [-10,10;-5,5] - multi-range argument for two channels\n"); mprintf("\tisDifferential - scalar or vector with measurement mode settings: %s - differential, %s - single-ended mode\n", "%T", "%F"); mprintf("\trate - scans per second rate (scan frequency)\n"); mprintf("\tduration - scan duration in seconds\n"); return; end else error('Unable to detect MicroDAQ configuration. Run mdaqHWInfo() function.'); end ch_count = size(channels, 'c'); if scan_time < 0 then scan_time = -1; end if size(channels, 'r') > 1 then error('Wrong channel - scalar or single row vector expected') end if size(aiRange, 'c') <> 2 then error('Wrong range - matrix range [low,high;low,high;...] expected') end aiRangeSize = size(aiRange, 'r'); if aiRangeSize <> 1 & aiRangeSize <> ch_count then error('Range vector should match selected AI channels') end if type(aiMode) == 1 then if size(find(aiMode>1), '*') > 0 error('Wrong mode (isDifferential parameter) - boolean value expected (%T/1, %F/0)') end end if size(aiMode, 'r') > 1 then error('Wrong mode (isDifferential parameter) - scalar or single row vector expected') end aiModeSize = size(aiMode, 'c'); if aiModeSize <> 1 & aiModeSize <> ch_count then error('Mode (isDifferential parameter) vector should match selected AI channels') end if aiRangeSize == 1 then range_tmp = aiRange; aiRange = ones(ch_count,2); aiRange(:,1) = range_tmp(1); aiRange(:,2) = range_tmp(2); clear range_tmp; end aiRange_t = aiRange; aiRange = matrix(aiRange', 1, ch_count*2); aiMode(find(aiMode==%T))=1; if aiModeSize == 1 then aiMode = ones(1, ch_count) * aiMode; end if argn(2) == 5 then link_id = mdaqOpen(); if link_id < 0 then error("Unable to connect to MicroDAQ device!"); end end result = []; real_freq = scan_freq; [result real_freq] = call("sci_mlink_ai_scan_init",.. link_id, 1, "i",.. channels, 2, "i",.. ch_count, 3, "i",.. aiRange, 4, "d",.. aiMode, 5, "i",.. scan_freq, 6, "d",.. scan_time, 7, "d",.. "out",.. [1, 1], 9, "i",.. [1, 1], 8, "d"); if result < 0 & result <> -88 then if argn(2) == 5 then mdaqClose(link_id); end error(mdaq_error2(result), 10000 + abs(result)); else if result == -88 then disp("Warninng: AI scanning interrupted!") mdaqAIScanStop() // time to terminate TCP connection sleep(200); [result real_freq] = call("sci_mlink_ai_scan_init",.. link_id, 1, "i",.. channels, 2, "i",.. ch_count, 3, "i",.. aiRange, 4, "d",.. aiMode, 5, "i",.. scan_freq, 6, "d",.. scan_time, 7, "d",.. "out",.. [1, 1], 9, "i",.. [1, 1], 8, "d"); end if argn(2) == 5 then mdaqClose(link_id); end if result < 0 then error(mdaq_error2(result), 10000 + abs(result)); end if result == 1 then limited_cap = %t; else limited_cap = %f; end rows = []; row = ''; adc_res = strtod(part(adc_info.resolution, 1:2)) for j=1:ch_count if aiMode(j) == 1 then measure_type = "Differential" elseif (aiMode(j) == 0) measure_type = "Single-ended" end adc_range = aiRange_t(j, 2) - aiRange_t(j, 1); resolution = string((int(adc_range/2^adc_res * 1000000)) / 1000); rangeStr=""; if aiRange_t(j, 1) < 0 then rangeStr = "±" + string(aiRange_t(j, 2))+"V"; else rangeStr = "0-" + string(aiRange_t(j, 2))+"V"; end rows = [rows; "AI"+string(channels(j)), measure_type, rangeStr, resolution+"mV"] end mprintf("\nAnalog input scanning session settings:\n"); mprintf("\t--------------------------------------------------\n") str2table(rows, ["Channel", "Measurement type", "Range", "Resolution"], 3) mprintf("\t--------------------------------------------------\n") if scan_freq >= 1000 mprintf("\tScan frequency:\t\t%.5f kHz\n", scan_freq/1000); mprintf("\tActual scan frequency:\t%.5f kHz\n", real_freq/1000); else mprintf("\tScan frequency:\t\t%.5f Hz\n", scan_freq); mprintf("\tActual scan frequency:\t%.5f Hz\n", real_freq); end if 1 /real_freq > 0.001 then mprintf("\tScan period: \t\t%.5f seconds\n", 1 / real_freq); end if 1 /real_freq <= 0.001 then mprintf("\tScan period: \t\t%.5f ms\n", 1 / real_freq * 1000); end if scan_time < 0 mprintf("\tNumber of channels:\t%d\n", ch_count) mprintf("\tNumber of scans:\tInf\n"); mprintf("\tDuration:\t\tInf\n"); else mprintf("\tNumber of channels:\t%d\n", ch_count) mprintf("\tNumber of scans:\t%d\n", scan_time * scan_freq); if scan_time == 1 mprintf("\tDuration:\t\t%.2f second\n", scan_time); else mprintf("\tDuration:\t\t%.2f seconds\n", scan_time); end end mprintf("\t--------------------------------------------------\n") end endfunction
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clear //Given C1=2 //micro F C2=2 //micro F C3=2 C4=2 //Calculation Cs=C1*C2/(C1+C2) Cab=C3*C4/(C3+C4) //Result printf("\n The capacitance of the Capacitors %0.3f micro F", Cab)
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3_6.sce
//mason's gain formula applied to SFG in figure 3-16 //y2 as output node syms G1 G2 G3 G4 G5 H1 H2 H3 H4 M1=1 L11=-G1*H1 L21=-G3*H2 L31=G1*G2*G3*-H3 L41=-H4 L12=G1*H1*G3*H2 L22=G1*H1*H4 L32=G3*H2*H4 L42=-G1*G2*G3*H3*H4 L13=-G1*H1*G3*H2*H4 delta=1-(L11+L21+L31+L41)+(L12+L22+L32+L42)+L13 delta1=1-(L21+L41)+(L32) x=M1*delta1/delta disp(x,"y2/y1=") //y7 as output node M1=G1*G2*G3*G4 M2=G1*G5 delta1=1 delta2=1-(L21) y=(M1*delta1+M2*delta2)/delta disp(y,"y7/y1=") z=y/x // (y7/y2)=(y7/y1)/(y2/y1) disp(z,"y7/y2=")
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clc //initialisation of variables t=10//C s=74.2//days c=0.01//mm d=245//mm //CALCULATIONS h=s/(d*c)//cm //RESULTS printf('the high will water at a temperature =% f cm',h)
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PL/SQL Developer Test script 3.0 8 -- Created on 2014/8/25 by XINHUAZHOU declare -- Local variables here i integer; begin -- Test statements here sys.dbms_job.run(job => i); end; 0 0
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equil.sci
function [t]=equil(p,q) t=chol(q); [u,s,u]=svd(t*p*t'); s=diag(s); ll=ones(s)./sqrt(sqrt(s)); t=diag(ll)*u'*t
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function Y=cleancomplex(X) e=1D-14 n=length(X) Y=X; for i=1:n if(abs(X(i))<e) Y(i)=0 else if(abs(real(X(i)))<e) Y(i) = %i*imag(X(i)) else if (abs(imag(X(i)))<e) Y(i) = real(X(i)) end end end end endfunction
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Ex2_4.sce
//Initilization of variables Tac=3.5 //kN Tbc=3.5 //kN alpha=20 //degree //angle made by Tac with -ve X axis beta=50 //degree //angle made by Tbc with +ve X axis //Calculations theta=atand(((Tac*sind(alpha))+(Tbc*sind(beta)))/((Tac*cosd(alpha))-(Tbc*cosd(beta)))) //degree P=Tac*(cosd(alpha)-cosd(beta))/(cosd(theta)) //kN // from eq'n 1 //Results clc printf('The maximum force that can be applied is %f kN \n',P) printf('The direction of applied force is %f degree \n',theta)
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Example_16_6.sci
clear; clc; printf("\n Example 16.6"); H = 0.036; //Humidity is in kg/kg at 811 K //Taking R as 90 per cent and P as 101.3 kN/m2, then, for assumed values of Tb of 321, 333 and 344 K //Pw = 13,20 and 32 kN/m2, respectively //G = 27.8, 12.9 and 6.02 kg/s, respectively. //for Tb = 321, 333 and 344 K, //G = 7.16, 7.8 and 7.54 kg/s respectively. Tb = [321 333 344]; G1 = [27.8 12.9 6.02]; //Temperature is in kelvins G = [7.16 7.8 7.54]; //flow rate in kg/secs plot2d(Tb,G,style=3); plot2d(Tb,G1,style=2); xtitle("Temperature vs Flow rate","Temperature Tb(K)","Flow rate G(kg/secs)"); //Plotting G against Tb for each equation on the same axis, then Go = 8.3; //Gas flow rate is in kg/secs Tb = 340; //temperature is in Kelvins uf = 0.61; //velocity is in m/secs D = sqrt(340*(8.3+(1.58*1.26))/(278*0.61)); printf("\n D = %.2f m",D);
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//Chapter-10,Example 9,Page 255 clc(); close(); E0_Ag = 0.799 //standard potential for copper Ksp=8.3*10^-17 I=1 Ag= Ksp/I n= 2 R=8.314 //gas constant F=96500 //Farade's constant n=2 T=298 //temperature in Kelvin E_Ag=E0_Ag+(2.303*R*T/(n*F))*log10(Ag) printf('the single electrode potential of Ag is %.5f V ',E_Ag)
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clear; clc; v=220; s=5; z=4.5; Vb=11; sb=50; Zb=(Vb^2)/s; Zpu=z/Zb; mprintf("pu leakage reactance is %f\n",Zpu); a=Vb/v; Zs=z/(a^2); //case2 vb1=220; Zb1=(vb1^2)/s; Zpu1=Zs/Zb1; mprintf("Ratio of pu leakage reactances are %f",Zpu1);
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*Testcase fix-page: Test the Fix Page E502 Assist # Created and placed into the public domain 09 OCT 2020 by Bob Polmanter. # Runtest *Compare dependency removed on 2022-03-08 by Fish. # Suppress logging of program checks. Processing of this test script # intentionally generates program checks as it runs as part of the # instuction's test and validation. ostailor quiet archlvl S/370 sysclear loadcore "$(testpath)/fix-page.core" runtest ostailor default *Done
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clc; l=0.1; //length in m A=10^-4; //area in m square R=0.01; //resistance in Ohm p=(A*R)/l; //calculating resistivity disp(p,"Resistivity in Ohm metre = "); //displaying result
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#************************************************************ # Scenario of Ikea # # date : Thu Aug 23 16:43:06 2012 #************************************************************ p3d_sel_desc_name P3D_ENV Ikea p3d_sel_desc_name P3D_ROBOT HUMAN_ACHILE p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 1.604000 -1.790000 0.760000 1.116000 0.830000 135.000000 0.000000 0.000000 14.540000 -30.350000 9.770000 7.740000 72.995000 22.460000 -6.399000 16.856000 3.330000 -148.270000 -8.210000 -76.970000 30.000000 -4.790000 -34.400000 0.000000 -100.420000 0.000000 4.320000 -80.930000 8.000000 84.360000 0.000000 0.000000 0.000000 4.760000 -83.140000 -0.210000 94.570000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -10.000000 0.000000 0.000000 0.000000 0.000000 -180.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT JUSTIN_ROBOT p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -0.102000 -1.282000 20.772000 -47.384000 -20.972493 69.017768 -48.045275 -1.327433 3.871682 -45.000000 -94.000000 -50.000000 115.000000 2.000000 14.000000 40.000000 25.841768 -111.803735 -45.594000 69.898098 33.291390 -27.455391 6.043048 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.470044 -1.892000 1.112000 -13.845620 16.481564 -169.873548 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -0.102000 -1.282000 20.772000 -47.384000 -20.972493 69.017768 -48.045275 -1.327433 3.871682 -45.000000 -94.000000 -50.000000 115.000000 2.000000 14.000000 40.000000 44.482241 -77.122447 -35.972000 84.496293 16.680790 17.970387 -38.622868 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.965000 -1.614000 1.360538 23.587517 -22.056058 -106.344000 p3d_constraint p3d_kuka_arm_ik 6 10 11 13 14 15 16 1 29 0 3 12 1 3 p3d_constraint p3d_kuka_arm_ik 6 18 19 21 22 23 24 1 30 0 3 20 -1 1 p3d_set_cntrt_Tatt 1 -0.982797 0.018403 -0.183754 -0.036039 -0.003530 0.992963 0.118341 -0.346482 0.184640 0.116955 -0.975819 -0.017708 p3d_constraint p3d_fix_jnts_relpos 1 30 1 24 0 0 p3d_set_cntrt_Tatt 2 -0.982795 -0.003528 0.184639 -0.033370 0.018406 0.992963 0.116959 0.346768 -0.183752 0.118344 -0.975820 0.017099 p3d_constraint p3d_fixed_jnt 1 29 0 6 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0 p3d_constraint p3d_min_max_dofs 0 2 4 3 2 0.000000 135.000000 0 p3d_constraint p3d_lin_rel_dofs 1 5 2 3 4 3 -1.000000 -1.000000 0.000000 0 p3d_constraint p3d_fixed_jnt 1 1 0 3 1.020000 -0.440000 -53.460000 0 p3d_constraint p3d_fixed_jnt 1 7 0 1 -1.327433 0 p3d_constraint p3d_fixed_jnt 1 8 0 1 3.871682 0 p3d_constraint p3d_fixed_jnt 1 10 0 1 -45.000000 0 p3d_constraint p3d_fixed_jnt 1 11 0 1 -94.000000 0 p3d_constraint p3d_fixed_jnt 1 12 0 1 -50.000000 0 p3d_constraint p3d_fixed_jnt 1 13 0 1 115.000000 0 p3d_constraint p3d_fixed_jnt 1 14 0 1 2.000000 0 p3d_constraint p3d_fixed_jnt 1 15 0 1 14.000000 0 p3d_constraint p3d_fixed_jnt 1 16 0 1 40.000000 0 p3d_set_object_base_and_arm_constraints 29 1 0 2 0 1 p3d_set_arm_data 0 3 29 p3d_set_arm_data 1 3 30 p3d_sel_desc_name P3D_ROBOT Lampe p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.766000 -1.740000 0.770000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT Assiette p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 1.020000 -1.470000 0.787611 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT Pommes p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.442478 -1.622419 0.762537 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT Verre p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -6.156000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT Tabouret p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -13.930000 0.220000 0.000000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT sailLamp1 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -3.743000 -0.090000 0.286000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT sailLamp2 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 -3.200000 0.000000 0.573000 0.000000 0.000000 0.000000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_sel_desc_name P3D_ROBOT sailLamp3 p3d_set_robot_steering_method Linear p3d_set_robot_current 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.760000 -1.712000 2.501000 0.000000 0.000000 -19.300000 p3d_set_robot_goto 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 0.000000 p3d_set_camera_pos 0.441313 -1.179626 0.716971 2.521610 5.223810 0.747500 0.000000 0.000000 1.000000 0.000000
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// Problem 3.1,Page no.54 clc;clear; close; P=40 //mm //Force applied to stretch a tape L=30 //m //Length of steel tape A=6*1 //mm //Cross section area E=200*10**9*10**-6 //KN/m**2 //Modulus of Elasticity //Calculations sigma_L=(P*L*10**3)*(A*E)**-1 //mm //Result printf("The Elongation of steel tape is %.1f mm",sigma_L)
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// Copyright (C) 2018 - IIT Bombay - FOSSEE // // This file must be used under the terms of the CeCILL. // This source file is licensed as described in the file COPYING, which // you should have received as part of this distribution. The terms // are also available at // http://www.cecill.info/licences/Licence_CeCILL_V2-en.txt // Original Source : https://octave.sourceforge.io/signal/ // Modifieded by:Sonu Sharma, RGIT Mumbai // Organization: FOSSEE, IIT Bombay // Email: toolbox@scilab.in function [n, Wp] = ellipord(Wp, Ws, Rp, Rs) //Minimum filter order of a digital elliptic or Cauer filter with the desired response characteristics. //Calling Sequence //[n] = ellipord(Wp, Ws, Rp, Rs) //[n, Wp] = ellipord(Wp, Ws, Rp, Rs) //Parameters //Wp: scalar or vector of length 2 (passband edge(s)), all elements must be in the range [0,1] //Ws: scalar or vector of length 2 (stopband edge(s)), all elements must be in the range [0,1] //Rp: passband ripple in dB. //Rs: stopband attenuation in dB. //n: Minimum order of filter satisfying given specs. //Description //This function computes the minimum filter order of an elliptic filter with the desired response characteristics. //Stopband frequency ws and passband frequency wp specify the the filter frequency band edges. //Frequencies are normalized to the Nyquist frequency in the range [0,1]. //Rp is measured in decibels and is the allowable passband ripple and Rs is also measured in decibels and is the minimum attenuation in the stop band. //If ws>wp then the filter is a low pass filter. If wp>ws, then the filter is a high pass filter. //If wp and ws are vectors of length 2, then the passband interval is defined by wp and the stopband interval is defined by ws. //If wp is contained within the lower and upper limits of ws, the filter is a band-pass filter. If ws is contained within the lower and upper limits of wp, the filter is a band-stop or band-reject filter. //Examples //Wp = [60 200]/500; //Ws = [50 250]/500; //Rp = 3; //Rs = 40; //[n,Wp] = ellipord(Wp,Ws,Rp,Rs) //Output : // Wp = // // 0.12 0.4 // n = // // 5. funcprot(0); [nargout nargin] = argn(); if (nargin ~= 4) error("ellipord: invalid number of inputs"); else validate_filter_bands ("ellipord", Wp, Ws); end // sampling frequency of 2 Hz T = 2; Wpw = tan(%pi.*Wp./T); // prewarp Wsw = tan(%pi.*Ws./T); // prewarp // pass/stop band to low pass filter transform: if (length(Wpw)==2 & length(Wsw)==2) wp=1; w02 = Wpw(1) * Wpw(2); // Central frequency of stop/pass band (square) w3 = w02/Wsw(2); w4 = w02/Wsw(1); if (w3 > Wsw(1)) ws = (Wsw(2)-w3)/(Wpw(2)-Wpw(1)); elseif (w4 < Wsw(2)) ws = (w4-Wsw(1))/(Wpw(2)-Wpw(1)); else ws = (Wsw(2)-Wsw(1))/(Wpw(2)-Wpw(1)); end elseif (Wpw > Wsw) wp = Wsw; ws = Wpw; else wp = Wpw; ws = Wsw; end k=wp/ws; k1=sqrt(1-k^2); q0=(1/2)*((1-sqrt(k1))/(1+sqrt(k1))); q= q0 + 2*q0^5 + 15*q0^9 + 150*q0^13; //(....) D=(10^(0.1*Rs)-1)/(10^(0.1*Rp)-1); n=ceil(log10(16*D)/log10(1/q)); endfunction
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// exa 3.8 Pg 70 clc;clear;close; // Given Data M=15;// N.m P=5;// kW N=500;// rpm tau_d=40;// Mpa sigma_d=58;// MPa T=P*60*10**3/(2*%pi*N);// N.m Te=sqrt(M**2+T**2);// N.m //Te=(%pi/16)*d**3*tau_d d=(Te/((%pi/16)*tau_d)*1000)**(1/3);// mm printf('\n Using equivalent torque equation,\n shaft diameter d = %.f mm',d) Me=(1/2)*(M+sqrt(M**2+T**2));// N.m //Me=(%pi/32)*d**3*sigma_d d=(Me/((%pi/32)*sigma_d)*10**3)**(1/3);//mm printf('\n Using equivalent bending moment equation,\n shaft diameter d = %.2f mm or %.f mm',d, ceil(d)) printf('\n Adopt d=23 mm.')
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<?xml version="1.0" encoding="UTF-8"?> <!DOCTYPE html PUBLIC "-//W3C//DTD XHTML 1.0 Transitional//EN" "http://www.w3.org/TR/xhtml1/DTD/xhtml1-transitional.dtd"> <html xmlns="http://www.w3.org/1999/xhtml"> <head> <meta http-equiv="Content-Type" content="application/xhtml+xml;charset=UTF-8" /> <meta name="robots" content="noindex, nofollow" /> <link rel="stylesheet" title="common" type="text/css" href="stylesheet.css" /> <title>CheckDig Main Page</title> </head> <body> <!-- function="iban", parm1="", parm2=" --> <h2>Checkdigits</h2> <form action="servlet" method="post"> <table> <tr><th align="left">Check Method</th> <th>&nbsp;</th> <th align="left">Number to be checked</th> </tr> <tr valign="top"> <td><select name="function" size="11"> <option value="acc">German Bank Account Number (+ BLZ)</option> <option value="ean">Internat. Article Number (EAN)</option> <option value="iban" selected>Internat. Bank Account Number (IBAN)</option> <option value="isbn">Internat. Standard Book Number (ISBN)</option> <option value="isin">Internat. Stock Id Number (ISIN)</option> <option value="ismn">Internat. Standard Music Number (ISMN)</option> <option value="issn">Internat. Standard Serial Number (ISSN)</option> <option value="pnd">Person-Name Database Id (PND-Id)</option> <option value="taxid">German Tax Identification Number</option> <option value="uci">SEPA Unique Creditor Id (UCI)</option> <option value="vat">European Value Added Tax (VAT) Id</option> </select> <br /> <a title="account" href="spec/de_account.xml">XML definition</a> of <br />&nbsp;&nbsp;German account check methods<br /> <a title="xsl" href="xslt/account.xsl">Stylesheet</a> generating<br />&nbsp;&nbsp;corresponding Java Methods<br /> <a title="deblz" href="servlet?spec=blz/blz_search">German BLZ search</a><br /> <a title="wiki" href="http://www.teherba.org/index.php/CheckDig" target="_new">Wiki</a> Documentation<br /> <a title="github" href="https://github.com/gfis/checkdig" target="_new">Git Repository</a><br /> <a title="api" href="docs/api/index.html">Java API</a> Documentation<br /> <a title="manifest" href="servlet?view=manifest">Manifest</a>, <a title="license" href="servlet?view=license">License</a>, <a title="notice" href="servlet?view=notice">References</a><br /> </td> <td>&nbsp;&nbsp;&nbsp;&nbsp;</td> <td> <input name="parm1" maxsize="80" size="40" value=""/> <br />&nbsp; <br />Optional Parameter (BLZ): <br /> <input name="parm2" maxsize="80" size="40" value=""/> <br /> <input type="submit" value="Submit"> <h3> <pre> AD<span class="OK">12</span> 0001 2030 2003 5910 0100 !OK AT<span class="OK">61</span> 1904 3002 3457 3201 !OK AT<span class="OK">35</span> 1200 0515 6805 2701 !OK BE<span class="OK">68</span> 5390 0754 7034 !OK BE<span class="OK">62</span> 5100 0754 7061 !OK CH<span class="OK">93</span> 0076 2011 6238 5295 7 !OK CY<span class="OK">17</span> 0020 0128 0000 0012 0052 7600 !OK CZ<span class="OK">65</span> 0800 0000 1920 0014 5399 !OK DE<span class="OK">89</span> 3704 0044 0532 0130 00 !OK DK<span class="OK">50</span> 0040 0440 1162 43 !OK EE<span class="OK">38</span> 2200 2210 2014 5685 !OK ES<span class="OK">91</span> 2100 0418 4502 0005 1332 !OK FI<span class="OK">21</span> 1234 5600 0007 85 !OK FO<span class="OK">62</span> 6460 0001 6316 34 !OK FO<span class="OK">95</span> 6460 0002 0016 77 !OK FO<span class="OK">36</span> 9181 0002 9324 33 !OK FR<span class="OK">76</span> 1820 6000 1030 5696 6400 117 !OK FR<span class="OK">14</span> 2004 1010 0505 0001 3M02 606 !OK GB<span class="OK">29</span> NWBK 6016 1331 9268 19 !OK GL<span class="OK">50</span> 6471 0001 4414 82 !OK GL<span class="OK">41</span> 6471 0001 0015 55 !OK GI<span class="OK">75</span> NWBK 0000 0000 7099 453 !OK GR<span class="OK">16</span> 0110 1250 0000 0001 2300 695 !OK HR<span class="OK">12</span> 1001 0051 8630 0016 0 !OK HU<span class="OK">42</span> 1177 3016 1111 1018 0000 0000 !OK IE<span class="OK">29</span> AIBK 9311 5212 3456 78 !OK IL<span class="OK">62</span> 0108 0000 0009 9999 999 !OK IS<span class="OK">14</span> 0159 2600 7654 5510 7303 39 !OK IT<span class="OK">60</span> X054 2811 1010 0000 0123 456 !OK LI<span class="OK">21</span> 0881 0000 2324 013A A !OK LV<span class="OK">80</span> BANK 0000 4351 9500 1 !OK LT<span class="OK">12</span> 1000 0111 0100 1000 !OK LU<span class="OK">28</span> 0019 4006 4475 0000 !OK MC<span class="OK">58</span> 1244 8610 1776 1053 3010 111 !OK MC<span class="OK">75</span> 1273 9000 7201 0919 0000 J37 !OK MC<span class="OK">58</span> 1149 8000 0162 5023 9000 377 !OK MC<span class="OK">58</span> 1261 9000 2300 0038 2435 419 !OK MC<span class="OK">10</span> 1273 9000 7201 1468 3000 U30 !OK MK<span class="OK">07</span> 3000 0000 0042 425 !FORM MT<span class="OK">84</span> MALT 0110 0001 2345 MTLC AST0 01S !OK NL<span class="OK">91</span> ABNA 0417 1643 00 !OK NO<span class="OK">93</span> 8601 1117 947 !OK PL<span class="OK">27</span> 1140 2004 0000 3002 0135 5387 !OK PT<span class="OK">50</span> 0002 0123 1234 5678 9015 4 !OK RO<span class="OK">49</span> AAAA 1B31 0075 9384 0000 !OK CS<span class="OK">73</span> 2600 0560 1001 6113 79 !OK SA<span class="OK">03</span> 8000 0000 6080 1016 7519 !OK SE<span class="OK">35</span> 5000 0000 0549 1000 0003 !OK SI<span class="OK">56</span> 1910 0000 0123 438 !OK SK<span class="OK">31</span> 1200 0000 1987 4263 7541 !OK SM<span class="OK">86</span> U032 2509 8000 0000 0270 100 !OK TN<span class="OK">59</span> 1420 7207 1007 0712 9648 !OK TR<span class="OK">62</span> 0001 2009 8890 0058 0088 88 !OK TR<span class="OK">07</span> 0006 2000 0140 0006 2996 08 !OK ?CHAR DE<span class="NOK">20</span> 6601 0075 0352 3097 57 ?NOK DE<span class="NOK">50</span> 6723 0000 4059 5290 56 ?NOK </pre> </h3> </td> </tr> </table> </form> <!-- language="en", features="quest" --> <p><span style="font-size:small"> Questions, remarks: email to <a href="mailto:punctum@punctum.com?&subject=CheckDig">Dr. Georg Fischer</a></span></p> </body></html>
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// Exampple 8.1 //Write a program to read a series of words from terminal using scanf function. //Read data using scanf function disp("Enter text:") [word1,word2,word3,word4]=scanf("%s %s %s %s"); //Printing the results printf("word1 = %s\nword2 = %s\n",word1,word2); printf("word3 = %s\nword4 = %s\n",word3,word4);
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// Example 7_5 clc;funcprot(0); // Given data m=0.035;// kg p_1=0.100;// MPa T_1=20.0;// °C p_2=5.00;// MPa k=1.4;// The specific heat ratio for air R_air=0.286;// kJ/kg.K // Solution T_2=((T_1+273.15)*(p_2/p_1)^((k-1)/k))-273.15;// °C v_1=(m*R_air*(T_1+273.15))/(p_1*10^3);// m^3/kg v_2=v_1*((T_2+273.15)/(T_1+273.15))^(1/(1-k));// m^3/kg printf('\nThe final temperature,T_2=%3.0f°C \nThe specific volume of the air,v_2=%0.5f m^3/kg',T_2,v_2);
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// chapter 14 // example 14.11 // Determine the firing angle, power factor, active power and reactive power at rated speed and its 10 % and their ratio // page-886-887 clear; clc; // given P=100; // in kW (power rating of motor) N=1000; // in rpm Ea=460; // in V I=300; // in A E=415; // in V (3 phase input voltage) neta=10; // in % (% of rated speed for new speed) // calculate P=P*1E3; Em=sqrt(2/3)*E; // calculation of peak value of phase voltage // since Ea=(3*sqrt(3)*Em/%pi)*cosd(alpha), therefore we get alpha1=acosd((Ea/Em)*(%pi/(3*sqrt(3)))); PF1=cosd(alpha1); Ea_alpha=(neta/100)*Ea; alpha2=acosd((Ea_alpha/Em)*(%pi/(3*sqrt(3)))); PF2=cosd(alpha2); Ia=P/Ea; I=sqrt(2/3)*Ia; P_active1=sqrt(3)*E*I*cosd(alpha1); P_reactive1=sqrt(3)*E*I*sind(alpha1); P_active2=sqrt(3)*E*I*cosd(alpha2); P_reactive2=sqrt(3)*E*I*sind(alpha2); ratio=P_reactive2/P_reactive1; printf("\nAt rated speed, the firing angle is \t alpha=%.2f degree and the power factor is \t PF=%.2f",alpha1,PF1); printf("\n\nAt %.f %% rated speed, the firing angle is \t alpha=%.2f degree and the power factor is \t PF=%.3f",neta,alpha2,PF2); printf("\n\nAt rated speed, the active power is \t P_active=%.1f kW and reactive power is \t P_reactive=%.2f kVAR",P_active1*1E-3,P_reactive1*1E-3); printf("\n\nAt %.f %% rated speed, the active power is \t P_active=%.2f kW and reactive power is \t P_reactive=%.2f kVAR",neta,P_active2*1E-3,P_reactive2*1E-3); printf("\n\nThe ratio of reactive power at %.f %% rated speed and rated speed is %.2f",neta,ratio); // Note: The answer vary slightly due to precise calculations
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//clc() MKClO3 = 122.55 mKClO3 = 100;//kg NKClO3 = mKClO3 / MKClO3; NO2 = 3 * NKClO3 / 2; V1 = 22.4143;//m^3/kmol; V = V1 * NO2; disp("m^3",V,"volume of oxygen produced = ")
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clear; clc; exec('/home/debdeep/Desktop/TEST NOW!!/impzlength.sci'); b = [1+3*%i -0.9 2 3 4 4]; a=[1 -0.9 2 3 4 4]; len = impzlength(b,a); disp(len); //output //!--error 246 //Function not defined for given argument type(s), // check arguments or define function %p_bezout for overloading. //at line 31 of function gcd called by : //at line 54 of function impzlength called by : //len = impzlength(b,a); //matlab // 20
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clc k = 12400 // constant lambda = 6943 // wavelength of radiation in angstrom n = 3e19 // Total number of ions // Sample Problem 5 on page no. 243 printf("\n # PROBLEM 5 # \n") E = k/(lambda) // Energy difference E_total = E*n*1.6e-19 // Total Energy emitted printf("\n Energy of one photon is %feV. \n Total energy is %fJ",E,E_total)
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function [c] = PCM_Encoding(x,L,en_code) //Encoding:Converting Quantized decimal sample values into binary //x=input sequence //L=number of qunatization levels //encode=normalized input sequence n=log2(L); c=zeros(length(x),n); fori=1:length(x) forj=n:-1:0 if(fix(en_code(i)/(2^j))==1) c(i,(n-j))=1; en_code(i)=en_code(i)-2^j; end end end disp(c)
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//chapter 3 //example 3.21 //page 167 Ro=100; x=0.00392; T1=25;//temp at 25c R(25)=Ro*(1+(x*T1)); disp(R(25))// resistance at 25 degree T2=100; R(100)=Ro*(1+(x*T2)); disp(R(100))//resistance at 100 degree
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//Section-14,Example-4,Page no.-PC.113 //To calculate the pH in the following cases. clc; K_a=7.3*10^-6 c_1=0.23 //(M) alpha_1=sqrt(K_a/c_1) C_1=c_1*alpha_1 //(M) pH_1=-log10(C_1) disp(pH_1,'pH of the given weak acid') c_2=0.2 //(M) K_b=4.4*10^-5 alpha_2=sqrt(K_b/c_2) C_2=c_2*alpha_2 //[OH-] (M) pOH=-log10(C_2) pH_2=14-pOH disp(pH_2,'pH of CH_3NH_2')
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s = %s; to = 10^-4; num = 1; dem = 1 + to*s; sys = syslin('c', num/dem); t = (0:to/100:7*to)'; y = csim('step', t, sys); plot2d(t, y'); tmp = find(y>=0.95); tr5 = t(tmp(1));
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//clc() T = 510;//K P = 26.6;//bar Tc = 425.2;//K Pc = 38;//bar Zc = 0.274; R = 8.314; Pr = P / Pc; Tr = T / Tc; disp(Pr,"Pr = ") disp(Tr,"Tr = ") //From fig. 5.4 and 5.5 from the text book Z = 0.865; D = 0.15; Z1 = Z + D * ( Zc - 0.27); V = R * T * Z1 / (P * 10^5); disp("m^3/mol",V,"Molar volume of n-butane = ")
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clc;funcprot(0);//Example 2.24 //Initilisation of Variables L1=0.01;....//thickness of blocks in m b=0.08;...//length of blocks in m W=0.06;....//width of blocks in m K1=20;....//thermal conductivity of blocks in W/m*degrees celcius h=10000;....//the contact conductance of 2 blocks W/m^2*degrees celcius T1=120;....//outer temparature of 1st block in degrees celcius T4=70;....//outer temparature of 2nd block in degrees celcius //calculations A=b*W;.....//area of the blocks in m R1=L1/(K1*A);....//resistance of 2 blocks in degrees celcius/W R2=1/(h*A);.....//contact resistance of 2 blocks in degrees celcius/W Q=(T1-T4)/(R1+R2+R1);....//heat transfer through the blocks W T=Q*R2;.....//temparature drop at the interface in degrees celcius disp(Q,"heat transfer through the blocks W:") disp(Q*R2,"temparature drop at the interface in degrees celcius:")
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<?xml version="1.0" encoding="UTF-8"?> <html xmlns="http://www.w3.org/1999/xhtml"><head><title>Namespace Crossreference</title> <link rel="stylesheet" type="text/css" href="stylesheet.css"></link> <style> <!-- dt { font-family:Lucida Console,Courier,monospace; font-weight: bold; } dd { font-family:Lucida Console,Courier,monospace ; } --> </style> </head> <body><h2>List of Namespace URIs</h2> <dl><a href="#http_//www_w3_org/2001/XMLSchema-instance"><dt>http://www.w3.org/2001/XMLSchema-instance</dt> </a> <a href="#http_//www_w3_org/2001/XMLSchema"><dt>http://www.w3.org/2001/XMLSchema</dt> </a> <a href="#urn_iso_std_iso_20022_tech_xsd_camt_052_001_01"><dt>urn:iso:std:iso:20022:tech:xsd:camt.052.001.01</dt> </a> <a href="#urn_iso_std_iso_20022_tech_xsd_pacs_004_001_01"><dt>urn:iso:std:iso:20022:tech:xsd:pacs.004.001.01</dt> </a> <a href="#urn_iso_std_iso_20022_tech_xsd_pacs_006_001_01"><dt>urn:iso:std:iso:20022:tech:xsd:pacs.006.001.01</dt> </a> <a href="#urn_iso_std_iso_20022_tech_xsd_pacs_008_001_01"><dt>urn:iso:std:iso:20022:tech:xsd:pacs.008.001.01</dt> </a> <a href="#urn_iso_std_iso_20022_tech_xsd_pain_001_001_02"><dt>urn:iso:std:iso:20022:tech:xsd:pain.001.001.02</dt> </a> <a href="#urn_iso_std_iso_20022_tech_xsd_pain_002_001_02"><dt>urn:iso:std:iso:20022:tech:xsd:pain.002.001.02</dt> </a> <a href="#urn_iso_std_iso_20022_tech_xsd_pain_008_001_01"><dt>urn:iso:std:iso:20022:tech:xsd:pain.008.001.01</dt> </a> </dl> <h2>Namespace URI and Prefix Crossreference</h2> <dl><dt><a name="http_//www_w3_org/2001/XMLSchema-instance" />http://www.w3.org/2001/XMLSchema-instance</dt> <dd>xsi: pacs.008.001.01.xml</dd> <dd>xsi: pain.001.001.02.xml</dd> <dt><a name="http_//www_w3_org/2001/XMLSchema" />http://www.w3.org/2001/XMLSchema</dt> <dd>xs: camt.052.001.01.xsd</dd> <dd>xs: iso.pacs.008.001.01.xsd</dd> <dd>xs: pacs.004.001.01.xsd</dd> <dd>xs: pacs.006.001.01.xsd</dd> <dd>xs: pacs.008.001.01.xsd</dd> <dd>xs: pain.001.001.02.xsd</dd> <dd>xs: pain.002.001.02.xsd</dd> <dd>xs: pain.008.001.01.xsd</dd> <dt><a name="urn_iso_std_iso_20022_tech_xsd_camt_052_001_01" />urn:iso:std:iso:20022:tech:xsd:camt.052.001.01</dt> <dd>(default): camt.052.001.01.xsd</dd> <dd>(targetNamespace): camt.052.001.01.xsd</dd> <dt><a name="urn_iso_std_iso_20022_tech_xsd_pacs_004_001_01" />urn:iso:std:iso:20022:tech:xsd:pacs.004.001.01</dt> <dd>(default): pacs.004.001.01.xsd</dd> <dd>(targetNamespace): pacs.004.001.01.xsd</dd> <dt><a name="urn_iso_std_iso_20022_tech_xsd_pacs_006_001_01" />urn:iso:std:iso:20022:tech:xsd:pacs.006.001.01</dt> <dd>(default): pacs.006.001.01.xsd</dd> <dd>(targetNamespace): pacs.006.001.01.xsd</dd> <dt><a name="urn_iso_std_iso_20022_tech_xsd_pacs_008_001_01" />urn:iso:std:iso:20022:tech:xsd:pacs.008.001.01</dt> <dd>(default): iso.pacs.008.001.01.xsd</dd> <dd>(targetNamespace): iso.pacs.008.001.01.xsd</dd> <dd>pc8: pacs.008.001.01.xml</dd> <dd>(default): pacs.008.001.01.xsd</dd> <dd>(targetNamespace): pacs.008.001.01.xsd</dd> <dt><a name="urn_iso_std_iso_20022_tech_xsd_pain_001_001_02" />urn:iso:std:iso:20022:tech:xsd:pain.001.001.02</dt> <dd>pi1: pain.001.001.02.xml</dd> <dd>(default): pain.001.001.02.xsd</dd> <dd>(targetNamespace): pain.001.001.02.xsd</dd> <dt><a name="urn_iso_std_iso_20022_tech_xsd_pain_002_001_02" />urn:iso:std:iso:20022:tech:xsd:pain.002.001.02</dt> <dd>(default): pain.002.001.02.xsd</dd> <dd>(targetNamespace): pain.002.001.02.xsd</dd> <dt><a name="urn_iso_std_iso_20022_tech_xsd_pain_008_001_01" />urn:iso:std:iso:20022:tech:xsd:pain.008.001.01</dt> <dd>(default): pain.008.001.01.xsd</dd> <dd>(targetNamespace): pain.008.001.01.xsd</dd> </dl> </body> </html>
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clear all; clc; disp("a)") disp("Convert: 1) Q=5 m^3/s=10595 cfm") disp("2) rhoa=0.0761lbm/ft^3") disp("3) SP=deltap/(rhow*g)") delta_ps=500 rho_w=1000 g=9.8 SP=delta_p/(rho_w*g) printf("Hence SP = %0.3f m",SP) disp("Thus SP= 2.01 in.wg.") disp("b)") disp("Calculating the specific speed:Ns") N_s=1500*((10575)^0.5)/(2.01)^0.75 printf("The value of Ns is equal to %0.2f rpm*(cfm^0.5)/(in of water^0.75)",N_s) N=1500 omega=N*%pi/30 printf("\nOmega = %0.0f rad/s",omega) omega_s=157*(5^0.5)/((500/1.22)^0.75) printf("\nSo omegas = %0.2f ",omega_s) disp("From figure 5.10b,we select v=Dh/Dt=0.5 and the blade number Zb=6*v/(1-v)") v=0.5 Zb=6*v/(1-v) printf("Hence Zb= %0.2f",Zb) disp("From figure 2.2,the specific diameter obtained as deltas is approximately equal to 1.5") D_t=1.5*(5^0.5)/((500/1.22)^0.25) printf("\nHence Dt = %0.3f m",D_t) v=0.5 D_t=0.74//rounded off D_h=v*D_t printf("\nDh= %0.2f m",D_h) A=%pi*(D_t^2)*(1-v^2)/4 printf("\nAlso A = %0.4f m^2",A) D_m=((D_t^2+D_h^2)/2)^0.5 printf("\nDm = %0.4f m",D_m) A=0.322//rounded off Q=5 V_a=Q/A printf("\nVa= %0.1f m/s",V_a) U_m=omega*D_m/2 printf("\nUm = %0.2f",U_m) V_a=15.5//rounded off PHI_m=V_a/U_m printf("\nPHIm = %0.3f",PHI_m) disp("Now from figure 5.10c we can obtain Phim*(s/c)=0.65") //let s/c=x PHI_m=0.337//rounded off x=0.65/PHI_m printf("\nThus (s/c)= %0.2f",x) disp("Here s= pi*Dm/Zb") s= %pi*D_m/Zb printf("\n Thus s= %0.3f m",s) disp("Assuming V1=V3=Va=15.5 m/s the total head can be calculated from g*Ht=deltaps/rho+Va^2/2") //let y=g*Ht=deltaps/rho+(Va^2)/2 rho_a=1.22 y=delta_ps/rho_a+(V_a^2)/2 printf("\ng*Ht = %0.0f (m/s)^2",y) disp("or TP=2.59 in.wg") disp("c)") ETA_h=0.77 V_u2=(y)/(ETA_h*U_m)//Since y=(g*Ht) printf("\nVu2 is equal to %0.0f m/s",V_u2) beta_1=(atan(U_m/V_a))*180/%pi printf("\nß1= %0.2f degrees",beta_1) beta_2=(atan(((U_m-V_u2)/V_a)))*180/%pi printf("\n ß2= %0.2f degrees",beta_2) //let m=tanßm=0.5*(tanß1+tanß2) beta_1=71.3//rounded off beta_2=63.4//rounded off m=0.5*(tan(beta_1*%pi/180)+tan(beta_2*%pi/180)) printf("\ntanßm=0.5*(tanß1+tanß2) =%0.3f",m) beta_m=(atan(m))*180/%pi printf("\n ßm = %0.0f",beta_m) disp("We know that Cl=2*(s/c)*(tanß1-tanß2)*cosßm") x=1.93//rounded off beta_1=71.3 beta_2=63.4 beta_m=68 //Let a=tanß1 //Let b=tanß2 //Letc=cosßm a=tan(beta_1*%pi/180) b=tan(beta_2*%pi/180) c=cos(beta_m*%pi/180) a=2.95//rounded off b=2.0//rounded off c=0.374//rounded off Cl=2*x*(a-b)*c//Since x=(s/c) printf("\nCl= %0.2f ",Cl) disp("This is the cascade coefficient required.To use the isolated airfoil data,we obtain K=1.2 from figure 5.9 with gamma=60 degrees. Hence we can determine Cli") C_li=1.37/1.2 printf("\nCli= %0.2f",C_li) disp("d)") disp("If NACA 4312 airfoil selection is selected,at Alpha=12 degrees,Cli=1.14 and Cl/Cd=L/D=12") disp("Substituting the above mentioned data in Rr=Wmu/Um=phi*tan(ßm)") phi=0.337 d=tan(beta_m*%pi/180) R_r=phi*d printf("\n Thus Rr= %0.3f",R_r) disp("deltar is approximately=deltas is approximately=0.08") Eta_h=0.337*(((0.834-(0.337*0.08))/(0.337+(0.08*0.834)))+((1-0.834-(0.337*0.08))/(0.337+(0.08*(1-0.834))))) printf("\nETAh= %0.2f",Eta_h) disp("Etah=0.80 is approximately equal to 0.77") disp("Also gamma=betam-alpha=68-12=56 degrees") disp("c=s/1.93") c=s/1.93 printf("\nThus c = %0.2f m",c) disp("e)") disp("Double check the data obtained with those given in Figure 5.1.It is shown that Etas=0.74,Ds=0.35=c.") SP=2.01 CFM=10595 Dt=0.35*(CFM^0.5)/(SP^0.25) printf("\nHence the value of Dt= %0.1f in",D_t) disp("On converting,Dt=0.77m") disp("It is close to what we have. However, some alternative design maybe performed with the selection of a little higher hub-tip ratio v and other availabe airfoil sections")
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ex1_17.sce
// Exa 1.17 clc; clear; close; // Given data V1 = 0.7;// in V V2 = 5;// in V V_o = V1-V2;// in V R = 2.2*10^3;// in ohm I_D = -V_o/R; I_D = I_D * 10^3;// in mA disp(V_o,"The output voltage in volts is : ") disp(I_D,"The current through diode in mA is");
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function [r,k]=mtlb_max(a) // Copyright INRIA if size(a,1)==1|size(a,2)==1 then [r,k]=max(a) else [r,k]=max(a,'r') end
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12_4_3.sce
clc; //page no 421 //problem no 12.4.3 SNR=9;//SNR in dB //conversion of dB to power ratio p=10^(9/10); // for Polar Pbe1=1/2 * erfc(sqrt(7.94/2)); disp(Pbe1); // for Unipolar Pbe2=1/2 * erfc(sqrt(7.94)/2); disp(Pbe2);
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ex_4_4.sce
//1.)calculate the stress on the lower washers before the nuts are tightened,refer fig 4.5 //2.)what could be the stress in upper and lower washers... clc //solution //given d=20//mm d1=22//mm d2=50//mm d3=22//mm d4=44//mm P1=120000//N P2=5000//N //1)stress on lower washer before the nuts are tightened pi=3.14 A1=(pi/4)*(d2^2-d1^2)//(mm^2) A2=(pi/4)*(d4^2-d3^2)//(mm^2) //since load is equally distributed on 4 washers,therfore load Q1=P1/4 Q1=P1/4//N //calculating stress on lower washer f2=Q1/A1//(N/mm^2) printf("\n the stress on lower washer when nuts are not tightened is,%f N/mm^2\n",f2) //2) //stres on upper washers P2=5000//N f3=P2/A2//stress//(N/mm^2) printf("the stress on upper washer is,%f N/mm^2\n",f3) //stress on lower washer when nuts are tightened f4=(Q1+P2)/A1//(N/mm^2) printf("the stress on lower washer when nuts are tightened is,%f N/mm^2",f4)
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DictionaryDecoder.tst
load DictionaryDecoder.hdl, output-file DictionaryDecoder.out, compare-to DictionaryDecoder.cmp, output-list in%B1.16.1 outA%B1.16.1 outB%B1.16.1 outC%B1.16.1 outD%B1.16.1; // Loads Dictionary Decoder // Program loads 2 16 bit inputs ROM32K load DictionaryInv.hack, output; set in %B1010000010000010, eval, output; set in %B0100001001000010, eval, output; set in %B0100001101000010, eval, output; set in %B0100001101000100, eval, output; set in %B0100101001000100, eval, output; set in %B1001010110010110, eval, output; // set in %B0100101001001111, eval, output; // set in %B0100101101001111, eval, output; // set in %B0100101101001111, eval, output; // set in %B0100101101001001, eval, output; // set in %B1001000100000100, eval, output; // set in %B0101010101001000, eval, output; // set in %B0100101001001000, eval, output; // set in %B1001010011010011, eval, output; // set in %B1001001011001011, eval, output; // set in %B1001000110000110, eval, output; // set in %B0100111001001000, eval, output; //
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clc; clear; printf("\t\t\tChapter5_example2\n\n\n"); // properties of Freon-12 from appendix table C3 T1_Fr=-50; T2_Fr=-40; rou1_Fr=1.546*1000; rou2_Fr=1.518*1000; beta_Fr=-(rou1_Fr-rou2_Fr)/(rou1_Fr*(T1_Fr-T2_Fr)); printf("\nThe volumetric thermal expansion coefficient calculated for Freon-12 is %.3e /K",beta_Fr); beta_acc_Fr=2.63e-3; // the accurate value of volumetric thermal expansion coefficient for Freon-12 error_Fr=(beta_acc_Fr-beta_Fr)*100/beta_acc_Fr; printf("\nThe error introduced in the case of Freon-12 is %d percent",error_Fr); // properties of helium from appendix table D3 T1_He=366; T2_He=477; rou1_He=0.13280; rou2_He=0.10204; beta_He=-(rou1_He-rou2_He)/(rou1_He*(T1_He-T2_He)); printf("\nThe volumetric thermal expansion coefficient calculated for Freon-12 is %.3e /K",beta_He);
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eg9_10a.sce
x1= [679 1420 1349 296 6975 323 4200 633]; x2 = [30.4 34.1 17.2 26.8 29.1 18.7 32.6 32.5]; y = ones(8,1); y= [11.6 ;16.1; 9.3; 9.1; 8.4; 7.7; 11.3; 8.4]; x = ones(8,3); for i=1:8 x(i,2)= x1(i); x(i,3)= x2(i); end pro1 = x'; //disp(pro1); pro2= pro1*x; //disp(pro2); pro3 = inv(pro2); //disp(pro3); pro4 = pro3*pro1; pro5 = pro4*y; //disp(pro4); //disp(y); B= ones(3,1); for i=1:3 B(i,1)= 0; for k=1:8 B(i,1)=B(i,1)+(pro4(i, k)*y(k, 1)); end end disp(B); //SSR = y'*y - B'*x'y; SSR = y'; SSR= SSR*y; sub = B'; sub = sub*x'; sub= sub*y; SSR =SSR - sub; disp(SSR, "SSr is");
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SPLIT_f.sci
function [x,y,typ]=SPLIT_f(job,arg1,arg2) x=[];y=[],typ=[]; select job case 'plot' then case 'getinputs' then graphics=arg1(2); orig=graphics(1) x=orig(1) y=orig(2) typ=ones(x) case 'getoutputs' then graphics=arg1(2); orig=graphics(1) x=[1 1]*orig(1) y=[1 1]*orig(2) typ=ones(x) case 'getorigin' then [x,y]=standard_origin(arg1) case 'set' then x=arg1; case 'define' then model=list('lsplit',1,3,0,0,[],[],[],[],'c',%f,[%t %f]) x=standard_define([1 1]/2,model) end
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/2417/CH11/EX11.8/Ex11_8.sce
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2020-04-09T02:43:26.499817
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Ex11_8.sce
//scilab 5.4.1 clear; clc; printf("\t\t\tProblem Number 11.8\n\n\n"); // Chapter 11 : Heat Transfer // Problem 11.8 (page no. 561) // Solution deltaX=4/12; //4 inch = 6/12 feet //deltaX=length //unit:ft A=7*2; //area //area=hight*width //unit:ft^2 k=0.090; //Unit:Btu/(hr*ft*F) //k=proportionality constant //k=thermal conductivity for fir //From the table Rfir=deltaX/(k*A); //Resistance of fir //Unit:(hr*F)/Btu printf("For fir,\n"); printf("The resistance is %f (hr*F)/Btu\n\n",Rfir); deltaX=4/12; //4 inch = 6/12 feet //deltaX=length //unit:ft A=7*2; //area //area=hight*width //unit:ft^2 k=0.065; //Unit:Btu/(hr*ft*F) //k=proportionality constant //k=thermal conductivity for pine //From the table Rpine=deltaX/(k*A); //Resistance of pine //Unit:(hr*F)/Btu printf("For pine,\n"); printf("The resistance is %f (hr*F)/Btu\n\n",Rpine); deltaX=4/12; //4 inch = 6/12 feet //deltaX=length //unit:ft A=7*2; //area //area=hight*width //unit:ft^2 k=0.025; //Unit:Btu/(hr*ft*F) //k=proportionality constant //k=thermal conductivity for corkboard //From the table Rcorkboard=deltaX/(k*A); //Resistance of corkboard //Unit:(hr*F)/Btu printf("For corkboard,\n"); printf("The resistance is %f (hr*F)/Btu\n\n",Rcorkboard); Roverall=inv(inv(Rfir)+inv(Rpine)+inv(Rcorkboard)); printf("The overall resistance is %f (hr*F)/Btu\n\n",Roverall); T1=60; //temperature maintained at one face //unit:fahrenheit T2=80; //tempetature maintained at other face //unit:fahrenheit deltaT=T2-T1; //Change in temperature //unit:fahrenheit Qtotal=deltaT/Roverall; //Q=Total Heat loss //Unit:Btu/hr; //ohm's law (fourier's equation) printf("Total Heat loss from the wall is %f Btu/hr\n",abs(Qtotal)); //As a check, Qfir=deltaT/Rfir; //Q=Fir Heat loss //Unit:Btu/hr; //ohm's law (fourier's equation) printf("Heat loss from the wall made of fir is %f Btu/hr\n",abs(Qfir)); Qpine=deltaT/Rpine; //Q=Pine Heat loss //Unit:Btu/hr; //ohm's law (fourier's equation) printf("Heat loss from the wall made of pine is %f Btu/hr\n",abs(Qpine)); Qcorkboard=deltaT/Rcorkboard; //Q=corkboard Heat loss //Unit:Btu/hr; //ohm's law (fourier's equation) printf("Heat loss from the wall made of corkboard is %f Btu/hr\n",abs(Qcorkboard)); Qtotal=Qfir+Qpine+Qcorkboard; //Total Heat loss from the wall //unit:Btu/hr printf("Total Heat loss from the wall is %f Btu/hr\n",abs(Qtotal));
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/2966/CH1/EX1.64/Ex1_64.sce
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//water// //page 1.87 example 4// clc Hardness=500//Hardness of water(mg/lit) or ppm// H=Hardness/100//Hardness of water(gms/lit)// volume_NaCl=100//Volume of NaCl// conc_NaCl=120//% NaCl consumed by zeolite bed// Wt_per_Litre=conc_NaCl*10//gms NaCl consumed by zeolite bed per litre// total_wt=Wt_per_Litre*volume_NaCl//total gms NaCl consumed by zeolite bed// CaCO3_equivalent=total_wt*50/58.48//in terms of (gms/lit)// volume_hardwater=CaCO3_equivalent/H printf("\nQuantity of water softened using zeolite bed is %.f litres",volume_hardwater);
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/1271/CH15/EX15.16/example15_16.sce
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example15_16.sce
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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/Skeet Pistol.sce
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Skeet Pistol.sce
Name=Skeet Pistol PlayerCharacters=Skeet Challenger BotCharacters=Skeet Target.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Skeet Challenger AddedBots=Skeet Target.bot;Skeet Target.bot;Skeet Target.bot;Skeet Target.bot PlayerMaxLives=0 BotMaxLives=0;0;0;0 PlayerTeam=1 BotTeams=2;2;2;2 MapName=skeet_field.map MapScale=1.0 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1.0 ScorePerDamage=0.0 ScorePerKill=1.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=0.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag= WeaponHeroTag=Semi-auto DifficultyTag=3 AuthorsTag=pleasewait, Cody, Sackboy_Clank5 BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=false BlockFCT=true Description=Small parabolic motion targets move to both sides of the map. Shoot them, try not to miss and have to reload! GameVersion=2.0.2.0 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=false LockedFOVMin=60.0 LockedFOVMax=120.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=Skeet Target DodgeProfileNames=Skeet Direction DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=100.0 DodgeProfileMinChangeTime=100.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=Skeet Target SeeThroughWalls=true NoDodging=false NoAiming=true AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Character Profile] Name=Skeet Challenger MaxHealth=100.0 WeaponProfileNames=pistol;;;;;;; MinRespawnDelay=0.000001 MaxRespawnDelay=0.000001 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=36.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=160.0 Acceleration=2560.0 AirAcceleration=16000.0 Friction=1.0 BrakingFrictionFactor=0.5 JumpVelocity=0.0 Gravity=1.0 AirControl=0.25 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=1.000 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=0.000 Y=0.000 Z=1.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=72.0 MainBBRadius=12.0 MainBBHasHead=false MainBBHeadRadius=10.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=72.0 ProjBBRadius=12.0 ProjBBHasHead=false ProjBBHeadRadius=10.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=512.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=Skeet Target MaxHealth=80.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=0.000001 MaxRespawnDelay=0.000001 StepUpHeight=16.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=0.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=160.0 Acceleration=2560.0 AirAcceleration=16000.0 Friction=1.0 BrakingFrictionFactor=0.5 JumpVelocity=0.0 Gravity=1.0 AirControl=0.0 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=1.000 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=0.000 Y=0.000 Z=1.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=256.0 MainBBType=Spheroid MainBBHeight=32.0 MainBBRadius=16.0 MainBBHasHead=false MainBBHeadRadius=10.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Spheroid ProjBBHeight=32.0 ProjBBRadius=16.0 ProjBBHasHead=false ProjBBHeadRadius=10.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=0.3 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=320.0 JetpackAirControlWithThrust=1.0 AbilityProfileNames=Skeet Movement.abilmov;;; HideWeapon=true AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=128.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=true LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=1.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=512.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Skeet Direction MaxTargetDistance=100000.0 MinTargetDistance=0.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.01 MaxLRTimeChange=0.01 MinFBTimeChange=0.01 MaxFBTimeChange=0.01 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.0 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.3 MaxJumpTime=0.6 LeftStrafeTimeMult=10000.0 RightStrafeTimeMult=10000.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.0 BlockedMovementReactionMin=0.1 BlockedMovementReactionMax=0.1 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Weapon Profile] Name=pistol Type=Hitscan ShotsPerClick=1 DamagePerShot=80.0 KnockbackFactor=4.0 TimeBetweenShots=0.1 Pierces=false Category=SemiAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=true HeadshotMultiplier=2.0 MagazineMax=3 AmmoPerShot=1 ReloadTimeFromEmpty=1.0 ReloadTimeFromPartial=1.0 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.08 HitSoundCooldown=0.08 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=0 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=0.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=1.0 TaggingHitFactor=1.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=false AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=false MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=2 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.1 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=None ParticleHitscanTrace=None ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 MinRecoilUp=0.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=false TimeToRecoilPeak=0.05 TimeToRecoilReset=0.35 AAMode=0 AAPreferClosestPlayer=false AAAlpha=1.0 AAMaxSpeed=360.0 AADeadZone=0.0 AAFOV=360.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.175 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Movement Ability Profile] Name=Skeet Movement MaxCharges=1.0 ChargeTimer=2.0 ChargesRefundedOnKill=0.0 DelayAfterUse=0.0 FullyAuto=false AbilityDuration=0.0 LockDirectionForDuration=true NegateGravityForDuration=true MainVelocity=480.0 MainVelocityCanGoVertical=false MainVelocitySetToMovementKeys=true UpVelocity=640.0 EndVelocityFactor=1.0 Hurtbox=false HurtboxRadius=50.0 HurtboxDamage=50.0 HurtboxGroundKnockbackFactor=1.0 HurtboxAirKnockbackFactor=1.0 AbilityBlocksTurning=false AbilityBlocksMovement=true AbilityBlocksAttack=false AttackCancelsAbility=false AbilityReloadsWeapon=false HealthRestore=-40.0 AIUseInCombat=true AIUseOutOfCombat=true AIUseOnGround=true AIUseInAir=true AIReuseTimer=0.01 AIMinSelfHealth=0.0 AIMaxSelfHealth=100.0 AIMinTargHealth=0.0 AIMaxTargHealth=100.0 AIMinTargDist=0.0 AIMaxTargDist=1000000.0 AIMaxTargFOV=360.0 AIDamageReaction=false AIDamageReactionIgnoreChance=0.0 AIDamageReactionMinDelay=0.125 AIDamageReactionMaxDelay=0.25 AIDamageReactionCooldown=1.0 AIDamageReactionThreshold=0.0 AIDamageReactionResetTimer=0.1 [Map Data] reflex map version 8 global entity type WorldSpawn String32 targetGameOverCamera end UInt8 playersMin 1 UInt8 playersMax 16 brush vertices -73.000000 240.000000 320.000000 -308.000000 240.000000 464.000000 -129.000000 240.000000 200.000000 -404.000000 256.000000 368.000000 -129.000000 256.000000 200.000000 -404.000000 240.000000 368.000000 -308.000000 256.000000 464.000000 -73.000000 256.000000 320.000000 faces 0.000000 0.000000 1.000000 1.000000 0.000000 2 0 1 5 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 3 4 2 5 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 3 5 1 6 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 0 2 4 7 0x00000000 0.000000 0.000000 1.000000 1.000000 0.000000 6 1 0 7 0x00000000 0.000000 0.000000 1.000000 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k = 0.0141; //lb.mol/atm.lb cat.h FA0 = 1.08; //lb.mol/h FB0 = 0.54; // lb.mol/h FI = 2.03; // lb.mol/h bita0 = 0.0775; // atm/ft Ac = 0.01414; // ft^2 phi = 0.45; rhoc = 120; // lb cat/ft^3 P0 = 10; // atm X = 0.6;
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// Initilization of variables v_o=500 // m/s // velocity of the projectile alpha=30 // angle at which the projectile is fired t=30 // seconds g=9.81 // m/s^2 // acc due to gravity // Calculations v_x=v_o*cosd(alpha) // m/s // Initial velocity in the horizontal direction v_y=v_o*sind(alpha) // m/s // Initial velocity in the vertical direction // MOTION IN HORIZONTA DIRECTION: V_x=v_x // m/s // V_x=Horizontal velocity after 30 seconds // MOTION IN VERTICAL DIRECTION: // using the eq'n v=u+a*t V_y=v_y-(g*t) // m/s // -ve sign denotes downward motion // Let the Resultant velocity be v_R. It is given as, v_R=sqrt((V_x)^2+(-V_y)^2) // m/s theta=atand((-V_y)/V_x) // degree // direction of the projectile // Results clc printf('The velocity of the projectile is %f m/s \n',v_R) // The answer of velocity is wrong in the text book. printf('The direction of the projectile is %f degree \n',theta) // -ve value of theta indicates that the direction is in downward direction
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//Hougen O.A., Watson K.M., Ragatz R.A., 2004. Chemical process principles Part-1: Material and Energy Balances(II Edition). CBS Publishers & Distributors, New Delhi, pp 504 //Chapter-5, Illustration 4, Page 114 //Title: Calculation of dew point //============================================================================= clear clc //INPUT v1 = 10.1; //Composition by volume of benzene P = [750 750 700]; //Various pressurea in mm Hg at which dew point is to be computed //CALCULATIONS P1 = P(1)*v1/100; //Partial pressure of benzene in mm Hg at 25 degree C and 750 mm Hg T1 = 20; //Temperature in degree C corresponding to pressure P1 obtained from vapor-pressure data of Benzene Fig. 15 Page 84 P2 = P(2)*v1/100; //Partial pressure of benzene in mm Hg at 30 degree C and 750 mm Hg T2 = 20; //Temperature in degree C corresponding to pressure P2 obtained from vapor-pressure data of Benzene Fig. 15 Page 84 P3 = P(3)*v1/100; //Partial pressure of benzene in mm Hg at 30 degree C and 700 mm Hg T3 = 18.7; //Temperature in degree C corresponding to pressure P3 obtained from vapor-pressure data of Benzene Fig. 15 Page 84 //OUTPUT // Console output mprintf('\n Dew point of benzene vapor and air mixture at \n (a) 25 degree C and 750 mm Hg = %2.0f degee C ',T1); mprintf('\n (b) 30 degree C and 750 mm Hg = %2.0f degree C ',T3); mprintf('\n (c) 30 degree C and 700 mm Hg = %3.1f degree C',T3); mprintf('\n Above results shows that the dew point does not depend on temperature but vary with the total pressure'); // File output fd= mopen('.\Chapter5_Example4_Output.txt','w'); mfprintf(fd,'\n Dew point of benzene vapor and air mixture at \n (a) 25 degree C and 750 mm Hg = %2.0f degee C ',T1); mfprintf(fd,'\n (b) 30 degree C and 750 mm Hg = %2.0f degree C ',T3); mfprintf(fd,'\n (c) 30 degree C and 700 mm Hg = %3.1f degree C',T3); mfprintf(fd,'\n Above results shows that the dew point does not depend on temperature but vary with the total pressure'); mclose(fd); //=========================END OF PROGRAM======================================
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//Exa 8.6 clc; clear; close; //given data CN=0.4;//in uF V=33;//in KV VP=V/sqrt(3);//in KV f=25;//in Hz //Capacitance between 2 cores for 15 Km length CN_1=15*CN;//in uF //Capacitance of each core to neutral CN=2*CN_1;//in uF //Charging current per phase I=2*%pi*f*VP*1000*CN*10^-6;//in Ampere disp(round(I),"Charging current per phase in Ampere : ");
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//8.2 clc; I=125/10; ZL=50/I; printf("Load impedance=%.1f ohm",ZL) Z_total=150/I; printf("\nImpedance of the combination=%.2f ohm",Z_total) I1=125; I2=50; I3=150; P=(1/(2*10))*(I3^2-I1^2-I2^2); printf("\nPower absorbed by load=%.2f W",P) Pr=I^2*10; printf("\nPower consumed by the resistor=%.2f W",Pr) pf=P/(50*I); printf("\npower factor of load=%.2f",pf)
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// Ex 8 Page 348 clc;clear;close; // Given Z1=(6.25+%i*1.25);//ohm Z2=(5+%i*0);//ohm //Z3=(5-%i*XC);//ohm V=100;//V f=50;//Hz //Z23=(250+5*Xc**2)/(100+Xc**2)-%i*(25*Xc)/(100+Xc**2) //for in phase condition imag part must be zero //5*Xc**2-100*Xc+5*100=0 A=[5 -100 500];//polynomal XC=roots(A); XC=XC(1);//ohm C=1/(2*%pi*f*XC)*10**6;//uF printf("Capacitance of XC = %.f uF",C) Z=XC;//ohm I=V/Z;//A P=I**2*Z/1000;//kW printf("\n Circuit current = %.f A and power = %.f kW",I,P)
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//Check for the following system. //Example 2.7 <i> clc; clear ;//a>check whether static or dynamic t=-10:.1:10;T=length(t) s=2; for i=1:length(t) x(i)=i; y(i)=abs(x(i)); end if y(2)==x(2)& y(2)==x(1) then disp('The given signal is dynamic' ); else disp('the given signal is static'); end //b>check whether linear or non linear x1=x; y1=y; for i=1:length(t) x2(i)=-2; y2(i)=abs(x2(i)); end for i=1:length(t) z(i)=y1(i)+y2(i); end for i=1:length(t) y3(i)=abs(x1(i)+x2(i)); end if z==y3 then disp('The given signal is linear'); else disp('Not linear'); end //c>check whether time invariant or not IP=x(T-s); OP=y(T-s); if IP == OP then disp('the given signal is time invariant'); else disp('The given signal is not time invariant'); end //Check for the following systems //Example 2.7 <ii> clc; clear all;//a>check whether static or dynamic t=0:5;T=length(t);w=1; s=2; for i=1:length(t) x(i)=i; y(i)=x(i)*cos(w*t(i)); end if y(2)==x(2)& y(2)==x(1) then disp('The given signal is dynamic' ); else disp('the given signal is static'); end //b>check whether linear or non linear x1=x; y1=y; for i=1:length(t) x2(i)=2*i; y2(i)=x2(i)*cos(w*t(i)); y3(i)=cos(w*t(i))*(x1(i)+x2(i)); end z=y1+y2; if z~=y3 then disp('The given signal is not linear'); else disp('linear'); end //c>check whether time invariant or not IP=x(T-s); OP=y(T-s); if IP == OP then disp('the given signal is time invariant'); else disp('The given signal is not time invariant'); end
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function _cmd = jplot2d(varargin) _arg = " -2D -l SOUTH "; i=1; while (i<=length(varargin)) //disp(i); i_arg=0; q=%f; while ((length(varargin)>= i_arg+i+1) & (size(varargin(i+i_arg+1))==1)) i_arg = i_arg+1; _arg = _arg + " " +varargin(i+i_arg); end _tmp(i) = ".xyz."+string(grand(1,1,"uin",0,10000))+".tmp"; if ((size(varargin(i),2)==1)) fprintfMat(_tmp(i),[(1:length(varargin(i)))' varargin(i)]); else fprintfMat(_tmp(i),varargin(i)); end _arg = _arg + " " + _tmp(i); i = i+1+i_arg; end _cmd = "java -cp jmathplot.jar org.math.plot.PlotPanel"+_arg; //disp(_cmd); _res = unix_g(_cmd); endfunction function _cmd = jplot3d(varargin) _arg = " -3D -l SOUTH "; i=1; while (i<=length(varargin)) i_arg=0; while ((length(varargin)>= i_arg+i+1) & (size(varargin(i+i_arg+1))==1)) i_arg = i_arg+1; _arg = _arg + " " +varargin(i+i_arg); end _tmp(i) = ".xyz."+string(grand(1,1,"uin",0,10000))+".tmp"; fprintfMat(_tmp(i),varargin(i)); _arg = _arg + " " + _tmp(i); i = i+1+i_arg; end _cmd = "java -cp jmathplot.jar org.math.plot.PlotPanel"+_arg; //disp(_cmd); _res = unix_g(_cmd); endfunction
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clc; clear all; disp("1-D heat flow") disp("Fourier''s equation: q = -k*dt/dx") disp("k=k0*(1+at+bt^2)") disp("q = k0*(1+at+bt^2)*dt/dx") disp("q.dx = k0*(1+at+bt^2)*dt") disp("integrating above equation within limits t1 to t2") disp("the required expression is, q = -k*(t2-t1)*(1+a*(t1+t2)/2+b*(t1^2+t2^2+t1*t2)/3)/L")
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pathname=get_absolute_file_path('2_3.sce') filename=pathname+filesep()+'2_3_data.sci' exec(filename) //For N2 p1=(m1*RN2*T)/V //For O2 p2=(m2*RO2*T)/V //For CO2 p3=(m3*RCO2*T)/V //Total pressure of the mixture p=p1+p2+p3 //Gas constant of the mixture R=(m1*RN2+m2*RO2+m3*RCO2)/(m1+m2+m3) printf("\n\nRESULTS\n\n") printf("\npressure for N2:%f\n",p1) printf("\npressure for O2:%f\n",p2) printf("\npressure for CO2:%f\n",p3) printf("\ntotal pressure:%f\n",p) printf("\ngas consant of the mixture:%f\n",R)
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function [Q,R]=gsc(A) [tamLinha,tamColuna]=size(A) Q=A R=zeros(tamColuna,tamColuna) for j=1:tamColuna Q(:,j)=A(:,j) for i=1:j-1 R(i,j)=Q(:,i)'*A(:,j) Q(:,j)=Q(:,j)-R(i,j)*Q(:,i) end R(j,j)=norm(Q(:,j)) Q(:,j)=Q(:,j)/R(j,j) end disp (Q*R==A) endfunction function [Q,R]=gsm(A) [tamLinha,tamColuna]=size(A) v=A Q=zeros(tamColuna, tamColuna) R=zeros(tamColuna, tamColuna) for i=1:tamColuna R(i,i)=norm(v(:,i)) Q(:,i)=v(:,i)/R(i,i) for (j=i+1:tamColuna) R(i,j)=Q(:,i)'*v(:,j) Q(:,j)=Q(:,j)-R(i,j)*Q(:,i) v(:,j)=v(:,j)-R(i,j)*Q(:,i) end end disp (Q*R==A) endfunction function []=teste() e=0.00000000000000000001 A=[1,1,1;e,0,0;0,e,0;0,0,e] [Q,R]=gsm(A) disp (Q'*Q) [Q,R]=gsc(A) disp (Q'*Q) endfunction
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errcatch(-1,"stop");mode(2);// sum 3-16 ; ; D=22; d=20; r=1; K=2.2; sigmax=130; sigmax=sigmax/K; Z=%pi*d^3/32; M=sigmax*Z*10^-3; // printing data in scilab o/p window printf("M is %0.3f Nm ",M); exit();
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// Exa 3.10 format('v',7);clc;clear;close; // Given data Rm = 50;//resistance of meter in ohm Im = 2;//current in mA Im = Im * 10^-3;// in A V4 = 10;//voltage in V R4 = (V4/Im) - Rm;// in ohm R4= R4*10^-3;// in k ohm disp(R4,"The value of R4 in kΩ is"); R4= R4*10^3;// in ohm V3 = 50;// in V // (R3+R4) = (V3/Im) - Rm; R3 = (V3/Im) - Rm-R4;// in ohm R3= R3*10^-3;// in k ohm disp(R3,"The value of R3 in kΩ is"); R3= R3*10^3;// in ohm V2 = 100;// in V //(R2+R3+R4) = (V2/Im) - Rm; R2 = (V2/Im) - Rm - R3 - R4;// in ohm R2= R2*10^-3;// in k ohm disp(R2,"The value of R2 in kΩ is"); R2= R2*10^3;// in ohm V1 = 500;// in V // (R1+R2+R3+R4) = (V1/Im) - Rm; R1 = (V1/Im) - Rm - R4 - R3 - R2;// in ohm R1= R1*10^-3;// in k ohm disp(R1,"The value of R1 in kΩ is");
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tst
bod.tst
འཁྱོང་། V;FUT གཡབ། V;PST གྱར། V;PST དྲ། V;FUT གླ། V;IMP གློད། V;FUT ལན། V;PST མཚོན། V;PRS འགྱེལ། V;PST འབྱོར། V;PST བཙུམ། V;FUT ཡུར། V;IMP ལང་། V;IMP ལབ། V;PST བརྫུ། V;PRS བཤོར། V;PST གཏུག། V;IMP བསག། V;PRS ཀེར། V;PRS ལྷུང་། V;PST བཙོག། V;PST བསྟང་། V;PRS འཐེན། V;FUT བཤེད། V;PRS བླང་། V;PRS བཅག། V;PRS བསྐུམ། V;PRS སྤྱད། V;PRS བསྲོ། V;PST བམ། V;FUT བརྣབ། V;PRS བརྩིག། V;FUT བསྟིང་། V;IMP བསྒུར། V;IMP སྤུར། V;IMP བཅོས། V;PST བརྫུ། V;IMP བལྡབ། V;IMP བབ། V;PRS བཅང་། V;IMP བཏེག། V;PST སྦོལ། V;IMP ལྡོབ། V;PRS བཟི། V;FUT ཐེ། V;PRS བསྐྱོར། V;IMP ཕྱོགས། V;PST འཚོ། V;FUT བཅོལ། V;FUT འཕྱ། V;IMP བསྟབ། V;PRS འབྱོལ། V;IMP གཅིལ། V;IMP འཁྱོག། V;FUT མཉམ། V;PRS འབྱི། V;FUT ཟད། V;FUT འཕྱོ། V;PRS དོགས། V;PRS འཆལ། V;FUT འཚོ། V;FUT བསྡེབ། V;PRS སྦྱང་། V;PST བགྲུ། V;PST མགར། V;FUT འཁྱུར། V;PRS བསྙག། V;PST མཉེས། V;FUT འབྱོར། V;PRS བཤུ། V;IMP དཔོད། V;FUT གོན། V;PRS བསྣན། V;FUT ལན། V;FUT བསྒྲོན། V;PST འབྱོན། V;FUT ཡེར། V;PST དམུལ། V;FUT གཞག། V;PST གོན། V;FUT བསྒབ། V;IMP འཐོབ། V;PRS གཅུར། V;PST གཞེས། V;PRS བསྣོར། V;PST འཕྱོར། V;IMP འཛུལ། V;PST གླེབ། V;IMP ཡོད། V;PST དམན། V;PRS རེད། V;FUT བརྒྱུ། V;PRS བཞུགས། V;IMP གོག། V;FUT བསྲུལ། V;PST དགས། V;IMP བརྟུལ། V;IMP སྦོལ། V;FUT བཀླུབ། V;IMP མགུ། V;PST མནལ། V;IMP གཏུག། V;FUT སྡང་། V;PRS བསྡམ། V;PST བྲི། V;PST འགྱུར། V;PST བསྒག། V;PRS མནོལ། V;FUT བླད། V;IMP འཚག། V;IMP སོན། V;PRS བཞུད། V;FUT བསྒྲེ། V;IMP བཤོལ། V;IMP ཞ། V;PST དཀྲི། V;PST རྨོངས། V;PST བསྒྲིག། V;FUT གནོང་། V;PRS གཙབ། V;FUT འདྲོང་། V;FUT དགྱེལ། V;FUT གཏུལ། V;IMP གཅེས། V;PRS བདའ། V;PST བསྙལ། V;PRS གྱག། V;FUT འབྲི། V;PRS འགྲིལ། V;PST སྐྱོ། V;PRS བགྲུ། V;PRS འཕྱུག། V;PRS བསྐྱུར། V;PRS བསླུག། V;PST འབྲང་། V;PST ཞེན། V;PRS བརྩོན། V;PRS ཤན། V;IMP བྲན། V;FUT གཏམས། V;PST བསྒྲིལ། V;FUT མཁྱེན། V;FUT བསྒྲོ། V;FUT བསྲུང་། V;PRS འབྱང་། V;PST འཐུལ། V;PRS དྲན། V;FUT རྙེད། V;FUT བདག། V;PST འཁྱུད། V;PRS ལྷགས། V;FUT འཁྲུ། V;PRS བསྒྲིམ། V;IMP བསྒྲིན། V;PRS དགོངས། V;FUT ཁྲུལ། V;PST བཟློ། V;PRS བསོད། V;FUT བགྱེད། V;FUT རྔུལ། V;FUT གཡོལ། V;FUT བརླིང་། V;PST གདོན། V;FUT གཞོམ། V;PRS བཤོལ། V;PST འཛག། V;PST རྒྱ། V;FUT བྲེག། V;IMP དཀྲི། V;PRS དབོག། V;PST ཧྲལ། V;FUT ཡལ། V;PST སྦྱར། V;PRS གཞེས། V;FUT དགར། V;PRS བསྐུམ། V;IMP མཐུན། V;PST གསུར། V;PST གཅག། V;IMP བཞོ། V;IMP བཞེས། V;PRS འཆལ། V;PRS རྒ། V;FUT ངེར། V;PST བཀོལ། V;IMP དོར། V;PST དཔྲུལ། V;PST འཕྲོད། V;PRS འགྱང་། V;FUT སྤར། V;IMP བརྔོན། V;IMP དགྱེད། V;PRS འཕྱི། V;PST འབག། V;FUT བསྔས། V;PRS བཤང་། V;PST འཕམ། V;PST གསང་། V;PST བརྡབ། V;PST བགོར། V;PRS བཙུམ། V;PRS འཕྱིང་། V;PST འཚམ། V;PRS བཀོན། V;PST དར། V;PRS གཡུར། V;PST ཡོར། V;PST ཧད། V;PRS དཔྲུལ། V;FUT ནུད། V;PRS འགྲོགས། V;PST འདར། V;FUT སྤྲུལ། V;PST བགྲད། V;FUT ཐེང་། V;FUT བཅང་། V;PST བཀྱོན། V;IMP འཆོར། V;PRS ཞོམ། V;PST བཞུགས། V;PST བསྣུབ། V;PRS བསྡུར། V;IMP གསུར། V;PRS འཁྲེན། V;FUT མཉན། V;PST བཏིག། V;PST བརྙང་། V;PST གཟུང་། V;PST གཞོབ། V;FUT ལྡང་། V;PRS ཚ། V;PRS འཛོལ། V;PST གཡེང་། V;PRS གཟབ། V;PST བཤམ། V;PST འཁོབ། V;PRS སྐྱེངས། V;FUT བརྒྱུང་། V;PRS གཏོད། V;FUT འཚང་། V;FUT དགོལ། V;FUT སྤུང་། V;PRS སླེབ། V;PST བསྒོམ། V;IMP དབྲི། V;IMP བཤེར། V;FUT བསྟང་། V;IMP བབ། V;FUT བསྣན། V;IMP འབུང་། V;PRS བསྡུར། V;FUT ཉོག། V;FUT བསྡོང་། V;IMP དཀྲིག། V;FUT བླད། V;PST གཏོག། V;PST གཉིད། V;FUT སྨན། V;PRS འཁོང་། V;PRS བཟོ། V;FUT བརྒལ། V;PRS བསླང་། V;IMP གཡོག། V;IMP བཤུང་། V;PST དགལ། V;PST བལྡེག། V;PRS མཚོན། V;FUT བསྐྱུར། V;PST རེམ། V;IMP གུས། V;FUT བཀླག། V;IMP གློད། V;PST སྤྱུག། V;FUT ཕན། V;FUT སྤར། V;PRS འབྲལ། V;PRS སྤྱོ། V;PST འཐིབ། V;PST བཤུམ། V;PST ཤིང་། V;PRS སྦང་། V;FUT བསྐོང་། V;IMP འགྲས། V;PRS བསྟུན། V;PST འཁྱམ། V;FUT བུངས། V;PRS བརློང་། V;IMP བཀྲེས། V;PRS བཀྱག། V;IMP བསྣོར། V;PRS དོར། V;IMP གདམ། V;PRS ཆེས། V;PST འཕོག། V;FUT གདེང་། V;PST ཉོབ། V;PRS གཟིང་། V;PST དབྲལ། V;IMP མནར། V;PRS གདང་། V;PST བཏོག། V;IMP བསལ། V;PST སྨྱུང་། V;PRS བསླེ། V;PRS མནོ། V;PST འཁུན། V;FUT ལྡུར། V;PST གསེད། V;PST དགྲོང་། V;PST སྦྲེང་། V;FUT འཁེང་། V;FUT ཟེར། V;PST ལྟོགས། V;PST ཞེད། V;PST ངོམས། V;PST བཤའ། V;FUT འཁྱུག། V;PST ཧོལ། V;PRS ཡན། V;PST དབང་། V;PRS བཙོང་། V;FUT འབྲིད། V;PST ལགས། V;FUT བསྟན། V;FUT འདྲོག། V;FUT བསྙུན། V;PST ཁེག། V;PRS དབོག། V;IMP འཛེག། V;PRS འབྱོང་། V;PRS བརློང་། V;FUT གཙེ། V;FUT འཆད། V;FUT ཁྱག། V;PST བལྟ། V;IMP འཁྲིམས། V;PST བསྟུན། V;IMP འཛོལ། V;PRS སྦང་། V;IMP མནན། V;FUT འབབ། V;PRS བརྒྱལ། V;PRS སྦྱིན། V;FUT འཁྲེབ། V;PST འཁྲུང་། V;PRS བྲིན། V;FUT འབྱང་། V;FUT གོག། V;PST གདུལ། V;PRS མདུད། V;IMP བྲུབ། V;PRS གླེང་། V;IMP འཕོག། V;PRS མཆོད། V;FUT བགྲོད། V;IMP བརྒྱང་། V;FUT རྒྱ། V;PRS ཚར། V;PRS བསྙེན། V;FUT ཞལ། V;PRS བསྙིལ། V;PST འཕོ། V;PST འཐེང་། V;PRS འཆག། V;PST བགྲེས། V;PRS ཞུམ། V;PRS ངེར། V;PRS བསུབ། V;IMP མནབ། V;PRS བཅིབ། V;PRS བསོ། V;PRS བཞད། V;FUT བརྔོ། V;PST གཏམ། V;IMP དོང་། V;PRS ཤིས། V;FUT རལ། V;PRS བགྱི། V;PRS གཡོར། V;IMP མྱུལ། V;PST གདིང་། V;PST འཆར། V;PST གཏུབ། V;FUT ལྡང་། V;PRS བསིལ། V;PST བསྒྲོ། V;PRS རེང་། V;PRS རེ། V;PRS འབྱོན། V;IMP འཁྲོག། V;FUT བཙིར། V;PST གླེབ། V;PST གཞིལ། V;PST འཕྱུག། V;FUT བརྒལ། V;FUT བདལ། V;IMP ཁེན། V;PRS འཕང་། V;FUT ཀླས། V;PST བསྲི། V;IMP འཕྲེང་། V;PRS འཁྲིད། V;PRS གྱེད། V;FUT བསྐྱུད། V;PST ཧང་། V;FUT ནུ། V;PST འཁམས། V;PST བརྒལ། V;FUT ཚིམ། V;FUT འཁྱལ། V;PST འབྲུལ། V;PRS འཐད། V;FUT བགམ། V;FUT བརྙབ། V;FUT ཧྲོལ། V;PST འགག། V;PRS བདག། V;PRS དཀྲོག། V;FUT འཛེར། V;PRS ཟིང་། V;PST ཞུད། V;IMP གནོང་། V;FUT སྤྱིང་། V;FUT མཉེལ། V;FUT བཀྱིག། V;PRS གཟིར། V;IMP འབག། V;PRS ཟེར། V;PST གྱེར། V;FUT ཡོར། V;FUT འཇོ། V;PST བསྟང་། V;FUT གཞོག། V;IMP གཟའ། V;FUT གསོར། V;IMP གཏོར། V;PRS ཟེགས། V;IMP བད། V;FUT རོལ། V;PST དྲེད། V;PRS བརྙོག། V;PST བརྡལ། V;FUT བསྐྲུན། V;PST ཤེས། V;PST གླན། V;FUT འདེད། V;IMP བསྙོན། V;FUT ཐིམ། V;FUT འབའ། V;PRS བསྒྲང་། V;PST བསྐྱབ། V;PST བདའ། V;PST འགུལ། V;PST མཆོང་། V;PST བསྒྲེང་། V;PRS བསབ། V;FUT བསྒྲིབ། V;PST བྲ། V;PST བཤོར། V;PRS ཐེ། V;PST ལྕེབ། V;FUT འཕར། V;PRS བསྲབ། V;PST སྨྱུར། V;PRS ཁེང་། V;PST གསེང་། V;PRS བསྐྲུ། V;FUT འབྲི། V;PST བགད། V;PRS དགྱེལ། V;IMP སངས། V;PRS བསྟད། V;PRS རྨྱ། V;PST སྙིགས། V;PST ཁྱབ། V;FUT བྲོད། V;PST གཉེར། V;FUT མཆེད། V;FUT གཞུར། V;PRS གཟར། V;PST ཡན། V;FUT བསྒྲག། V;FUT སྦ། V;PST གཉེར། V;IMP བསྡེབ། V;FUT འཁྱོང་། V;PST གཉག། V;PST རངས། V;PST བརྗེ། V;PST གཡོར། V;PST བསྐྲོག། V;FUT སྐྱོ། V;PST གདིང་། V;PRS འཁུམ། V;PRS གསང་། V;IMP བཟོ། V;PST སྤྲུག། V;PRS འཚོབ། V;FUT རྩེན། V;FUT གཡེམ། V;IMP དཔྲུལ། V;PRS འབྲལ། V;PST བསྒྱེལ། V;FUT སྤག། V;IMP འགྱོད། V;PRS བསྒབ། V;PST གཏོད། V;PRS བཀྲུ། V;IMP བརྒྱུང་། V;FUT འཁྱོམ། V;PST བརྟིབ། V;PRS ཐེབས། V;PRS བསླན། V;PRS བཅོལ། V;IMP རྨྱ། V;PRS ལྷོང་། V;PRS སྲེད། V;PRS སྤུད། V;PST བསྐྱུད། V;IMP གསན། V;PST བརྡར། V;PRS སྤེལ། V;IMP འཚལ། V;PRS བསག། V;PST བྱ། V;PRS འབུར། V;PST འགེམ། V;PRS འཕྱུར། V;PST འགྲུལ། V;PST བརྟབ། V;PRS མྱོས། V;PRS མཁས། V;FUT འཐུལ། V;FUT གཤེགས། V;FUT དབུབ། V;PRS འཕྲོ། V;FUT གཏན། V;FUT སྤང་། V;PST དགོག། V;PRS གདང་། V;IMP ཚིམ། V;PRS འཕྲ། V;PST བསྟར། V;PRS གློང་། V;PRS འཚང་། V;FUT ཡེར། V;FUT ལྡོབ། V;PST དགྲོལ། V;PRS འཁར། V;PST བཏིག། V;PRS གནས། V;PRS ལབ། V;IMP བདལ། V;PRS བསབ། V;PRS དབྱུང་། V;FUT གཙུབ། V;FUT བརྩམ། V;PST ཟེམ། V;FUT བསྒྲེང་། V;PST ལྡོན། V;PST གཞའ། V;FUT ཕྱེད། V;PST བཅུ། V;PRS ཐེ། V;FUT ཀུམ། V;PRS བྲི། V;PRS རྨེལ། V;FUT ལྡིང་། V;FUT འདྲོང་། V;PRS ཚོས། V;PRS བརྣང་། V;IMP འགྲིག། V;PST ལབ། V;PRS ཕྱག། V;PRS འཇོལ། V;PST དད། V;PST བསྐྱང་། V;PST བརྒྱོ། V;PST བསྡམ། V;IMP བརྩད། V;IMP སྦྲེལ། V;PRS དྲི། V;FUT འཆི། V;PST བསྐྱེད། V;PST འཆུ། V;FUT བསྟིམ། V;PST འབྲིད། V;FUT གླེབ། V;FUT ཆུམ། V;PST བྱང་། V;FUT ལྡན། V;FUT གཏོག། V;PRS གཏུལ། V;FUT སད། V;PST གཟོ། V;PRS གཞར། V;IMP བརྫང་། V;PRS རིགས། V;PRS བསླུག། V;FUT ལྡན། V;PST སྤྱིལ། V;PST གླེབ། V;PRS བཏིག། V;FUT ལད། V;FUT བསྐྱོག། V;IMP བསྟིང་། V;FUT བླག། V;PRS དམས། V;FUT འབ། V;PST དང་། V;FUT བཙིར། V;PRS སྤོ། V;IMP འཆི། V;FUT བསྒྲད། V;PRS བསྒར། V;FUT བཅའ། V;PRS བསྐུལ། V;FUT བཙལ། V;PST བཟླུམ། V;IMP གློང་། V;FUT བསྣད། V;PST བསྣོ། V;PST ངར། V;PST འདང་། V;PST ཚད། V;PST དགོས། V;FUT གླལ། V;PST དབྲལ། V;PST བསྙེར། V;PRS གཏང་། V;IMP བསྩལ། V;PRS ཟུག། V;FUT གསེང་། V;IMP འཚོབ། V;PST དགུག། V;IMP སྐྲུག། V;PRS ཡེང་། V;FUT བསུམ། V;PST གཞབ། V;PRS མནལ། V;PRS འཁྱོམ། V;PRS བརྣོག། V;PRS བཀྲི། V;IMP བསྣོལ། V;IMP མྱག། V;FUT བཀྱིག། V;IMP འཛར། V;PRS འཕེར། V;PST བཤད། V;IMP འགལ། V;PST གཅུན། V;IMP ཟག། V;FUT ཁེབས། V;PRS གཙུབ། V;PRS རྙིད། V;PRS སླེབ། V;FUT གཞིག། V;PRS འབྲ། V;PRS སྣང་། V;PST སྦག། V;PST དབྱུང་། V;IMP བསྒྲུབ། V;FUT བསྐྱར། V;PST བརྔ། V;IMP བརྩེད། V;PST འཁྱུས། V;PST ཡོག། V;FUT དགྲོལ། V;PST མཆི། V;PST བསྣུབ། V;PST ལྷག། V;FUT འགྲུབ། V;FUT བསྒྱུར། V;PRS གཤིབ། V;IMP འཁོབ། V;FUT བྲུག། V;FUT ཟློ། V;PRS འཇོལ། V;FUT ཐེགས། V;PRS མནམ། V;PST འགྲོ། V;FUT བཟོད། V;PST འདེང་། V;PST ཟུམ། V;PRS བཞེད། V;FUT སྤུར། V;FUT ཉལ། V;PST གཏང་། V;PRS དབྱི། V;PST མགུ། V;FUT རྒུད། V;FUT བརྫེ། V;IMP བླུ། V;IMP ངུར། V;PRS ཁྱག། V;FUT འཕྱུར། V;FUT དབུར། V;FUT འདའ། V;FUT ཚར། V;FUT འབྲིད། V;PRS བསྒྱུར། V;FUT བརྐུ། V;PST བཙལ། V;IMP རིག། V;PST བརྟིབ། V;PST གཏད། V;PST བསྒྲུན། V;FUT བསྙོར། V;FUT བསྟེན། V;PRS དྲི། V;PST གཏོགས། V;PST གཅུ། V;IMP བདུང་། V;IMP བསྐྱུང་། V;PST མཐུད། V;PRS བཙམ། V;FUT འཐད། V;PRS གྱེར། V;PRS བསྐོ། V;PST བརློང་། V;PST འགོང་། V;FUT བདམ། V;IMP བཟླུམ། V;PST བསྐུག། V;IMP གཤེ། V;PRS སྤར། V;PST བམ། V;PST བསྐྱལ། V;PRS བཙམ། V;PST བསག། V;IMP གཤིབ། V;PST འཐེམ། V;PRS བླུག། V;PST བཀླུབ། V;PST རྒྱལ། V;FUT བསྙེལ། V;FUT འཛོམ། V;PRS འཁུན། V;PRS སྤྲུག། V;PRS བརྔུབ། V;FUT དབྲི། V;FUT དཀྲུག། V;PST བསྲེ། V;FUT བལྟབ། V;FUT འགྲུལ། V;PRS བསོད། V;PRS གཅགས། V;IMP བསྒབ། V;FUT རྣག། V;FUT དྲང་། V;FUT འཆུ། V;FUT འཐོན། V;FUT ཆོམ། V;PRS བགྱང་། V;IMP གདས། V;PST གཟར། V;PST འཁྱེར། V;PRS རོལ། V;IMP འཁུལ། V;FUT འཁྱིལ། V;FUT འཕུལ། V;FUT བསྐྱོར། V;PST ཞུལ། V;FUT བཙག། V;FUT ཕེབས། V;PST མངའ། V;PST དགོས། V;PST ཀླས། V;PRS འཚེམ། V;PRS འཁྱུག། V;PRS བརྒྱོ། V;IMP འབྱོར། V;FUT བྲེག། V;FUT བསྡད། V;PRS མྱུག། V;PRS བརྒྱལ། V;PST མཚོན། V;PST བསྣུར། V;FUT ཕྱིད། V;PST བཞུད། V;PST གདལ། V;PRS མཆོང་། V;FUT ཧལ། V;PST ཁྲོ། V;FUT འཕགས། V;FUT བཀྲབ། V;PST བསམ། V;PST མྱག། V;PRS བསྔགས། V;IMP འཇང་། V;PRS འཕོངས། V;PST འཁྱིག། V;FUT བཤག། V;IMP ཐེགས། V;FUT དབབ། V;PST བཀྲལ། V;FUT མཐོང་། V;PST བསྐམ། V;IMP གཙི། V;IMP སྤྱོ། V;FUT ཡར། V;PST ཐིང་། V;PRS བསྙོར། V;PRS བསྐུག། V;PRS མྱུལ། V;PST དཔྱ། V;PST སྦྲིད། V;FUT གཤོ། V;IMP གཏོགས། V;FUT འཇེབས། V;PST དཀུ། V;FUT མཛད། V;PST བཙོག། V;FUT དྲག། V;FUT བགྲུ། V;IMP གཤག། V;PST འཁྲེང་། V;FUT བཅམ། V;FUT བསྡོང་། V;PRS དམིགས། V;IMP གུས། V;PST དཀྲུག། V;IMP སྤྱུག། V;PRS གཅག། V;PST གཏུགས། V;PRS ཞུ། V;PRS འཁང་། V;FUT འཕྲིག། V;PST བྱུག། V;PST འཚམ། V;FUT གཉུལ། V;PST རི། V;PRS གདག། V;PST བསྙོན། V;PST འཕྲད། V;PST གདལ། V;PST ངུར། V;PST གཤག། V;FUT ཤིང་། V;FUT མཆོད། V;PRS བལྡག། V;FUT དྲན། V;PST གསད། V;PRS བརྟན། V;PST བསྐྱིལ། V;IMP འཇའ། V;PST འབྲ། V;IMP གཡའ། V;PST བལྡག། V;PST བསྟེན། V;IMP བསྲུང་། V;FUT འཛེར། V;PRS འགྲན། V;PRS འབབ། V;IMP སྤོབས། V;PRS འབོག། V;FUT བསྐྱོག། V;FUT ཤབ། V;FUT བཞུད། V;PRS འཁུམ། V;PRS དྲིལ། V;IMP བསྡུ། V;IMP བསྙེན། V;PST བསྐྱུང་། V;PRS བསྡུམ། V;IMP བསྒྲུང་། V;FUT བརྫུ། V;FUT གཡར། V;FUT འཆུམ། V;FUT འཛེམ། V;IMP བྲབ། V;IMP བགད། V;FUT དགྱེལ། V;PRS བཤའ། V;PRS འབད། V;FUT བཟློ། V;PST བགྱེད། V;PST འབོག། V;FUT འབྱོ། V;IMP སྦོ། V;PST འདྲུ། V;IMP སད། V;PST འཕག། V;PRS བརྔོན། V;PST བསླན། V;IMP གསུད། V;PRS བསྣོག། V;PRS འཐུས། V;FUT བླག། V;IMP འགྲས། V;FUT ལྷོད། V;PST སྦྱང་། V;PRS བཀུ། V;FUT འཕྲིག། V;PRS དངར། V;PRS བསྒྲུག། V;FUT མངལ། V;PRS བཀྲ། V;PRS བསྒྲིབ། V;FUT འཇེབས། V;PRS ཀེར། V;PST རངས། V;FUT བཀྱིག། V;FUT བརྟག། V;PST འཕུད། V;IMP བཤུག། V;FUT ཧྲིངས། V;PST བསྒྲིན། V;PST གཅགས། V;PST སྦྲུ། V;FUT བསྡུ། V;PRS འབྲིད། V;IMP འགོང་། V;PST བཤམ། V;PRS འཆུམ། V;PST བརྒལ། V;PRS 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// Exa 17.5 // To calculate uplink cell load factor, number of voice users and poll capacity of the cell. clc; clear all; Ri=12.2*10^3;//Information rate in bps Rc=3.84*10^6;//Chip rate in cps(chips per second) Eb_Nt=4; //in dB Imargin=2; //Interference margin(3 dB) B=0.5;//Interference factor due to other cells Vi=0.65;//Channel activity factor //solution Eb_Ntreqd=10^(Eb_Nt/10); LF_peruser=(1+B)*(1/(1+(Rc/Ri)*(1/Eb_Ntreqd)*(1/Vi))); //M(no of users=1) in Eq 17.13 printf("Cell load factor per voice user is %.5f \n ',LF_peruser); CellLoading=(Imargin-1)/Imargin; VoiceUsers=CellLoading/LF_peruser; printf('No of Voice Users are %d per cell \n ',VoiceUsers); //From EQ 17.6 assuming Power control efficiency=1 Polecap=Rc/(Ri*Vi*(1+B)*Eb_Ntreqd); printf('Pole Capacity is %d \n',Polecap);
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tst
test09.tst
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fc50d814550139ccecb288f0b8823e20efbae936
449d555969bfd7befe906877abab098c6e63a0e8
/1658/CH22/EX22.14/Ex22_14.sce
24c91586cc087c0506f328fe6d19282924630296
[]
no_license
FOSSEE/Scilab-TBC-Uploads
948e5d1126d46bdd2f89a44c54ba62b0f0a1f5e1
7bc77cb1ed33745c720952c92b3b2747c5cbf2df
refs/heads/master
2020-04-09T02:43:26.499817
2018-02-03T05:31:52
2018-02-03T05:31:52
37,975,407
3
12
null
null
null
null
UTF-8
Scilab
false
false
185
sce
Ex22_14.sce
clc; //e.g 22.14; gm=4*10**-3; RD=1.5*10**3; RG=10*10**6; rs=500; rl=RD; AV=-(gm*rl)/(1+gm*rs); disp(AV); RL=100*10^3; rL=(RD*RL)/(RD+RL); AV=-(gm*rL)/(1+gm*rs); disp(AV);
6944ee493df5626437e7a0f7fc14eba385a682a5
449d555969bfd7befe906877abab098c6e63a0e8
/1379/CH1/EX1.1.1/example1_1.sce
6f54b6da832ff0b29efc9acb3188b1d31aab8bca
[]
no_license
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//exapple 1.1 clc; funcprot(0); // Initialization of Variable //part1 mu=6.3/100;//viscosity rho=1170;//density d=.3;//diameter of pipe b=0.142;//conversion factor pi=3.14; //calculation Q=150000*b/24/3600//flow rate u=Q/pi/d^2*4//flow speed Re=rho*u*d/mu if Re>4000 then disp(Re,"the system is in turbulent motion as reynolds no is greater than 4000:"); elseif Re<2100 then disp(Re,"the system is in laminar motion" ); else disp(Re, "the system is in transition motion"); end //part 2 mu=5.29/1000; d=0.06; G=0.32;//mass flow rate Re= 4*G/pi/d/mu; if Re>4000 then disp(Re,"the system is in turbulent motion as reynolds no is greater than 4000:"); elseif Re<2100 then disp(Re,"the system is in laminar motion as Re is less than 2100" ); else disp(Re, "the system is in transition motion"); end
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//To find speed of gears B and C clc //Given: TA=72, TC=32 NEF=18 //Speed of arm EF, rpm //Solution: //Refer Table 13.5 //Speed of gear C: y=18 //rpm x=y*(TA/TC) NC=x+y //Speed of gear C, rpm //Speed of gear B: //Calculating the number of teeth on gear B TB=(TA-TC)/2 //Calculating the speed of gear B NB=y-x*(TC/TB) //Speed of gear B, rpm //Solution: printf("\n\n Speed of gear C = %.1f rpm.\n\n",NC) printf(" Speed of gear B = %.1f rpm in the opposite direction of arm.\n\n",-NB)
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// Functions for getting feature vectors of training characters in ./training folder exec preprocessing.sci exec feature_extract.sci exec rm_ws.sci // Dictionary dic = ['a' 'b' 'c' 'd' 'e' 'f' 'g' 'h' 'k' 'm' 'n' 'o' 'p' 'q' 'r' 's' 't' 'u' 'v' 'w' 'x' 'y' 'z']; dic_size = size(dic) path = "./training/" //// // Write function to generate character image from lines of character for training //// // Accepts feature vector struct, path and its name, writes three files name.row_vector, name.content and name.col_vector function [] = write_feature(feature_struct, path, name) fprintfMat(path+name+".content", feature_struct.content); fprintfMat(path+name+".row_vector", feature_struct.row_vector); fprintfMat(path+name+".col_vector", feature_struct.col_vector); endfunction // Read features from given path, "./training/training_feature_data" function [content_vector,list_rowsum, list_colsum] = read_feature(path, dic) dic_size = size(dic); // row dictionary // defining variables content_vector = []; // list data type is awesome list_rowsum = list(); list_colsum = list(); for i = 1 : dic_size(2) content_vector($+1) = fscanfMat(path+dic(i)+".content"); list_rowsum($+1) = fscanfMat(path+dic(i)+".row_vector"); list_colsum($+1) = fscanfMat(path+dic(i)+".col_vector"); end endfunction write_path = path + "training_feature_data/" // Extrtact features from all alphabets from ./training and save it in ./training/training_feature_data // Make this A FUCTION for i = 1 : dic_size(2) // ReadImage char_image = ReadImage(path+dic(i)+".png"); char_image = RGB2Gray(char_image); char_bin_image = gray2inv_bin(char_image); // inverted binary image char_image = rm_ws(char_bin_image,"cols"); char_feature = extract_feature(char_image); // Write feature write_feature(char_feature, write_path, dic(i)); end
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Ex2_1.sce
//Ex 2.1 page 67 clc; clear; close; V1=1;//V across SCR IG=0;//A Ih=2;//mA holding current R=50;//ohm // Applying kirchoff law //VA-(IAK*R)-V1=0 VA=(Ih*10**-3*R)+V1;//V (let IAK=Ih) printf('VA = %.2f V',VA)
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clc //initialisation of variables dv=360//ft/sec v1=1564//ft/sec H1=1188//B th u g=32.2//ft/sec^2 J=778 cf=0.005 p=0.12//ft A=8.75*10^-4//ft^2 p1=67//lb/in^2 dx=0.0234//ft A1=8.5*10^-4//ft^2 W=0.203//lb/sec g=32.2//ft/sec^2 q2=0.989 Vs2=8.902//ft^3/lb A2=9*10^-4//ft^2 //CALCULATIONS v2=v1+dv H2=H1-((v2^2-v1^2)/(2*g*J)) p2=p1-(W*(dv+(cf*p*dv*dx/(2*A))))/(144*A1*g) W=(A2*v2)/(q2*Vs2) nv2=1866//ft/sec np2=51.2//lb/in^2 nT2=742.2//R nVs2=8.331//ft^3/lb nq2=0.99 nH2=1167.5//b th u vs2=72.5*sqrt(np2*nq2*nVs2) Ma2=v2/vs2 //RESULTS printf ('velocity = %.2f ft/sec',nVs2 ) printf ('\n Ma2 = %.2f ',Ma2-0.04)
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//reflection coefficent //given clc S=2//voltage standing wave ratio(VSWR) Zo=50//ohm row=((S-1)/(S+1)) row=round(row*1000)/1000///rounding off decimals disp(row,'the value of reflection coefficent as modulus row')
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//clear// p = [ 1.44 .95 .74]'; dt = 2.5 t = [0 2.5 5]'; dp(1) =( 3*p(1)+4*p(2)-p(3))/(2*dt); for i=2:n1 dp p(i+3
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clear clc disp('Exa-2.6(a)'); L=65; c=3*10^8;u=0.8*c; t=L/u ; //The value of time taken as measured by the observer printf('The time for rocket to pass a point as measured by O is %.2e.\n',t); //The value of time taken as measured by the observer disp('Exa-2.6(b)'); Do=65; //given length Lo= L/sqrt(1-(u/c)^2); //contracted length of rocket printf('Actual length according to O is %.2f.\n',Lo); disp('Exa-2.6(c)'); D=Do*(sqrt(1-(u/c)^2)); //contracted length of platform. printf('Contracted length according to O'' is %.2e.\n',D); disp('Exa-2.6(d)'); t1=Lo/u; //time needed to pass according to O'. printf('Time taken according to O is %.2e.\n',t1); disp('Exa-2.6(e)'); t2=(Lo-D)/u; //time intervals between the two instancs printf('Time taken according to O'' is %.2e.\n',t2); disp('The value of t1 and t2 did not match');
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7_1.sce
clear; clc; printf("\t\t\tExample Number 7.1\n\n\n"); // constant heat flux from vertical plate // Example 7.1 (page no.-330-331) // solution q_w = 800;// [W/square meter] radiant energy flux H = 3.5;// [m] height of metal plate surface W = 2;// [m] width of metal plate Ta = 30;// [degree celsius] surrounding air temperature // we treat this problem as one with constant heat flux on the surface since we do not know the surface temperature, we must make an estimate for determining Tf and the air properties. // an approximate value of h for free convection problems is h = 10;// [W/square meter degree celsius] dT = q_w/h;// [degree celsius] // then Tf = (dT/2)+Ta;// [degree celsius] approximately // at Tf the properties of air are v = 2.005*10^(-5);// [square meter/s] k = 0.0295;// [W/m degree celsius] Pr = 0.7;// prandtl number Beta = 1/(Tf+273);// [K^(-1)] // from equation (7-30), with x = 3.5;// [m] g = 9.8;// [square meter/s] acceleration due to gravity Gr_x = (g*Beta*q_w*x^(4))/(k*v^(2)); // we may therefore use equation (7-32) to evaluate h_x h_x = (k*0.17*(Gr_x*Pr)^(1/4))/x;// [W/square meter degree celsius] // in the turbulent heat transfer governed by equation (7-32), we note that // Nu_x = h*x/k ~ (Gr_x)^(1/4) ~ x // or h_x doest noy vary with x, and we may take this as the average value. the value of h h = 5.41;// [W/square meter degree celsius] // is less than the approximate value we used to estimate Tf, recalculating dT, we obtain dT1 = q_w/h_x;// [degree celsius] // our new film temperature would be Tf1 = Ta+dT1/2;// [degree celsius] // at Tf the properties of air are v1 = 2.354*10^(-5);// [square meter/s] k1 = 0.0320;// [W/m degree celsius] Pr1 = 0.695;// prandtl number Beta1 = 1/(Tf1+273);// [K^(-1)] // then Gr_x1 = (g*Beta1*q_w*x^(4))/(k1*v1^(2)); // and h_x is caalculated from h_x1 = (k1*0.17*(Gr_x1*Pr1)^(1/4))/x;// [W/square meter degree celsius] // our new temperature difference is calculated as dT2 = q_w/h_x1;// [degree celsius] // the average wall temperature is therefore T_w_avg = dT2+Ta;// [degree celsius] printf("the average wall temperature is therefore %f degree celsius",T_w_avg);
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@relation led7digit @attribute Led1 real[0.0,1.0] @attribute Led2 real[0.0,1.0] @attribute Led3 real[0.0,1.0] @attribute Led4 real[0.0,1.0] @attribute Led5 real[0.0,1.0] @attribute Led6 real[0.0,1.0] @attribute Led7 real[0.0,1.0] @attribute number{0,1,2,3,4,5,6,7,8,9} @inputs Led1,Led2,Led3,Led4,Led5,Led6,Led7 @outputs number @data 0 0 4 4 0 0 1 1 2 5 2 7 2 2 3 1 3 5 6 6 8 8 3 3 4 4 5 5 7 1 8 6 3 9 7 1 8 0 0 6 3 2 7 1 8 0 9 9 9 9 0 6 0 0 1 1 8 0 9 9 2 1 3 9 6 5 6 9 5 5 6 6 6 6 7 1 1 1 4 4 4 9 5 6 6 6 7 1 8 8 9 9 1 0 4 4 5 5 8 0
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(unwatch all) ; templerr.clp test (clear) (open "Results//templerr.rsl" templerr "w") (load "compline.clp") (dribble-on "Actual//templerr.out") (load "templerr.clp") (list-deftemplates) (dribble-off) (printout templerr "templerr.clp differences are as follows:" crlf) (compare-files "Expected//templerr.out" "Actual//templerr.out" templerr) ; close result file (close templerr)
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Example_10_3.sce
clear; clc; //To find Approx Value function[A]=approx(V,n) A=round(V*10^n)/10^n;//V-Value n-To what place funcprot(0) endfunction //Example 10.3 //Caption : Program to Find Pressure,Temperature and Composition for a system //Equations to be Used // ln v1=A*(x2^2) ln v2=A*(x1^2) Where A=2.771-0.00523T //Antoine Equations //ln P1_sat = 16.59158-(3643.31/(T-33.424)) //ln P2_sat = 14.25326-(2665.54/(T-53.424)) //P = E(xi * Vi * Pi_sat) E--Summation Eqn 10.6 //P = 1/E(yi / (vi * Pi_sat)) E--Summation Eqn 10.7 //(a) Calculate P and (yi) , for T=318.15K and x1=0.25 //BULB P Calculation T=318.15;//[K] Given x1=0.25; //Given x2=1-x1; P1_sat = approx(exp(16.59158-(3643.31/(T-33.424))),2);//[KPa] P2_sat = approx(exp(14.25326-(2665.54/(T-53.424))),2);//[KPa] A=approx(2.771-(0.00523*T),3); v1=approx(exp(A*(x2^2)),3); v2=approx(exp(A*(x1^2)),3); //Form Eqn(10.6) P_a=approx((x1*v1*P1_sat)+(x2*v2*P2_sat),2);//[KPa] y1_a=approx((x1*v1*P1_sat)/P_a,3); y2_a=approx((x2*v2*P2_sat)/P_a,3); disp('(a)P and [yi] for T=318.15K and x1=0.25') disp('BUBL P calculations') disp('KPa',P_a,'P = ') disp(y1_a,'y1 = ') disp(y2_a,'y2 = ') //(b) Calculate P and (xi) , for T=318.15K and y1=0.60 //DEW P calculation y1=0.6; y2=1-y1; T=318.15;//[K] P1_sat = approx(exp(16.59158-(3643.31/(T-33.424))),2);//[KPa] P2_sat = approx(exp(14.25326-(2665.54/(T-53.424))),2);//[KPa] A=approx(2.771-(0.00523*T),3); v1=0.1;//Assumed v2=0.1;//Assumed a1=v1; a2=v2; i=-1; while(i==-1) P=approx(1/((y1/(a1*P1_sat))+(y2/(a2*P2_sat))),2); x1=approx(y1*P/(a1*P1_sat),4); x2=1-x1; b1=approx(exp(A*(x2^2)),4); b2=approx(exp(A*(x1^2)),4); dt=abs(b1-a1); if(dt==0) i=0; v1=b1; v2=b2; break; end a1=b1; a2=b2; end x1_b=x1; x2_b=1-x1_b; P_b=P; v1_b=v1; v2_b=v2; disp('(b)P and [xi] for T=318.15K and y1=0.60') disp('DEW P calculations') disp('kPa',P_b,'P = ') disp(x1_b,'x1 = ') disp(x2_b,'x2 = ') //(c) Calculate T and (yi) for P = 101.33 KPa and x1=0.85 //BUBL T calculation P=101.33; x1=0.85; x2=1-x1; T1_sat=approx((3643.31/(16.59158-log(P)))+33.424,2); T2_sat=approx((2665.54/(14.25326-log(P)))+53.424,2); T=(x1*T1_sat)+(x2*T2_sat); a=T;//Initial i=-1; while(i==-1) A=approx(2.771-(0.00523*a),4); v1=approx(exp(A*(x2^2)),4); v2=approx(exp(A*(x1^2)),4); P1_sat = approx(exp(16.59158-(3643.31/(a-33.424))),2);//[KPa] P2_sat = approx(exp(14.25326-(2665.54/(a-53.424))),2);//[KPa] alpha=P1_sat/P2_sat; P1_sat=approx(P/((x1*v1)+(x2*v2/alpha)),2); b=approx((3643.31/(16.59158-log(P1_sat)))+33.424,2); dt=abs(b-a); if(dt==0) i=0; T=b; break; end a=b; end T_c=T; y1_c=approx(x1*v1*P1_sat/P,3); y2_c=1-y1_c; disp('(c)T and [yi] for P=101.33kPa and x1=0.') disp('BUBL T calculations') disp('K',T_c,'Temperature = ') disp(y1_c,'y1 = ') disp(y2_c,'y2 = ') //(d) Calculate T and (xi) for P = 101.3 KPa and y1=0.4 P=101.3; y1=0.4; y2=1-y1; T1_sat=approx((3643.31/(16.59158-log(P)))+33.424,2); T2_sat=approx((2665.54/(14.25326-log(P)))+53.424,2); T=(y1*T1_sat)+(y2*T2_sat); v1=1; //Initially v2=1; //Initially a=T;//Initial i=-1; while(i==-1) A=approx(2.771-(0.00523*a),4); P1_sat = approx(exp(16.59158-(3643.31/(a-33.424))),2);//[KPa] P2_sat = approx(exp(14.25326-(2665.54/(a-53.424))),2);//[KPa] alpha=P1_sat/P2_sat; x1=approx((y1*P)/(v1*P1_sat),4); x2=1-x1; v1=approx(exp(A*(x2^2)),4); v2=approx(exp(A*(x1^2)),4); P1_sat=P*((y1/v1)+(y2*alpha/v2)); b=approx((3643.31/(16.59158-log(P1_sat)))+33.424,2); dt=abs(a-b); if(dt==0) T=a; i=0; break; end a=b; end T_d=T; x1_d=x1; x2_d=x2; disp('(d)T and [xi] for P=101.33kPa and y1=0.40') disp('DEW T calculations') disp('K',T,'T = ') disp(x1_d,'x1 = ') disp(x2_d,'x2 = ') //(e) Taz , (xi_az) and (yi_az) for T = 318.15K T = 318.15; // Relative Volatility alpha_12=(y1/x1)/(y2/x2) //At Azeotrope y1=x1 and y2=x2 and alpha_12=1 P1_sat = approx(exp(16.59158-(3643.31/(T-33.424))),2);//[KPa] P2_sat = approx(exp(14.25326-(2665.54/(T-53.424))),2);//[KPa] //From eqn (10.5) alpha_12=(v1*P1_sat)/(v2*P2_sat) A=approx(2.771-(0.00523*T),4); //When x1=0 v2=1 and v1=exp(A) alpha_12_x10=P1_sat*exp(A)/P2_sat; //When x1=1 v1=1 and v2=exp(A) alpha_12_x11=P1_sat/(P2_sat*exp(A)); //But this is not Azeotrope (at Azeotrope alpha_12=1) //v1_az/v2_az=(P2_sat/P1_sat)=K K=P2_sat/P1_sat; //ln(v1/v2)=ln(K)=A(1-(2*x1)) x1_az=approx((A-log(K))/(2*A),3); x2_az=1-x1_az; y1_az=x1_az; y2_az=x2_az; v1_az=approx(exp(A*(x2_az^2)),3); v2_az=approx(exp(A*(x1_az^2)),3); P_az=approx(v1_az*P1_sat,2); disp('Azeotropic Pressure and Azeotropic Composition for T = 318.15K') disp('KPa',P_az,'Azeotropic Pressure = ') disp(x1_az,'x1_az') disp(y1_az,'y1_az') //End
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/1760/CH5/EX5.41/EX5_41.sce
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FOSSEE/Scilab-TBC-Uploads
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EX5_41.sce
//EXAMPLE 5-41 PG NO-332-333 VTH=10; V=10; R1=10; R2=10; R3=16.67; R4=50; R5=5.56; R6=3.33; RTH=V+R5+(((R1+R3)*(R4+R6))/(R1+R3+R4+R6)); I=(V/RTH)-0.4; disp('i) Resistance (RTH) is = '+string (RTH) +' ohm '); disp('i) Currrent (I) is = '+string (I) +' A ');
e1efec171a621083e7fc1fa2f72661d63ed8382d
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/sablona_berliner/zapisnik/graf.sce
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pirati-cz/plisty
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815dbc58f7a47f1b2740ffa068a2ff5f909ecba8
refs/heads/master
2020-12-24T19:04:07.572707
2016-05-16T20:52:51
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graf.sce
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EX8_47.sce
// Example 8.47 // Calculation of incident optical power. // Page no 499 clc; clear; close; //Given data h=6.62*10^-34; // Planck constant c=3*10^8; // velocity of light lambda=1.55*10^-6; // Wavelength B=400*10^6; // Speed of communication // Maximum repeater spacing P=(36*h*c*B)/lambda; P=10*log10(P/10^-3); //Displaying results in the command window printf("\n Incident optical power(in nW) = %0.3f ",P); // The answers vary due to round off error
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Example_9_8.sce
// Chapter9 // Page.No-412, Figure.No-9.24(a) // Example_9_8 // Freq of free running ramp generator // Given clear;clc; R=10*10^3; // Resistance in ohm Vcc=5 // Supply voltage in volt Vbe=0.7 // Base to emitter voltage in volt C=0.05*10^-6; // Capacitance in farad Ic=(Vcc-Vbe)/R; // Collector current in ampere fo=(3*Ic)/(Vcc*C); printf("\n Freq of free running ramp generator is = %.1f Hz \n",fo) // Result
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ex1_12.sce
// Example 1.12 page no-34 clear clc l=2 //cm D=24 //cm s=0.5 //cm Vd=30 //Volts Va=1000 //Volts //(a) d=Vd*l*D/(2*s*Va) printf("\n(a)\nDeflection Produce, d=%.2f cm\n",d) //(b) theta=(atan(d/D))*(180/%pi) printf("\n(b)\nTheta=%.2f°",theta) //(c) e=1.6*10^-19//C m=9.1*10^-31//kg v=sqrt(2*e*Va/m) vr=v/cos(theta*%pi/180) printf("\n\n(c)\nResultant Velocity, Vr=%.2f *10^6 m/sec",vr/10^6)