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clc // Given that l_0 = 100// let initial length of rod in m l = 99 // Observed length in m c = 3e8 // speed of light in m/s // Sample Problem 13 on page no. 29 printf("\n # PROBLEM 13 # \n") printf(" Standard formula used \n") printf(" l = l_0/((1-v^2/c^2)^1/2) \n") v = c* sqrt(1-(l/l_0)^2)// speed of rocket in m/s printf("\n Speed of rocket ship is %e m/s.",v)
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Ex13_1.sce
clear //Initialization c=10*10**-6 //capacitance in Farad v=10 //voltage //Calculation q=c*v //charge in coulomb //Results printf("\n Charge, q = %.1f uC",q*10**6)
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wCu=0.0230;//weight of Cu deposited in the coulometer in grams// MW=63.54;//molecular weight of Cu in grams// n=wCu*2/MW;//no. of equivalents of Cu deposited// printf('In the coulometer,wt of Cu deposited=0.0230grams'); printf('\nNumber of equivalents of Cu deposited=n=%fequivalents or Farads.',n); printf('\nThis would have resulted in deposition of 7.24*10^-4equivalents of Ag+ at the cathode \nand dissolution of the same amount at the anode.'); wAgNO3=7.39; w1AgNO3=0.2360;//after electrolysis weight of AgNO3// MWAgNO3=170;//molecular weight of AgNO3// BEAgNO3=wAgNO3/MWAgNO3; printf('\n Anolyte solution \nBefore electrolysis 1000grams of water contains %fequivalents of AgNO3',BEAgNO3); AEAgNO3=w1AgNO3/MWAgNO3; printf('\nAfter electrolysis 23.14grams of water contains %fequivalents of AgNO3.',AEAgNO3); w=23.14; BE=w*BEAgNO3/1000; printf('\n23.14grams of water before electrolysis would have contained %fequivalents of AgNO3',BE); IC=AEAgNO3-BE; printf('\nIncrease in the concentration of anolyte=IC=%fequivalents.',IC); printf('\n0.000382gram equivalents of NO3- ions must have migrated into the anode compartment.\nAs a result of passin 7.24*10^-4Farads into the solution.\n0.000724equivalents of Ag should have dissolved to give the same amount of Ag+ ion.\nOut of this 0.000382gram equivalents are present in the anolyte.'); ME=n-IC;//no of equivalents of migrated anodes// printf('\n%fgram equivalents of Ag+ ions must have migrated from the anode.',ME); tAg=ME/n;//transport number// printf('\nTransport number of Ag=tAg=%f',tAg); tSO3=1-tAg; printf('\nTransport number of SO3=tSO3=%f',tSO3);
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Example_4_20.sce
//A Textbook of Chemical Engineering Thermodynamics //Chapter 4 //Second Law of Thermodynamics //Example 20 clear; clc; //Given: T = 473; //temperature at entropy is to be determined (K) Tf = 273; //base temperature (K) Tb = 373; //boiling temperature (K) Cpl = 4.2; //avearge heat capacity of water (kJ/kg K) Cpg = 1.9; //avearge heat capacity of water vapour between 373 K and 473 K Hv = 2257; //latent heat of vaporisation at 373 K (kJ/kg) //To determine the absolute entropy of water vapour //Entropy of water vapour is calculated using last three terms of equation of 4.55 (Page no. 108) S = (Cpl*log(Tb/Tf))+(Hv/Tb)+(Cpg*log(T/Tb)); mprintf('Absolute entropy of water vapour at 473 K and 101.3 kPa is %f kJ/kg K',S); mprintf('\nIt compares favourably with the value reported in steam tables'); //end
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//fiber optic communications by joseph c. palais //example 3.7 //OS=Windows XP sp3 //Scilab version 5.4.1 clc clear all //given c=3*10^8//velocity of light in m/s l=0.3*10^-3//length of cavity in m lambda=0.82*10^-6//mean (center) wave length in m n=3.6//refractive index of AlGaAs //to find delta_fc=c/(2*l*n)//mode spacing in Hz delta_lambdac=(lambda^2)*delta_fc/c//wavelength spread in m mprintf("mode spacing= %f x10^9Hz",delta_fc*10^-9)//for representation mprintf("\nwavelength spread =%f nm",delta_lambdac*10^9)//multiplication factor 10^9 to convert m to nm
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// **** Purpose **** // PiLab k-point information calculator. // This function is to calculate k-points using distributed parallel // calculations, so dense k-mesh becomes possible. // **** Variables **** //==== << PiLab inputs >> ==== // # System setup //[kif.Command]: 1x1, string, //<= specify how do you submit a scilab job to the background in your //machine. The input file name and output file name should be replaced //by @input_name and @output_name. PiLab will use correct name for them. //Note: In linux, it is usually: //'scilab -nwni -f @input_name > @output_name &' //In windows, it is usually: //'start /b scilex -nwni -f @input_name > @output_name' // # k-generation //[kif.KptGen]: 1x1, string, 'grid'/'path'/'manual' //<= Define how to generate k-points. If 'grid',PiLab will use //kif.SpanVec and kif.Mesh to generate grid k-points. //If 'path', PiLab use kif.Path and kif.Div to generate k-path //If 'manual', PiLab will ignore kif.SpanVec and kif.Mesh and read the //k-points from a file called "kif_kpoint.dat". In this file, there //should be a nx3 matrix which lists all the k-points in PiLib variable //format. //[kif.Format]: 1x1, string, 'red'/'cart' //<= Define whether the k-points are in reduced or cartisian coordinate // * If 'grid' -------------- //[kif.SpanVec]: 4x3, real //<= Define 3 vectors to span a mesh box. The first row will be the //origin and the next three are three positions from the origin //to span the mesh box. Whether these points are defined in reduced //or cartisna coordinate show be defined in kif.Format. //[kif.Mesh]: 1x3, int //<= Define mesh number of each vector. Note that, the mesh will //include head and tail of each vector. If any mesh number=1, means //there is no mesh. If mesh number=2, means only the origin and the //end point are included in that direction. // * If 'path' --------------- //[kif.Path]: nx3, real //<= k_path in reduced coordinates //[kif.Div]: 1x1, int //<= k_mesh along k_path of each unit length k // # Job allocation //[kif.Allocation]: 1x1, int //<= how many allocations to disturbut this calculation. //[kif.Thread]: 1x1, int //<= how many threads to run at the same time //[kif.MaxRAM]: 1x1, real //<= set the Max RAM usage for the calculation. If the PiLab estimeted //RAM is larger than this, calculation will be stopped in the beginning. //If so, try to increase Kif.Allocation so each allocation will need //less RAM. //==== << PiLab output >> ==== //[kif.k_point]: nx3, real //=> k-points //[kif.k_num]: 1 x tot_alloc, int //=> number of k-points in each allocation // **** Version **** // Apr 29, 2016 // **** Comment **** function PiLab_kif(project_name) disp('{kif}: starting calculation '); c1=clock(); printf('\n'); printf(' => start time: %4d/%02d/%02d %02d:%02d:%02d\n',c1); // loading variables =============================================== disp('{kif}: loading variables '); PiLab_loader(project_name,'kif','user','trim'); load(project_name+'_kif.sod'); load(project_name+'_ham.sod'); disp(' => all variables loaded'); // variable check =================================================== disp('{kif}: checking variables ') if grep(kif.Command,'&')==[] & grep(kif.Command,'start /b')==[] then disp('Warning: PiLab_kif, kif.Command must have send-to-background'.. +' command, e.g. & (linux) / start /b (windows) !'); end if kif.KptGen~='grid' & kif.KptGen~='path' & kif.KptGen~='manual' then disp('Error: PiLab_kif, kif.KptGen can only be ''grid/path/manual'''); abort end if kif.Format~='red' & kif.Format~='cart' then disp('Error: PiLab_kif, kif.Format can only be ''red'' or ''cart'''); abort end select kif.KptGen case 'grid' if length(kif.SpanVec(1,:))~=3 | length(kif.SpanVec(:,1))~=4 then disp('Error: PiLab_kif,kif.SpanVec must be 4x3 matrix'); abort end if length(kif.Mesh)~=3 | find(kif.Mesh<=0)~=[] then disp('Error: PiLab_kif,kif.Mesh be a 1x3 and all >=1'); abort end case 'path' if length(kif.Path(1,:))~=3 then disp('Error: PiLab_kif, kif.Path must be nx3 !'); abort end if length(kif.Div)~=1 | kif.Div-fix(kif.Div)~=0 then disp('Error: PiLab_kif, kif.Div must be an integer !'); abort end end disp(' => all variables passed') // core Part ======================================================== // generate k-point disp('{kif}: running core part '); disp(' => generating k-points'); select kif.KptGen case 'grid' [kif.k_point]=PIL_k_mesh(ham.rec_vec,kif.Mesh,kif.SpanVec,kif.Format,'on'); case 'path' if kif.Format=='red' then [kif.k_point,kif.k_div]=PIL_k_path(kif.Path*ham.rec_vec,kif.Div,'unit'); else [kif.k_point,kif.k_div]=PIL_k_path(kif.Path,kif.Div,'unit'); end case 'manual' fid=mopen('kif_kpoint.dat','r'); kif.k_point=PIL_read_mat(fid); mclose(fid); if kif.Format=='red' then kif.k_point=kif.k_point*ham.rec_vec; end end // estimate memory usage for each allocation disp(' => estimate memory usage '); tot_k=length(kif.k_point(:,1)); tot_state=length(ham.state_info(:,1)); n_k=ceil(tot_k/kif.Allocation); tot_ele=(5*tot_state*tot_state+tot_state)*n_k; // Vk+Hk part // estimated RAM in MB=matrix in RAM + file size when store+10% buffer est_mem=((tot_ele/1e7)*76+(tot_ele/1e6)*15.2)*1.1; disp(' estimated memory per allocation= '+string(est_mem)+'MB'); if est_mem > 2040.0 then disp('Warning: estimated memory is larger than 2GB !'); disp(' Reset to 2GB, job could fail!'); est_mem=2040.0; end if est_mem*kif.Thread > kif.MaxRAM then disp('Error: PiLab_kif, estimeted memory is larger than kif.MaxRAM!'); disp(' Please increase kif.Allocation.'); abort; else disp(' total memory needed is '+string(est_mem*kif.Thread)+'MB'); end disp(' => estimate file size ') est_size=(n_k*tot_state^2)/65000; disp(' estimated Vk size per allocation= '+string(est_size)+'MB') if est_size > 350.0 then disp('Error: PiLab_kif, estimated file size > 350.0 MB !'); disp(' Please increase allocations!'); abort end clear ham // perform distrubited parallel calculation disp(' => running distributed calculation '); disp(' check ./kif/runtime.log for runtime status'); [kif.k_alloc]=PIL_Hk_solver_dist(pwd(),project_name,'kif',kif.Command,.. kif.k_point,3,kif.Allocation,kif.Thread,est_mem); // output information ============================================== disp('{kif}: output information '); fid(1)=mopen(project_name+'_kif.plb','a+'); PIL_print_mat('kif.k_alloc, @f:f, number of k-point at each allocation'.. +' [tot_k,ini_k,final_k]',kif.k_alloc,'i',fid(1)); if kif.KptGen=='path' then PIL_print_mat('kif.k_div, @f:f, k_div',kif.k_div,'i',fid(1)); end PIL_print_mat('kif.k_point, @f:f, k_points',kif.k_point,'r',fid(1)); mclose(fid(1)); // finishing program =============================================== save(project_name+'_kif.sod','kif'); disp('{kif}: finishing {kif} calculation '); disp(' => time elapse '+string(etime(clock(),c1))+ ' seconds'); endfunction
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supprimerNonMax.sci
function image_traitee = supprimerNonMax(Es, Eo) afficherLogs("Suppression des non-maximums"); [N,M] = size(Es); for x = 1 : N for y = 1 : M [x1, y1, x2, y2] = recupererPixelsVoisins(Eo(x,y),x,y); // disp("pixels voisins:"+string(x)+':'+string(y)+":"+string(Eo(x,y))); // disp("x1: "+string(x1)) // disp("y1: "+string(y1)) // disp("x2: "+string(x2)) // disp("y2: "+string(y2)) voisin1 = verifierSiPixelExiste(x1,y1, Es); voisin2 = verifierSiPixelExiste(x2,y2, Es); // Si la valeur du pixel courant est inférieure à l'un de ses deux voisins // on affiche le pixel en noir if (Es(x,y) < voisin1) | (Es(x,y) < voisin2) then image_traitee(x,y) = 0; else image_traitee(x,y) = Es(x,y); end end end afficherLogs(image_traitee) endfunction
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run.sce
exec distance.sci; //TK_EvalFile('gui.tcl'); TCL_EvalFile('gui.tcl');
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//Compute the control limits //page no 109 clear clc; //(a) X1=15350; R1 = 411.4; SR = 411.4 K = 25; n = 4; X2=X1/K; R2=R1/K; A2 = 0.73; d2 = 2.059; D3 = 0.0; D4 = 2.28; USL = X2 + A2*R1; LCL = X2 - A2*R1; CL=X2; //Control limits for R-chart UCL1 = D4*R1; LCL1 = D3*R1; CL1 = R1; mprintf("\UCL = %.2f ",UCL1); mprintf("\LCL = %.2f ",LCL1); mprintf("\CL = %.2f ",CL1); //(b) Specification limits are USL = 625; LCL = 595; sd=R1/d2; UNTL = X1 + 3*sd; LNTL = X1 - 3*sd; PC=6*sd; mprintf("\Process capability = %.2f ",PC); Z=(595-614)/sd; mprintf("\nPercentage of rejection = %.2f ",Z); mprintf("\n a) Probability from table 0.947 = 91.47 percent "); mprintf("\n Rework = 8.53 percent "); Z1=(625-618.97)/sd; mprintf("\nPercentage of rejection = %.2f ",Z1); mprintf("\n Probability from table 0.7734 = 77.34 percent "); mprintf("\n Rework = 22.66 percent ");
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binden V;IND;SG;1;PST werden V;SBJV;PL;PST werden V;IND;SG;2;PST bruken V;IMP;PL;2 ewich ADJ;DAT;LGSPEC1 drepen V;IND;SG;2;PRS geven V;IND;SG;2;PST nemen V;IND;SG;3;PRS vrisch ADJ;ACC;NEUT;SG;LGSPEC1 andrepen V;IMP;SG;2 dunker ADJ;DAT;FEM;SG;LGSPEC2 sniden V;IND;SG;3;PRS jachteren V;IND;SG;1;PRS vrie ADJ;GEN;PL;LGSPEC2 dach N;DAT;PL riden V;IND;SG;2;PST drepen V;IMP;SG;2 afwolteren V;IMP;PL;2 anvechten V;NFIN vrie ADJ;GEN;NEUT;SG;LGSPEC2 afwolteren V;IND;SG;3;PRS achten V;SBJV;SG;2;PST nemen V;SBJV;PL;PRS vrisch ADJ;GEN;FEM;SG;LGSPEC2 tellen V;IND;SG;2;PST helpen V;NFIN afwolteren V;SBJV;SG;3;PRS snorren V;NFIN bedriven V;IND;SG;1;PST geven V;IND;PL;PST vechten V;NFIN kolt ADJ;GEN;MASC;SG;LGSPEC2 bedriven V;IMP;PL;2 valsch ADJ;ACC;MASC;SG;LGSPEC1 beschriven V;IND;SG;2;PST beden V;NFIN vechten V;SBJV;SG;1;PST afwolteren V;NFIN tellen V;NFIN bedriven V;NFIN kleine ADJ;ACC;MASC;SG;LGSPEC1 vorswinden V;SBJV;SG;1;PST waren V;SBJV;SG;2;PRS vorswinden V;SBJV;PL;PRS schone ADJ;GEN;NEUT;SG;LGSPEC2 andrepen V;SBJV;PL;PRS sniden V;SBJV;SG;3;PRS water N;NOM;PL vorgeten V;SBJV;SG;1;PRS stigen V;SBJV;SG;2;PRS schriven V;SBJV;SG;1;PST snorren V;IMP;SG;2 jagen V;SBJV;SG;1;PRS binden V;SBJV;PL;PST schone ADJ;ACC;NEUT;SG;LGSPEC1 drinken V;SBJV;SG;1;PRS valsch ADJ;GEN;MASC;SG;LGSPEC2 riden V;IND;SG;2;PRS vechten V;IND;SG;3;PRS anvechten V;IND;PL;PRS anvechten V;SBJV;SG;1;PRS sugen V;IND;PL;PST binden V;IND;SG;3;PST anvechten V;NFIN valsch ADJ;DAT;LGSPEC1 leven V;IND;SG;1;PST andrepen V;IND;SG;3;PRS kolt ADJ;ACC;NEUT;SG;LGSPEC2 ewich ADJ;ACC;NEUT;SG;LGSPEC2 valsch ADJ;GEN;FEM;SG;LGSPEC2 drepen V;IND;PL;PST anvechten V;IND;SG;1;PRS vogen V;NFIN tellen V;SBJV;PL;PRS valsch ADJ;ACC;PL;LGSPEC1 beden V;IND;SG;1;PST andrucken V;IND;PL;PRS olt ADJ;GEN;FEM;SG;LGSPEC2 andrucken V;SBJV;PL;PRS beden V;SBJV;SG;1;PST leven V;NFIN olt ADJ;NOM;PL;LGSPEC1 afwaschen V;SBJV;SG;2;PST andrucken V;SBJV;SG;1;PST vorsupen V;SBJV;SG;3;PRS geven V;SBJV;SG;2;PRS drepen V;NFIN nemen V;IND;SG;1;PRS drepen V;SBJV;SG;1;PRS andrucken V;SBJV;PL;PST andrepen V;SBJV;PL;PRS snorren V;SBJV;SG;1;PST sugen V;SBJV;PL;PRS riden V;IND;SG;1;PRS sniden V;IND;PL;PST kleine ADJ;GEN;FEM;SG;LGSPEC2 ewich ADJ;DAT;NEUT;SG;LGSPEC2 drepen V;SBJV;PL;PST nemen V;NFIN andrucken V;IND;SG;1;PRS werden V;IND;SG;2;PRS vechten V;IND;SG;3;PRS afwaschen V;IND;SG;3;PRS beschriven V;IND;SG;3;PRS vechten V;SBJV;SG;2;PRS kleine ADJ;ACC;PL;LGSPEC2 beden V;NFIN water N;DAT;PL ewich ADJ;NOM;SG;LGSPEC2 anvechten V;IND;PL;PRS dunker ADJ;ACC;PL;LGSPEC1 binden V;IMP;SG;2 helpen V;IND;SG;1;PRS afwaschen V;IND;SG;3;PRS drinken V;IND;SG;2;PRS kolt ADJ;ACC;PL;LGSPEC1 andrucken V;IND;SG;2;PST varen V;SBJV;SG;1;PRS leven V;IND;PL;PST olt ADJ;DAT;LGSPEC1 helpen V;IND;PL;PRS schone ADJ;DAT;NEUT;SG;LGSPEC2 afwaschen V;IND;PL;PRS bedriven V;IND;SG;3;PST vrisch ADJ;GEN;PL;LGSPEC2 krossen V;IND;SG;3;PRS jachteren V;SBJV;PL;PST kolt ADJ;DAT;NEUT;SG;LGSPEC2 binden V;IND;PL;PRS geven V;IND;SG;3;PST afwaschen 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bedriven V;IND;SG;2;PRS vrisch ADJ;DAT;FEM;SG;LGSPEC2 helpen V;IND;SG;2;PRS spoden V;SBJV;SG;3;PST vorgeten V;IND;SG;2;PRS varen V;IND;SG;2;PST kolt ADJ;GEN;NEUT;SG;LGSPEC2 kolt ADJ;GEN;PL;LGSPEC2 andrepen V;SBJV;SG;2;PRS valsch ADJ;NOM;SG;LGSPEC1 riden V;IND;SG;3;PRS varen V;IND;PL;PST sniden V;IMP;PL;2 valsch ADJ;GEN;FEM;SG;LGSPEC2 varen V;SBJV;SG;2;PRS drepen V;IND;SG;2;PST supen V;IND;SG;2;PST wolteren V;SBJV;PL;PRS tellen V;SBJV;SG;3;PST vorswinden V;IND;SG;2;PST tellen V;SBJV;PL;PST jachteren V;IND;SG;2;PRS ewich ADJ;DAT;FEM;SG;LGSPEC2 sugen V;IND;PL;PRS andrucken V;SBJV;SG;2;PRS afwolteren V;SBJV;PL;PST snorren V;IND;PL;PST wolteren V;SBJV;SG;2;PRS drinken V;SBJV;PL;PST nemen V;IMP;SG;2 valsch ADJ;DAT;PL;LGSPEC2 krossen V;IND;PL;PRS bedriven V;SBJV;SG;1;PST andrucken V;SBJV;SG;3;PRS olt ADJ;NOM;SG;LGSPEC1 bedriven V;IMP;SG;2 stigen V;IMP;SG;2 geven V;IND;SG;2;PRS vorsupen V;SBJV;PL;PST avent N;NOM;SG schone ADJ;GEN;FEM;SG;LGSPEC2 vrisch ADJ;DAT;LGSPEC1 geven V;NFIN tellen 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clc; disp("Example 2.2"); v=120000; //volume in metre cube. t=1.5; //time in second. s=25000; //area in metre cube. a=(0.16*v)/(t*s); //using Sabine formula for calculating a disp(a,"Average Absorbing Power of Surface = "); //Displaying Result.
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clear clc //to find tension in the string and normal force exerted on the block by the plane //to analyse the motion when the string is cut // GIVEN:: //refer to problem 5.7 from page no. 95 //mass of first block m1 = 9.5//in kg //angle of inclination of plane theta = 34//in degrees //mass of second block m2 = 2.6//in kg //acceleration due to gravity g = 9.81//in m/s^2 //coefficient of static friction mew_s = 0.24 //coefficient of kinetic friction mew_k = 0.15 // SOLUTION: //T is tension in the spring and N is normal reaction force by surface. //refer to the free body diagrams 5-17a from page no. 99 //for mass m1 and m2 //assuming m1 moves in positive x direction //equating forces in x direction and applying newton's second law of motion //equating forces in y direction and applying newton's second law of motion //acceleration of blocks a = (m2-(m1*(sind(theta)- (mew_k*cosd(theta)))))*g/(m1 + m2)//in m/s^2 //if ans. for a is -ve then our assumption is wrong i.e. m1 is moving in -ve x direction but magnitude of ans is correct //tension in the string T = (((m1*m2*g)*(1 + sind(theta) - (mew_k*cosd(theta))))/(m1 + m2))//in N T = round(T) printf ("\n\n Acceleration of blocks a = \n\n %.1f m/s^2",a); printf ("\n\n Tension in the string T = \n\n %2i N",T);
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//developed in windows XP operating system 32bit //platform Scilab 5.4.1 clc;clear; //example 18.14w //calculation of angle of rotation of the mirror in given setup //given data mu=1.5; //refractive index of convex lens A=4; //angle of prism (in degree) //calculation delta=(mu-1)*A disp(delta,'the mirror should be rotated by angle(in degree) of');
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////Variable Declaration n1 = 2 //Two spin states for 1st electron in orbit 1 n2 = 2 //Two spin states for 2nd electron in orbit 2 //Calculation M = n1*n1 //Results printf("\n Possible spin states for excited state are %2d",M)
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//Condición inicial Ciclohexano_Tolueno clear clc //Dirección de la carpeta donde se encuentran los experimentos path='/Users/Jarvis/Desktop/Datosnmr/2019-07-18-ciclohexano_tolueno/' //Carpeta inicial nb=170 //Carpeta final nf=849 //Numero de puntos nt=17 //Numero de mapeos nm=40 //BUCLE DE MAPEOS// M=linspace(nb,nb+nm-1,nm) //Carpeta que hace el seguimineto a las carpetas iniciales de cada mapeo n1=nb for j=1:size(M,2) if n1<nf then //Matriz de procesamiento N=linspace(n1,n1+nt-1,nt) for i=1:size(N,2) idr=mopen(path+string(N(1,i))+'/pdata/1/1r','rb'); Spectrum(:,i) = mtlb_fread(idr, 1*16384,'int32'); mclose(idr); idr = mopen(path+string(N(1,i))+'/pdata/1/procs','r'); procs = mgetl(idr,-1); mclose(idr); [w,r]=grep(procs,'##$NC_proc'); [a,b,c,d]=regexp(procs(w),'/(?P<name>\w+)=\s+(?P<digit>\D*\d+)/'); fa = strtod(d(2)); Spectrum(:,i)= Spectrum(:,i).*(2^fa); end mclose('all') //Limites de integracion //------------------------------------------------------------------------------ //Ciclohexano_Para_Aromatico //plot2d(Spectrum(9900:11200,:)) signal_1_int_reg_low=9900 signal_1_int_reg_upp=11200 for i=1:size(N,2) I1(1,i)=sum(real(Spectrum(signal_1_int_reg_low:signal_1_int_reg_upp,i))); end //Tolueno_Aromatico //plot2d(Spectrum(3800:4900,:)) signal_2_int_reg_low=3800 signal_2_int_reg_upp=4900 for i=1:size(N,2) I2(1,i)=sum(real(Spectrum(signal_2_int_reg_low:signal_2_int_reg_upp,i))); end //------------------------------------------------------------------------------ //Ciclohexano_Para_Metilo //plot2d(Spectrum(9900:11200,:)) signal_4_int_reg_low=9900 signal_4_int_reg_upp=11200 for i=1:size(N,2) I4(1,i)=sum(real(Spectrum(signal_4_int_reg_low:signal_4_int_reg_upp,i))); end //Tolueno_Metilo //plot2d(Spectrum(9000:9900,:)) signal_3_int_reg_low=9000 signal_3_int_reg_upp=9900 for i=1:size(N,2) I3(1,i)=sum(real(Spectrum(signal_3_int_reg_low:signal_3_int_reg_upp,i))); end //------------------------------------------------------------------------------ //Tratamiento espacial a la coordenada z OMEG_low=-36000 OMEG_upp=+36000 OMEGA=linspace(OMEG_upp,OMEG_low,nt) r=42.57747892*10.^2 z= OMEGA./(r*10.6104) + 2.0 z=z(1,$:-1:1) //Tramiento para encontrar la fraccion molar a partir de las integrales for i=1:nt X_CA(1,i)=I1(1,i)*1/12/((I2(1,i))*1/5+(I1(1,i))*1/12); X_A(1,i)=I2(1,i)*1/5/((I2(1,i))*1/5+(I1(1,i))*1/12); X_M(1,i)=I3(1,i)*1/3/((I3(1,i))*1/3+(I4(1,i))*1/12); X_CM(1,i)=I4(1,i)*1/12/((I3(1,i))*1/3+(I4(1,i))*1/12); X_CT(1,i)=(((I1(1,i)*1/12/((I2(1,i))*1/5+(I1(1,i))*1/12))+(I4(1,i)*1/12/((I3(1,i))*1/3+(I4(1,i))*1/12)))/2); X_TT(1,i)=(((I2(1,i)*1/5/((I2(1,i))*1/5+(I1(1,i))*1/12))+(I3(1,i)*1/3/((I3(1,i))*1/3+(I4(1,i))*1/12)))/2); end X_CA0=cat(1,z,X_CA) X_A0=cat(1,z,X_A) X_CM0=cat(1,z,X_CM) X_M0=cat(1,z,X_M) X_CT0=cat(1,z,X_CT) X_TT0=cat(1,z,X_TT) X_CA0=X_CA0' X_A0=X_A0' X_CM0=X_CM0' X_M0=X_M0' X_CT0=X_CT0' X_TT0=X_TT0' //Graficas //------------------------------------------------------------------------------ //plot2d(X_CA0(:,1),X_CA0(:,2),style=-11)//Ciclohexano_Para_Aromatico (Cuadro) //plot2d(X_A0(:,1),X_A0(:,2),style=-5)//Tolueno_Aromatico (Diamante) //------------------------------------------------------------------------------ //plot2d(X_CM0(:,1),X_CM0(:,2),style=-9)//Ciclohexano_Para_Metilo (Circulo) //plot2d(X_M0(:,1),X_M0(:,2),style=-3)//Tolueno_Metilo(Circulo_Cruz) //------------------------------------------------------------------------------ plot2d(X_CT0(:,1),X_CT0(:,2),style=-12)//Ciclohexano (Triangulo) plot2d(X_TT0(:,1),X_TT0(:,2),style=-8)//Tolueno (Rombo cruz) //------------------------------------------------------------------------------ //Solapamiento de espectros //plot2d(Spectrum(:,j)) //for i=1:nt // plot2d([1:16384], Spectrum(:,i)) //end //Angulo //+100*i //+1e5*i //------------------------------------------------------------------------------ n1=n1+nt end end
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<?php include ('knights.php'); $array=newBoard(); $array[1][1]=1; printBoard($array); $array=solve($array,1,1,2); printBoard($array); ?>
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function V=WT2Dext(wt,Sc,Num) // This Software is ( Copyright INRIA . 1998 1 ) // // INRIA holds all the ownership rights on the Software. // The scientific community is asked to use the SOFTWARE // in order to test and evaluate it. // // INRIA freely grants the right to use modify the Software, // integrate it in another Software. // Any use or reproduction of this Software to obtain profit or // for commercial ends being subject to obtaining the prior express // authorization of INRIA. // // INRIA authorizes any reproduction of this Software. // // - in limits defined in clauses 9 and 10 of the Berne // agreement for the protection of literary and artistic works // respectively specify in their paragraphs 2 and 3 authorizing // only the reproduction and quoting of works on the condition // that : // // - "this reproduction does not adversely affect the normal // exploitation of the work or cause any unjustified prejudice // to the legitimate interests of the author". // // - that the quotations given by way of illustration and/or // tuition conform to the proper uses and that it mentions // the source and name of the author if this name features // in the source", // // - under the condition that this file is included with // any reproduction. // // Any commercial use made without obtaining the prior express // agreement of INRIA would therefore constitute a fraudulent // imitation. // // The Software beeing currently developed, INRIA is assuming no // liability, and should not be responsible, in any manner or any // case, for any direct or indirect dammages sustained by the user. // // Any user of the software shall notify at INRIA any comments // concerning the use of the Sofware (e-mail : FracLab@inria.fr) // // This file is part of FracLab, a Fractal Analysis Software [wti, wtl]=WT2DStruct(wt); V=zeros(wtl(Sc,1), wtl(Sc,2)); index=0; for i=0:(wtl(Sc,1)-1), for j=0:(wtl(Sc,2)-1), V(i+1,j+1)=wt(wti(Sc,Num)+index), index = index+1; end; end;
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clc// // // //Variable declaration ni=1.5*10^16; //carrier density(per m^3) mew_e=0.13; //electron mobility(m^2/Vs) mew_h=0.05; //hole mobility(m^2/Vs) e=1.6*10^-19; d=2.33*10^3; //density(kg/m^3) n=28.1; na=6.02*10^26; //number of atoms //Calculation sigma=ni*e*(mew_e+mew_h); //conductivity(ohm-1 m-1) Nd=d*na/(n*10^8); p=ni^2/Nd; sigma_ex1=Nd*e*mew_e; //conductivity(ohm-1 m-1) n=p; Na=Nd; sigma_ex2=Na*e*mew_h; //conductivity(ohm-1 m-1) //Result printf("\n conductivity is %0.3f *10^-3 ohm-1 m-1",sigma*10^3) printf("\n conductivity is %0.2f ohm-1 m-1",sigma_ex1) printf("\n conductivity is %0.2f ohm-1 m-1",sigma_ex2)
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function xt = sampled2continuous( xn , T, t ) //This function calculates the output reconstructed from the samples n supplied as input, at a rate of 1/s samples per unit time. //Calling Sequence //x = sampled2continuous (xn, T, t) //Parameters //xn:sampled signal //T:sampling rate //t:all the instants of time when you need x(t) from x[n] //Description //This is an Octave function. //This function calculates the output reconstructed from the samples n supplied as input, at a rate of 1/s samples per unit time. //The third parameter t is all the instants where output x is needed from intput n and this time is relative to x(0). //Examples //sampled2continuous([1,2,3],5,6) //ans = // 2.4166806 if ( argn(2) < 3 ) error('wrong number of input parameters') end N = length( xn );//finding the length of input sequence xn = matrix( xn, N, 1 );//stacking the matrix xn in columnwise manner [TT,tt]= meshgrid(T*(0:N-1)',t); S = sinc(%pi.*(tt -TT)./T); xt = S*xn;//recontructing the samples return endfunction
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function %i_plot2d1(str,x,y,varargin) plot2d1(str,double(x),double(y),varargin(:))
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// Exa Misc. 6.2 clc; clear; close; format('v',6) // Given data R1 = 10;// in k ohm R_F = 1000;// in k ohm // Vin/R1 = -Vo/R_F and Vo/Vin = Ao = -R_F/R1 Ao = abs(-R_F/R1);// in k ohm disp(Ao,"The closed loop gain is"); Vin = 30;// in mV Vin = Vin * 10^-3;// in V // The output voltage, Vo =-Ao*Vin;// in V disp(Vo,"The output voltage in V is"); // Note: The loop gain will be unit less.
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clc; Vs=200; Imax=700*10**-3; Iavg=250*10**-3; Imax=0.8*Imax; disp('mA',Imax*10**3,"Imax="); Vm=sqrt(2)*Vs; RL=Vm/Imax; disp('ohm',RL*1,"RL="); Vdc=2*Vm/%pi; disp('V',Vdc*1,"Vdc="); Idc=Vdc/RL; disp('A',Idc*1,"Idc="); PIV=2*Vm; disp(PIV);
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// Example 4.8 format('v',5) clc; clear; close; // given data V2rms= 12.6;// in V V_Z= 6.8;// in V V2peak= V2rms/0.707;// in V Vin= V2peak;// in V Vout= V_Z;// in V R_L= 1.2;// in kΩ R_L= R_L*10^3;//in Ω Rs= 1;// in kΩ Rs= Rs*10^3;// in Ω Is= (Vin-Vout)/Rs;// in A I_L= Vout/R_L;// in A // The zener current Iz= Is-I_L;// in A Iz= Iz*10^3;// in mA disp(Iz,"The zener current in mA is : ") // Note: The calculation in the book is not accurate.
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//Example 1_30 clc(); clear; //To find the wavelength of the light D5=0.336 //units in centimeters D5=0.336*10^-2 //units in meters D15=0.59 //units in centimeters D15=0.59*10^-2 //units in meters m=10 R=100 //units in centimeters R=100*10^-2 //units in meters lemda=((D15^2-D5^2)/(4*m*R))*10^9 printf("Wavelength of the light is %.0f nanometers",lemda)
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//pathname=get_absolute_file_path('4.18.sce') //filename=pathname+filesep()+'4.18-data.sci' //exec(filename) //Maximum temperature(in K): T1=800+273 //Minimum temperature(in K): T2=50+273 //Temperature of the 3rd reservoir(in K): T3=50+273 //Temperature of the 4th reservoir(in K): T4=10+273 //Heat picked up by Carnot cycle(in kW): Q3=15 //Energy required to run a machine(in kW): E=25 //Efficiency: n=1-T2/T1 //From the relation of COP: Q4=Q3*T3/T4 //Work by heat pump(in kW): Whp=Q4-Q3 //Work in the heat engine(in kW): Whe=Whp+E //Heat from source at 1173 K(in kW): Q1=Whe/n //Heat rejected to the reservoir from engine 1(in kW): Q2=Q1-Whe //Total heat rejected to the reservoir(in kW): Qt=Q2+Q4 printf("\nRESULT\n") printf("\nHeat rejected to the reservoir = %f kW",Qt) printf("\nHeat received from the highest temperature reservoir = %f kW",Q1)
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clear; clf; clc; x = [1 2 3]; disp(x,"This is x :"); y = [6 4 5 8]; disp(y, "This is y :"); [z l1]= xcorr(x,y); disp(z, "This is w = xcorr(x,y) :"); disp(l1,"Log index of z"); [w l2]= xcorr(y,x); disp(w,"This is w = xcorr(y,x) : "); disp(l2,"Log index of w");
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clc; clear; mprintf('MACHINE DESIGN \n Timothy H. Wentzell, P.E. \n EXAMPLE-11.5 Page No.241\n'); //Gear train value Na=12; Nb=36; Nc=16; Nd=64; Vr=(Nb/Na)*(Nd/Nc); mprintf('\n Gear train value is %f ',Vr); //Motor torque hp=1.5; n=1750; T=63000*hp/n; mprintf('\n Motor torque is %f in-lb.',T); //Output torque Tout=T*Vr; mprintf('\n Output torque is %f in-lb.',Tout); //Output speed nout=n/Vr; mprintf('\n Output speed is %f rpm.',nout); //Directions mprintf('\n Directions\n Gear A is clockwise.\n Gear B is counterclockwise.\n Gear C is counterclockwise.\n Gear D is clockwise.'); //Output power hp=T*n/63000; mprintf('\n Output power is %f hp.',hp);
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//Example 9.11 clc disp("Choose op-amp LM318 with V_sat as +- 13.5 V with supply voltage +- 15 V") disp(" V_UT = + 5 V") disp("Now V_UT = (R2 / R1+R2)*V_sat") disp("Therefore, 5 = (R2 / R1+R2)*13.5") disp("Therefore, R1 + R2 = 2.7*R2") disp("Therefore, R1 = 1.7*R2") disp("Choose R2 = 10 k-ohm") r1=1.7*10 disp(r1,"Therefore, R1(in k-ohm) =") disp("The designed circuit is shown in fig.9.46")
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clc; clear all; disp("upper surface temperature") thf=1020;// temperature of hot gases L=1.2*10^(-3);// thickness of blade k=12;//W/(m*C) A=1;// area hhf=2750;//W/(m^2*C) heat transfer coefficients hcf=1400;//W/(m^2*C) heat transfer coefficients t1=900;// temperature of the upper surface Q=hhf*A*(thf-t1);//W/m^2 rate of heat transfer per unit area disp ("W/m^2",Q,"rate of heat transfer per unit area = ") //Q=k*A*(t1-t2)/L; t2=t1-(Q*L/(k*A)); disp("degree C",t2,"t2 is =") //Q=hcf*A*(t2-tcf) tcf=t2-(Q/(hcf*A)); disp("degree C",tcf,"tcf is =")
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clc; p1=1; // Atmospheric pressure in bar T1=348; // Atmospheric temperature in kelvin V1=800; // Volume of air sucked into the cylinder in cm^3 p2=15; // pressure of air after compression in bar V2=V1/8; // volume of air after compression in cm^3 p3=50; // pressure of air after heat addition in bar Cvo=0.7165; // Specific heat at constant volme in kJ/kg K R=0.287; // characteristic gas constant of air in kJ/kg K // (a).Index of compression process n=log (p2/p1)/log (V1/V2); // Index of compression process disp ("which is less than 1.4. The compression process is polytropic.",n,"Index of compression process = ","(a).Index of compression process"); // (b).Change in entropy of air during each process m=(p1*10^2*V1*10^-6)/(R*T1); // Mass of air in cylinder T2=T1*(p2/p1)*(V2/V1); // Temperature after compression T3=T2*(p3/p2); // Temperature after heat addition delta_s21=m*(Cvo*log (T2/T1)+R*log (V2/V1)); // change in entropy during compression delta_s32=m*Cvo*log (T3/T2); //change in entropy during heat addition disp ("kJ/K",delta_s32,"change in entropy during heat addition = (Error in textbook)","kJ/K",delta_s21,"change in entropy during compression = (Error in textbook)","(b).Change in entropy of air during each process"); // (c).Heat transfer during polytropic compression process k=1.4;// Index of isentropic preocess Q=m*Cvo*((k-n)/(1-n))*(T2-T1); // Heat transfer during polytropic compression process disp ("kJ",Q,"Heat transfer during polytropic compression process = (Error in textbook)","(c).Heat transfer during polytropic compression process");
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${ using Typewriter.Extensions.WebApi; Template(Settings s) { s.OutputFilenameFactory = (file) => { return Singularize(file.Classes.First().Name.Replace("Controller", "").ToLower()) + ".service.ts"; }; } string Singularize(string s) { // use Humanizer or something actually good if (s.EndsWith("s")) { return s.Remove(s.Length-1, 1); } else if (s.EndsWith("ies")) { return s.Remove(s.Length - 3, 3) + "y"; } return s; } string ServiceName(Class c) { return Singularize(c.Name.Replace("Controller", "")) + "Service"; } string ImportDependencies(Class c) { var types = c.Methods.Select(m => m.Type.Name.TrimEnd('[',']')).Distinct(); return String.Join("\n", types.Select(t => $"import {{{t}}} from './{t}'")); } string ModelMap(Method m) { var type = m.Type; if (type.FullName.Contains("Models.")) { if (type.IsEnumerable) { return $"(<{type}>res.json().data).map({type.Name.TrimEnd('[', ']')}.fromJson)"; } else { return $"{type}.fromJson(res.json().data)"; } } return $"(<{type}>res.json().data)"; } } $Classes(:ApiController)[ import {Injectable} from 'angular2/core' import {Http, Response} from 'angular2/http' import {Observable} from 'rxjs/Observable' $ImportDependencies @Injectable() export class $ServiceName { constructor(private _http: Http) { } $Methods[ $name($Parameters[$name: $Type][,]) { return this._http.$HttpMethod(`$Url`, $RequestData) .map(res => $ModelMap) .catch(this._handleError); }] private _handleError(error: Response) { console.error(error); return Observable.throw(error.json().error || 'Server Error'); } }]
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// 08.07.11 function Ang=Phidegree() global PHI; Ang=PHI*180/%pi; endfunction
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//Exa 2.2 clc; clear; close; //given data Iio=20;//in nA IB=100;//in nA //Iio=IB1-IB2 disp("Eqn(1) : Iio=IB1-IB2=20"); //IB=(IB1+IB2)/2 disp("Eqn(2) : 2*IB=IB1+IB2=200"); disp("Adding two equations gives :"); IB1=(200+20)/2;//in nA disp(IB1,"IB1 in nA is : "); IB2=IB1-Iio;//in nA disp(IB2,"IB2 in nA is : ");
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//ex_5 d even and odd signals of x(t) clear; clc; close; t=0:5; x=[ 0 2 4 2 0 0]; figure a=gca(); plot2d3(t,x) plot(t,x,'r.') xtitle('x[n]','n') a.thickness=2; figure a=gca(); t2=-5:5 ; y=[ x($:-1:2)./2 x(1) x(2:6)./2 ] plot2d3(t2,y) plot(t2,y,'r.') xtitle('even','n') a.y_location='right'; a.thickness=2; figure a=gca(); z=[ -x($:-1:2)./2 0 x(2:6)./2 ] plot2d3(t2,z) plot(t2,z,'r.') xtitle('odd','n') a.y_location='right'; a.x_location='origin'; a.thickness=2;
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n=[2:10];u5=2*n+3 // first solution u5=2*[2:10]+3 // using one command u5=[7:2:23] // second solution
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//30/11/18 //Anandou Candassamy //TP1 de Méthode Numérique exo 2 clear(); //sclf(); function [v, lambda, iter] = puissanceInv(A, x0, tol, itermax) xk = x0; lambda1 = 1; lambda2 = 0; iter = 0; while (abs(lambda2 -lambda1) >= tol & iter<itermax) do lambda1 = lambda2; yk = xk/norm(xk); Ainv = A^-1; xk = A\yk; lambda2 = 1/(yk'*xk); iter = iter + 1; end v = yk; lambda = lambda2; endfunction A = [-4,14,0; -5,13,0; -1,0,2] A2 = [2 0 0; 0 0 0; 0 -2 1]; A3 = [2 1 0; 0 2 0; 0 0 1]; x0 = [6; 6; 6]; [first, scd, thrd] = puissanceInv(A, x0, 1e-10, 100); disp(first); disp(scd); disp(thrd); disp(bdiag(A)); disp(spec(A)); //[first, scd, thrd] = puissanceInv(A2, x0, 1e-10, 100); //disp(first); //disp(scd); //disp(thrd); //disp(bdiag(A2)); //disp(spec(A2)); [first, scd, thrd] = puissanceInv(A3, x0, 1e-10, 100); disp(first); disp(scd); disp(thrd); disp(bdiag(A3)); disp(spec(A3));
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clear //In this problem, it is required to find out the moment of inertia of the section about an axis AB. So there is no need to find out the position of the centroid. //The given section is split up into simple rectangles //Moment of inertia about AB = Sum of moments of inertia of the rectangle about AB //variable declaration A1=400*20.0 A2=100*10 A3=10*380.0 A4=100*10.0 IAB=(400.0*(20**3)/12)+(A1*(10**2))+((100*(10**3)/12)+(A2*(25**2)))*2+((10*(380**3)/12)+(A3*(220**2)))*2+((100*(10**3)/12)+(A4*(415**2)))*2 printf("\n IAB= %0.0f mm^4",IAB)
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//ques-5.34 //Calculating transport number of silver and nitrate ions clc x=0.06227;//Siver nitrate contained in 20g anode solution after electrolysis(in g) y=0.001788;//Siver nitrate contained in 1g anode solution before electrolysis(in g) y=y*20;//Siver nitrate contained in 20g anode solution before electrolysis(in g) m=0.0322;//mass of Ag deposited on voltameter (in g) z=(m*170)/108;//total weight of Silver nitrate electrolysed (in g) t1=(z-(x-y))/z;//transport number of silver ions t2=1-t1;//transport number of nitrate ions printf("Transport number of silver and nitrate ions are %.3f and %.3f respectively.",t1,t2);
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clear;lines(0); s=poly(0,'s'); G=[1/(s+1),s;1+s^2,3*s^3];Sl=tf2ss(G); S=ss2des(Sl) S1=ss2des(Sl,"withD") Des=des2ss(S);Des(5)=clean(Des(5)) Des1=des2ss(S1)
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Hp=10000; //pressure altitude in m Po=4.24*10^4; //Total pressure measured by pitot tube,N/m^2 P1=2.65*10^4; //pressure at pressure altitude 10000m from standard atmospheric table,N/m^2 T=230; //ambient temperature in Kelvin R=287 ;//gas constant for air,J/Kg.K y=1.4; //specific heat ratio for air a=340.3; //speed of sound at sea level,m/s P=1.01*10^5 ;//stmospheric pressure at sea level
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I(A(char *p = str, *p != '\0', p++, islower(*p))); I(A(int i = 0, i < 10, i++, E1(int j = 0, j < 10, j++, a[i] == a[j])));
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//Initilization of variables W=50 //lb g=32.2 //Calculations //Using equations of motion a=(10/(W/g)) //ft/s^2 B=((2.5*(W/g)*a)+4*W-1.5*10)/8 //lb A=50-B //lb //Result clc printf('The solution is A=%f lb B=%f lb and a=%f ft/s^2',A,B,a)
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// Copyright (C) 2012 - Prateek Papriwal // // 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 function y = distfun_chi2pdf(varargin) // Chi-square PDF // // Calling Sequence // y = distfun_chi2pdf(x,k) // // Parameters // x : a 1x1 or nxm matrix of doubles, the outcome, greater or equal to zero // k : a 1x1 or nxm matrix of doubles, the number of degrees of freedom. k belongs to the set {1,2,3.......} // y : a nxm matrix of doubles, the probability density. // // Description // Computes the probability distribution function of // the Chi-square distribution function. // // Any scalar input argument is expanded to a matrix of doubles // of the same size as the other input arguments. // // Examples // // Test with x scalar, k scalar // computed = distfun_chi2pdf(4,5) // expected = 0.1439759 // // // Test with expanded x, k scalar // computed = distfun_chi2pdf([2 6],5) // expected = [0.1383692 0.0973043] // // // Test with x scalar, k expanded // computed = distfun_chi2pdf(4,[4 7]) // expected = [0.1353353 0.1151807] // // // Test with both x,k expanded // computed = distfun_chi2pdf([2 6],[3 4]) // expected = [0.2075537 0.0746806] // // // Plot the function // h=scf(); // k = [2 3 4 6 9 12]; // cols = [1 2 3 4 5 6]; // lgd = []; // for i = 1:size(k,"c") // x = linspace(0,10,1000); // y = distfun_chi2pdf ( x , k(i) ); // plot(x,y) // str = msprintf("k=%s",string(k(i))); // lgd($+1) = str; // end // for i = 1:size(k,"c") // hcc = h.children.children; // hcc.children(size(k,"c") - i + 1).foreground = cols(i); // end // xtitle("Chi-square PDF","x","f(x)") // legend(lgd); // // Bibliography // http://en.wikipedia.org/wiki/Chi-squared_distribution // // Authors // Copyright (C) 2012 - Prateek Papriwal [lhs,rhs] = argn() apifun_checkrhs("distfun_chi2pdf",rhs,2) apifun_checklhs("distfun_chi2pdf",lhs,0:1) x=varargin(1) k=varargin(2) // // Check type apifun_checktype("distfun_chi2pdf",x,"x",1,"constant") apifun_checktype("distfun_chi2pdf",k,"k",2,"constant") // // Check content apifun_checkgreq("distfun_chi2pdf",x,"x",1,0) apifun_checkgreq("distfun_chi2pdf",k,"k",2,1) [x,k] = apifun_expandvar(x,k) y = distfun_gampdf(x,k ./ 2,2) endfunction
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--> w=[ 171*3^0.5/1000 -2349/2500 171/1000 2349*3^0.5/5000 171/500 2349/5000 -1/2 0 3^0.5/2 ] w = 0.2961807 -0.9396 0.171 0.8137175 0.342 0.4698 -0.5 0. 0.8660254 --> j=[1 0 0 0 Cos90 -Sen90 0 Sen90 Cos90] Undefined variable: Cos90 --> j=[1 0 0 0 0 -1 0 1 0] j = 1. 0. 0. 0. 0. -1. 0. 1. 0. --> h=w*j h = 0.2961807 0.171 0.9396 0.8137175 0.4698 -0.342 -0.5 0.8660254 0.
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//AC Circuits : example 4.48 :(pg 4.37) f=50; pi=3.14; Vdc=12; Idc=2.5; Vac=230; Iac=2; Pac=50; R=(Vdc/Idc); Z=(Vac/Iac); Pi=(Pac-((Iac^2)*R)); RT=(Pac/(Iac^2)); XL=sqrt((Z^2)-(RT^2)); L=(XL/(2*pi*f)); pf=(RT/Z); i=(Pi/(Iac^2)); printf("\nFor dc V=12 V, I=2.5 A \nFor ac V=230 V, I=2 A, P=50 W"); printf("\nIn an iron-cored coil,there are two types of losses \n(i)Losses in core known as core or iron loss \n(ii)Losses in winding known as copper loss"); printf("\nP=(I^2)*R+Pi \nP/(I^2)=R+((Pi)/(I^2)) \nRT=R+(Pi/(I^2)) \nwhere R is the resistance of the coil and (Pi/I^2) is the resistance which is equivalent to the effect of iron loss"); printf("\nFor dc supply, f=0 \nXL=0"); printf("\nR=%.1f Ohm",R); printf("\nFor ac supply \nZ=%.f Ohms",Z); printf("\nIron loss Pi=P-I^2*R=%.1f W",Pi); printf("\nRT=(P/I^2)=%.1f Ohm",RT); printf("\nXL=sqrt((Z^2)-(RT^2))=%.1f Ohm",XL); printf("\nXL=2*pi*L \nInductance L=%.3f H",L); printf("\nPower factor =RT/Z=%.3f (lagging)",pf); printf("\nThe series resistance equivalent to the effect of iron loss= Pi/(I^2)=%.1f Ohms",i);
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//Example 6-4// //minterm designation of AB''C''D''// clc //clears the window// clear //clears all existing variables// disp('copy original term') disp(' AB''C''D'' ') disp(' substitute ones for nonbarred letters and zeroes for barred letters ') disp('after substitution') disp(' 1000 ') a=bin2dec('1000') disp('the decimal equivalent of 1000 is:') disp(a) disp(' Therefore decimal subscript of m is 8 ') disp(' AB''C''D'' = m8 ') //result is displayed//
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clc clear //Input data k=1.3 //Adiabatic constant R=287 //Specific gas constant in J/kg-K P1=1 //Inlet pressure in bar T1=400 //Inlet temperature in K D=0.3 //Duct diameter in m M1=2 //Mach number at entry Mx=1.5 //Mach number upstream of shock M2=1 //Mach number at outlet f=0.003 //Friction factor //Calculation d1=P1*10^5/(R*T1) //Density at inlet in kg/m^3 a1=sqrt(k*R*T1) //Velocity of sound at inlet in m/s C1=M1*a1 //Gas velocity at inlet in m/s A1=%pi*D^2/4 //Inlet Area of the duct in m^2 m=d1*C1*A1 //Mass flow rate in kg/s p1=0.131 //Static to Stagnation pressure ratio at entry from gas tables (M1,k=1.4,isentropic) Po1=P1/p1 //Stagantion pressure at inlet in bar t1=0.625 //Static to Stagnation temperature ratio at entry from gas tables (M1,k=1.4,isentropic) To1=T1/t1 //Stagnation temperature at inlet in K p2=0.424 //Static to Critical pressure ratio at inlet from gas tables,fanno flow tables @M1,k=1.4 Pt1=P1/p2 //Critical pressure in bar p3=1.773 //Stagnation pressure ratio at entry to critical state from gas tables,fanno flow tables @M1,k=1.4 Pto1=Po1/p3 //Stagnation pressure at critical state in bar t2=0.719 //Static to Critical temperature ratio at inlet from gas tables,fanno flow tables @M1,k=1.4 Tt1=T1/t2 //Critical temperature in K X1=0.357 //frictional constant fanno parameter from gas tables,fanno flow tables @M1,k=1.4 p4=0.618 //Ratio of Static pressure before shock to critical pressure at entry from gas tables (fanno flow,Mx,k=1.4) Px=Pt1*p4 //pressure before shock in bar t3=0.860 //Ratio of Static temperature before shock to critical temperature at entry from gas tables (fanno flow,Mx,k=1.4) Tx=Tt1*t3 //Temperature before shock in K p5=1.189 //Ratio of Stagnation pressure before shock to Stagnation pressure at critical state at entry from gas tables (fanno flow,Mx,k=1.4) Pox=Pto1*p5 //Stagnation pressure at critical state in bar Xx=0.156 //frictional constant fanno parameter from gas tables,fanno flow tables @Mx,k=1.4 X3=X1-Xx //Overall frictional constant fanno parameter upstream of duct L1=(X3*D)/(4*f) //Length upstream of duct in m My=0.7 //Mach number downstream of shock from gas tables @Mx p6=2.413 //Static pressure ratio after and before the shock from gas tables @My Py=Px*p6 //Pressure after shock in bar t4=1.247 //Temperature ratio after and before the shock from gas tables @My Ty=Tx*t4 //temperature after shock in K p7=0.926 //Stagnation pressure ratio after and before the shock from gas tables @My Poy=Pox*p7 //Stagnation pressure after shock in bar p8=1.479 //Ratio of pressure after shock to pressure at critical state from gas tables @My Pt=Py/p8 //Critical pressure in bar p9=1.097 //Ratio of Stagnation pressure after shock to Stagnation pressure at critical state from gas tables @My Pot=Poy/p9 //Stagnation pressure at critical state in bar t5=1.071 //Ratio of temperature after shock to temperature at critical state from gas tables @My Tt=Ty/t5 //Critical temperature in K Xy=0.231 //frictional constant fanno parameter from gas tables,fanno flow tables @My,k=1.4 X2=0 //frictional constant fanno parameter from gas tables,fanno flow tables @M=1,k=1.4 X4=Xy-X2 //Overall frictional constant fanno parameter downstream of duct L2=(X4*D)/(4*f) //Length downstream of duct in m ds1=R*log(Po1/Pox) //Change of entropy upstream of the shock in J/kg-K ds2=R*log(Pox/Poy) //Change of entropy across the shock in J/kg-K ds3=R*log(Poy/Pot) //Change of entropy downstream of the shock in J/kg-K //Output printf('(A)Length of the duct upstream and downstream of the duct is %3.3f m and %3.3f m respectively\n (B)Mass flow rate of the gas is %3.3f kg/s\n (C)Change of entropy:\n Upstream of the shock is %3.2f J/kg-K\n Across the shock is %3.3f J/kg-K\n Downstream of the shock is %3.4f J/kg-K',L1,L2,m,ds1,ds2,ds3)
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//Example 18.7// y=[0 9 9.2 5.3 0]; //B(webers/m^2) x=[0 0.30 0.46 0.53 0.56]; //(BH(weber A/m^3 = J/m^3) plot2d(x,y, style=1) mprintf("(BH)max ~10*10^3 J/m^3") ylabel("BH*(kJ/m^3)","fontsize",4); xlabel("B(web/m^2)","fontsize",4);
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//chapter 19 Ex 5 clc; clear; close; sStill=7.5; sRiver=1.5; tTotal=50/60; sDown=sStill+sRiver; sUp=sStill-sRiver; dist=tTotal/(1/sDown+1/sUp); printf("The required distance is %d km",dist);
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//Example 18.2.a : saturation magnetization clc; clear; close; //given data : mu_b=9.27*10^-24;// A.m^2 p=8.9; // in g/cm^3 Na=6.023*10^23;// avogadro's number A=58.71; // in g/mol n=((p*Na)/A)*10^6; Ms=0.60*mu_b*n; disp(Ms,"saturation magnetization,Ms(A/m) = ")
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clear; clc; printf('FUNDAMENTALS OF HEAT AND MASS TRANSFER \n Incropera / Dewitt / Bergman / Lavine \n EXAMPLE 5.6 Page 288 \n'); //Example 5.6 // Burial Depth //Operating Conditions k = .52; //[W/m.K] Thermal Conductivity rho = 2050; //[kg/m^3] Density c = 1840; //[J/kg.K] Specific Heat Ti = 20+273; //[K] Initial Temp Ts = -15+273; //[K] Temp of surrounding T = 0+273; //[K] Temp at depth xm after 60 days t = 60*24*3600; //[sec] time perod alpha = k/(rho*c); //[m^2/s] //Using eqn 5.57 xm = erfinv((T-Ts)/(Ti-Ts))*2*(alpha*t)^.5; printf("\n Depth at which after 60 days soil freeze = %.2f m",xm); //END
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clc clear //Input data h=3000 //Altitude in m Pi=0.701 //Inlet pressure in bar Ti=268.65 //Inlet temperature in K u=525*(5/18) //Flight velocity in m/s eff_d=0.875 //Diffuser efficiency eff_c=0.79 //Compressor efficiency C1=90 //Velocity of air at compressor in m/s dTc=230 //Temperature rise through compressor k=1.4 //Adiabatic constant of air Cp=1005 //Specific heat capacity at constant pressure of air in J/kg-K R=287 //Specific gas constant in J/kg-K //Calculation ai=sqrt(k*R*Ti) //Sound velocity in m/s Mi=u/ai //Inlet mach number Toi=(1+((0.5*(k-1)*Mi^2)))*Ti //Stagnation temperature at diffuser inlet in K To1=Toi //Inlet Stagnation temperature of compressor in K, since hoi=ho1 T1=To1-(C1^2/(2*Cp)) //Temperature at inlet of compressor in K P1=Pi*((1+(eff_d*((T1/Ti)-1)))^(k/(k-1))) //Inlet pressure of compressor in bar dPc=P1-Pi //Pressure rise through inlet diffuser in bar pr_c=(((eff_c*dTc)/To1)+1)^(k/(k-1)) //Pressure ratio of compressor P=Cp*(dTc) //Power required by the compressor in kW/(kg/s) eff=1-(1/pr_c^((k-1)/k)) //Air standard efficiency //Output printf('(A)Pressure rise through diffuser is %3.4f bar\n (B)Pressure developed by compressure is %3.4f bar\n (C)Air standard efficiency of the engine is %3.4f',dPc,P1,eff)
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//Exa5(a) clc; clear; close; //given data is : P=4000;//in rupees N=9;// months R=6;// in % per annum //if interest is reckoned quarterly r=R/4;// in % per quarter,as there are 4 quarters in a year n=(N/12)*4;//in quarters Amount1=P*(1+r/100)^n; CI1=Amount1-P; disp(CI1,"Compound interest while reckoned quarterly :") //Ans in the book is not correct
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//Ex14_1 Pg-695 clc n1=1.545 //core refracrive index n2=1.510 //cladding refractive index d=3*10^(-6) //diamter of optical fiber in m a=d/2 //core radius in m del=(n1-n2)/n1 //fractional difference of refractive indices lamda_c=(2*%pi*a*n1*sqrt(2*del))/2.405 //cut-off wavelength printf("Cut-off wavelength = %.2f um",lamda_c*1e6)
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//ques-18.46 //Calculating decrease in chemical potential of benzene clc T=298;//temperature (in K) x_s=0.1;//mole-fraction of solute x_b=1-x_s;//mole-fraction of benzene C_P=8.314*T*log(x_b); printf("The decrease in chemical potential is %.2f J/mol.",C_P);
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//taylor series //example 1.12 //page 12 clc;clear;close; deff('y=f(x)','y=x^3+5*x-10'); deff('y=f1(x)','y=3*x^2-6*x+5')//first derivative deff('y=f2(x)','y=6*x-6')//second derivative deff('y=f3(x)','y=6')//third derivative D=[f(0) f1(0) f2(0) f3(0)] S1=0; h=1; for i=1:4 S1=S1+h^(i-1)*D(i)/factorial(i-1); end printf('the third order taylors series approximation of f(1) is :%d',S1);
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exec("mnprobln.sci",2); function ok=test_mnprobln() mu=[1;-1]; Sigma=[5 6;6 9]; n1=51; y1=linspace(-10,10,n1); n2=51; y2=linspace(-10,10,n2); y=zeros(2,n1*n2); for i1=1:n1 b=(i1-1)*n2; y(1,b+1:b+n2)=y1(i1); y(2,b+1:b+n2)=y2; end dy=((y1(n1)-y1(1))/(n1-1))*((y2(n2)-y2(1))/(n2-1)); p=exp(mnprobln(y,mu,Sigma))*dy; m0=sum(p); m1=zeros(2,1); m1(1)=sum(p .* y(1,:))/m0; m1(2)=sum(p .* y(2,:))/m0; m2=zeros(2,2); for i=1:2 for j=1:2 m2(i,j)=sum(p .* (y(i,:)-mu(i)).*(y(j,:)-mu(j)))/m0; end end assert_checkalmostequal(m0,1,0.025); assert_checkalmostequal(m1,mu,0.025); assert_checkalmostequal(m2,Sigma,0.025); ok=%T; endfunction
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//Ex 1.2 clc; clear; close; format('v',5); Iout=1;//mA VBE=0.7;//V Beta=100;//unitless VCC=30;//V IREF=Iout*(1+2/Beta);//mA R=(VCC-VBE)/IREF;//kohm disp(IREF,"Reference current(mA)"); disp(R,"Resistance required(kohm)");;
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////Variable Declaration dGf298 = 370.7 //Std. free energy of formation for Fe (g), kJ/mol dHf298 = 416.3 //Std. Enthalpy of formation for Fe (g), kJ/mol T0 = 298.15 //Temperature in K T = 400. //Temperature in K R = 8.314 //Calculations dGf = T*(dGf298*1e3/T0 + dHf298*1e3*(1./T - 1./T0)) //Results printf("\n Std. free energy of formation for Fe(g at 400 K is %4.1f kJ/mol",dGf/1000)
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Introduction to heat transfer by S.K.Som, Chapter 1, Example 4") //The average forced convective heat transfer coefficient(hbr) is 200 W/( m^2 °C) //The fluid temprature(Tinf) upstream of the cold surface is 100°C //The surface temprature(Ts) is 20°C hbr=200; Tinf=100; Ts=20; //The rate of heat transfer per unit area is q disp ("The rate of heat transfer per unit area q=hbr*(Tinf-Ts) in W/m^2") q=hbr*(Tinf-Ts)
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// 08.05.08 function Out=Arrowdata(varargin) global YaSize YaAngle YaPosition YaThick YaStyle; Nargs=length(varargin); P=varargin(1); Q=varargin(2); R=Q; Futosa=YaThick; Ookisa=YaSize; Thickness=1; Hiraki=YaAngle; Yapos=YaPosition; Position=1; Str=YaStyle; Flg=0; for I=3:Nargs Tmp=varargin(I); if type(Tmp)==1 if length(Tmp)>1 R=Tmp else if Flg==0 Ookisa=Ookisa*Tmp; end if Flg==1 if Tmp<5 Hiraki=Tmp*Hiraki; else Hiraki=Tmp; end end if Flg==2 R=P+Tmp*(Q-P); else R=P+Yapos*(Q-P); end if Flg==3 Futosa=Tmp end Flg=Flg+1; end end if type(Tmp)==10 if mtlb_findstr(Tmp,'=')~=[] execstr(Tmp); Futosa=Futosa*Thickness; R=P+Position*(Q-P); else Str=Tmp end end end Tmp1=Listplot([P,Q]); Tmp2=Arrowheaddata(R,Q-P,Ookisa,Hiraki,Futosa,Str); Out=Joingraphics(Tmp1,Tmp2); endfunction
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//check o/p for sting i/p y='character' Y=rms(y); disp(Y); //output // 104.81995
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#valve example $thermo = VirtualMaterials.RK / -> $thermo thermo + METHANE units SI v = Valve.Valve() v.In.T = 50 v.In.P = 7000.0 v.In.MoleFlow = 100.0 v.In.Fraction = 1.0 v.Out v.Out.P = 500.0 v.Out
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x=linspace(3,7,8); plot(x) linspace(1,2,10) linspace(1+%i,2+2*%i,10)
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TDR=2 dtt=16//data transfer time Size=TDR*dtt//size disp(Size,'size of a file transferred in Mb')
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errcatch(-1,"stop");mode(2);// Example 7.6, page no-163 d=10.5*10^3 //kg/m^3 sig=6.8*10^7//per Ohm-m wt=107.9//kg/m^3 e=1.6*10^-19//C avg=6.023*10^26//atoms/m^3 n=avg*d/wt mu=sig/(n*e) printf("The mobility of electron is %.3f *10^-2 m^2.V/s",mu*10^2) exit();
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## Tag reference test read <<EOF blob mark :1 data 35 Not an obfuscated C contest entry. blob mark :2 data 46 The quick brown fox jumped over the lazy dog. commit refs/heads/master mark :3 committer foo <foo> 101800 +0000 data 13 First commit M 100644 :1 bar.c M 100644 :2 foo.c M 100644 inline .gitignore data 199 # CVS default ignores begin tags TAGS .make.state .nse_depinfo *~ \#* .#* ,* _$* *$ *.old *.bak *.BAK *.orig *.rej .del-* *.a *.olb *.o *.obj *.so *.exe *.Z *.elc *.ln core # CVS default ignores end reset refs/tags/first from :3 commit refs/heads/master mark :4 committer foo <foo> 102400 +0000 data 14 Second commit from :3 D bar.c reset refs/tags/tag from :4 reset refs/heads/master from :4 EOF set echo <master> inspect <tag> inspect <first> inspect
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// b=blackman(4,'symmetric'); disp(b); //output // - 1.388D-17 // 0.63 // 0.63 // - 1.388D-17 //
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//clc() per1 = 20;//% ( 1 = ammonia) Vstp = 22.4143;//m^3/kmol Pstp = 101.325;//kPa Tstp = 273.15;//K V1 = 100;//m^3 P1 = 120;//kPa T1 = 300;//K P2 = 100;//kPa T2 = 280;//K per2 = 90;//% (absorbed) N = V1 * P1 * Tstp / (Vstp * Pstp * T1);//kmol Nair = (1 - per1 / 100) * N; N1 = per1 * N/100; Nabs = per2 * N1 / 100; N2 = N1 - Nabs;//leaving Ntotal = Nair + N2; Vstp1 = Ntotal * Vstp;//m^3 V2 = Vstp1 * Pstp * T2 / (Tstp * P2); disp("m^3",V2,"Volume of gas leaving = " )
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// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Engineering Thermodynamics by Onkar Singh Chapter 3 Example 2") m=0.5;//mass of gas in kg u1=26.6;//internal energy of gas at 200 degree celcius u2=37.8;//internal energy of gas at 400 degree celcius W=0;//work done by vessel in KJ disp("as the vessel is rigid therefore work done shall be zero") disp("W=0") disp("from first law of thermodynamics,heat required(Q)in KJ") disp("Q=U2-U1+W=Q=m(u2-u1)+W") Q=m*(u2-u1)+W disp("so heat required =5.6 KJ")
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function y = linspace(d1, d2, n) // Linearly spaced vector. // linspace(x1, x2) generates a row vector of 100 linearly // equally spaced points between x1 and x2. // linspace(x1, x2, n) generates n points between x1 and x2. [nargout,nargin]=argn(0) if nargin == 2 n = 100; end y = [d1*ones(1,n-1)+(0:n-2)*(d2-d1)/(n-1),d2];
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clc //initialisation of variables Ve=100//ft/sec P=50 //lbf/in^2 Vi=20 //ft/sec v=0.01608 //ft^3/lbm g=32.17//lbm-ft/lbf-sec^2 Pe=90//lbf/in^2 h=778 //ft-lbf/Btu T=540//f t=144//ft //CALCULATIONS P1=((Ve^2)-(Vi^2))/(v*2*g*t)//lbf/in^2 Ps=P+P1//lbf/in^2 he=((Ve^2)-(Vi^2))/(2*g*h)//Btu/lbm U=he-v*(Pe-P)*t/h //Btu/lbm S=U/T//Btu/lbm-R //RESULTS printf('The increase in enthalpy internal energy and entropy =% f Btu/lbm-R',S)
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Ch06Exa6_5_2.sci
// Scilab code Exa6.5.2 : To calculate the length of the first and last drift tubes which accelerate the protons whose frequency and energies are given. Page 268 (2011) f = 200e+06; // Frequency of applied the voltage, Hz V_0 = 750e+03; // Applied potential difference, V q = 1.6e-019; // Charge of proton, C m = 1.67e-027; // Mass of proton, Kg n_1 = 1; // For first tube L_1 = sqrt(2*n_1*q*V_0/m)/(2*f); // Length of the first tube, m n_n = 128; // For last tube L_n = 1/(2*f)*sqrt(2*n_n*q*V_0/m); // Length of the last tube,m printf("\n Length of the first tube = %4.2f m \n Length of the last tube = %4.2f m ", L_1,L_n); // Result // Length of the first tube = 0.03 m // Length of the last tube = 0.34 m
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/3537/CH1/EX1.41/Ex1_41.sce
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Ex1_41.sce
//Example 1_41 clc(); clear; //To calculate the wavelength of monochromatic light betaa=0.4 //units in mm betaa=0.4*10^-1 //units in cm d=0.1 //units in cm D=80 //units in cm lemda=(d*betaa)/D*10^8 printf("The wavelength of monochromatic light is %.0f angstroam",lemda)
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/libs/to_native_img.sci
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Exia-Aix-2016/ExoLife
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2021-09-07T01:47:04.742247
2018-02-15T11:57:47
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to_native_img.sci
function img=to_native_img(image) xmax = size(image,1) ymax = size(image,2) img=[] for x=1:xmax for y=1:ymax img(y,x) = image(x,y) end end img = uint8(img) endfunction
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prob12_1.sce
// page no 536 // Example 12.1 // Let the received signal be km(t)cos(wct) , demodulator input is [km(t)+nc(t)]cos(wct)+[ns(t)sin(wct)]. When this is multiplied by 2coswct and low pass filtered the output is s0(t)+n0(t)=km(t)+nc(t). // Hence So=k^2*m^2' , No=nc^2'. But the power of the received signal km(t)cos(wct)= 1uW. Hence k^2*m^2'/2=10^-6 clc; So=2*10^-6; // to compute nc: (nc^2)'=(n^2)'=x t0=496000; t1=504000 ; a=10^6 * %pi; y=integrate ('1/((t^2)+(a^2))','t',t0,t1); // to compute output SNR SNR=So/y; val=(10*(log (SNR))); disp(+'dB',val,"output SNR = ");
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/L3_TSI_Photoshop/Photoshop/app.sce
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2020-04-25T07:15:31.450109
2020-01-07T19:16:06
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//Configuration formats = ["JPG/JPEG format","*.jp*g";"*.png","PNG format"]; window = figure(); window.background = color(50, 50, 50); window.figure_name = gettext("MyPhotoshop Cc"); handle.Axesl = newaxes(); handle.Axesl.margins = [0 0 0 0]; handle.Axesl.axes_bounds = [0.05, 0.2, 0.66, 0.5]; handle.Axesl.background = color(30, 30, 30); handle.Axesl.auto_clear = 'on'; //Création d'un module pour charger l'image via chargement_image h1= uimenu("parent",window,"label",gettext("Charger une image"),"callback","chargement_image(formats)"); //Cacher les menu delmenu(window.figure_id,gettext("&File")); delmenu(window.figure_id,gettext("&Tools")); delmenu(window.figure_id,gettext("&Edit")); delmenu(window.figure_id,gettext("&?")); delmenu(window.figure_id,gettext("off")); //Textes //Photoshop CC photoshopCc = uicontrol(window,"style","text"); photoshopCc.string = "Photoshop CC"; photoshopCc.fontweight = "bold"; photoshopCc.position = [160 370 150 25]; photoshopCc.BackgroundColor = [0.20 0.20 0.20]; photoshopCc.ForegroundColor = [1 0 0.4]; photoshopCc.HorizontalAlignment = "center"; //Filtres filtres = uicontrol(window,"style","text"); filtres.string = "Filtres"; filtres.fontweight = "bold"; filtres.position = [448 320 130 25]; filtres.BackgroundColor = [0.12 0.12 0.12]; filtres.ForegroundColor = [1 0 0.4]; filtres.HorizontalAlignment = "center"; //La Filtre Box filtres_box=uicontrol(window,"style","listbox"); filtres_box.BackgroundColor=[0.12 0.12 0.12]; filtres_box.ForegroundColor=[0.25 0.25 0.25]; filtres_box.Position = [448 170 130 150]; filtres_box.String = ["Canny","Bonus","Horizontal","Vertical","Horivertical","Gaussien","N/B","Negatif","Prewitt","Sobel","Rouge","Vert","Bleu", "Cyan","Jaune","Violet"]; filtres_box.Value = 1; //Les bouttons //quitter quitter = uicontrol(window,"style","pushbutton"); quitter.String = "Quitter"; quitter.BackgroundColor=[0.12 0.12 0.12]; quitter.ForegroundColor=[1 0 0.4]; quitter.Position = [28 75 130 50]; quitter.Callback = "delete(window)"; //cleaner cleaner = uicontrol(window,"style","pushbutton"); cleaner.String = "Cleaner"; cleaner.BackgroundColor=[0.12 0.12 0.12]; cleaner.ForegroundColor=[1 0 0.4]; cleaner.Position = [168 75 130 50]; cleaner.Callback = "[current_ns_image] = cleaner_picture(handle);"; //sauvegarder sauvegarder = uicontrol(window,"style","pushbutton"); sauvegarder.String = "Sauvegarder"; sauvegarder.BackgroundColor=[0.12 0.12 0.12]; sauvegarder.ForegroundColor=[1 0 0.4]; sauvegarder.Position = [308 75 130 50]; sauvegarder.Callback = "sauvegarder_image(formats,handle)"; //etaler etaler = uicontrol(window,"style","pushbutton"); etaler.String = "Étaler"; etaler.BackgroundColor=[0.12 0.12 0.12]; etaler.ForegroundColor=[1 0 0.4]; etaler.Position = [448 75 130 50]; etaler.Callback = "[current_s_image] = etaler_filtre(filtres_box,handle)";
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pe3_7.sce
//example 3.7 clc; funcprot(0); // Initialization of Variable Vp=170; f=60; Vr=Vp/2; disp(Vr,"rms voltage in V") clear()
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clear; clc; close; V = 4; Vk = 0.3; id = 0; vd = 0.3; vi = V-Vk; disp(vi,'new transition level : '); t = 0:0.1:20; for i = 1:length(t); if(t(i)<=5) x(i) = (16/5)*t(i); elseif(t(i)>=5 & t(i)<=16) x(i) = -3.2*t(i) + 32; elseif(t(i)>=16 & t(i)<=20) x(i) = (16/5)*t(i)-64; end end for i = 1:length(t) if(x(i)>vi) y(i)=x(i); elseif(x(i)<=3.7) y(i)=3.7; end end plot2d(t,y,2,'011','',[0,0,20,16]); a = gca(); a.x_label.text = 't'; a.y_label.text = 'Vo'; xset('thickness',2); xstring(10,0,'T/2');
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/sim/scripts/setthermo.tst
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psy007/NNPC-CHEMICAL-SIM-
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2020-04-12T15:37:04.174834
2019-02-06T10:10:20
2019-02-06T10:10:20
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setthermo.tst
#Test the creation of the thermo cases and preserving compounds $thermo1 = VirtualMaterials.RK . -> $thermo1 /thermo1 + METHANE ETHANE PROPANE ISOBUTANE $thermo2 = VirtualMaterials.RK $thermo2 + ISOBUTANE PROPANE METHANE ETHANE $thermo3 = VirtualMaterials.Advanced_Peng-Robinson $thermo3 + PROPANE ISOBUTANE n-BUTANE ISOPENTANE n-PENTANE n-OCTANE $thermo4 = VirtualMaterials.RK thermo5 = VirtualMaterials.RK $thermo5 + NITROGEN CARBON_DIOXIDE HYDROGEN_SULFIDE /s = Stream.Stream_Material() /s.In.T = 20 /s.In.P = 101 /s.In.MoleFlow = 10 /s.In.Fraction = 1 2 3 4 /s.In /sep = Flash.SimpleFlash() /sep.In -> /s.Out copy / paste / /RootClone -> $thermo2 /RootClone.s.In /RootClone -> $thermo3 /RootClone.s.In /RootClone -> $thermo1 /RootClone.s.In /RootClone -> $thermo5 /RootClone.s.In /RootClone.s.In.Fraction = 1 2 3 /RootClone.s.In /RootClone -> $thermo4 /RootClone.s.In /RootClone -> $thermo2 /RootClone.s.In /RootClone.s.In.Fraction = 1 2 3 4 /RootClone.s.In /RootClone -> /RootClone.s.In /RootClone -> $thermo2 /RootClone.s.In copy /s /sep paste /RootClone /RootClone.sClone.In copy / paste /RootClone /RootClone.RootClone.s.In /RootClone.RootClone.RootClone.s.In
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/Playground Long Strafes Invincible Thin.sce
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Playground Long Strafes Invincible Thin.sce
Name=Playground Long Strafes Invincible Thin PlayerCharacters=Quaker BotCharacters=Quaker Bot Long Strafes.bot IsChallenge=true Timelimit=60.0 PlayerProfile=Quaker AddedBots=Quaker Bot Long Strafes.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=2 BotTeams=1 MapName=playgroundmap4.map MapScale=4.55 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=3.0 ScorePerKill=0.0 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=Reflex, Quake WeaponHeroTag=LG, Lightning Gun DifficultyTag=2 AuthorsTag=aestheticgoose BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Low pressure hitscan tracking against an easy to hit target. medium distance tracking. GameVersion=1.0.7.2 ScorePerDistance=0.0 [Aim Profile] Name=At Feet 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=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Low Skill At Feet MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=-200.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Low Skill MinReactionTime=0.35 MaxReactionTime=0.45 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=20.0 TrackSpeed=3.0 TrackError=5.0 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=60.0 ShootFOV=25.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 [Bot Profile] Name=Quaker Bot Long Strafes DodgeProfileNames=Long Strafes DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;2.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=At Feet;Low Skill At Feet;Low Skill;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=false CharacterProfile=quaker player SeeThroughWalls=false NoDodging=false NoAiming=false [Character Profile] Name=Quaker MaxHealth=300.0 WeaponProfileNames=;;LG;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=true BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=58.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 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=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 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=2048.0 VerticalSpawnOffset=0.0 [Character Profile] Name=quaker player MaxHealth=300.0 WeaponProfileNames=;;LG;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=2.0 CameraOffset=X=0.000 Y=0.000 Z=80.000 HeadshotOnly=false DamageKnockbackFactor=4.0 MovementType=Base MaxSpeed=1300.0 MaxCrouchSpeed=500.0 Acceleration=9000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=3.0 AirControl=0.25 CanCrouch=true CanPogoJump=false CanCrouchInAir=true CanJumpFromCrouch=false EnemyBodyColor=X=0.771 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=1.000 Z=1.000 TeamBodyColor=X=1.000 Y=0.888 Z=0.000 TeamHeadColor=X=1.000 Y=1.000 Z=1.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=true BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=0.0 MainBBType=Cylindrical MainBBHeight=320.0 MainBBRadius=29.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=29.0 ProjBBHasHead=false ProjBBHeadRadius=45.0 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=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.5 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=2048.0 VerticalSpawnOffset=0.0 [Dodge Profile] Name=Long Strafes MaxTargetDistance=2500.0 MinTargetDistance=750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.5 MaxLRTimeChange=1.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=50.0 DamageReactionResetTimer=0.5 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=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Weapon Profile] Name=LG Type=Hitscan ShotsPerClick=1 DamagePerShot=6.0 KnockbackFactor=2.0 TimeBetweenShots=0.046 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=false HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=7.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.05 WallParticleEffect=None HitParticleEffect=None 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AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=70.0 ADSFOVScale=Quake/Source ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=0.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 SpreadMSA=1.0,1.0,-1.0,0.0 SpreadMCA=1.0,1.0,-1.0,0.0 SpreadSSH=1.0,1.0,-1.0,0.0 SpreadSCH=1.0,1.0,-1.0,0.0 SpreadMSH=1.0,1.0,-1.0,0.0 SpreadMCH=1.0,1.0,-1.0,0.0 MaxRecoilUp=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=0.05 AAMaxSpeed=1.0 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=false TriggerBotDelay=0.0 TriggerBotFOV=1.0 StickyLock=false HeadLock=false VerticalOffset=0.0 DisableLockOnKill=false UsePerShotRecoil=false PSRLoopStartIndex=0 PSRViewRecoilTracking=0.45 PSRCapUp=9.0 PSRCapRight=4.0 PSRCapLeft=4.0 PSRTimeToPeak=0.095 PSRResetDegreesPerSec=40.0 UsePerBulletSpread=false PBS0=0.0,0.0 [Map Data] reflex map version 8 global entity type WorldSpawn brush vertices 64.000000 -16.000000 64.000000 64.000000 -16.000000 -64.000000 64.000000 16.000000 -64.000000 64.000000 16.000000 64.000000 -64.000000 16.000000 -64.000000 -64.000000 -16.000000 -64.000000 -64.000000 -16.000000 64.000000 -64.000000 16.000000 64.000000 faces 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//Example 7.23 // SRL Design for an Inverted Pendulum xdel(winsid())//close all graphics Windows clear; clc; //------------------------------------------------------------------ //Transfer function model of Inverted Pendulum. s=poly(0,'s'); nums=-(s+2); dens=(s^2-1) num_s=-(-s+2); den_s=((-s)^2-1) G0s=syslin('c',nums/dens); //G0(s) G0_s=syslin('c',num_s/den_s); //G0(-s) sysGG=G0s*G0_s; evans(sysGG) title('Symmetric root locus for Inverted Pendulum') zoom_rect([-3 -2 3 2]) f=gca(); f.x_location = "origin" f.y_location = "origin" xset("color",2); h=legend(''); h.visible = "off" //Title, labels and grid to the figure exec .\fig_settings.sci; // custom script for setting figure properties title('Symmetric root locus for the inverted pendulum','fontsize',3); //------------------------------------------------------------------ //Root locus design //choose rho=1 that places pole at -1.36+-j0.606 rho=1; p=[-1.36+0.606*%i, -1.36-0.606*%i]; sig=real(p); omega=imag(p); plot(sig,omega,'ro') xstring(-1.25,0.5,["pole locations at";"$\rho=1$"]) //------------------------------------------------------------------ //pole-placement design; Ac=[0 1;1 0];Bc=[0 -1]'; Cc=[2 1];Dc=0; exec('acker_dk.sci', -1); K=acker_dk(Ac,Bc,p); disp(K,"K=",spec(Ac-Bc*K),"Closed loop eigen values"); //input gain calculation n=sqrt(length(Ac)); A=[Ac Bc;Cc Dc]; N=A\[zeros(1,n) 1]'; Nx=N(1:n); Nu=N(n+1); //feedforward gain (input gain) Ntilde=Nu+K*Nx; //Step respose t=0:0.1:4.5; syscl=syslin('c',(Ac-Bc*K),Bc*Ntilde, Cc, Dc) [y x]=csim('step',t,syscl); //closed loop response figure, plot(t,y); //Title, labels and grid to the figure exec .\fig_settings.sci; // custom script for setting figure properties title('Step response for inverted pendulum','fontsize',3); xlabel('Time t (sec.)','fontsize',2); ylabel(["Position","$x_1$"],'fontsize',2); //------------------------------------------------------------------
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//Chapter-1, Example 1.55, Page 62 //============================================================================= clc; clear; //INPUT DATA RAB=1;//Resistance in ohms RBE=2;//resistance in ohms RED=3;//resistance in ohms REF=3;//resistance in ohms RDF=3;//resistance in ohms RAD=2;//resistance in ohms RAC=1;//resistance in ohms RBC=1;//resistance in ohms RFC=2;//resistance in ohms //CALCULATIONS //Delta DEF is converted into equivalent star where RDN=REN=RFN=1 ohm //series branches of inner star network are added //Star ABCN is converted to equivalent delta RDN=1; REN=RDN; RFN=REN; RAN=RAD+RDN;RBN=RBE+REN;RCN=RFC+RFN RAB1=((RAN*RBN)+(RBN*RCN)+(RCN*RAN))/(RCN);//by using star to delta conversion technique RBC1=((RAN*RBN)+(RBN*RCN)+(RCN*RAN))/(RAN);//by using star to delta conversion technique RCA1=((RAN*RBN)+(RBN*RCN)+(RCN*RAN))/(RBN);//by using star to delta conversion technique //parallel resistances in each branch are converted to single resistance RAB2=(RAB*RAB1)/(RAB+RAB1); RAB=RAB2;//equivalent resistance of RAB in ohms RBC2=(RBC*RBC1)/(RBC+RBC1); RBC=RBC2;//equivalent resistance of RBC in ohms RCA2=(RAC*RCA1)/(RAC+RCA1); RCA3=((RCA2)*(RAB+RBC))/(RBC+RAB+RCA2); RCA=RCA3; //OUTPUT mprintf("Thus equivalent resistance of CA is %1.1f ohms",RCA); //TO FIND EQUIVALENT RESISTANCE BETWEEN DF //=================================================================================== //node A is eliminated using star to delta conversion RBC=(RAB*RAD)+(RAD*RAC)+(RAC*RAB)/(RAD);//by using star to delta conversion technique RCD=(RAB*RAD)+(RAD*RAC)+(RAC*RAB)/(RAB);//by using star to delta conversion technique //node C is eliminated using star to delta conversion RDB=(0.72*5)+(5*2)+(2*0.72)/2; RBF1=(0.72*5)+(5*2)+(2*0.72)/5; RFD=(0.72*5)+(5*2)+(2*0.72)/0.72; //parallel branches between nodes B and D and nodes D and F are reduced as RBD=(RDB*5)/(RDB+5); RDF=(RFD*3)/(RFD+3); //node E is eliminated using star to delta conversion technique RBF=((2*3)+(3*3)+(3*2))/3; RFD=((2*3)+(3*3)+(3*2))/2; RDB=((2*3)+(3*3)+(3*2))/3; RDF1=4.2;//(R'=RDB+RDF) RDF=((RDF1)*(RDF1/2))/(RDF1+(RDF1/2)); //OUTPUT mprintf("\n Thus equivalent resistance of DF is %1.1f ohms",RDF); //=================================END OF PROGRAM==============================
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// problem 2.15 w=450000 y=5.5 w1=80*1000000 q=3 gm=(w*y)/(w1*tand(q)) p=12.5*1000 n=120 T=(p*60000)/(2*3.142*n) z=T/(w1*gm) theta=atand(z) disp(theta,"angle of heel in degree")
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//finding no. of bits// //example 20// clc //clears the command window//; clear //clears// E=10;//change in input voltage// R=10^-3;//resolution// n=log(E/R+1)/log(2);//no of bits// n=n+1; n=round(n) disp('no of bits:') disp(n);//result displayed//
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clc; close(); clear(); //page no 554 //prob no. 17.5 theta_3dB=.3; // minimum practical beamwidth in degree eta_1=.6; //illumination efficiency G=eta_1*48000/(theta_3dB)^2; //gain calculation mprintf('The Gain is G= %.0f \n',G) G_dB=10*log10(G); //dB gain mprintf('The Gain in dB is G(dB)= %.1f dB \n',G_dB)
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(set-strategy depth) (unwatch all) ; misclns3.bat test (clear) (open "misclns3.rsl" misclns3 "w") (dribble-on "misclns3.out") (batch "misclns3.bat") (dribble-off) (load "compline.clp") (printout misclns3 "misclns3.bat differences are as follows:" crlf) (compare-files misclns3.exp misclns3.out misclns3) ; close result file (close misclns3)
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function ok=test_mulprobln(n,verbose) if ~exists("n","local") then n=4 end if ~exists("verbose","local") then verbose=%F end ok=%F; p=[0.3;0.7]; for x1=0:n for x2=0:n x=[x1;x2]; c=gamma(x1+x2+1)/(gamma(x1+1)*gamma(x2+1)); ans1=mulprobln(x,p); ans2=log(c*p(1)^x1*p(2)^x2); if verbose printf("x=[%d,%d] ans1=%f, ans2=%f\n",x(1),x(2),ans1,ans2); end assert_checkalmostequal(ans1,ans2,0,sqrt(%eps)); end end p=[0.1;0.5;0.4]; for x1=0:n for x2=0:n for x3=0:n x=[x1;x2;x3]; c=gamma(x1+x2+x3+1)/(gamma(x1+1)*gamma(x2+1)*gamma(x3+1)); ans1=mulprobln(x,p); ans2=log(c*p(1)^x1*p(2)^x2*p(3)^x3); if verbose printf("x=[%d,%d,%d] ans1=%f, ans2=%f\n",x(1),x(2),x(3),ans1,ans2); end assert_checkalmostequal(ans1,ans2,0,sqrt(%eps)); end end end ok=%T; endfunction
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clc; pathname=get_absolute_file_path('5_7_soln.sce') filename=pathname+filesep()+'5_7_data.sci' exec(filename) // Solutions: // Area of piston, A=(%pi/4)*((d/1000)^2); //m^2 // offset angle, theta=(theta*%pi)/180; //rad // Theoretical flow rate, Qt=(D/1000)*A*N*Y*tan(theta); //m^3/min // Actual flow rate, Qa=Qt*(eta_v/100); //m^3/min // rounding off the above answer Qa=fix(Qa)+(fix(round((Qa-fix(Qa))*1000))/1000); //m^3/min // Actual flow rate in L/s, Qa=Qa/(60*0.001); //L/s // Results: printf("\n Results: ") printf("\n The flow rate of axial piston pump in L/s is %.3f L/s.",Qa)
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clc //calc gauge pressure of cylinder in a manometer //height of water above pt.C = 2.5ft rho_water=62.3;//lbm/ft^3; h1=2.5;//ft rho_gas=0.1;//lbm/ft^3 h2=0.5;//ft (height of gas) g=32.2;//ft/s^2 gauge_pressure=[(rho_water)*g*h1+(rho_gas)*g*h2]/144/32.2;//lbf/in^2 disp("Gauge pressure is") disp(gauge_pressure) disp("lbf/in^2")
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alpha20=0.00403; //Assigning values to the parameters t1=20; t2=60; R20=28.3; R60=R20*(1+alpha20*(t2-t1)); // Calculating value of resistance at 60 deg C disp(R60,"Resistance at 60 deg C is");
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clc // Given that m_0 = 9.1e-31 // mass of electron in kg c = 3e8 // speed of light in m/sec KE = 1.5e6 // kinetic energy in eV // Sample Problem 31 on page no. 56 printf("\n # PROBLEM 31 # \n") printf(" Standard formula used \n") printf("\n E = m*c^2 \n") m = m_0+ KE*1.6e-19/c^2 // mass of moving electron in kg v = c * sqrt(1-(m_0/m)^2) // velocity of moving electron in m/sec printf("\n Mass of moving electron is %e kg \n Velocity of moving electron is %e m/sec. ",m,v)
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//Eg-6.3 //pg-284 clear clc //Theoretical Problem disp("given example is Theoretical")
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ruga-kutta.sci
clc clear function ydot=f(x,y) ydot=x+y^2 endfunction x1=0; y1=1; h=input("enter step size h:") x(1)=x1; y(1)=y1; for i=1:2 k1=h*f(x(i),y(i)); k2=h*f(x(i)+0.5*h,y(i)+0.5*k1); k3=h*f((x(i)+0.5*h),(y(i)+0.5*k2)); k4=h*f((x(i)+h),(y(i)+k3)); k=(1/6)*(k1+2*k2+2*k3+k4); y(i+1)=x(i)+k; printf('\n the value of y at x=%f is %f',i*h,y(i+1)) x(i+1)=x(1)+i*h; end
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/1808/CH5/EX5.17/Chapter5_Exampl17.sce
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Chapter5_Exampl17.sce
clc clear //INPUT DATA p1=0.98;//suction pressure in bar p3=18;//delivery pressure in bar t1=293;//free conduction temperature in K t5=303;//suction temperature in K pa=1;//ambient temperature in bar n=1.3;//index of expansion ta=293;//ambient temperature in K N=150;//speed in rpm c=0.06;//clearence volume v1=5;//volume in m^3 R=0.287;//gas constant //CALCULATIONS m=p1*10^2*v1/(R*t1);//mass of air handled/min p2=(p1*p3)^(1/2);//pressure in bar ip=N*(n/(n-1))*(m/60)*R*t1*(((p3/p1)^((n-1)/(n*N)))-1);//indicated power in kW nv=1+c-(c*((p2/p1)^(1/n)));//volumetric efficiency in percentage va=4.5*1*t1/(p1*t5);//colume of air in m^2/min vs=va/nv;//swept volume in m^2/min d=(vs*4/(3.14*N))^(1/3)*100;//dimensions im cm //OUTPUT printf('(i)Indicated power is %3.3f kW \n (ii)The dimensions of the LP cylinder (d=l)%3.2f cm',ip,d)
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/3446/CH10/EX10.3/Ex10_3.sce
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Ex10_3.sce
// Exa 10.3 // To calculate gain of antenna. clc; clear all; Pin=12; //Input power in watts Ploss=3; //resistive losses in Watts D=5; //Directivity //solution Eff=(Pin-Ploss)/Pin; G=Eff*D; printf('Gain of the antenna is %.2f dB = %.2f \n',10*log10(G),G);
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/2195/CH2/EX2.3.4/ex_2_3_4.sce
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ex_2_3_4.sce
//Example 2.3.4: sensitivity and deflection error clc; clear; close; //given data : C=4;// change in output in mm M=8;// magnitude of input in ohm S=C/M; disp(S,"sensitivity,S(mm/ohm) = ") D=M/C; disp(D,"deflection factor,D(ohm/mm) = ")