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function [out,out1,out2]=basic_elt_test(varargin); // ELEMENT TESTS // //// eig, load, mat for all elements => comparisons with SDT5.1 // basic_elt_test('compare') // //// test of basic commands (integinfo, call, etc.) for all elements // basic_elt_test('integinfo') // //// testmat for all elements, //// the optional output argument is a cell array containing basic matrices // out = basic_elt_test('mat') // //// testeig for all elements, //// the optional output argument is a cell array containing frequencies // out = basic_elt_test('eig') // //// testload for all elements, //// the optional output argument is a cell array containing RHS norms // out = basic_elt_test('load') // //// test mat,eig,surf,... for element //// st=q4p,t3p,... //// st1=mat,eig,sur,vol // basic_elt_test(st,st1) or basic_elt_test (all the tests) // // example // basic_elt_test('penta15','mat') // check anisotropic material for 2D // Etienne Balmes, J.M. Leclere // Copyright (c) 2001-2003 by INRIA and SDTools,All Rights Reserved. // Use under OpenFEM trademark.html license and LGPL.txt library license // $Revision: 1.7 $ $Date: 2004/07/28 07:19:10 $ global withoutplot [nargout,nargin] = argn(0); carg=1; out = []; out1 = []; out2 = []; //----------------------------------------------------------------------- // To do the matrix, rhs, stress test for a specified element if carg<=nargin-1 st=varargin(carg); st1=varargin(carg+1);carg=carg+2; else // list of elements to check //st=makecell([1 1],'tria6'); st=makecell([1 20],'q4p','q8p','t3p','t6p',... 'hexa8','hexa20','penta6','penta15',... 'tetra4','tetra10','tria3','tria6',... 'quad4','quadb','quad9','bar1','flui4',... 'flui6','flui8','beam1'); // missing: mitc4, , beam3, , celas , q5p, q9a ,'dktp', if carg<=nargin; st1=varargin(carg);carg=carg+1; else; st1=''; end end //----------------------------------------------------------------------- // testmat for all elements if isempty(st1)|comstr(st1,'mat') st1='testmat'; ierr2 = execstr('host(''rm basic_elt_test.txt'');','errcatch'); filename = 'basic_elt_test.txt'; [fd,err] = mopen(filename,'a'); out=cell(); for j1=1:prod(size(st)) st3=['k='+st(j1).entries+'('''+st1+''');']; ierr = zeros(1,3); if any(strcmp(st(j1).entries,makecell([1 6],'q4p','q5p','q8p','t3p','t6p','q9a'))) st3=['k='+st(j1).entries+'('''+st1+'_0'+''');']; ierr(1) = execstr(st3,'errcatch'); if ierr(1)==0; out(size(out,1)+1,1:2)=makecell([1 2],st3,k); end st3=['k='+st(j1).entries+'('''+st1+'_1'+''');']; ierr(2) = execstr(st3,'errcatch'); if ierr(2)==0; out(size(out,1)+1,1:2)=makecell([1 2],st3,k); end st3=['k='+st(j1).entries+'('''+st1+'_2'+''');']; ierr(3) = execstr(st3,'errcatch'); if ierr(3)==0; out(size(out,1)+1,1:2)=makecell([1 2],st3,k); end else ierr(1) = execstr(st3,'errcatch'); if ierr(1)==0; out(size(out,1)+1,1:2)=makecell([1 2],st3,k); ierr = zeros(1,3); end end if any(ierr) disp(lasterror()); fprintf(fd,'------------------------------- error in %s %s\n',st(j1).entries,st1) out(size(out,1)+1,1:3)=makecell([1 3],st3,'error',lasterror()); elseif iscell(k) if isempty(find(isfinite(k(1).entries))) | isempty(find(k(1).entries)) error('Infinite or zeros matrix'); end end end //j1 mclose(fd); // diary off return; //----------------------------------------------------------------------- // testeig for all elements elseif comstr(st1,'eig') withoutplot = 1; st1='testeigstress'; ierr2 = execstr('host(''rm basic_elt_test.txt'');','errcatch'); filename = 'basic_elt_test.txt'; [fd,err] = mopen(filename,'a'); out=cell(); for j1=1:prod(size(st)) st3=['[model,def]='+st(j1).entries+'('''+st1+''');']; ierr = zeros(1,3); if any(strcmp(st(j1).entries,makecell([1 6],'q4p','q5p','q8p','t3p','t6p','q9a'))) st3=['[model,def]='+st(j1).entries+'('''+st1+'_0'+''');']; ierr(1) = execstr(st3,'errcatch'); if ierr(1)==0; out(size(out,1)+1,1:3)=makecell([1 3],st3,def,def.data(1:5)); end st3=['[model,def]='+st(j1).entries+'('''+st1+'_1'+''');']; ierr(2) = execstr(st3,'errcatch'); if ierr(2)==0; out(size(out,1)+1,1:3)=makecell([1 3],st3,def,def.data(1:5)); end st3=['[model,def]='+st(j1).entries+'('''+st1+'_2'+''');']; ierr(3) = execstr(st3,'errcatch'); if ierr(3)==0; out(size(out,1)+1,1:3)=makecell([1 3],st3,def,def.data(1:5)); end else ierr(1) = execstr(st3,'errcatch'); if ierr(1)==0 & isfield(def,'def') out(size(out,1)+1,1:3)=makecell([1 3],st3,def,def.data(1:5)); else out(size(out,1)+1,1:3)=makecell([1 3],st3,'error',lasterror()); ierr = zeros(1,3); end end if any(ierr) disp(lasterror()); fprintf('------------------------------- error in %s %s\n',st(j1).entries,st3); out(size(out,1)+1,1:3)=makecell([1 3],st3,'error',lasterror()); end end //j1 mclose(fd); withoutplot = 0; // diary off return; //----------------------------------------------------------------------- // testload for all elements elseif comstr(st1,'load') withoutplot = 1; st1='testload'; ierr2 = execstr('host(''rm basic_elt_test.txt'');','errcatch'); filename = 'basic_elt_test.txt'; [fd,err] = mopen(filename,'a'); out=cell(); for j1=1:prod(size(st)) st3=['[model,def]='+st(j1).entries+'('''+st1+''');']; ierr = zeros(1,3); if any(strcmp(st(j1).entries,makecell([1 6],'q4p','q5p','q8p','t3p','t6p','q9a'))) st3=['[model,def]='+st(j1).entries+'('''+st1+'_0'+''');']; ierr(1) = execstr(st3,'errcatch'); if ierr(1)==0; out(size(out,1)+1,1:3)=makecell([1 3],st3,def,norm(full(def.def),2)); end st3=['[model,def]='+st(j1).entries+'('''+st1+'_1'+''');']; ierr(2) = execstr(st3,'errcatch'); if ierr(2)==0; out(size(out,1)+1,1:3)=makecell([1 3],st3,def,norm(full(def.def),2)); end st3=['[model,def]='+st(j1).entries+'('''+st1+'_2'+''');']; ierr(3) = execstr(st3,'errcatch'); if ierr(3)==0; out(size(out,1)+1,1:3)=makecell([1 3],st3,def,norm(full(def.def),2)); end else ierr2 = execstr(st3,'errcatch'); if ierr(1)==0 & isfield(def,'def') out(size(out,1)+1,1:3)=makecell([1 3],st3,def,norm(full(def.def),2)); elseif ierr(1)~=0 out(size(out,1)+1,1:3)=makecell([1 3],st3,'error',lasterror()); ierr = zeros(1,3); else out(size(out,1)+1,1:3)=makecell([1 3],st3,'error','attempt to reference field of non-structure array ''def''.'); ierr = zeros(1,3); end end if any(ierr) disp(lasterror()); fprintf(fd,'------------------------------- error in %s %s\n',st(j1).entries,st1) out(size(out,1)+1,1:3)=makecell([1 3],st3,'error',lasterror()); end end //j1 mclose(fd); withoutplot = 0; //diary off return; //----------------------------------------------------------------------- // elseif comstr(st1,'compare') withoutplot = 1; st0=st; filename = 'basic_elt_test.txt'; [fd,err] = mopen(filename,'a'); [Eig_ref,Load_ref,Mat_ref] = ref_elt_test(); [st0,i1]=%ce_intersect_ce(st,st0); // - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Matrices Mat = basic_elt_test('mat'); result_Mat=Mat; for j1=1:size(Mat,1) i1=find(strcmp(Mat_ref,Mat(j1,1).entries)); if ~isempty(i1) if ~isstr(Mat_ref(i1,2).entries) & ~isstr(Mat(j1,2).entries) & iscell(Mat(j1,2).entries) result_Mat(j1,2).entries=[(Mat_ref(i1,2).entries(1)-max(svd(Mat(j1,2).entries(1).entries)))/Mat_ref(i1,2).entries(1) (Mat_ref(i1,2).entries(2)-max(svd(Mat(j1,2).entries(2).entries)))/Mat_ref(i1,2).entries(1) ]; else result_Mat(j1,2).entries='error'; end else result_Mat(j1,2).entries='not compared'; end end // j1 // - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - EIG Eig = basic_elt_test('eig');result_Eig=Eig; for j1=1:size(Eig,1) i1=find(strcmp(Eig_ref,Eig(j1,1).entries)); if ~isempty(i1) if ~isstr(Eig_ref(j1,2).entries) & ~isstr(Eig(j1,2).entries) result_Eig(j1,2).entries=Eig_ref(i1,2).entries(:)'-Eig(i1,3).entries(:)'; else result_Eig(j1,2).entries='error'; end else result_Eig(j1,2).entries='not compared'; end end // j1 // - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - LOAD Load = basic_elt_test('load');result_Load=Load; for j1=1:size(Load,1) i1=find(strcmp(Load_ref,Load(j1,1).entries)); if ~isempty(i1) if ~isstr(Load_ref(j1,2).entries) & ~isstr(Load(j1,2).entries) result_Load(j1,2).entries=Load_ref(i1,2).entries-Load(i1,3).entries; else result_Load(j1,2).entries='error'; end else result_Load(j1,2).entries='not compared'; end end // j1 out=makecell([1 3],result_Mat,result_Eig,result_Load); // - - - - - - - - - - - - - - - - - - - - - - - - - - - Comparisons output for j1=1:size(out(1).entries,1) // Mat if ~isstr(out(1).entries(j1,2).entries) & ~isempty(find(out(1).entries(j1,2).entries>sdtdef('epsl'))) fprintf(fd,'%s : ',out(1).entries(j1,1).entries); fprintf(fd,'%f ',out(1).entries(j1,2).entries); fprintf(fd,'\n'); elseif ~isstr(out(1).entries(j1,2).entries) & isempty(find(out(1).entries(j1,2).entries>sdtdef('epsl'))) fprintf(fd,'%s : comparison OK\n',out(1).entries(j1,1).entries); else fprintf(fd,'%s : error\n',out(1).entries(j1,1).entries); end end for j1=1:size(out(2).entries,1) // Eig if ~isstr(out(2).entries(j1,2).entries) & ~isempty(find(out(2).entries(j1,2).entries>sdtdef('epsl'))) fprintf(fd,'%s : ',out(2).entries(j1,1).entries); fprintf(fd,'%f ',out(2).entries(j1,2).entries); fprintf(fd,'\n'); elseif ~isstr(out(2).entries(j1,2).entries) & isempty(find(out(2).entries(j1,2).entries>sdtdef('epsl'))) fprintf(fd,'%s : comparison OK\n',out(2).entries(j1,1).entries); else fprintf(fd,'%s : error\n',out(2).entries(j1,1).entries); end end for j1=1:size(out(3).entries,1) // Load if ~isstr(out(3).entries(j1,2).entries) & ~isempty(find(out(3).entries(j1,2).entries>sdtdef('epsl'))) fprintf(fd,'%s : ',out(3).entries(j1,1).entries); fprintf(fd,'%f ',out(3).entries(j1,2).entries); fprintf(fd,'\n'); elseif ~isstr(out(3).entries(j1,2).entries) & isempty(find(out(3).entries(j1,2).entries>sdtdef('epsl'))) fprintf(fd,'%s : comparison OK\n',out(3).entries(j1,1).entries); else fprintf(fd,'%s : error\n',out(3).entries(j1,1).entries); end end withoutplot = 0; return; //----------------------------------------------------------------------- // test each basic command of elements elseif comstr(st1,'integinfo') st1=makecell([1 8],'call','rhscall','node','patch',... 'dof','line','face','parent'); ierr2 = execstr('host(''rm basic_elt_test.txt'');','errcatch'); filename = 'basic_elt_test.txt'; [fd,err] = mopen(filename,'a'); for j1=1:length(st) for j2=1:length(st1) st3=['r1='+st(j1).entries+'('''+st1(j2).entries+''');']; ierr = 0; ierr = execstr(st3,'errcatch'); if ierr==0 & isempty(r1); error('Empty return'); end if ierr~=0 disp(lasterror()); fprintf('------------------------------- error in %s\n',st3) end end //j2 end //j1 // test 'integinfo' (based on femesh test elt call) st1='integinfo'; for j1=1:length(st) st3=['i1='+st(j1).entries+'('''+st1+''',[100;110],model.pl,model.il);']; st4=['model=femesh(''test'+st(j1).entries+''');' ]; ierr = zeros(1,2); ierr(1) = execstr(st4,'errcatch'); ierr(2) = execstr(st3,'errcatch'); if ~any(ierr) & isempty(find(i1)); error('Empty constit'); end if any(ierr) disp(lasterror()); fprintf('------------------------------- error in %s\n',st3) end end //j1 mclose(fd); //diary off return; //----------------------------------------------------------------------- // no input argument => test all elseif nargin==0 st1=makecell([1 4],'mat','eig','loadStressMises','load'); ierr2 = execstr('host(''rm basic_elt_test.txt'');','errcatch'); filename = 'basic_elt_test.txt'; [fd,err] = mopen(filename,'a'); for j1=1:length(st) for j2=1:length(st1) basic_elt_test(st(j1).entries,st1(j2).entries); end //j2 end //j1 mclose(fd); // diary off return; else error('Not a valid test') end //----------------------------------------------------------------------- // Actually do the test for one specified element filename = 'basic_elt_test.txt'; [fd,err] = mopen(filename,'a'); st2=sprintf('%s test%s;',st,st1); ierr = execstr(st2,'errcatch'); if ierr~=0 disp(lasterror()); fprintf(fd,' ------------------ error in %s test\n%s\n', st2) end if any(strcmp(st,makecell([1 6],'q4p','q5p','q8p','t3p','t6p','q9a'))) st2=sprintf('%s test%s_0;',st,st1); ierr = execstr(st2,'errcatch'); if ierr~=0 disp(lasterror()); fprintf(fd,' ------------------ error in %s test\n%s\n',st2) end st2=sprintf('%s test%s_1;',st,st1); ierr = execstr(st2,'errcatch'); if ierr~=0 disp(lasterror()); fprintf(fd,' ------------------ error in %s test\n%s\n',st2) end st2=sprintf('%s test%s_2;',st,st1); ierr = execstr(st2,'errcatch'); if ierr~=0 disp(lasterror()); fprintf(fd,' ------------------ error in %s test\n%s\n',st2) end // test anisotropic material // plane stress E=2.1e11;nu=.285;C=E/(1.-nu*nu); e=[C C*nu C 0. 0. C*(1-nu)/2]; pl=[100 fe_mat('m_elastic','SI',4) e 7800 0 0 0 0 .1]; st2=sprintf('k=%s (''test%s_0'');',st,st1) execstr(st2); st2=sprintf('k1=%s (''test%s_0'',pl);',st,st1) execstr(st2); if iscell(k1) if norm(k(1).entries-k1(1).entries); error(['anisotropic element '+st2]); end end // plane strain unmnu=1.-nu; C=E*unmnu/(1+nu)/(1-2*nu); e=[C nu*C/unmnu C 0. 0. C*(1-2*nu)/(2*unmnu)]; pl=[100 fe_mat('m_elastic','SI',4) e 7800 0 0 0 0 .1]; st2=sprintf('k=%s (''test%s_1'');',st,st1); execstr(st2,'errcatch'); st2=sprintf('k1=%s (''test%s_1'',pl);',st,st1); execstr(st2); if iscell(k1) if norm(k(1).entries-k1(1).entries); error(['anisotropic element '+st2]); end end end mclose(fd); return; //----------------------------------------------------------------------- if 1==2 // anisotropic model=femesh('testq4p'); model.il(3)=0; E=2.1e11;nu=.285;C=E/(1.-nu*nu); e=[C C*nu C 0. 0. C*(1-nu)/2]; model.pl=[100 fe_mat('m_elastic','SI',4) e 7800 0 0 0 0 .1]; [constit,iopt,elmap]=q4p('integinfo',[100;110],model.pl,model.il); [k,m]=q4p(model.Node,model.Elt(2,:),[36 36 0 0 0 0 0 0 0],int32(iopt),constit,elmap); unmnu=1.-nu; C=E*unmnu/(1+nu)/(1-2*nu); e=[C nu*C/unmnu C 0. 0. C*(1-2*nu)/(2*unmnu)]; pl=[100 fe_mat('m_elastic','SI',4) e 7800 0 0 0 0 .1]; end //--------------------------------------------------------- RHS if 1==2 // st={'q4p','q5p','q8p','t3p','t6p',... // 'hexa8','hexa20','penta6',... // 'tetra4','tetra10'}; // st={'quad4','tria3','quadb'}; //st={'bar1','beam1'}; //st={'flui4','flui6','flui8'}; st=makecell([1 5],'q4p','q5p','q8p','t3p','t6p'); errors=cell(); for j2=1:4 for j1=1:length(st) st1=['[model,def1]=femesh(''teststruct'+st(j1).entries+'load'');' ]; st2=['[model,def2]=femesh(''teststruct'+st(j1).entries+'load'');' ]; st3=['[model,def3]=femesh(''teststruct'+st(j1).entries+'load'');' ]; execstr(st1);execstr(st2);execstr(st3); if ~isequal(def1.def,def2.def) | ~isequal(def1.def,def3.def) errors(size(errors,1)+1,1).entries=st1; if ~isequal(def1.def(:,1:2),def2.def(:,1:2)) |... ~isequal(def1.def(:,1:2),def3.def(:,1:2)) errors(size(errors,1),2).entries='gravity and/or surf'; else errors(size(errors,1),2)='pressure only'; end end end //j1 end //j2 end //------------------------------------------ compare basic matrices if 1==2 out=basic_elt_test('mat') loadmatfile 'basic_elt_test_matrices' result=out; for j1=1:size(out,1) i1=find(strcmp(k,out(j1,1).entries)); if ~isempty(i1) if ~isstr(out(j1,2).entries); result(j1,2).entries=norm(out(j1,2).entries(1).entries-k(i1,2).entries(1).entries); result(j1,3).entries=norm(out(j1,2).entries(2).entries-k(i1,2).entries(2).entries); else result(j1,2).entries='error'; result(j1,3).entries='error'; end else result(j1,2).entries='not compared'; end end end //--------------------------------------------------------- RHS if 1==2 out=basic_elt_test('load') loadmatfile 'basic_elt_test_load' result=out; for j1=1:size(out,1) i1=find(strcmp(k,out(j1,1).entries)); if ~isempty(i1) if ~isstr(out(j1,2).entries); result(j1,2).entries=norm(out(j1,3).entries-k(i1,3).entries); else result(j1,2).entries='error'; end else result(j1,2).entries='not compared'; end end end //--------------------------------------------------------- EIG if 1==2 out=basic_elt_test('eig') loadmatfile basic_elt_test_load result=out; for j1=1:size(out,1) i1=find(strcmp(k,out(j1,1).entries)); if ~isempty(i1) if ~isstr(out(j1,2).entries); result(j1,2).entries=norm(out(j1,3).entries-k(i1,3).entries); else result(j1,2).entries='error'; end else result(j1,2).entries='not compared'; end end end //---------------------------------------------------------
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// calculating Relative error (expressed as a percentage of f.s.d) clc; disp('calculating Relative error (expressed as a percentage of f.s.d)') Am = 1.46; At=1.50; e=Am-At; disp(e,'Absolute error(V)='); Sc=-e; disp(Sc,'Absolute Correction(V)='); RE=(e/At)*100; disp(RE,'Relative Error in terms of true value(in percentage)='); REF=(e/2.5)*100; disp(REF,'Relative Error in terms of true value(in percentage)=');
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// This file is part of www.nand2tetris.org // and the book "The Elements of Computing Systems" // by Nisan and Schocken, MIT Press. // File name: projects/03/a/RAM64.tst load RAM64.hdl, output-file RAM64alt.out, compare-to RAM64alt.cmp, output-list time%S1.4.1 in%D1.6.1 load%B2.1.2 address%D2.3.2 out%D1.6.1; set in 0, set load 0, set address 0, tick, output; tock, output; set load 1, tick, output; tock, output; set in 1313, set load 0, tick, output; tock, output; set load 1, set address 13, tick, output; tock, output; set load 0, set address 0, tick, output; tock, output; set in 4747, set address 47, tick, output; tock, output; set load 1, tick, output; tock, output; set in 5463, set load 1, tick, output; tock, output; set in 4747, set address 13, set load 1, tick, output; tock, output;
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clc // initialization of variables clear tau_xx= -1 // kgf/cm^2 tau_yy= 0 // kgf/cm^2 tau_xy= 7 // kgf/cm^2 // calculations sigma_1=(tau_xx+tau_yy)/2+sqrt((1/2*(tau_xx-tau_yy))^2+tau_xy^2) sigma_2=(tau_xx+tau_yy)/2-sqrt((1/2*(tau_xx-tau_yy))^2+tau_xy^2) x=sigma_1 // positive one is tension if(sigma_2>sigma_1) x=sigma_2 end // Results printf('The diagonal tension is %.3f kgf/cm^2',x)
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ex13_17.sce
// Exa 13.17 clc; clear; close; // Given data R_A = 20;// in k ohm R_A = R_A * 10^3;// in ohm C = 0.1;// in µF C = C*10^-6;// in F pulse_width = 1.1*R_A*C;// in s disp(pulse_width*10^3,"The output pulse width in ms is");
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example5_53.sce
clear; clc; // Stoichiometry // Chapter 5 // Energy Balances // Example 5.53 // Page 308 printf("Example 5.53, Page 308 \n \n"); // solution F = 1135 Benzenef = 400*.993 HNO3con = Benzenef*63/78 H1 = -186.5 C11 = 1.88 H11 = H1+C11*(298.15-273.15) H2 = -288.9 C12 = 1.96 H22 = H2+C12*(298.15-273.15) H3 = 0 C13 = 1.98 H33 = C13*(298.15-273.15) Hr = -285.83+12.5-(-174.1+49.08) Benzener = Benzenef/78.1118 fi = 903.84*H22+HNO3con*H33-F*H11+Benzener*Hr*1000 // kJ/h printf(" Total heat exchanged = "+string(fi)+" kJ/h.")
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HH_RG_3s.sce
//**************************** HH_RG_3s ********************************** if (blk_name.entries(bl) == "HH_RG_3s") then for ss=1:scs_m.objs(bl).model.ipar(1) mputl("# HH_RG_3s "+string(bl)+" "+string(scs_m.objs(bl).model.ipar(2))+" "+string(ss),fd_w); sci2blif_str= ".subckt HH_RG_3s"+" in[0]=net"+string(blk(blk_objs(bl),2))+"_"+string(ss)+" in[1]=net"+string(blk(blk_objs(bl),3))+"_"+string(ss)+" in[2]=net"+string(blk(blk_objs(bl),4))+"_"+string(ss)+" in[3]=net"+string(blk(blk_objs(bl),5))+"_"+string(ss)+" in[4]=net"+string(blk(blk_objs(bl),6))+"_"+string(ss)+" in[5]=net"+string(blk(blk_objs(bl),7))+"_"+string(ss)+" in[6]=net"+string(blk(blk_objs(bl),8))+"_"+string(ss)+" out[0]=net"+string(blk(blk_objs(bl),2+numofip))+"_"+string(ss)+" out[1]=net"+string(blk(blk_objs(bl),3+numofip))+"_"+string(ss)+" #HH_RG_3s_ls =0"+"&HH_RG_3s_Nafb_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(1-1)+ss)))+"&HH_RG_3s_syn0_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(2-1)+ss)))+"&HH_RG_3s_syn1_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(3-1)+ss)))+"&HH_RG_3s_syn2_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(4-1)+ss)))+"&HH_RG_3s_pfet_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(5-1)+ss)))+"&HH_RG_3s_nmr_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(6-1)+ss)))+"&HH_RG_3s_Na_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(7-1)+ss)))+"&HH_RG_3s_Na_pbias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(8-1)+ss)))+"&HH_RG_3s_Na_nbias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(9-1)+ss)))+"&HH_RG_3s_K_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(10-1)+ss)))+"&HH_RG_3s_K_pbias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(11-1)+ss)))+"&HH_RG_3s_K_nbias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(12-1)+ss)))+"&HH_RG_3s_buf_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(13-1)+ss)))+"&HH_RG_3s_comp_ibias ="+string(sprintf('%e',scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(14-1)+ss))) sci2blif_str=sci2blif_str+"&"; if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(15-1)+ss) == 1 then sci2blif_str=sci2blif_str+"HH_RG_3s_cap0_1x_cs =1"; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(15-1)+ss) == 2 then sci2blif_str=sci2blif_str+"HH_RG_3s_cap0_2x_cs =2"; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(15-1)+ss) == 3 then sci2blif_str=sci2blif_str+"HH_RG_3s_cap0_1x_cs =3&HH_RG_3s_cap0_2x_cs =0"; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(15-1)+ss) == 4 then sci2blif_str=sci2blif_str+"HH_RG_3s_cap0_4x_cs =4"; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(15-1)+ss) == 5 then sci2blif_str=sci2blif_str+"HH_RG_3s_cap0_1x_cs =5&HH_RG_3s_cap0_4x_cs =0"; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(15-1)+ss) == 6 then sci2blif_str=sci2blif_str+"HH_RG_3s_cap0_2x_cs =6&HH_RG_3s_cap0_4x_cs =0"; end if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(15-1)+ss) == 7 then sci2blif_str=sci2blif_str+"HH_RG_3s_cap0_1x_cs =7&HH_RG_3s_cap0_2x_cs =0&HH_RG_3s_cap0_4x_cs =0"; end mputl(sci2blif_str,fd_w); mputl(" ",fd_w); if scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(16-1)+1) == 1 then plcvpr = %t; plcloc=[plcloc;'net'+string(blk(blk_objs(bl),2+numofip))+"_"+string(ss),string(scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(16-1)+1+2*ss-1))+' '+string(scs_m.objs(bl).model.rpar(scs_m.objs(bl).model.ipar(1)*(16-1)+1+2*ss))+' 0']; end end end
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response_matching = simple_matching; begin; begin_pcl;
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clc; clear; close; x1=input('x(n)='); x2=input('h(n)='); L1=length(x1); L2=length(x2); N=max(L1,L2); x1=[x1,zeros(1,N-L1)]; x2=[x2,zeros(1,N-L2)]; //circular convolution in freq domain X1=fft(x1); X2=fft(x2); Y=X1.*X2; y=ifft(Y); disp(y,'Circular Convolution y=') subplot(3,1,1);plot2d3(x1);xtitle('input signal x1','n','x1[n]'); subplot(3,1,2);plot2d3(x2);xtitle('input signal x2','n','x2[n]'); subplot(3,1,3);plot2d3(Y);xtitle('output signal Y','n','Y[n]');
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syms a e; a is semimajor and e is eccentricity [a,e] = solve(a*(1-e)==6375+300,a*(1+e)==6375+10000,a,e); % earth radius = 6375km, hp=300, ha=10000 b=a*sqrt(1-e.^2); %b is semiminor b=double(b); a=double(a); e=double(e); u=0:pi/100:2*pi; %u is true anomaly r=(a*(1-e^2)./(1+e.*cos(u))); %r is radial distance from earth's center figure(1); plot(u,r); %Radial distance evolution over one revolution xlabel('true anomaly(degree)') ylabel('radial distance(km)') title('Radial distance evolution over one revolution')
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clear; //clc(); v=11; ct=0.7; cs=0.4; cc=(ct-cs)/2; printf("\n the capacitance between conductors is: %.2f uF\n ",cc); cl=0.5*(3*cc + cs); ic=(v*2*3.14*50*2*cl*.001)/sqrt(3);..//charging current in ka/phase printf("\n the charging current is: %.3f A\n ",ic);
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// Exa 2.31 clc; clear; close; // given : E_i=1 // magnitude of incident electric field in mV/m E_i=1*10^-3 // magnitude of incident electric field in V/m epsilon_0=8.854*10^-12 // permittivity in free space in F/m mu_0=4*%pi*10^-7 // permeability in free space in H/m theta_i=15 // incident angle in degrees epsilon_r1=8.5 // relative permittivity of medium 1 mu_r1=1 // relative permeability of medium 1 epsilon1=epsilon_r1*epsilon_0 // permittivity mu1=mu_0*mu_r1 // permeability eta1=sqrt(mu1/epsilon1) // intrinsic impedence of medium 1 in ohm epsilon2=epsilon_0 // permittivity of medium 2 mu2=mu_0 // permeability of medium 2 eta2=sqrt(mu2/epsilon2) // intrinsic impedence of medium 2 in ohm //formula : sind(theta_i)/sind(theta_t)=sqrt(epsilon2/epsilon1) theta_t=asind(sind(theta_i)/(sqrt(epsilon2/epsilon1))) // transmitted angle in degrees E_r=E_i*((eta2*cosd(theta_i)-(eta1*cosd(theta_i)))/(eta2*cosd(theta_i)+eta1*cosd(theta_i))) // reflection cofficient of electric field disp(E_r*1000,"reflection cofficient of electric field in mV/m:") H_i=E_i/eta1 // incident cofficient of magnetic field disp(H_i*10^6,"incident cofficient of magnetic field in micro*A/m:") H_r=E_r/eta1 // reflection cofficient of electric field disp(H_r*10^6,"reflection cofficient of magnetic field in micro*A/m:") // note : minute difference in decimal answer between scilab and book.
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//******************************************* // Scilab script for visualisation of the // Coriolis force. // // Use the help facility for more information // on individual functions used. // // Author: J. Kaempf, 2015 (update) //******************************************** clf; scf(0); a=gcf(); a.figure_size= [600,600]; T = 24.*3600.; // period fre = -2*%pi/T; // rotation rate radius = 20; time = 0; dt = T/200; // time step xp = 0; yp = 5; xf = xp; yf = yp; uf = 0.0; // speed in m/s vf = 0.15; // time loop starts here fact = 0.9; fac2 = fact*radius; xpp(1:200)= %nan; ypp(1:200)= %nan; for n = 1:200 // run for 1 period drawlater; clf; // isoview scaling plot2d(0,0,-1,"030"," ",[-20,-20,20,20]) time = time+dt; xx = radius*sin(fre*time); yy = radius*cos(fre*time); x1 = [fact*xx xx]; y1 = [fact*yy yy]; xset("color",5) xset("thickness",6) xpoly(x1,y1,"lines",1) xx = radius*cos(fre*time); yy = -radius*sin(fre*time); x2 = [fact*xx xx]; y2 = [fact*yy yy]; xset("color",0) xset("thickness",6) xpoly(x2,y2,"lines",1) xx = -radius*sin(fre*time); yy = -radius*cos(fre*time); x3 = [fact*xx xx]; y3 = [fact*yy yy]; xset("color",0) xset("thickness",6) xpoly(x3,y3,"lines",1) xx = -radius*cos(fre*time); yy = radius*sin(fre*time); x4 = [fact*xx xx]; y4 = [fact*yy yy]; xset("color",0) xset("thickness",6) xpoly(x4,y4,"lines",1) xset("color",2) xfarc(-fac2,fac2,2*fac2,2*fac2,0,360*64) x1 = [0 0]; y1 = [fact*fac2 fac2]; xset("color",5) xset("thickness",6) xpoly(x1,y1,"lines",1) x1 = [0 0]; y1 = [-fac2 -fact*fac2]; xset("color",0) xset("thickness",6) xpoly(x1,y1,"lines",1) y1 = [0 0]; x1 = [fact*fac2 fac2]; xset("color",0) xset("thickness",6) xpoly(x1,y1,"lines",1) y1 = [0 0]; x1 = [-fac2 -fact*fac2]; xset("color",0) xset("thickness",6) xpoly(x1,y1,"lines",1) //new ball position xf = xf + dt*uf/1000; yf = yf + dt*vf/1000; xp = xf*cos(fre*time)+yf*sin(fre*time); yp = yf*cos(fre*time)-xf*sin(fre*time); xpp(n) = xp; ypp(n) = yp; xset("color",1) xfarc(xp-1,yp+1,2.0,2,0,360*64) xset("color",7) xfarc(xp-0.8,yp+0.8,1.6,1.6,0,360*64) xset('thickness',2) plot2d(xpp,ypp,8,'000','',[-radius,-radius,radius,radius]) title("Rotating Frame of Reference","fontsize",3,"font_style",4); xpause(5d2); // creation of GIF files (optional) //if n < 10 then // xs2gif(0,'ex100'+string(n)+'.gif') //else // if n < 100 then // xs2gif(0,'ex10'+string(n)+'.gif') // else // xs2gif(0,'ex1'+string(n)+'.gif') // end //end drawnow; end;
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//example-12.3 //page no-396 //given //the molecular weight of polyisoprene monomer Mm=68 //gm //after vulcanisation with sulphur, it is observedthat the 2 molecules of isoprene monimer require 2 molecules of sulphur //hence for full cross linking ,(68*2) gm of isoprene requires (32*2)gm of sulphur. therefore 68kg of isoprene requires M=32*2*68/68/2 //kg of sulphur printf ("the weight of sulphur required for cross link polymerization of polyisoprene is %d of sulphur",M) printf ("the fully cross linked product will be EBONITE")
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ex1_19.sce
// Exa 1.19 clc; clear; close; // Given data M = 120; n = 2; N_A = 6.023*10^23; m1 = M/N_A;//mass of 1 atom in gm m2 = n*m1;//mass of unit cell in gm disp(20/m2,"Number of unit cell in 20 gms of element is : ")
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example11_12.sce
//clc() //Cp = 26.586 + 7.582 * 10 ^-3 * T - 1.12 * 10^-6 * T^2 T1 = 500;//K T2 = 1000;//K x = integrate('26.586 + 7.582 * 10^-3 * T - 1.12 * 10^-6 * T^2','T',T1,T2); Cpm = 1 *x / ( T2 - T1 ) ; disp("kJ/kmolK",Cpm,"(a)Mean molal heat capacity = ") V = 500;//m^3; N = V / 22.4143; Q = N * Cpm * ( T2 - T1 ); disp("kJ/h",Q,"(b)Heat to be supplied = ") T3 = 1500;//K Q1 = Cpm * (T3 - T1); y = integrate('26.586 + 7.582 * 10 ^-3 * T - 1.12 * 10^-6 * T^2','T',T1,T3); Q2 = y ; disp(Q2) Perror = (Q2 - Q1) * 100 / Q2; disp("%",Perror,"(c)Percent error = ")
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EX23_2.sce
//23.2 p=25//in cm f=10//in cm x=(1/f)-(1/p) q=1/x p=25 M=-(q/p) disp("part a") disp(M,"The magnification when object is at 25cm=") p=5//in cm f=10//in cm x=(1/f)-(1/p) q=1/x p=5 M=-(q/p) disp("part c") disp(M,"The magnification when object is at 5cm=")
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2019-03-02T22:27:19
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Or8Way.tst
// This file is part of the materials accompanying the book // "The Elements of Computing Systems" by Nisan and Schocken, // MIT Press. Book site: www.idc.ac.il/tecs // File name: projects/01/Or8Way.tst load Or8Way.hdl, output-file Or8Way.out, compare-to Or8Way.cmp, output-list in%B1.8.1 out%B2.1.2; set in %B00000000, eval, output; set in %B11111111, eval, output; set in %B00010000, eval, output; set in %B00000001, eval, output; set in %B00100110, eval, output;
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Ex4_3.sce
//======================================================================= // chapter 4 example 3 clc; clear; //input data E0 = 300*10^2; //local field in V/m P1 = 3.398*10^-7; //dipole moment Coulomb/m P2 = 2.124*10^-5; //dipole moment Coulomb/m e0 = 8.85*10^-12; //permittivity in F/m //formula //E10Ci=E0-(2*Pi/3*e0) //calculation E10C1 = E0-((2*P1)/(3*e0)); //local field of benzene in V/m E10C2 = E0-((2*P2)/(3*e0)); //local field of water in V/m //result mprintf('local field of benzene=%3.2e.V/m\n',E10C1); mprintf('local field of water=%3.2e.V/m\n',E10C2); //=======================================================================
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Exa_3_1.sce
//Exa 3.1 clc; clear; close; format('v',7); //Given Data : Q2=1800;//KJ/hr Q2=Q2/3600;//KJ/sec or KW W=0.35;//KW COP=Q2/W; disp(COP,"COP is : ");
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4_4.sce
//example 4.4 //linearization of non-linear law //page 131 clc;clear;close; x=[1 3 5 7 9]; y=[2.473 6.722 18.274 49.673 135.026]; for i=1:5 Y(i)=log(y(i)); x2(i)=x(i)^2; xy(i)=x(i)*Y(i); end S_x=0,S_y=0,S_x2=0,S_xy=0; printf('X\t Y=lny\t X^2\t XY\n\n'); for i=1:5 printf('%d\t %0.3f\t %d\t %0.3f\n',x(i),Y(i),x2(i),xy(i)); S_x=S_x+x(i); S_y=S_y+Y(i); S_x2=S_x2+x2(i); S_xy=S_xy+xy(i); end printf('----------------------------------------------------------------------------------------------------------------------------\n\n') printf('%d\t %0.3f\t %d\t %0.3f\t\n\n',S_x,S_y,S_x2,S_xy); A1=((S_x/5)*S_xy-S_x*S_y)/((S_x/5)*S_x2-S_x^2); A0=(S_y/5)-A1*(S_x/5); a=exp(A0); printf('y=%0.3fexp(%0.2fx)',a,A1);
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ex_3_6.sce
syms t s a y=laplace(%e^(-a*t)-%e^(a*t)) disp(y,"X(s)=") s1=%s; //a>0 a=2; t=-5:0.1:5; x=%e^(-a*abs(t)); subplot(2,1,1) plot(t,x) subplot(2,1,2) x=1/(s1+a)-1/(s1-a); plzr(x) //a<0 a=-0.5; t=-5:0.1:5; x=%e^(-a*abs(t)); figure subplot(2,1,1) plot(t,x) subplot(2,1,2) x=1/(s1+a)-1/(s1-a); plzr(x) disp("there is no region of convergence when a<0 hence no transform exists for a<0")
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1_9.sce
clc //initialisation of variables v=10//ft^3 p=100//lb/in^2 p1=18//lb/in^2 v1=50//ft^3 n=log(p/p1)/log(5) gama=1.4//air //CALCULATIONS W=[144*(p*v-p1*v1)]/(n-1)//ft lb H=(gama-n)/(gama-1)*W//ft lb E=W-H//ft lb //RESULTS printf('The heat supplied and the change of internal energy=% f ft lb',E)
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/iView X SDK/Examples/NBS Presentation/Slideshow/Slideshow.sce
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air2310/cpp_rep
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2016-12-06T12:25:00
2016-12-06T12:25:00
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Slideshow.sce
# ----------------------------------------------------------------------- # # (c) Copyright 1997-2013, SensoMotoric Instruments GmbH # # Permission is hereby granted, free of charge, to any person or # organization obtaining a copy of the software and accompanying # documentation covered by this license (the "Software") to use, # reproduce, display, distribute, execute, and transmit the Software, # and to prepare derivative works of the Software, and to permit # third-parties to whom the Software is furnished to do so, all subject # to the following: # # The copyright notices in the Software and this entire statement, # including the above license grant, this restriction and the following # disclaimer, must be included in all copies of the Software, in whole # or in part, and all derivative works of the Software, unless such # copies or derivative works are solely in the form of # machine-executable object code generated by a source language # processor. # # THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, # EXPRESS OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF # MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE, TITLE AND # NON-INFRINGEMENT. IN NO EVENT SHALL THE COPYRIGHT HOLDERS OR ANYONE # DISTRIBUTING THE SOFTWARE BE LIABLE FOR ANY DAMAGES OR OTHER # LIABILITY, WHETHER IN CONTRACT, TORT OR OTHERWISE, ARISING FROM, OUT # OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER DEALINGS IN # THE SOFTWARE. # # ----------------------------------------------------------------------- # Author: # (C) 2013 Sensomotoric Instruments ############################################################# # # # before running this scenario please set # # "Scenarios -> Stimulus Directory" to a path where all # # stimuli used in this scenario reside # # # ############################################################# scenario = "Slideshow"; no_logfile = true; active_buttons = 1; button_codes = 1; default_font_size = 24; default_font = "Times New Roman"; default_background_color = 230, 230, 230; # pcl file pcl_file = "Slideshow.pcl"; begin; picture {} default; ############################################################# # # # image definition # # # ############################################################# array { bitmap { filename = "image01.jpg"; preload = false; }; bitmap { filename = "image02.jpg"; preload = false; }; bitmap { filename = "image03.jpg"; preload = false; }; } graphics; trial { trial_duration = forever; trial_type = specific_response; terminator_button = 1; picture { # placeholder - set by PCL box { height = 1; width = 1; color = 0,0,0; }; x = 0; y = 0; } pic1; } trial1; #calibration bitmap picture { bitmap { filename = "black circle.bmp"; trans_src_color = 255,255,255; }; x = 0; y = 0; } et_calibration; # show error message if connection could not be established picture{ text{ caption = "Could not establish connection to Eye Tracker \n\n\n Check if the Eye Tracker \n is running and the \n Network Settings are set correctly"; font_size = 20; font_color = 20, 20, 20; transparent_color = 0,0,0; }; x = 0; y = 0; }connect_error; # show accuracy message after the calibration has been validated picture { text { caption = "Validation Results: \n\n Accuracy X: - \n Accuracy Y: -"; font_size = 20; font_color = 20, 20, 20; transparent_color = 0,0,0; preload = false; }accuracy_text; x = 0; y = 0; }accuracy_picture; # show error message if resolution is wrong picture{ text{ caption = "Please change \n the screen resolution \n of your computer \n to 1280 x 1024 or 1680 x 1050"; font_size = 20; font_color = 20, 20, 20; transparent_color = 0,0,0; }; x = 0; y = 0; }resolution_error; # show end message if experiment has been finished picture{ text{ caption = "End of Experiment"; font_size = 20; font_color = 20, 20, 20; transparent_color = 0,0,0; }; x = 0; y = 0; }end_experiment; picture{ text{ caption = "Try to acquire data..."; font_size = 20; font_color = 20, 20, 20; transparent_color = 0,0,0; }; x = 0; y = 0; }data_acquisition;
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/1627/CH10/EX10.3/Ex10_3.sce
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Ex10_3.sce
clc //initialisation of variables a=45//deg b=120//deg r=1750//rpm v=15//cm p=1000//N.s/m^4 u1=15*10^-2//m v1=0.5//m //CALCULATIONS U2=(2*%pi*r/60)*u1//m/s V1=U2-[(v*v1)]//m/s P=U2*V1//kPa //RESULTS printf('The pressure =% f kPa',P)
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exa_6_10.sce
// Exa 6.10 clc; clear; close; // Given data R1= 220;// in kohm R1=R1*10^3;// in ohm R2=R1;// in ohm C1= 250;// in pF C1= C1*10^-12;// in F C2=C1;// in F f= 1/(2*%pi*R1*C1); disp(f,"Frequency of oscilltions in Hz is : ")
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ex2.sce
//Example 2 Page 59 clc clear //creating C(x) function function y=C(x) y=100000+160*x-0.2*x^2 endfunction //the variable cost is the part of the cost function that depends on x VariableCost=poly([0 160 -0.2],'x','c')//variablecost polynomial disp(VariableCost,'VariableCost in dollars=') FixedCost=100000 disp(FixedCost,'FixedCost in dollars=') x=poly(0,'x')//x polynomial creation Rx=800*x//annual revence of x members //for the profit we use the formula Px=Rx-C(x)//displaying the P(x) value by subtracting C(x) from Rx disp('P(x)=R(x)-C(x)') disp(Px) r=roots(Px)//finding the roots of the quadratic equation obtained in P(x) disp(r) disp('since members cannot be in negative value we consider the positive value') x=[0 250]//taking random variables of x for graph y=C(x)//function calling plot(400,350000,x,y,'red')//plotting graph //creating the P(x) function function y=P(x) y=-100000+640*x+0.2*x^2 endfunction x=([0 150 350])//taking values of x for graph y=P(x) plot(x,y,'blue')//plotting graph xtitle(' ','x','y');
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Ex1_33.sce
clc; P=500000; // VA rating of transformer E2=400; // rated secondary voltage nmax=0.98; // maximum efficiency of transformer l=80; // percentage of full load at which maximum efficiency occurs ze2=4.5; // percentage impedance pt=((1/nmax)-1)*P*(l/100); // total losses pc=pt/2; // core loss = ohmic loss at maximum efficiency poh=pc; // ohmic loss pohl=poh*(100/l)^2; // full load ohmic losses re2=(pohl/P)*100; // percentage resistance xe2=sqrt(ze2^2-re2^2); // percentage leakage reactance pfl=re2/ze2; // load power factor vr=re2*pfl+xe2*sqrt(1-pfl^2); // voltage regulation dv=(E2*vr)/100; // change in terminal voltage V2=E2-dv; // Secondary terminal voltage printf('Load power factor at which secondary terminal voltage is minimum is %f\n',pfl); printf('Secondary terminal voltage is %f v',V2); // answer for total losses is given wrong in the book
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example_14.sce
clc clear printf("example 4.14 page number 151\n\n") //to find the discharge pressure d=0.025 //in m u=3 //in m/s density=894 //in kg/m3 viscosity=6.2*10^4 //in Pa-s Re=(u*d*density)/viscosity; f=0.0045; L=50; delta_P=2*f*density*u^2*(L/d) printf("frictional head loss = %f kPa",delta_P/1000) required_P=25*density*9.8; total_head=delta_P+required_P; printf("\n\ntotal pressure head = %f bar",total_head/10^5)
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Ex3_7.sce
clear; clc; printf("\t\t\tProblem Number 3.7\n\n\n"); // Chapter 3 : The First Law Of Thermodynamics // Problem 3.7 (page no. 97) // Solution Rho=62.4 //Unit:lbm/ft^3 //the density of the fluid V=100 //Unit:ft/s //Velocity of fluid d=1 //Unit:in //Diameter //1 ft^2=144 in^2 //A=(%pi/4)*d^2 A=(%pi*d^2)/(4*144) //Unit:ft^2 //area m=Rho*A*V; //Unit:lbm/s //mass rate of flow per unit time printf("Mass flow rate is %f lbm/s\n",m);
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; @Harness: disassembler ; @Result: PASS section .text size=0x00000100 vma=0x00000000 lma=0x00000000 offset=0x00000034 ;2**0 section .data size=0x00000000 vma=0x00000000 lma=0x00000000 offset=0x00000134 ;2**0 start .text: label 0x00000000 ".text": 0x0: 0xfb 0xf1 brvs .+126 ; 0x80 0x2: 0xf3 0xf1 brvs .+124 ; 0x80 0x4: 0xeb 0xf1 brvs .+122 ; 0x80 0x6: 0xe3 0xf1 brvs .+120 ; 0x80 0x8: 0xdb 0xf1 brvs .+118 ; 0x80 0xa: 0xd3 0xf1 brvs .+116 ; 0x80 0xc: 0xcb 0xf1 brvs .+114 ; 0x80 0xe: 0xc3 0xf1 brvs .+112 ; 0x80 0x10: 0xbb 0xf1 brvs .+110 ; 0x80 0x12: 0xb3 0xf1 brvs .+108 ; 0x80 0x14: 0xab 0xf1 brvs .+106 ; 0x80 0x16: 0xa3 0xf1 brvs .+104 ; 0x80 0x18: 0x9b 0xf1 brvs .+102 ; 0x80 0x1a: 0x93 0xf1 brvs .+100 ; 0x80 0x1c: 0x8b 0xf1 brvs .+98 ; 0x80 0x1e: 0x83 0xf1 brvs .+96 ; 0x80 0x20: 0x7b 0xf1 brvs .+94 ; 0x80 0x22: 0x73 0xf1 brvs .+92 ; 0x80 0x24: 0x6b 0xf1 brvs .+90 ; 0x80 0x26: 0x63 0xf1 brvs .+88 ; 0x80 0x28: 0x5b 0xf1 brvs .+86 ; 0x80 0x2a: 0x53 0xf1 brvs .+84 ; 0x80 0x2c: 0x4b 0xf1 brvs .+82 ; 0x80 0x2e: 0x43 0xf1 brvs .+80 ; 0x80 0x30: 0x3b 0xf1 brvs .+78 ; 0x80 0x32: 0x33 0xf1 brvs .+76 ; 0x80 0x34: 0x2b 0xf1 brvs .+74 ; 0x80 0x36: 0x23 0xf1 brvs .+72 ; 0x80 0x38: 0x1b 0xf1 brvs .+70 ; 0x80 0x3a: 0x13 0xf1 brvs .+68 ; 0x80 0x3c: 0x0b 0xf1 brvs .+66 ; 0x80 0x3e: 0x03 0xf1 brvs .+64 ; 0x80 0x40: 0xfb 0xf0 brvs .+62 ; 0x80 0x42: 0xf3 0xf0 brvs .+60 ; 0x80 0x44: 0xeb 0xf0 brvs .+58 ; 0x80 0x46: 0xe3 0xf0 brvs .+56 ; 0x80 0x48: 0xdb 0xf0 brvs .+54 ; 0x80 0x4a: 0xd3 0xf0 brvs .+52 ; 0x80 0x4c: 0xcb 0xf0 brvs .+50 ; 0x80 0x4e: 0xc3 0xf0 brvs .+48 ; 0x80 0x50: 0xbb 0xf0 brvs .+46 ; 0x80 0x52: 0xb3 0xf0 brvs .+44 ; 0x80 0x54: 0xab 0xf0 brvs .+42 ; 0x80 0x56: 0xa3 0xf0 brvs .+40 ; 0x80 0x58: 0x9b 0xf0 brvs .+38 ; 0x80 0x5a: 0x93 0xf0 brvs .+36 ; 0x80 0x5c: 0x8b 0xf0 brvs .+34 ; 0x80 0x5e: 0x83 0xf0 brvs .+32 ; 0x80 0x60: 0x7b 0xf0 brvs .+30 ; 0x80 0x62: 0x73 0xf0 brvs .+28 ; 0x80 0x64: 0x6b 0xf0 brvs .+26 ; 0x80 0x66: 0x63 0xf0 brvs .+24 ; 0x80 0x68: 0x5b 0xf0 brvs .+22 ; 0x80 0x6a: 0x53 0xf0 brvs .+20 ; 0x80 0x6c: 0x4b 0xf0 brvs .+18 ; 0x80 0x6e: 0x43 0xf0 brvs .+16 ; 0x80 0x70: 0x3b 0xf0 brvs .+14 ; 0x80 0x72: 0x33 0xf0 brvs .+12 ; 0x80 0x74: 0x2b 0xf0 brvs .+10 ; 0x80 0x76: 0x23 0xf0 brvs .+8 ; 0x80 0x78: 0x1b 0xf0 brvs .+6 ; 0x80 0x7a: 0x13 0xf0 brvs .+4 ; 0x80 0x7c: 0x0b 0xf0 brvs .+2 ; 0x80 0x7e: 0x03 0xf0 brvs .+0 ; 0x80 0x80: 0xfb 0xf3 brvs .-2 ; 0x80 0x82: 0xf3 0xf3 brvs .-4 ; 0x80 0x84: 0xeb 0xf3 brvs .-6 ; 0x80 0x86: 0xe3 0xf3 brvs .-8 ; 0x80 0x88: 0xdb 0xf3 brvs .-10 ; 0x80 0x8a: 0xd3 0xf3 brvs .-12 ; 0x80 0x8c: 0xcb 0xf3 brvs .-14 ; 0x80 0x8e: 0xc3 0xf3 brvs .-16 ; 0x80 0x90: 0xbb 0xf3 brvs .-18 ; 0x80 0x92: 0xb3 0xf3 brvs .-20 ; 0x80 0x94: 0xab 0xf3 brvs .-22 ; 0x80 0x96: 0xa3 0xf3 brvs .-24 ; 0x80 0x98: 0x9b 0xf3 brvs .-26 ; 0x80 0x9a: 0x93 0xf3 brvs .-28 ; 0x80 0x9c: 0x8b 0xf3 brvs .-30 ; 0x80 0x9e: 0x83 0xf3 brvs .-32 ; 0x80 0xa0: 0x7b 0xf3 brvs .-34 ; 0x80 0xa2: 0x73 0xf3 brvs .-36 ; 0x80 0xa4: 0x6b 0xf3 brvs .-38 ; 0x80 0xa6: 0x63 0xf3 brvs .-40 ; 0x80 0xa8: 0x5b 0xf3 brvs .-42 ; 0x80 0xaa: 0x53 0xf3 brvs .-44 ; 0x80 0xac: 0x4b 0xf3 brvs .-46 ; 0x80 0xae: 0x43 0xf3 brvs .-48 ; 0x80 0xb0: 0x3b 0xf3 brvs .-50 ; 0x80 0xb2: 0x33 0xf3 brvs .-52 ; 0x80 0xb4: 0x2b 0xf3 brvs .-54 ; 0x80 0xb6: 0x23 0xf3 brvs .-56 ; 0x80 0xb8: 0x1b 0xf3 brvs .-58 ; 0x80 0xba: 0x13 0xf3 brvs .-60 ; 0x80 0xbc: 0x0b 0xf3 brvs .-62 ; 0x80 0xbe: 0x03 0xf3 brvs .-64 ; 0x80 0xc0: 0xfb 0xf2 brvs .-66 ; 0x80 0xc2: 0xf3 0xf2 brvs .-68 ; 0x80 0xc4: 0xeb 0xf2 brvs .-70 ; 0x80 0xc6: 0xe3 0xf2 brvs .-72 ; 0x80 0xc8: 0xdb 0xf2 brvs .-74 ; 0x80 0xca: 0xd3 0xf2 brvs .-76 ; 0x80 0xcc: 0xcb 0xf2 brvs .-78 ; 0x80 0xce: 0xc3 0xf2 brvs .-80 ; 0x80 0xd0: 0xbb 0xf2 brvs .-82 ; 0x80 0xd2: 0xb3 0xf2 brvs .-84 ; 0x80 0xd4: 0xab 0xf2 brvs .-86 ; 0x80 0xd6: 0xa3 0xf2 brvs .-88 ; 0x80 0xd8: 0x9b 0xf2 brvs .-90 ; 0x80 0xda: 0x93 0xf2 brvs .-92 ; 0x80 0xdc: 0x8b 0xf2 brvs .-94 ; 0x80 0xde: 0x83 0xf2 brvs .-96 ; 0x80 0xe0: 0x7b 0xf2 brvs .-98 ; 0x80 0xe2: 0x73 0xf2 brvs .-100 ; 0x80 0xe4: 0x6b 0xf2 brvs .-102 ; 0x80 0xe6: 0x63 0xf2 brvs .-104 ; 0x80 0xe8: 0x5b 0xf2 brvs .-106 ; 0x80 0xea: 0x53 0xf2 brvs .-108 ; 0x80 0xec: 0x4b 0xf2 brvs .-110 ; 0x80 0xee: 0x43 0xf2 brvs .-112 ; 0x80 0xf0: 0x3b 0xf2 brvs .-114 ; 0x80 0xf2: 0x33 0xf2 brvs .-116 ; 0x80 0xf4: 0x2b 0xf2 brvs .-118 ; 0x80 0xf6: 0x23 0xf2 brvs .-120 ; 0x80 0xf8: 0x1b 0xf2 brvs .-122 ; 0x80 0xfa: 0x13 0xf2 brvs .-124 ; 0x80 0xfc: 0x0b 0xf2 brvs .-126 ; 0x80 0xfe: 0x03 0xf2 brvs .-128 ; 0x80 start .data:
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Ch03Ex7.sce
// Scilab code Ex3.7 : Pg:102 (2008) clc;clear; F = 9.0; // Focal length of the eye-piece, cm // As F = f1*f2/(f1 + f2 - d) and f1 = f; f2 = f; d = 2/3*f, solving for f f = poly(0, 'f'); f = roots(f*f-F*(f+f-2/3*f)); // Focal length of the eye-lens, cm d = 2/3*f(1); // Distance of separation of two lenses, cm f1 = f(1); // Focal length of the first plano-convex lens, cm f2 = f(1); // Focal length of the second plano-convex lens, cm alpha = F*d/f2; // Distance of first principal point from the field lens L1, cm bita = -F*d/f1; // Distance of second principal point from the field lens L2, cm L1F1 = -F*(1-d/f2); // Distance of first focal point from the lens L1, cm L2F2 = F*(1-d/f1); // Distance of second focal point from the lens L2, cm printf("\nThe focal lengths of the plano-convex lenses are %1.0f cm and %2.0f cm", f1, f2); printf("\nThe distance between the lenses = %1.0f cm", d); printf("\nThe distance of first principal point from the field lens L1 = %1.0f cm", alpha); printf("\nThe distance of second principal point from the field lens L2 = %1.0f cm", bita); printf("\nThe distance of first focal point from the field lens L1 = %1.0f cm", L1F1); printf("\nThe distance of second focal point from the field lens L2 = %1.0f cm", L2F2); // Result // The focal lengths of the plano-convex lenses are 12 cm and 12 cm // The distance between the lenses = 8 cm // The distance of first principal point from the field lens L1 = 6 cm // The distance of second principal point from the field lens L2 = -6 cm // The distance of first focal point from the field lens L1 = -3 cm // The distance of second focal point from the field lens L2 = 3 cm
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12_1_Plate_surface.sce
clear; clc; printf('FUNDAMENTALS OF HEAT AND MASS TRANSFER \n Incropera / Dewitt / Bergman / Lavine \n EXAMPLE 12.1 Page 731 \n')// Example 12.1 // a) Intensity of emission in each of the three directions // b) Solid angles subtended by the three surfaces // c) Rate at which radiation is intercepted by the three surfaces A1 = .001 ;//[m^2] Area of emitter In = 7000 ;//[W/m^2.Sr] Intensity of radiation in normal direction A2 = .001 ;//[m^2] Area of other intercepting plates A3 = A2 ;//[m^2] Area of other intercepting plates A4 = A2 ;//[m^2] Area of other intercepting plates r = .5 ;//[m] Distance of each plate from emitter theta1 = 60 ;//[deg] Angle between surface 1 normal & direction of radiation to surface 2 theta2 = 30 ;//[deg] Angle between surface 2 normal & direction of radiation to surface 1 theta3 = 45 ;//[deg] Angle between surface 1 normal & direction of radiation to surface 4 //From equation 12.2 w31 = A3/r^2; w41 = w31; w21 = A2*cos(theta2*0.0174532925)/r^2; //From equation 12.6 q12 = In*A1*cos(theta1*0.0174532925)*w21; q13 = In*A1*cos(0)*w31; q14 = In*A1*cos(theta3*0.0174532925)*w41; printf("\n (a) As Intensity of emitted radiation is independent of direction, for each of the three directions I = %i W/m^2.sr \n\n (b) By the Three Surfaces\n Solid angles subtended Rate at which radiation is intercepted \n w4-1 = %.2e sr q1-4 = %.1e W \n w3-1 = %.2e sr q1-3 = %.1e W\n w2-1 = %.2e sr q1-2 = %.1e W ",In,w41,q14,w31,q13,w21,q12); //END
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ex7_16.sce
//Part A Chapter 7 Example 16 clc; clear; close; mg=40;//kg mf=2.2;//kg p1=1.47;//MPa T=120;//degree C p2=107.88;//kPa cv=2.09;//kJ/kg.K Td=T-101.8;//degree C(DegreeSuperHeat) hf=2673.95;//kJ/kg h=hf+Td*cv;//kJ/kg hf2=918.926;//kJ/kg hfg2=1864.28;//kJ/kg x2=(h-hf2)/hfg2;//dryness fraction x1=(mg-mf)/mg;//dryness fraction x=x1*x2;//overall dryness fraction disp("Dryness fraction is "+string(x));
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Ex1_2_17.sce
//Section-1,Example-4,Page no.-AC.205 //To find the air required for the perfect combustion of 1 m^3 of the given gas. clc; T=0.22 L_O2=0.02 Net_O2=0.2 Plus_CO2=0.05 T_CO2=T+L_O2+Plus_CO2 T_N2=1.6 T_O2=Net_O2*(40/100) T_W=T_CO2+T_N2+T_O2 M_Q=Net_O2*(100/21) P_CO2=(T_CO2/T_W)*100 disp(P_CO2,'Percentage composition of CO_2') P_N2=(T_N2/T_W)*100 disp(P_N2,'Percentage composition of N_2') P_O2=(T_O2/T_W)*100 disp(P_O2,'Percentage composition of O_2')
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example7_6.sce
// to calculate the minimum change detectable by the bridge // example 7-6 in page 172 clc; //Given data P=3.5e+3; Q=7e+3; S=4e+3; R=2e+3; // bridge arm resistances in ohm Eb=10;// supply voltage in volt Ig=1e-6;//galvano meter reading in ampere rg=2.5e+3;//galvanometer resistance=2.5 K-ohm //calculations r=((P*R)/(P+R))+((Q*S)/(Q+S));// internal resistance of the bridge in ohm dVR=Ig*(r+rg);// open-circuit galvano meter voltage i,e VR-VS in volt VR=Eb*R/(R+P);// voltage across resistance R in volt VP=Eb-(VR+dVR);//voltage across resistance P in volt IR=VP/P;// current through P which is equal to current through R in ampere dR=((VR+dVR)/IR)-R;//Change in R value that the device can detect in ohm printf("the minimum change in R which is detected by the bridge is %f ohm\n",dR); //result // the minimum change in R which is detected by the bridge is 5.466141 ohm
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// Scilab Code Ex8.10: Page-175 (2010) c = 3e+008; // Speed of light in vacuum, m/s dE = 4e+026; // Energy radiated per second my the sun, J/s dm = dE/c^2; // Rate of decrease of mass of sun, kg/s printf("\nThe rate of decrease of mass of sun = %4.2e kg/s", dm); // Result // The rate of decrease of mass of sun = 4.44e+009 kg/s
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EX2_9.sce
//Chapter 2, Example 2.9, page 47 clc //Initialisation FSL=128 //FSL in dB Lb=135 //Sum of FSL and medium loss Lm Lc=5 Gt=30 //transmitter gain in dB Gr=30 //reciever gain in dB Pr=-60 //received signal level //Calculation Lm=Lb-FSL //medium loss in dB Lm1=10**(Lm*10**-1) //medium loss Pt=Lc+Lb-Gt-Gr+Pr //power in dBm Pt1=10**(Pt*10**-1) //power in watt //Result printf("Medium Loss = %d",Lm1) printf("\nPt = %.1f mW",(Pt1))
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Ex3_27.sce
//EX3_27 PG-3.60 clc Il=12e-3;//load current Es=200;//rms voltage Rf=0.02;//riplle factor Esm=sqrt(2)*Es;//peak value of input voltage Edc=2*Esm/%pi; Idc=Il; Rl=Edc/Idc;//load resistance f=50;//frequency of the supply in Hz disp(" For a half wave rectifier Ripple factor=1/(2*sqrt(3)*f*C*Rl)") C=(4*sqrt(3)*f*Rf*Rl)^(-1);//filter capacitor printf("\n Therefore minimum value of capacitance required is %.3f microF",C*1e6) //C=9.619 microF not 9.622 microF
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EXAMPLE8_20.SCE
//ANALOG AND DIGITAL COMMUNICATION //BY Dr.SANJAY SHARMA //CHAPTER 7 //WAVEFORM CODING TECHNIQUES clear all; clc; printf("EXAMPLE 8.20(PAGENO 415)"); //given SbyN_0dB = 40//signal to noise ratio in dB SbyN_0 = exp((SbyN_0dB/10)*log(10))//signal to noise ratio q = sqrt((2 / 3) * (SbyN_0));//quantizing level v = log2(q)//number of binary bits q_1 = 2^v//number of levels required SbyN_dB1 = 1.76 + 6.02*v//output signal-to-quantizing noise ratio in dB //results printf("\n\nNumber of required levels = %.2f ",v); printf("\n\nOutput signal-to-quantizing noise ratio = %.2f dB",SbyN_dB1); printf("\n\nNote : In the textbook they took number of levels as approximation so we get change\n in SbyN")
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Example11_8.sce
//clear// //Caption:Program to find the input impedance and power delivered to //the load //Example11.8 //page363 clc; close; ZR1 = 300; //input impedance of first receiver ZR2 = 300; //input impedance of second receiver Zo = ZR1; //characteristic impedance = 300 ohm Zc = -%i*300;//capacitive impedance L = 80e-02;//length = 80 cm Lambda = 1; //wavelength = 1m Vth = 60; // voltage 300 volts Zth = Zo; ZL1 = (ZR1*ZR2)/(ZR1+ZR2); ZL = (ZL1*Zc)/(ZL1+Zc); //net load impedane T = (ZL-ZR2)/(ZL+ZR2);//reflection coefficient [R,teta1] = polar(T); //reflection coefficient in polar form teta1 = real(teta1)*57.3;//teta value in degrees S = (1+R)/(1-R); //voltage standing wave ratio EL = 2*%pi*L/Lambda; //electrical length in degrees Zin = Zo*(ZL*cos(EL)+%i*Zo*sin(EL))/(Zo*cos(EL)+%i*ZL*sin(EL)); disp(Zin,'Input Impedance in ohms Zin =') Is = Vth/(Zth+Zin);//source current in amps [Is,teta2] = polar(Is);//source current in polar form Pin = (1/2)*(Is^2)*real(Zin); PL = Pin; //for lossless line disp(Pin,'Power delivered to a loss less line in watss PL =') //Result //Input Impedance in ohms Zin = 755.49551 - 138.46477i // Power delivered to a loss less line in watss PL = 1.2
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/microdaq/macros/microdaq_blocks/mdaq_mem_read.sci
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2020-12-25T17:12:56.934984
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mdaq_mem_read.sci
function [x,y,typ] = mdaq_mem_read(job,arg1,arg2) mem_write_desc = ["This block reads data from MicroDAQ memory."; "Block with mdaq_mem_set function can be used to"; "change Standalone and Ext model parameters"; ""; "Set block parameters:"]; x=[];y=[];typ=[]; select job case 'set' then x=arg1 model=arg1.model; graphics=arg1.graphics; exprs=graphics.exprs; while %t do try [ok,start_idx, data_size, vec_size,do_increment,exprs]=.. scicos_getvalue(mem_write_desc,.. ['Start index:'; 'Size:'; 'Vector size:'; 'Periodic:'],.. list('vec',1,'vec',1,'vec',1,'vec',1),exprs) catch [ok,start_idx, data_size,vec_size,do_increment,exprs]=.. getvalue(mem_write_desc,.. ['Start index:'; 'Size'; 'Vector size:'; 'Periodic:'],.. list('vec',1,'vec',1,'vec',1,'vec',1),exprs) end; if ~ok then break end //~16MB = 16 000 000B = 4 000 000 floats max_index = 4000000; if start_idx < 1 | start_idx > max_index then ok = %f; message("Incorrect memory start index - use index from 1 to "+string(max_index)); end if vec_size > 10000 | vec_size < 1 then ok = %f; message("Wrong vector size - use 10000 max!"); end size_mod = modulo(data_size, vec_size) if size_mod <> 0 then ok = %f; message("Incorrect size. Size is not multiple of array size!"); end if data_size < 1 | data_size > (max_index-start_idx) then ok = %f; message("Incorrect size (max "+string(max_index-start_idx)+")"); end if do_increment > 1 | do_increment < 0 then ok = %f; message("Use values 0 or 1 to set increment option."); end if ok then [model,graphics,ok] = check_io(model,graphics, [], vec_size, 1, []); graphics.exprs = exprs; model.rpar = []; model.ipar = [(start_idx-1);vec_size;do_increment;data_size]; model.dstate = []; x.graphics = graphics; x.model = model; break end end case 'define' then start_idx = 1; vec_size = 1; data_size = 100; do_increment = 0; model=scicos_model() model.sim=list('mdaq_mem_read_sim',5) model.in =[] model.out=vec_size model.out2=1 model.outtyp=1 model.evtin=1 model.rpar=[]; model.ipar=[(start_idx-1);vec_size;do_increment;data_size] model.dstate=[]; model.blocktype='d' model.dep_ut=[%t %f] exprs=[sci2exp(start_idx);sci2exp(data_size);sci2exp(vec_size);sci2exp(do_increment)] gr_i=['xstringb(orig(1),orig(2),['''' ; ],sz(1),sz(2),''fill'');'] x=standard_define([4 3],model,exprs,gr_i) x.graphics.in_implicit=[]; x.graphics.exprs=exprs; end endfunction
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/1766/CH4/EX4.11/EX4_11.sce
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appucrossroads/Scilab-TBC-Uploads
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refs/heads/master
2021-01-22T04:15:15.512674
2017-09-19T11:51:56
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EX4_11.sce
clc;funcprot(0);......//Example 4.11 //Initialization of variables L=0.05;.........//Distance between 2 verticle plates in m L1=1;...........//Length of the plate in m W=1;...........// Tw=100;........//Temperature of hot plate in degrees celcius Ta=20;.............//Temperature of cold plate in degrees celcius v=18.97*10^-6;.......//Viscosity in m^2/s K=28.96;.......//Thermal conductivity in W/mK g=9.8;....//Gravitational constant Pr=0.696;......//Prandlt no //Calculations Tf=(Tw+Ta)/2;.........//Film temperature in K B=1/(Tf+273);........//Temp inverse in K^-1 Gr=(g*B*(Tw-Ta)*L*L*L)/(v^2);.......//Grashoff No Nu=0.42*(Gr*Pr)^0.25*(Pr)^0.012*(20)^-0.3;............//Nusselt no h=(Nu*K)/(L);.........//Heat transfer co-efficient in W/m^2 K Q=h*(L1*W)*(Tw-Ta);.........//Rate of heat loss in W disp(Q/1000,"Rate of heat transfer in kW:")
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/OW McCoy Dodge.sce
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2023-01-14T02:10:25.103083
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OW McCoy Dodge.sce
Name=OW McCoy Dodge PlayerCharacters=McCoy BotCharacters=McCoy Bot.bot IsChallenge=true Timelimit=60.0 PlayerProfile=McCoy AddedBots=McCoy Bot.bot PlayerMaxLives=0 BotMaxLives=0 PlayerTeam=2 BotTeams=1 MapName=horizbounce.map MapScale=2.5 BlockProjectilePredictors=true BlockCheats=true InvinciblePlayer=true InvincibleBots=true 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=Overwatch, Fortnite, Quake WeaponHeroTag=Tracking, LG DifficultyTag=4 AuthorsTag=Hud BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=McCoy 1v1 Practice with movement scoring GameVersion=1.0.8.0 ScorePerDistance=0.0 MBSEnable=true MBSTime1=0.08 MBSTime2=1.0 MBSTime3=1.0 MBSTime1Mult=90.0 MBSTime2Mult=150.0 MBSTime3Mult=150.0 MBSFBInstead=false MBSRequireEnemyAlive=false [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=McCoy Bot DodgeProfileNames=Long Strafes Jumping;Short Strafes Jumping;Mimic;Circle Strafe DodgeProfileWeights=2.0;1.0;3.0;2.0 DodgeProfileMaxChangeTime=3.0 DodgeProfileMinChangeTime=0.1 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=true CharacterProfile=McCoy SeeThroughWalls=false NoDodging=false NoAiming=false [Character Profile] Name=McCoy MaxHealth=200.0 WeaponProfileNames=Six Shooter;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=30.0 CrouchHeightModifier=0.69 CrouchAnimationSpeed=5.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=1.0 MovementType=Base MaxSpeed=488.888885 MaxCrouchSpeed=270.0 Acceleration=10000.0 AirAcceleration=16000.0 Friction=100.0 BrakingFrictionFactor=0.0 JumpVelocity=270.0 Gravity=1.0 AirControl=0.16 CanCrouch=true CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=true EnemyBodyColor=X=0.778 Y=0.000 Z=0.000 EnemyHeadColor=X=1.000 Y=0.265 Z=0.000 TeamBodyColor=X=0.000 Y=0.000 Z=0.787 TeamHeadColor=X=1.000 Y=0.265 Z=0.000 BlockSelfDamage=true InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=true AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=120.0 MainBBRadius=20.0 MainBBHasHead=true MainBBHeadRadius=12.5 MainBBHeadOffset=-12.5 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=120.0 ProjBBRadius=20.0 ProjBBHasHead=true ProjBBHeadRadius=12.5 ProjBBHeadOffset=-12.5 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.5 JetpackFullFuelTime=1000.0 JetpackFuelIncPerSec=100.0 JetpackFuelRegensInAir=true JetpackThrust=6000.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=Rush.abilmov;Stun Gren.abilwep;;Melee.abilmelee HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=0.9 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 SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false [Dodge Profile] Name=Long Strafes Jumping MaxTargetDistance=1245.901611 MinTargetDistance=373.770477 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.5 MaxLRTimeChange=1.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 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=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Short Strafes Jumping MaxTargetDistance=1245.901611 MinTargetDistance=373.770477 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 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=0.5 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.5 BlockedMovementReactionMin=0.125 BlockedMovementReactionMax=0.2 [Dodge Profile] Name=Mimic MaxTargetDistance=1245.901611 MinTargetDistance=373.770477 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Mimic 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 [Dodge Profile] Name=Circle Strafe MaxTargetDistance=1245.901611 MinTargetDistance=373.770477 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.2 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=true DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Oppose 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=Six Shooter Type=Hitscan ShotsPerClick=1 DamagePerShot=70.0 KnockbackFactor=0.1 TimeBetweenShots=0.5 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=true HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=1.5 ReloadTimeFromPartial=1.5 DamageFalloffStartDistance=2200.0 DamageFalloffStopDistance=4500.0 DamageAtMaxRange=20.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.5 WallParticleEffect=None HitParticleEffect=None BounceOffWorld=false BounceFactor=0.0 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=-80.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.1 RecoilNegatable=true DecalType=1 DecalSize=15.0 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 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false 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=72.099998 ADSFOVScale=Overwatch 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=4.0 MinRecoilUp=4.0 MinRecoilHoriz=0.0 MaxRecoilHoriz=0.0 FirstShotRecoilMult=1.0 RecoilAutoReset=true TimeToRecoilPeak=0.05 TimeToRecoilReset=0.44 AAMode=2 AAPreferClosestPlayer=false AAAlpha=0.05 AAMaxSpeed=0.5 AADeadZone=0.0 AAFOV=30.0 AANeedsLOS=true TrackHorizontal=true TrackVertical=true AABlocksMouse=false AAOffTimer=0.0 AABackOnTimer=0.0 TriggerBotEnabled=true TriggerBotDelay=0.01 TriggerBotFOV=0.1 StickyLock=false HeadLock=true 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 [Weapon Profile] Name=Stun Gren Type=Projectile ShotsPerClick=1 DamagePerShot=25.0 KnockbackFactor=4.0 TimeBetweenShots=0.8 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=1.0 MaxHitscanRange=100000.0 GravityScale=1.0 HeadshotCapable=false HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=0 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 HitscanVisualEffect=Tracer ProjectileGraphic=Ball VisualLifetime=0.1 WallParticleEffect=Flare HitParticleEffect=Flare BounceOffWorld=false BounceFactor=0.0 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=0.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=4.0 RecoilNegatable=false DecalType=0 DecalSize=15.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.8 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 ProjectileTrail=None RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false 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=72.099998 ADSFOVScale=Overwatch ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 Explosive=true Radius=230.0 DamageAtCenter=25.0 DamageAtEdge=25.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=true DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.15 BlockedByWorld=true SpreadSSA=1.0,1.0,-1.0,0.0 SpreadSCA=1.0,1.0,-1.0,0.0 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clc //Example 6.5 //Calculate volumetric flow rate of gasoline through a pipe d=0.1//m internal diameter of pipe A=%pi*d^2/4//m^2 dx=100//m length of pipe f=0.005//dimentionless fanning friction factor dz=10//m difference in water level g=9.81//m/s^2 v=((2*g*dz/4/f)*d/dx)^0.5//m/s printf("The velocity of gasoline through pipe is %f m/s\n",v); q=A*v//m^3/s printf("The volumteric flow arte od gasoline through the pipe is %f m^3/s",q);
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errcatch(-1,"stop");mode(2);; //need to find absorption coefficient V=5600 //in m^3 T=2 //in second s=700 //in m^2 a=0.16*V/(s*T) disp(a,"absorption coefficient =") exit();
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clear;lines(0); a(1,1,1,1:2)=[1 2] a=[1 2;3 4];a(:,:,2)=rand(2,2) a(1,1,:) [a a]
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//Ex 1.11.8 clc;clear;close; format('v',9); //Given : n=5*10^22;//per cm^3 ni=1.52*10^10*10^6;//per m^3 q=1.6*10^-19;//Coulomb mu_n=0.135;//m^2/V-s mu_p=0.048;//m^2/V-s impurity=1/10^8;//atoms sigma_i=ni*q*(mu_n+mu_p);//(ohm-cm)^-1 rho_i=1/sigma_i;//ohm-cm disp(rho_i,"Resistivity of intrinsic Si in ohm-m : "); ND=n*impurity*10^6;//per m^3 sigma_n=ND*mu_n*q;//(ohm-m)^-1 rho_n=1/sigma_n;//ohm-m disp(rho_n,"Resistivity of doped Si in ohm-m : "); //Answer in the book is not accurate.
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//Transport Processes and Seperation Process Principles //Chapter 4 //Example 4.3-4 //Principles of Steady State Heat Transfer //given data //nomenclature of unmentioned specifications similar to previous example I=200;//current in A R=0.126;// resistance in ohms P=I*I*R;//Power in watts Tw=422.1;//watt temp in K L=0.91;//length of wire r=0.001268;//radius of wire qdot=P/(%pi*L*r*r); k=22.5; T0=(qdot*r*r/(4*k))+Tw mprintf("centre temperature= %f K",T0)
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// question 1 // spec permet de renvoyer les valeurs propres d'une matrice eye(4,4) // matrice identité 4x4 // question 2 // 1) A = [1,0,3,1;1,2,0,1;0,1,3,0] size(A) // taille matrice A // 2) A(1,:) // première ligne A(:,4) // dernière colonne A(2,3) // élément deuxième ligne troisième colonne // 3) diag(A) // diagonale matrice A triu(A) // triangulaire supérieure tril(A) // triangulaire inférieure // question 3 // matrice identité 10x10 B=ones(1,10) C=diag(B) // question 4 // traçage courbe fonction sin sur [0,2pi] pour 6 points de discrétisation puis 21 points de discrétisation (en une autre couleur) avec titre et légendes x=linspace(0,2*%pi,6) y=linspace(0,2*%pi,21) plot(x, sin(x), "r", y, sin(y), "b") xtitle("Graphes de la fonction sin") legend("sin (6 points discrétisation)","sin (21 points discrétisation)")
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clc //initialization of varaibles P1=100 //psia T1=2000+460 //R P2=15 //psia g=1.4 cp=0.276 cv=0.207 T2=1520 //R //calculations k=cp/cv v1=53.34*T1/(P1*144) v2=v1*(P1/P2)^(1/k) dh=cp*(T2-T1) dv=v2-v1 //results printf("Enthalpy change = %d B/lb",dh) printf("\n Volume change = %.1f cu t/lb",dv)
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//Example 2_12 page no:96 clc; //current source are parallel so added them up I1=5; I2=5; I3=10; I=I1+I2+I3; R1=2; R2=2; R3=3; R4=2; R5=1; R=1/((1/R1)+(1/R2)+(1/R3)+(1/R4)+(1/R5)); V=I*R; disp(V,"the voltage source is (in V)"); disp(R,"the resistance connected in series is (in ohm)"); //in text book resistance calculationg is wrong //R valus is 0.35
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clc;clear;close; A=[] disp("-------------------------------------------------------------------------") printf(" Enter a 3x3 matrix:\n\n") for i=1:3 for j=1:3 printf("Enter element A(%d,%d):",i,j) A(i,j)=input("") end end disp(A,"The matrix is:") x0=[] disp("-------------------------------------------------------------------------") printf("\nEnter the initial Eigen Vector:\n") for i=1:3 x0(i,1)=input("") end disp(x0,"Initial Eigen Vector") a=max(x0) disp(a,"Initial Largest Eigen Value") disp("-------------------------------------------------------------------------") v=A*x0 i=1 while abs(max(v)-a)>0.002 then printf(" Iteration Number = %d\n",i) i=i+1 a=max(v) disp(a,"Current Eigen Value:") x1=v/a disp(x1,"Current Eigen Vector:") v=A*x1 disp("-------------------------------------------------------------------------") end format('v',5) disp("-------------------------------------------------------------------------") printf(" Iteration Number = %d \n",i) printf(" (Equal Eigen Vectors in iteration number %d and %d)\n",i-1,i) disp("The largest Eigen Value:") disp(max(v)) disp("The largest Eigen Vector:") disp(v/a) disp("-------------------------------------------------------------------------")
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//Example 3.21 //Relaxation Method //Page no. 79 clc;clear;close; A=[10,-2,-2,-6;-1,10,-2,-7;-1,-1,10,-8] deff('y=R(i,x,y,z)','y=A(i,1)*x+A(i,2)*y+A(i,3)*z+A(i,4)') printf('dx\tdy\tdz\tdR1\tdR2\tdR3\n---------------------------------------------') I=eye(3,3) for i=1:3 printf('\n') for j=1:3 printf(' %g\t',I(i,j)) end for j=1:3 printf('%g\t',A(j,i)) end end printf('\n\n\n\n\n xi\tyi\tzi\tR1\tR2\tR3\n---------------------------------------------\n') I1=[0,0,0;0,0,1;0,1,0;1,0,0] for i=1:4 for j=1:3 l=0; for k=1:i l=l+I1(k,j) end I(i,j)=l end end X=eye(1,6)-eye(1,6) for i=1:4 printf('\n') for j=1:3 printf(' %g\t',I1(i,j)) X(j)=X(j)+I1(i,j) end for j=1:3 printf('%g\t',R(j,I(i,1),I(i,2),I(i,3))) if i==4 then X(j+3)=X(j+3)+R(j,I(i,1),I(i,2),I(i,3)) end end end printf('\n---------------------------------------------\n') for i=1:6 printf(' %g\t',X(i)) end printf('\n\n\nHence the solution is \n\t x = %g\n\t y = %g\n\t z = %g',X(1),X(2),X(3))
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//example-4.6 //page no-125 //given //radii of cation and anion in CaO rc=0.94*10^-10 //m ra=1.32*10^-10 //m //so the lattice side will be a=2*(rc+ra) //m //effective no of atoms in FCC lattice structure Ne=4 //because CuO has FCC cubic structure //molecular weight of CuO Aw=40.08+16 //atomic weight unit amu=1.66*10^-27 //amu //mass of atom per unit cell M=Aw*amu //density rho=M*Ne/a^3 //kg/m^3 printf ("density of CuO is 4032 Kg/m^3")
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function [gcd]=gd(n1,n2) if (n1>n2) then (n1==n1, n2==n2) else temp==n1 n1==n2 n2==temp end while((remainder=n1 % n2)!=0) n1==n2 n2==remainder end gcd==n2 endfunction
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// Example 5.23:corner frequency and bandwidth clc; clear; close; tr=16;//rise time in micro second V=100;//voltage in milli volts Vd=90;//voltage in milli volts f=5;//frequecny in killo hertz fh= (0.35/(tr*10^-6))*10^-3;//upper cut off frequency in killo hertz P= ((V-Vd)/V)*100;// fl=(P*10^3*f)/(100*%pi);//lower cut off frequency in hertz BW=(fh*10^3-fl)*10^-3;//bandwith in killo hertz disp(fh,"upper cut off frequency in killo hertz") disp(fl,"lower cut off frequency in hertz") disp(BW,"bandwith in killo hertz")
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//Programming Example 8.5 //read several lines of text & determine the average number of characters per line function[]= mainAvg() global Sum //total number of characters Sum=0 global Lines //total number of lines Lines=0 printf("Enter the text below") //read a line of text and update the cumulative counters //n=number of chars in agiven line //avg=average number of chars per line n=linecount(); //expression can not b evaluated inside while, //hence first calculated outside and used within while() while ( n>0) Sum=Sum+n; Lines=Lines+1; n=linecount(); end avg = Sum/Lines; //average number of characters per line printf("\nAverage number of character per line: %5.2f", avg) endfunction //read a line of text and count the number of charcters function[count]= linecount() count=0 //as the getchar is used to used with while loop to //read character array which is here replced by read command // and the count of characters along with white spaces is made // with the help of length(). s=read(%io(1), 1, 1, '(a)'); if (s == " ") then return; else count=length(s); end endfunction //calling routine mainAvg()
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//Exa 2.9 clc; clear; close; //given data k_in=0.3;// in W/mK k_gw=0.038;// in W/mK ro=1.5;// in cm ho=12;// in W/m^2 degree C rc=k_in/ho;// in m rc=rc*10^2;// in cm disp(rc,"Critical radius in cm") if ro<rc then disp("Since radius of insulation ("+string(ro)+" cm) is less than critical radius of insulation ("+string(rc)+" cm), so heat transfer rate will increase by adding thsi insulation"); disp("and hence it is not effective") end ro=ro*10^-2;// in meter // For effective insulation // ro>=rc // Kin/ho<= ro roho=ro*ho;// in W/mK /// Kin<= ro*ho disp(roho,"Maximum value of thermal conductivity in W/mK")
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//Exa 4.6 clc; clear; close; //Given data : r=2/2;//cm rdash=0.7788*r;//cm d12=0.12*100;//cm d11dash=300;//cm d12dash=sqrt(300^2+100^2);//cm d21dash=d12dash;//cm d22dash=d11dash;//cm d11=rdash;//cm d22=rdash;//cm d12=100;//cm d21=100;//cm Dm=(d11dash*d12dash*d21dash*d22dash)^(1/4);//cm Ds=(d11*d12*d21*d22)^(1/4);//cm L=0.4*log(Dm/Ds);//mH/km disp(L,"Loop inductance of line(mH/km)");
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V_01 ok V_02 ok V_03 ok V_04 ok V_05 ok V_06 ok V_07 ok V_08 ok V_09 ok V_10 ok V_11 no V_12 no V_13 no V_14 ok V_15 ok V_16 ok V_17 ok V_18 no V_19 ok V_20 ok V_21 ok V_22 ok V_23 no V_24 no V_25 ok V_26 ok V_27 ok V_28 no V_29 ok V_30 no V_31 no V_32 no V_33 no V_34 ok V_35 ok V_36 ok V_37 ok D_01 no D_02 no D_03 no D_04 no D_05 ok D_06 no e_01 ok e_02 ok l_01 ok E1_01 ok E1_02 ok E1_03 ok E1_04 ok E2_01 ok E2_02 ok E2_03 ok E2_04 ok E3_01 ok E3_02 no E3_03 ok E3_04 no E3_05 ok E3_06 no E3_07 ok E3_08 ok E3_09 ok E3_10 ok E3_11 ok E3_12 ok E3_13 ok E3_14 no
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clc //initialisation of variables m1= 1 //kg h1= 2967.6 //kJ/kg h2= 83.96 //kJ/kg m2= 10 s1= 7.5166 //kJ/kg K s2= 0.2966 //kJ/kg K s3= 1.1654 //kJ/kg K //CALCULATIONS h3= (m1*h1+m2*h2)/(m1+m2) S= -m1*s1-m2*s2+(m1+m2)*s3 //RESULTS printf (' enthalpy = %.1f kJ/kg',h3) printf (' \n entropy change = %.4f kJ/kg K',S)
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clear ; clc; // Example 2.8 printf('Example 2.8\n\n'); //Page no. 63 // Solution // 1 kg of the air/HCN mixture // (a) m1 = 27.03 ;//[g] m2 = 29.0 ;//[g] cn = (10*m1*1000*1000)/(10^6*m2) ;//[mgHCN/kg air] printf('(a) 10.0 ppm HCN is %.2f mg HCN/kg air.\n',cn); // (b) ld = 300 ;//[mg/kg air] fr = cn/ld; printf(' (b) Fraction of lethal dose is 10.0 ppm is %.3f.',fr);
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//------------------------------------------------------------------------------ // Simule le système avec discrétisation en temps //------------------------------------------------------------------------------ //------------------------------------------------------------------------------ // Simule une trajectoire de l'état du système à l'aide d'une discrétisation en // temps. //------------------------------------------------------------------------------ // // lambda : (reel) Parametre de la loi d'arrivee des paquets // mu : (reel) Parametre de la loi d'envoi des paquets. // tmax : (reel) Temps jusqu'auquel on désire simuler le système. // h : (reel) Pas de la discrétisation en temps. // nbSimulations : (entier) Le nombre de simulations à effectuer // // T : (vecteur ligne) Discrétisation du temps entre 0 et tmax avec un pas h. // X: (matrice) Valeur de l'encombrement aux instants donnés par t. Chaque ligne // correspond à une simulations. // function [T,X]=trajectoireDiscrete2(lambda, mu, tmax, h, nbSimulations) X = zeros(nbSimulations, 1) T = zeros(nbSimulations, 1) F = ones(nbSimulations, 1) Ones = ones(nbSimulations, 1) n = 1000 while or(F) j = 1 T1 = h*grand(nbSimulations, n, 'geom', lambda*h) T2 = h*grand(nbSimulations, n, 'geom', (lambda+mu)*h) U = grand(nbSimulations, n, 'def') e = 1*(U<=lambda/(lambda+mu)) + (-1)*(U>lambda/(lambda+mu)) while or(F) & (j<=n) T = [T, T(:,$) + (T1(:,j).*(X(:,$)==0) + T2(:,j).*(X(:,$)>0))] X = [X, X(:,$) + ((Ones.*(X(:,$)==0)) + e(:,j).*(X(:,$)>0))] F = T(:,$)<tmax j = j+1 end end endfunction [t,X] = trajectoireDiscrete2(0.36, 0.4,2000,1, 1) plot2d(t,X, style=[color('red')])
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clc clear //Input data p1=1//Inlet pressure in bar p2=32.425//Pressure at the end of isentropic compression in bar r=6//Ratio of expansion r1=1.4//Isentropic index //Calculations rc=(p2/p1)^(1/r1)//Compression ratio b=(rc/r)//cut-off ratio n=(1-((b^r1-1)/(rc^(r1-1)*r1*(b-1))))*100//Air-standard efficiency pm=((p1*rc^r1*n/100*r1*(b-1))/((r1-1)*(rc-1)))//Mean effective pressure in bar //Output printf('Air-standard efficiency is %3.2f percent \n Mean effective pressure is %3.3f bar',n,pm)
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Tint 255 0 0 0 Label Here1 TintAlphaChange 100 0.5 Linear Wait 0.5 TintAlphaChange 0 0.5 Linear Wait 0.5 Goto Here1
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## Test for correct side effects of lightweight tag deletion. read <lighttag.fi tag first-tag delete write -
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//Exa 4.5 clc; clear; close; disp("The given circuit is basically an inverting amplifier with node A at virtual ground. Writing KCL at node A yields "); disp("I1+I2=If"); disp("-2/10Kohm+3/20Kohm=-Vo/100Kohm"); Vo=-(-20+15);//in Volts disp(Vo,"Output voltage in Volt is : ")
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function Res = min_bd_rastrigin() Res = [-1 -1]'; endfunction
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//CHAPTER 3- THREE-PHASE A.C. CIRCUITS //Example 3 clc; disp("CHAPTER 3"); disp("EXAMPLE 3"); //VARIABLE INITIALIZATION r_ph=30; //resistance of coils in Ohms l=0.07; //inductance of coils in Henry v_l=400; //line voltage in Volts f=50; //frequency in Hertz //SOLUTION //solution (a) x_ph=2*(%pi)*f*l; //inductive reactance z_ph=sqrt((r_ph^2)+(x_ph^2)); I_ph=v_l/z_ph; //phase voltage = line voltage for delta connection disp(sprintf("(a) The phase current is %f A",I_ph)); //solution (b) I_l=sqrt(3)*I_ph; //phase current = (line current)/sqrt(3) for delta connection disp(sprintf("(b) The line current is %f A",I_l)); //solution (c) pow_fact=r_ph/z_ph; disp(sprintf("(c) The power factor is %f (lagging)",pow_fact)); //solution (d) p=sqrt(3)*v_l*I_l*pow_fact; disp(sprintf("(d) The power absorbed is %f W",p)); //Answer is different due to precision of floating point numbers //END
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function d=%spb_diag(a,k) // g_diag - implement diag function for sparse matrix, rational matrix ,.. // Copyright INRIA [lhs,rhs]=argn(0) if rhs==1 then k=0,end [ij,v,sz]=spget(a) m=sz(1);n=sz(2) if m>1&n>1 then l=find(ij(:,1)==(ij(:,2)-k)) if k<=0 then mn=mini(m,n-k) else mn=min(m+k,n) end kk=abs(k) d=sparse([ij(l,1),ones(ij(l,1))],v(l),[mn,1]) else nn = max(m,n)+abs(k) if ij==[] then d=sparse([],[],[nn,nn]) else d=sparse([ij(:,1),ij(:,1)+k],v,[nn,nn]) end end
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clear; clc; close; Vcc = 16; Vbe = 0.7; Vt = 26*(10^(-3)); R1 = 90*(10^(3)); R2 = 10*(10^(3)); Re = 0.68*(10^(3)); Rc = 2.2*(10^(3)); ro = 50*(10^(3)); Beta = 210; Vb = (R2/(R1+R2))*Vcc; Ve = Vb - Vbe; Ie = Ve/Re; re = Vt/Ie; disp(re,"Value of diode resistive element is(in ohms) :"); Rb = (R1*R2)/(R1+R2); Zb = Beta*Re; Zi = (Rb*Zb)/(Rb+Zb); disp(Zi,"Input Impedance(ohms) :"); Zo = Rc; disp(Zo,"Output Impedance(ohms) :"); Av = -Rc/Re; disp(Av,"Voltage gain :");
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// Scilab Code Ex5.10 Determining resolved componet of shearing force in a given direction: Page-168 (2010) h1 = 1; k1 = 1; l1 = 1 // Miller indices for first set of planes h2 = 1; k2 = 1; l2 = 0; // Miller indices for second set of planes F_111 = 660; // Shearing force along [111] direction, N cos_theta = (h1*h2+k1*k2+l1*l2)/(sqrt(h1^2+k1^2+l1^2)*sqrt(h2^2+k2^2+l2^2)); // Cosine of angle between [1 -1 0] and [100] directions // As F_110/F_111 = cos_theta, solving for F_110 F_110 = F_111*cos_theta; // Resolved component of shearing force along [110] direction, N printf("\nThe resolved component of shearing force along [110] direction, F_110 = %3d N", F_110); // Result // The resolved component of shearing force along [110] direction, F_110 = 538 N
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[Bus1] BusNumber = "1" EvtPluginINIFilePath = "EventFromCSVPlugin/EventFromCSVPlugin.ini" EvtParams.<size(s)> = "1 1" EvtParams 0 = "C:\Projects\PARTF\trunk\Framework\Applications\AppPlugins\Mathscript\Ringdown\RealEvent_case1_1pmus.csv" EvtConfig.UTC Time 0 = "\00\00\00\00\00\00\00\00\00\00\00\00\00\00\00\00" EvtConfig.Nominal Frequency = "60" EvtConfig.Reporting Rate = "60" EvtConfig.Fsamp = "960" EvtConfig.PosSeq = "FALSE" Start Time = "0" End Time = "8.2" PmuImpairPluginINIFilePath = "NoPmuImpairPlugin/NoPmuImpairPlugin.ini" PmuImpairParams .<size(s)> = "0 0" PmuImpairConfig.FilterType = "Blackman" PmuImpairConfig.bPosSeq = "FALSE" NetImpPluginINIFilePath = "NetworkPluginNone/NetworkPluginNone.ini" NetImpParams.<size(s)> = "0 0" FlagImpPluginINIFilePath = "NoFlagImpairPlugin/NoFlagImpairPlugin.ini" FlagImpParams.<size(s)> = "0 0" [AppData] AppData.AppPluginIniFilePath = "RingdownPlugin/RingdownPlugin.ini" AppData.Config = "<Cluster>\0D\0A<Name>Accessors:RingdownConfig</Name>\0D\0A<NumElts>5</NumElts>\0D\0A<Cluster>\0D\0A<Name>Config</Name>\0D\0A<NumElts>12</NumElts>\0D\0A<I32>\0D\0A<Name>Addmod</Name>\0D\0A<Val>-1</Val>\0D\0A</I32>\0D\0A<I32>\0D\0A<Name>Scalmod</Name>\0D\0A<Val>0</Val>\0D\0A</I32>\0D\0A<I32>\0D\0A<Name>Lpocon</Name>\0D\0A<Val>-1</Val>\0D\0A</I32>\0D\0A<I32>\0D\0A<Name>Pircon</Name>\0D\0A<Val>-1</Val>\0D\0A</I32>\0D\0A<I32>\0D\0A<Name>Dmodes</Name>\0D\0A<Val>0</Val>\0D\0A</I32>\0D\0A<U16>\0D\0A<Name>Lpmcon</Name>\0D\0A<Val>3</Val>\0D\0A</U16>\0D\0A<U16>\0D\0A<Name>Lpacon</Name>\0D\0A<Val>1</Val>\0D\0A</U16>\0D\0A<U16>\0D\0A<Name>Fbcon</Name>\0D\0A<Val>1</Val>\0D\0A</U16>\0D\0A<I32>\0D\0A<Name>Ordcon</Name>\0D\0A<Val>1</Val>\0D\0A</I32>\0D\0A<DBL>\0D\0A<Name>Trimre</Name>\0D\0A<Val>-1.00000000000000</Val>\0D\0A</DBL>\0D\0A<DBL>\0D\0A<Name>Ftrimh</Name>\0D\0A<Val>-1.00000000000000</Val>\0D\0A</DBL>\0D\0A<DBL>\0D\0A<Name>Ftriml</Name>\0D\0A<Val>-1.00000000000000</Val>\0D\0A</DBL>\0D\0A</Cluster>\0D\0A<Cluster>\0D\0A<Name>Window</Name>\0D\0A<NumElts>3</NumElts>\0D\0A<I32>\0D\0A<Name>StOffset</Name>\0D\0A<Val>0</Val>\0D\0A</I32>\0D\0A<I32>\0D\0A<Name>EndOffset</Name>\0D\0A<Val>10000</Val>\0D\0A</I32>\0D\0A<I32>\0D\0A<Name>Length</Name>\0D\0A<Val>0</Val>\0D\0A</I32>\0D\0A</Cluster>\0D\0A<I32>\0D\0A<Name>V index</Name>\0D\0A<Val>0</Val>\0D\0A</I32>\0D\0A<I32>\0D\0A<Name>I index</Name>\0D\0A<Val>3</Val>\0D\0A</I32>\0D\0A<Boolean>\0D\0A<Name>PosSeq</Name>\0D\0A<Val>0</Val>\0D\0A</Boolean>\0D\0A</Cluster>\0D\0A" [OutToFileConfig] OutToFileConfig.OutputToFilePluginINIFilePath = "OutputToFileBasePlugin/OutputToFileBasePlugin.ini" OutToFileConfig.Output File Path = "Output" OutToFileConfig.clConfigOptions.TIME_BASE = "\00\00\00\00\00\0FB@" OutToFileConfig.clConfigOptions.STN = "Bus_1" OutToFileConfig.clConfigOptions.IDCODE = "0" OutToFileConfig.clConfigOptions.rdoPolRect = "Rectangular" OutToFileConfig.clConfigOptions.rdoFloatInt = "Float" OutToFileConfig.clConfigOptions.PHUNIT = "\00\00\00\00\00\0FB@" OutToFileConfig.clConfigOptions.rdoFreqDfreq = "Float" OutToFileConfig.clConfigOptions.CHNAM.<size(s)> = "8" OutToFileConfig.clConfigOptions.CHNAM 0 = "VA" OutToFileConfig.clConfigOptions.CHNAM 1 = "VB" OutToFileConfig.clConfigOptions.CHNAM 2 = "VC" OutToFileConfig.clConfigOptions.CHNAM 3 = "V+" OutToFileConfig.clConfigOptions.CHNAM 4 = "IA" OutToFileConfig.clConfigOptions.CHNAM 5 = "IB" OutToFileConfig.clConfigOptions.CHNAM 6 = "IC" OutToFileConfig.clConfigOptions.CHNAM 7 = "I+" OutToFileConfig.clConfigOptions.chkCfg2Prefix = "TRUE"
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// Ex5_12 clc; // Given: w=0.1189; flux=10^16; // Solution: A=w/(flux*3.16*10^7);// in m^2 A1=A*10000/(10^-24);// in Barns printf("The cros section area is = %d b", A1)
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//ques4 clear clc disp('See figure in question'); disp('using numerical poissons equation u(i-1)(j)+u(i+1)(j)+u(i)(j-1)+u(i)(j+1)=h^2f(ih,jh)'); disp('Here f(x,y)=-10(x^2+y^2+10'); disp('Here for u1 i=1,j=2 putting in equation this gives : '); disp('u1=1/4(u2+u3+150'); disp('similarly '); disp('u2=1/4(u1+u4+180'); disp('u3=1/4(u1+u4+120'); disp('u4=1/4(u2+u3+150'); disp('reducing therse equations since u4=u1'); disp('4u1-u2-u3-150=0'); disp('u1-2u2+90=0'); disp('u1-2u3+60=0'); disp('Solvng these equations by Gauss jordon method '); A=[4 -1 -1;1 -2 0;1 0 -2]; r=[150;-90;-60]; D=A;d=r; n=3; //create upper triangular matrix s=0; for j=1:n-1 if A(j,j)==0 k=j; for k=k+1:n if A(k,j)==0 continue end break end B=A(j,:); C=r(j); A(j,:)=A(k,:); r(j)=r(k); A(k,:)=B; r(k)=C; end for i=1+s:n-1 L=A(i+1,j)/A(j,j); A(i+1,:)=A(i+1,:)-L*A(j,:); r(i+1)=r(i+1)-L*r(j); end s=s+1; end //Solution of equations x(n)=r(n)/A(n,n); for i=n-1:-1:1 sum=0; for j=i+1:n sum=sum+A(i,j)*x(j); end x(i)=(1/A(i,i))*(r(i)-sum); end //hecking with scilab functions p=inv(D)*d; //Output disp('@----------------------------------------------------------@') disp('Output [B][x]=[b]') disp('Upper riangular Matrix [B] =');disp(A) disp('Matrix [b] =');disp(r) disp('solution of linear equations :');disp(x')
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function [stk,txt,top]=sci_cumsum() // Copyright INRIA txt=[] if stk(top-rhs+1)(5)=='4' then v='bool2s('+stk(top-rhs+1)(1)+')', else v=stk(top-rhs+1)(1), end if rhs==1 then [m,n]=checkdims(stk(top)) x=stk(top)(1) if m==-1&n==-1 then set_infos([ 'mtlb_cumsum('+x+') may be replaced by ' 'cumsum('+x+')'+' if '+x+'is a vector' 'cumsum('+x+',1)'+' if '+x+'is a matrix'],1) stk=list('mtlb_cumsum('+x+')','0','?','?','1') elseif m==1|n==1 then stk=list('cumsum('+x+')','0','1','1','1') else stk=list('cumsum('+x+',1)','0','1',stk(top)(4),'1') end else if stk(top)(1)=='1' then stk=list('cumsum('+v+',1)','0','1',stk(top-1)(4),stk(top-1)(5)) elseif stk(top)(1)=='2' then stk=list('cumsum('+v+',2)','0',stk(top-1)(3),'1',stk(top-1)(5)) else x=stk(top)(1) stk=list('cumsum('+v+','+x+')','0','?','?',stk(top-1)(5)) end top=top-1 end
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(set-sequence-operator-recognition FALSE) (set-dynamic-constraint-checking FALSE) (set-strategy depth) (unwatch all) (watch rules) ; mab.clp test (clear) (open "example.rsl" example "w") (load "compline.clp") (load "mab.clp") (reset) (progn (dribble-on "mab.out") (run) (dribble-off)) (printout example "mab.clp differences are as follows:" crlf) (compare-files mab.exp mab.out example) ; dilemma1.clp test (clear) (load "compline.clp") (load "dilemma1.clp") (reset) (progn (dribble-on "dilemma1.out") (run) (dribble-off)) (printout example "dilemma1.clp differences are as follows:" crlf) (compare-files dilemma1.exp dilemma1.out example) ; dilemma2.clp test (clear) (load "compline.clp") (load "dilemma2.clp") (reset) (watch deffunctions) (progn (dribble-on "dilemma2.out") (run) (dribble-off)) (unwatch deffunctions) (printout example "dilemma2.clp differences are as follows:" crlf) (compare-files dilemma2.exp dilemma2.out example) ; wordgame.clp test (clear) (load "compline.clp") (load "wordgame.clp") (reset) (progn (dribble-on "wordgame.out") (run) (dribble-off)) (printout example "wordgame.clp differences are as follows:" crlf) (compare-files wordgame.exp wordgame.out example) ; zebra.clp test (clear) (load "compline.clp") (load "zebra.clp") (reset) (progn (dribble-on "zebra.out") (run) (dribble-off)) (printout example "zebra.clp differences are as follows:" crlf) (compare-files zebra.exp zebra.out example) ; electronic.clp test (clear) (set-strategy mea) (load "compline.clp") (load "electrnc.clp") (load "circuit3.clp") (reset) (progn (dribble-on "electrnc.out") (run) (dribble-off)) (printout example "electronic.clp differences are as follows:" crlf) (compare-files electrnc.exp electrnc.out example) ; object monkeys & bananas test (set-strategy depth) (watch rules) (clear) (setgen 1) (load "compline.clp") (load "mabobj.clp") (reset) (progn (dribble-on "mabobj.out") (run) (dribble-off)) (printout example "mabobj.clp differences are as follows:" crlf) (compare-files mabobj.exp mabobj.out example) ; object farmer's dilemma example (clear) (setgen 1) (load "compline.clp") (load "objfarm.clp") (reset) (progn (dribble-on "objfarm.out") (run) (dribble-off)) (printout example "objfarm.clp differences are as follows:" crlf) (compare-files objfarm.exp objfarm.out example) ; object wordgame example (clear) (setgen 1) (load "compline.clp") (load "wrdgmobj.clp") (reset) (progn (dribble-on "wrdgmobj.out") (run) (dribble-off)) (printout example "wrdgmobj.clp differences are as follows:" crlf) (compare-files wrdgmobj.exp wrdgmobj.out example) ; close result file (unwatch all) (set-strategy depth) (close example)
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//Author: Parthasarathi Panda //parthasarathipanda314@gmail.com //Convert digital filter second-order section parameters to state-space form //Calling Sequence //[A,B,C,D] = sos2ss(sos) //[A,B,C,D] = sos2ss(sos,g) // //sos2ss converts a second-order section representation of a digital filter to an equivalent state-space representation. //A,B,C,D:Steady state parameters //sos:6 column second order section matrix //g:gain //EXAMPLES: //sos = [1 1 1 1 0 -1 ; // -2 3 1 1 10 1]; //[A,B,C,D] = sos2ss(sos,2); // //EXPECTED OUTPUT: //D =- 4. //C =42. 4. - 32. - 2. //B =[1. 0. 0. 0. 0.]' //A =[- 10. 0. 10. 1. ; 1. 0. 0. 0. ; 0. 1. 0. 0. ; 0. 0. 1. 0. ] function [A,B,C,D]=sos2ss(sos,g) [nargout,nargin]=argn(); if nargin==1 then g=1; end if type(sos)~=1 | type(g)~=1 then error('check the data type of input'); //to check if the inputs are real/complex arrays end if size(g)~=[1,1] then error('check the data type of input'); //to check that n is single dimensional end //checking if sos is a 6 column matrix [d,j]=size(sos); if j~=6 then error('sos should be a 6-column matrix'); end num=[1]; den=[1]; //convolving the numerator and denominator to get the coefficient of the numerator and the denominator at the top and bottom for i=[1:d] num=convol(num,sos(i,1:3)); den=convol(den,sos(i,4:6)); end t=2*d+1; //polynomial degree must be defined here if den(t)==0 then error('improper transfer function check input'); end // t=2*d+1; //polynomial degree A=zeros(t-1,t-1); if t>2 then A(2:(t-1),1:(t-2))=eye(t-2,t-2); end A(1,:)=-1*den(2:t)/den(1); B=zeros(t,1); B(1)=1/den(1); //constructing (A,B) in canonical controllable form C=g*(num(2:t)-den(2:t)*num(1)/den(1));//appropiate C and D D=g*num(1)/den(1); endfunction
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clf(); clc //Chapter3: Modulation //Example3.11, page no 144 //Given deff("[y]=f(x)","y=Ec*(1+ma*(sin(wm*x)))*sin(wc*x)") Ec=10,ma=0.5,wm=10000*%pi,wc=2*%pi*1e7 x=[0:0.01:20]*%pi/10; subplot(2,1,1) fplot2d(x,f) xlabel("t", "fontsize", 3); ylabel("Modulated Wave", "fontsize", 3, "color", "red"); Fc=wc/(2*%pi) Fm=wm/(2*%pi) Fusb=(wm+wc)/(2*%pi) Flsb=(wm-wc)/(2*%pi) mprintf('USB freq=%d k5Hz\nUSB amplitude=%f V\nLSB freq=%d kHz\nLSB amplitude=%f V\nCarrier amplitude=%d V',Fusb*1e-3,2.5,Flsb*-1e-3,2.5,10) F=[0,2.5,10,2.5,0] T=[-2,-1,0,1,2] subplot(2,1,2) plot2d3(T,F,5) xlabel("Freq", "fontsize", 3); ylabel("Amplitude", "fontsize", 3, "color", "blue"); xlabel("fc-fm fc fc+fm", "fontsize", 2);
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//example 9.5 clc;funcprot(0); //Initialization of Variable I=22.6;//current V=120;//voltage Id=28;//A Vd=280;//V //calculation P=3*I*V; disp(P/1000,"total power in kW:") Pl=Id*Vd; disp(Pl/1000,"load power in kW:") Pf=Pl/P; disp(Pf,"power factor:") clear()
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// Example 1.7, page no-55 clear clc E_rec_pyro=0.95*0.85 T=1100/E_rec_pyro printf("Pyrometer reading T = %.2f°C",T)
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//Compression ratio r=6; //Ratio specific heats for air y=1.4; //Pressure at beginning of compression(in bar) p1=1; //Temperature at beginning of compression(in K) T1=27+273; //Heat added during the constant volume combustion process(in kJ/kg) qs=1170; //Specific heat at constant volume(in kJ/kgK) Cv=0.717;
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<?xml version="1.0" encoding="utf-8" ?> <test> <description>Structured grid generation from NekMesh wrapper</description> <executable python="true">StructuredGrid.py</executable> <parameters> 5 6 0.0 1.0 2.0 3.0 2 Quad output.xml </parameters> <files /> <metrics> <metric type="regex" id="1"> <regex>^.*Total negative Jacobians: (\d+)</regex> <matches> <match> <field id="0">0</field> </match> </matches> </metric> </metrics> </test>
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function eyes(result,L,Na) N=length(result); tt=0:1:Na*L; set(gca(),"auto_clear","off"); for jj=1:Na*L:N-Na*L plot(tt,result(jj:jj+Na*L)); end set(gca(),"auto_clear","on"); endfunction
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// Program to demonstarte usage of comet x=linspace(-%pi,%pi,500); comet(x,%s^5-%s^3+%s+5) xtitle('Using comet function to animate an equation') xlabel('x') ylabel('y')
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clc // Example 3.10.py // In example 3.9, how much heat per unit mass must be added to choke the flow// // Variable declaration from example 3.9 To1 = 840 // upstream total temperature (in K) M1 = 3.0 // upstream mach number To1_by_Tostar = 0.6540 // To1/Tostar from Table A3 cp = 1004.5 // specific heat at constant pressure for air (in J/Kg K) // Calculations Tostar = To1 / To1_by_Tostar // Tostar = To1 * Tostar/To1 (in K) M2 = 1.0 // for choked flow To2 = Tostar // since M2 = 1.0 q = cp * (To2 - To1) // required heat = cp(To2 - To1) (in J/kg) // Result printf("\n Heat require to choke the flow is %.2e J/kg", q)
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clear all; clc; fileName='e:\corr_out.csv'; [fd, err] = mopen(fileName, 'rt'); s = mgetl(fd); [Ie s] = strtod(s); [Qe s] = strtod(s); [Ip s] = strtod(s); [Qp s] = strtod(s); [Il s] = strtod(s); [Ql s] = strtod(s); [cross s] = strtod(s); [dot s] = strtod(s); [freqErr s] = strtod(s); [carrErr s] = strtod(s); [codeErr s] = strtod(s); carrFreq = strtod(s); mclose(fd); plot(Ie, 'r'); plot(Qe, 'b'); plot(Ip, 'g'); plot(Qp, 'c'); plot(Il, 'y'); plot(Ql, 'm'); // figure; // plot(dot, 'r'); // plot(cross, 'b'); // // figure; // plot(freqErr, 'b'); // // figure; // plot(carrErr, 'b'); // // figure; // plot(codeErr, 'b');s // // figure; // plot(freqErr, 'r'); // plot(dot, 'g'); // plot(cross, 'b');
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w=24; q=0.2; v=w/q; disp("the potential difference (in V) is "); disp(v);
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clc clear printf("example 3.18 page number 108\n\n") //to find the temperature of combustion H_combustion = 1560000 //in kJ/kmol H0_CO2 = 54.56 //in kJ/kmol H0_O2 = 35.2 //in kJ/kmol H0_steam = 43.38 //in kJ/kmol H0_N2 = 33.32 //in kJ/kmol t = H_combustion/(2*H0_CO2+3*H0_steam+0.875*H0_O2+16.46*H0_N2); printf("theoritical temperature of combustion = %f degree C",t)
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*Testcase CBUC (Concurrent Block Update Consistency) defsym testdur 10 # (maximum test duration in seconds) mainsize 1 numcpu 2 sysclear archlvl z/Arch loadcore "$(testpath)/CBUC.core" script "$(testpath)/CBUC.subtst" & # ('&' = async thread!) runtest 300 # (subtst will stop it) *Done numcpu 1 # (reset back to default)
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Ex11_6.sce
//Fluid Systems - By - Shiv Kumar //Chapter 11- Centrifugal Pumps //Example 11.6 //To Calculate the Blade angle at Outlet, Power Required and Overall Efficiency of Pump. clc clear //Given Data:- Do=80; //Outer Diameter of the Impeller, cm Q=1; //Discharge, m^3/s H=80; //Head, m N=1000; //Speed, rpm bo=8; //Width at Outlet, cm Delta_Q_per=3; //Percentage of Leakage Loss(of the Discharge) Delta_P=10; //Mechanical Loss, kW eta_H=80/100; //Hydraulic Efficiency //Data Used:- rho=1000; //Density of water, kg/m^3 g=9.81; //Acceleration due to gravity, m/s^2 //Computations:- Do=Do/100; //m bo=bo/100; //m uo=%pi*Do*N/60; //m/s Vfo=Q/(%pi*Do*bo); //m/s Vwo=g*H/(uo*eta_H); //m/s Vrwo=uo-Vwo; //m/s //(a) beta_o=atand(Vfo/Vrwo); //Blade Angle at Outlet, degrees //Result1 printf(" Blade Angle at Outlet, beta_o=%.2f Degrees \n",beta_o) //The answer vary due to round off error //(b)Power Required Pi=rho*(1+Delta_Q_per/100)*Q*Vwo*uo; //Power delivered by the Impeller, W P=Pi/1000+Delta_P; //Power required, kW //Result2 printf(" Power Required, P =%.3f kW \n",P) //The answer vary due to round off error //(c)Overall Efficiency, eta_o eta_V=1/(1+Delta_Q_per/100); //Volumetric Efficiency eta_m=(P-Delta_P)/P; //Mechanical Efficiency eta_o=eta_H*eta_V*eta_m*100; //In Percentage //Result3 printf(" Overall Efficiency, eta_o =%.2f Percent \n",eta_o) //The answer vary due to round off error //Also, Overall Efficiency eta_o=rho*Q*g*H/(P*1000)*100; //In Percentage printf("Also, Overall Efficiency, eta_o=%.2f Percent\n",eta_o)
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ampmod.sci
function[x,Vm,Vc]=ampmod(Ec,Em,fm,fc,fs) //Ec -carrier amplitude in volts //Em - message signal amplitude in volts //fm - modulating signal frequency Hz //fc - carrier signal frequency in Hz //fs - sampling frequency in samples/sec t = 0:1/fs:1; Vm = Em*sin(2*%pi*fm*t); Vc = Ec*sin(2*%pi*fc*t); x = (Ec+Em*sin(2*%pi*fm*t)).*(sin(2*%pi*fc*t)); subplot(3,1,1) plot(Vm) title('Modulating Signal') subplot(3,1,2) plot(Vc) title('Carrier Signal') subplot(3,1,3) plot(x); title('Amplitude Modulated Signal') endfunction //Example //Em = 8; //8 volts //Ec = 10; //20 volts //fm = 2; //2 Hz //fc = 10; //10 Hz //fs = 100; samples/sec //ampmod(Ec,Em,fm,fc,fs)
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ex7.sce
//example 7 //determining the pressure of water clear clc vg=0.12736 //specific volume in m^3/kg for water at 200C v=0.4 //specific volume in m^3/kg P1=500 //in kPa v1=0.42492 //specific volume at P1 in m^3/kg P2=600 //in kPa v2=0.35202 //specific volume at P2 in m^3/kg P=P1+(P2-P1)*(v-v1)/(v2-v1) //calculating pressure by interplotation disp('hence,the pressure of water is 534.2 kPa')
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Chapter2_Example37.sce
//Chapter-2, Example 2.37, Page 2.68 //============================================================================= clc clear //INPUT DATA nFL=0.98;//Efficiency of transformer at full load 0.8 power factor upf=0.99;//Efficiency of the transformer at half load Q=500;//Transformer rating in KVA cosq=0.8;//Power facotor //CALCULATIONS L=((Q*1000*cosq)/nFL)-(Q*1000*cosq);//Full load losses in W L2=((0.5*Q*1000*100)/99)-(0.5*Q*1000);//Half load losses in W A=[0.25,0.25; 1,0.25] B=[(0.25*L); L2] A=inv(A)*B;//Soving for Pi and Pc //OUTPUT mprintf('Constant losses are %3.2f W\nFull load copper losses are %3.2f W',A(1),A(2)) //=================================END OF PROGRAM==============================
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exa7_1.sce
// Example 7-1 // Steady state sinusoidal output clear; clc; xdel(winsid()); //close all windows // please set the path // cd "/<your code directory>/" // exec("plotresp.sci") s = %s; w = 1; K = 5; T = 0.1; G = syslin('c',K,T*s + 1); t = 0:0.1:20; u = sin(w*t); plotresp(u,t,G,'Response to sinusoidal input'); // as T*w is small amplitude of output is ~ K (5)
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B_7.sce
// sum 23-7 clc; clear; Vi=20*5/18; Vf=0; m=80; pmax=1; u=0.1; S=50; KE=0.5*m*Vi^2; N=KE/(u*S*2); t=sqrt(N/(pmax*3)); b=3*t; // printing data in scilab o/p window printf("KE is %0.1f Nm ",KE); printf("\n N is %0.2f N ",N); printf("\n t is %0.1f mm ",t); printf("\n b is %0.1f mm ",b); //The difference in the answers are due to rounding-off of values.
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Ex6_3.sce
clear; clc; //Example 6.3 Vdd=10; R1=70.9;//(Kohm) R2=29.1;//(Kohm) Rd=5;//(Kohm) Vtn=1.5; Kn=0.5;//(mA/V^2) //lambda=y y=0.01;//V^-1 Rsi=4;//(Kohm) Vgsq=Vdd*R2/(R1+R2); printf('\ngate to source voltage=%.2f V\n',Vgsq) Idq=Kn*(Vgsq-Vtn)^2; printf('\ndrain current=%.3f mA\n',Idq) Vdsq=Vdd-Idq*Rd; printf('\ndrain to source voltage=%.2f V\n',Vdsq) g_m=2*Kn*(Vgsq-Vtn); printf('\ntransconductance=%.3f mA/V\n',g_m) ro=(y*Idq)^-1; printf('\noutput resistance=%.2f KOhm\n',ro) Ri=R1*R2/(R1+R2); printf('\namplifier input resistance=%.2f Kohm\n',Ri) Av=-g_m*(ro*Rd/(ro+Rd))*Ri/(Ri+Rsi); printf('\nsmall signal voltage gain=%.2f\n',Av) printf('\namplifier input resistance=%.2f Kohm\n',Ri) Ro=Rd*ro/(Rd+ro); printf('\namplifier output resistance=%.2f Kohm\n',Ro)
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Ex_9_1.sce
// Example 9.1;//quantum efficiency clc; clear; close; re=4.2*10^6;// Average no. of electron hole pair generated rp=6*10^6;//no. of photons h=1200;//wavelength in nano meter n=round((re/rp)*100);//quantum efficiency disp(n,"quantum efficiency is")