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//Example 2-2// //Binary to Decimal Conversion// a=bin2dec('1011101001') //Decimal equivalent of the binary number// disp(a) //answer in decimal form//
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//Exa 6.12 clc; clear; close; //given data : format('v',5); ETAext=1.5;//in % I=25;//in mA V=4;//in Volt F=0.8;//Transmission factor at crystal-air interface nm=3.6;//refractive index of GaAs;unitless n=1;//refractive index of air ;unitless disp("ETAext=Pint*100*F*n^2/(4*P*nm^2)"); //P=V*I Pint=(ETAext*4*V*I*10^-3*nm^2)/(F*100);//in watts disp(Pint*1000,"Optical power generated in the device in mWatts : ");
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clear; clc; printf("\t Example 5.3 "); //Assumption: Resistance force F on an isolated sphere is given by Stoke's law:F = 3*%pi(meu)d*u C = poly([0],'C'); x=roots(-4.8*C+(1-C)); printf("\n concentration is:%.3f",x); //terminal falling velocity u can be calculated by force balance //u = d^2*g/(18*meu)*(ps-p) function[u]=terminal_velocity() d = 10^(-4); //diameter is in meters g = 9.81; //acceleration due to gravity is in m/sec^2 meu = 10^(-3); //viscosity is in N.s/m^2 ps = 2600; //density is in kg/m^3 p = 1000; //density is in kg/m^3 u = (d^2)*g*(ps-p)/(18*meu); funcprot(0); endfunction function[si]=si_max() u=terminal_velocity() printf("\n The terminal falling velocity is %.5f m/sec",u); si=u*x*(1-x)^(4.8); funcprot(0); endfunction si = si_max(); printf("\nThe maximum value is %f*10^(-4) m^3/m^2sec",si*10^4)
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function [expfre]=unifit(x, obsfre) n=length(x)-1; N=sum(obsfre); xbar=sum(x*obsfre')/N; prob(1)=1/(n+1); for r=0:n prob(r+1)=1/(n+1); end expfre=round(prob*N); printf('expected frequencies\n'); printf('------------------------------\n'); return(expfre); endfunction x=[0,1,2,3,4,5]; obsfre=[12,50,100,80,45,5]; unifit(x,obsfre)
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// Scilab Code Ex12.2 Rate of fission of U-235: Pg:246 (2008) e = 1.6e-019; // Energy equivalent of 1 eV, J/eV E1 = 32e+06; // Energy released per second, J E2 = 200e+06; // Energy released per fission, J N = E1/E2; // Number of atoms undergoing fission per second printf("\nThe number of atoms undergoing fission per second = %1.0e", N/e); // Result // The number of atoms undergoing fission per second = 1e+018
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//Example 32.3 m_prod=94.919388+139.921610+3*(1.008665);//Total mass of products (Sr 95, Xe 140, n)(u) delta_m=238.050784-m_prod;//Mass lost (u) E=delta_m*931.5;//Energy released (MeV) //E=delta_m*(931.5MeV/c^2)/u*c^2 printf('Energy released = %0.1f MeV',E) //Openstax - College Physics //Download for free at http://cnx.org/content/col11406/latest
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//Example 7_5 clc(); clear; //To find the angular acceleration and angular velocity of one wheel vtf=20 //units in meters/sec r=0.4 //units in meters wf=vtf/r //units in rad/sec vf=20 //units in meters/sec v0=0 //units in meters/sec^2 t=9 //units in sec a=(vf-v0)/t //units in meters/sec^2 alpha=a/r //units in rad/sec^2 printf("Angular accelertion is a=%.2f meters/sec^2\n",a) printf("Angular velocity is alpha=%.2f rad/sec^2",alpha)
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//Chapter 14 //Example 14_3 //Page 360 clear;clc; r=0.1; x=0.15; Vb=200+%i*0; i1=100; pf2=0.8; i2=100; pf1=0.6; z=r*2+%i*x*2; Zam=z/2; Zmb=z/2; printf("Impedance of distributor/km = %.2f+j(%.2f) ohm \n\n", real(z), imag(z)); printf("Impedance of section AC = Zac = %.2f+j(%.2f) ohm \n", real(Zam), imag(Zam)); printf("Impedance of section CB = Zcb = %.2f+j(%.2f) ohm \n\n\n", real(Zmb), imag(Zmb)); //part 1 I2=i2*(pf2-%i*sin(acos(pf2))); printf("(i)Load current at point B = %.2f+j(%.2f) A \n", real(I2), imag(I2)); Imb=I2; printf("Current in section MB = %.2f+j(%.2f) A \n", real(Imb), imag(Imb)); Vmb=Imb*Zmb; printf("Voltage drop in section MB = %.2f+j(%.2f) A \n", real(Vmb), imag(Vmb)); Vm=Vb+Vmb; printf("Voltage at point M = %.2f+j(%.2f) \n", real(Vm), imag(Vm)); printf("Magnitude of Vm = %.2f V \n", abs(Vm)); alpha=atan(imag(Vm)/abs(Vm)); printf("Phase angle between Vm and Vb = %.2f degrees \n\n\n", alpha*180/%pi); //part 2 phi1=acos(pf1)-alpha; printf("Phase angle between I1 and Vb = %.2f degrees \n", phi1*180/%pi); I1=i1*(cos(phi1)-%i*sin(phi1)); printf("(ii)Load current at point M = %.2f+j(%.2f) A \n", real(I1), imag(I1)); Iam=I1+I2; printf("Current in section AM = %.2f+j(%.2f) A \n", real(Iam), imag(Iam)); Vam=Iam*Zam; printf("Voltage drop in section AM = %.2f+j(%.2f) A \n", real(Vam), imag(Vam)); Va=Vm+Vam; printf("Sending end voltage = %.2f+j(%.2f) \n", real(Va), imag(Va)); printf("Magnitude of sending end voltage = %.2f V \n\n\n", abs(Va)); pd=atan(imag(Va)/abs(Va)); printf("(iii)The phase difference between Va and Vb = %.2f degrees \n\n", pd*180/%pi);
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[DTR-index-test-via-opendap] # DTR index indice_name: DTR in_files: [['http://opendap.knmi.nl/knmi/thredds/dodsC/IS-ENES/TESTSETS/tasmax_day_EC-EARTH_rcp26_r8i1p1_20060101-20251231.nc'], ['http://opendap.knmi.nl/knmi/thredds/dodsC/IS-ENES/TESTSETS/tasmin_day_EC-EARTH_rcp26_r8i1p1_20060101-20251231.nc']] dt1: 2022-01-01 dt2: 2022-12-31 slice_mode: JJA
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s=%s; sys1=syslin('c',k*(0.05*s+1)*(1+s)/((10*s+1)*(s-1))) nyquist(sys1) show_margins(sys1,'nyquist')
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<scriptConfig name="SS_mid" script="SA11_ramp_rate"> <params> <param name="rr.n_r" type="int">1</param> <param name="eut.rr_up_min" type="float">1.0</param> <param name="eut.i_low" type="float">1.0</param> <param name="eut.rr_msa" type="int">5</param> <param name="eut.t_dwell" type="float">5.0</param> <param name="eut.i_rated" type="float">10.0</param> <param name="rr.t_reconnect" type="float">60.0</param> <param name="eut.rr_up_max" type="float">100.0</param> <param name="eut.v_nom" type="float">120.0</param> <param name="rr.v_trip" type="float">120.0</param> <param name="pvsim.mode" type="string">Disabled</param> <param name="das_das_wf.mode" type="string">Disabled</param> <param name="gridsim.mode" type="string">Disabled</param> <param name="loadsim.mode" type="string">Disabled</param> <param name="der.mode" type="string">Disabled</param> <param name="rr.rr_max" type="string">Disabled</param> <param name="das_das_rms.mode" type="string">Disabled</param> <param name="gridsim.auto_config" type="string">Disabled</param> <param name="rr.rr_min" type="string">Disabled</param> <param name="rr.soft_start" type="string">Enabled</param> <param name="rr.rr_mid" type="string">Enabled</param> </params> </scriptConfig>
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ScreenName String 'Display Options Screen' ImplName String 'NULL SCREEN' ElementChunkArray Int 26 ScreenElementType Int 0 ImplName String 'Front End Screen Backdrop' TabIndex Int 1 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 113, 800, 507 ) # left,top,right,bottom ScreenElementType Int 1 ImplName String 'Open Prev Arrow Button' TabIndex Int 5 Selectable Bool True Enabled Bool True ReferenceArea Rect( 349, 500, 451, 602 ) # left,top,right,bottom Font String 'BlackChancery16' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_CANCEL' Color Colour( 255.000000, 255.000000, 0.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Detail Model Scrollbar Button' TabIndex Int 6 Selectable Bool True Enabled Bool True ReferenceArea Rect( 360, 320, 640, 355 ) # left,top,right,bottom Font String 'Univers10' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_BUTTON' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Detail Effect Scrollbar Button' TabIndex Int 7 Selectable Bool True Enabled Bool True ReferenceArea Rect( 360, 230, 640, 265 ) # left,top,right,bottom Font String 'Univers10' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_BUTTON' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Detail Texture Scrollbar Button' TabIndex Int 8 Selectable Bool True Enabled Bool True ReferenceArea Rect( 360, 275, 640, 310 ) # left,top,right,bottom Font String 'Univers10' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_BUTTON' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Video Modes Toggle Button' TabIndex Int 9 Selectable Bool True Enabled Bool True ReferenceArea Rect( 360, 185, 640, 220 ) # left,top,right,bottom Font String 'Univers10' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_BUTTON' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Render Background Toggle Button' TabIndex Int 10 Selectable Bool True Enabled Bool True ReferenceArea Rect( 360, 410, 640, 445 ) # left,top,right,bottom Font String 'Univers10' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_BUTTON' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Restore Default Settings Button' TabIndex Int 42 Selectable Bool False Enabled Bool True ReferenceArea Rect( 69, 530, 279, 574 ) # left,top,right,bottom Font String 'BlackChancery16' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_RESTORE_DEFAULTS' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 2 ImplName String 'Detail Model Label' TabIndex Int 20 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 324, 320, 356 ) # left,top,right,bottom Font String 'UniversLightBold14' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) ScreenElementType Int 2 ImplName String 'Detail Texture Label' TabIndex Int 22 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 280, 320, 314 ) # left,top,right,bottom Font String 'UniversLightBold14' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) ScreenElementType Int 2 ImplName String 'Detail Effect Label' TabIndex Int 24 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 236, 320, 261 ) # left,top,right,bottom Font String 'UniversLightBold14' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) ScreenElementType Int 1 ImplName String 'Apply Render Device Changes' TabIndex Int 42 Selectable Bool False Enabled Bool True ReferenceArea Rect( 656, 180, 785, 224 ) # left,top,right,bottom Font String 'BlackChancery16' Text String 'IDGS_TPFRONTENDTEXT02_APPLY_CHANGES' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Detail Terrain Toggle Button' TabIndex Int 43 Selectable Bool True Enabled Bool True ReferenceArea Rect( 360, 365, 640, 400 ) # left,top,right,bottom Font String 'Univers10' Text String 'IDGS_TPFRONTENDTEXT_BUTTON_CREW' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Render Flag Button' TabIndex Int 46 Selectable Bool True Enabled Bool True ReferenceArea Rect( 360, 455, 640, 490 ) # left,top,right,bottom Font String 'Univers10' Text String 'IDGS_TPFRONTENDTEXT_BUTTON_SHIPS' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Open Next Screen Button' TabIndex Int 49 Selectable Bool False Enabled Bool True ReferenceArea Rect( 521, 530, 731, 574 ) # left,top,right,bottom Font String 'BlackChancery16' Text String 'IDGS_TPFRONTENDTEXT01_ADVANCED_OPTIONS' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Center Justify Label' TabIndex Int 50 Selectable Bool False Enabled Bool True ReferenceArea Rect( 4, 126, 800, 165 ) # left,top,right,bottom Font String 'BlackChancery22' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_DISPLAY_OPTIONS' Color Colour( 0.000000, 0.000000, 0.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Center Justify Label' TabIndex Int 51 Selectable Bool True Enabled Bool True ReferenceArea Rect( 0, 127, 800, 161 ) # left,top,right,bottom Font String 'BlackChancery22' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_DISPLAY_OPTIONS' Color Colour( 1.000000, 0.796100, 0.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 52 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 193, 322, 220 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_RENDERER_AND_BIT_DEPTH' Color Colour( 0.000000, 0.000000, 0.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 53 Selectable Bool False Enabled Bool True ReferenceArea Rect( 3, 191, 320, 215 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_RENDERER_AND_BIT_DEPTH' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 54 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 371, 322, 410 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT02_TERRAIN_VISIBILITY' Color Colour( 0.000000, 0.000000, 0.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 55 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 369, 320, 393 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT02_TERRAIN_VISIBILITY' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 56 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 417, 322, 453 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_RENDER_BACKGROUND' Color Colour( 0.000000, 0.000000, 0.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 57 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 415, 320, 441 ) # left,top,right,bottom Font String 'UniversLightBold14' Text String 'IDGS_TPFRONTENDTEXT_SCREENS_RENDER_BACKGROUND' Color Colour( 1.000000, 1.000000, 1.000000, 1.000000 ) HotKey Int -1 ScreenElementType Int 1 ImplName String 'Right Justify Label' TabIndex Int 58 Selectable Bool False Enabled Bool True ReferenceArea Rect( 0, 463, 322, 514 ) # 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Abilityguy/Linear-Algebra-Scilab
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Normal Form.sce
//Program to find the solution to a system of equations through the normal equation of a matrix A = input("Enter matrix A: ") b = input("Enter matrix b: ") //normal equation - A'.A.x = A'.b //Solving for x = inv(A'.A)A'.b disp("X: ") disp(inv(A'*A)*A'*b)
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app.sce
//Configuration formats = ["JPG/JPEG format","*.jp*g";"*.png","PNG format"]; window = figure(); window.background = color(50, 50, 50); window.figure_name = gettext("MyPhotoshop Cc"); handle.Axesl = newaxes(); handle.Axesl.margins = [0 0 0 0]; handle.Axesl.axes_bounds = [0.05, 0.2, 0.66, 0.5]; handle.Axesl.background = color(30, 30, 30); handle.Axesl.auto_clear = 'on'; //Création d'un module pour charger l'image via chargement_image h1= uimenu("parent",window,"label",gettext("Charger une image"),"callback","chargement_image(formats)"); //Cacher les menu delmenu(window.figure_id,gettext("&File")); delmenu(window.figure_id,gettext("&Tools")); delmenu(window.figure_id,gettext("&Edit")); delmenu(window.figure_id,gettext("&?")); delmenu(window.figure_id,gettext("off")); //Textes //Photoshop CC photoshopCc = uicontrol(window,"style","text"); photoshopCc.string = "Photoshop CC"; photoshopCc.fontweight = "bold"; photoshopCc.position = [160 370 150 25]; photoshopCc.BackgroundColor = [0.20 0.20 0.20]; photoshopCc.ForegroundColor = [1 0 0.4]; photoshopCc.HorizontalAlignment = "center"; //Filtres filtres = uicontrol(window,"style","text"); filtres.string = "Filtres"; filtres.fontweight = "bold"; filtres.position = [448 320 130 25]; filtres.BackgroundColor = [0.12 0.12 0.12]; filtres.ForegroundColor = [1 0 0.4]; filtres.HorizontalAlignment = "center"; //La Filtre Box filtres_box=uicontrol(window,"style","listbox"); filtres_box.BackgroundColor=[0.12 0.12 0.12]; filtres_box.ForegroundColor=[0.25 0.25 0.25]; filtres_box.Position = [448 170 130 150]; filtres_box.String = ["Canny","Bonus","Horizontal","Vertical","Horivertical","Gaussien","N/B","Negatif","Prewitt","Sobel","Rouge","Vert","Bleu", "Cyan","Jaune","Violet"]; filtres_box.Value = 1; //Les bouttons //quitter quitter = uicontrol(window,"style","pushbutton"); quitter.String = "Quitter"; quitter.BackgroundColor=[0.12 0.12 0.12]; quitter.ForegroundColor=[1 0 0.4]; quitter.Position = [28 75 130 50]; quitter.Callback = "delete(window)"; //cleaner cleaner = uicontrol(window,"style","pushbutton"); cleaner.String = "Cleaner"; cleaner.BackgroundColor=[0.12 0.12 0.12]; cleaner.ForegroundColor=[1 0 0.4]; cleaner.Position = [168 75 130 50]; cleaner.Callback = "[current_ns_image] = cleaner_picture(handle);"; //sauvegarder sauvegarder = uicontrol(window,"style","pushbutton"); sauvegarder.String = "Sauvegarder"; sauvegarder.BackgroundColor=[0.12 0.12 0.12]; sauvegarder.ForegroundColor=[1 0 0.4]; sauvegarder.Position = [308 75 130 50]; sauvegarder.Callback = "sauvegarder_image(formats,handle)"; //etaler etaler = uicontrol(window,"style","pushbutton"); etaler.String = "Étaler"; etaler.BackgroundColor=[0.12 0.12 0.12]; etaler.ForegroundColor=[1 0 0.4]; etaler.Position = [448 75 130 50]; etaler.Callback = "[current_s_image] = etaler_filtre(filtres_box,handle)";
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Cbro/Oracle-scripts
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refs/heads/master
2020-12-24T14:36:20.643782
2011-05-07T18:55:51
2011-05-07T18:55:51
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TopArtists_7.tst
PL/SQL Developer Test script 3.0 36 -- Created on 11/04/2008 by MKAUL declare -- Local variables here i integer; vTrackID track.id%type; vRankNum INTEGER; begin for x in ( -- Test statements here select x.artist_id, x.rank_num from ( select /*+ FIRST_ROWS */ v.artist_id artist_id, row_number() over ( order by v.play_count desc ) rank_num from artist a, service_artist sa, v_artist_count_forever v where a.id = v.artist_id and sa.service_id = v.service_id and sa.artist_id = a.id and sa.service_id = :sid and (a.first_release_date is null or a.first_release_date < sysdate) ) x where x.rank_num <= :topCount; ) loop dbms_output.put_line('Rel ID : '|| x.artist_id ); dbms_output.put_line('Rank : '|| x.rank_num ); end loop; end; 2 sid 1 50 3 topCount 1 20 3 0
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/Calculo Numerico/Scilab/Triangulação/Metodo Gaus&Jordan.sce
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no_license
GuilhermeGueds/Faculdade
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Metodo Gaus&Jordan.sce
clear clc Ab = input("Entre com a matriz : "); disp("entrada") disp(Ab) n = size(Ab,1) // Determina a triangulação Gaus&Jordan for j = n: -1:1 for i = (j-1):-1:1 //verifica se a diogonal não possui 0 if (Ab(j,j)== 0) then y=Ab(1,:) Ab(n,:)=Ab(n-1,:) Ab(n-1,:)=y end m(i,j) = Ab(i,j)/Ab(j,j); Ab(i,:) = m(i,j) * Ab(j,:) - Ab(i,:) disp(Ab) end end disp("Metodo Gaus&Jordan") disp(Ab) //Faz divisao de A e B para encontrar resultado for i = 1:n for j = 1:n A(i,j)= Ab(i,j) B(i,1)= Ab(i,(n+1)) end end disp("Metodo Gaus&Jordan") disp(Ab) //Faz divisao de A e B para encontrar resultado for i = 1:n for j = 1:n A(i,j)= Ab(i,j) B(i,1)= Ab(i,(n+1)) end end disp("Resultado final") C= rref([A,B]);disp(C)
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letyrobueno/Scilab
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2019-11-01T17:45:22
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square.sce
x = input("Give the square side length: ") area = x^2 perimeter = 4*x diagonal = sqrt(2)*x printf("The area is %2.2f\n The perimeter is %2.2f\n The diagonal is %2.2f",area,perimeter,diagonal)
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FOSSEE/Scilab-TBC-Uploads
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//ques23 //Reducing the Pressure Setting to Reduce Cost clear clc Preduced=885.6;//reduced pressure P1=85.6;//initial pressure in kPa P2=985.6;//final pressure in kPa n=1.4; f=1-((Preduced/P1)^((n-1)/n)-1)/((P2/P1)^(1-1/n)-1);//The fraction of energy saved as a result of reducing the pressure setting Cc=12000;//current cost in $/yr Csaving=Cc*f; printf('Cost saving = $%.0f/yr \n',Csaving);
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Example39_9.sce
// A Texbook on POWER SYSTEM ENGINEERING // A.Chakrabarti, M.L.Soni, P.V.Gupta, U.S.Bhatnagar // DHANPAT RAI & Co. // SECOND EDITION // PART IV : UTILIZATION AND TRACTION // CHAPTER 1: INDUSTRIAL APPLICATIONS OF ELECTRIC MOTORS // EXAMPLE : 1.9 : // Page number 686-687 clear ; clc ; close ; // Clear the work space and console // Given data I_f1 = 25.0 // Current without diverter(A) N_1 = 500.0 // Speed of dc series motor without diverter(rpm) // Calculations I_a2 = ((3.0/2)**0.5*I_f1**2*3/2)**0.5 // Field current with diverter(A) N_2 = I_f1*N_1*3/(2*I_a2) // Speed with diverter(rpm) // Results disp("PART IV - EXAMPLE : 1.9 : SOLUTION :-") printf("\nSpeed when field winding is shunted by a diverter, N_2 = %.f rpm", N_2) printf("\nCurrent when field winding is shunted by a diverter, I_a2 = %.1f A", I_a2)
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//chapter 11 //example 11.12 //page 338 clear all; clc ; //given Rl=50;//load resistance in kohm Vcc=12;//supply voltage V f1=150;//lower cutoff frequency Hz Vp=50;////op voltage mV hfe=70; ip=Vp/Rl; Ie2=2;//Ie2>ip Ve2=5; R4=Ve2/Ie2; printf("\nR4= %.1f kohm ,use standard value 2.2 kohm",R4);R4=2.2; Ic2=2; Ic1=Ic2; VR1=Vcc-(Ve2+0.7); R1=VR1/Ic1; printf("\nR1= %.2f kohm,use standard value 3.3 kohm ",R1);R1=3.3; Ib1=1000*Ic1/hfe; R23=1000*(Ve2-0.7)/Ib1; R2=47; R3=R23-R2; hfe1=100;hie1=1; Zi=1000*(R2*hie1)/(R2+hie1); XC1=Zi/10; C1=10^6/(2*%pi*f1*XC1); printf("\nC1=%.1f microF,use standard value 15 microF",C1); XC2=floor(R3/100); C2=10^3/(2*%pi*f1*XC2); printf("\nC2=%.2f microF,use standard value 1.2 microF",(C2)); XC3=Rl; C3=10^6/(2*%pi*f1*XC3); printf("\nC3=%.1f microF,use standard value 22 microF",(C3));
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Chapter3_Example16.sce
clc clear //INPUT DATA //continous flow calorimeter r=120/60;//rate of flow of water in gm/sec T1=27.30;//temperature at initial in deg.C T2=33.75;//temperature at final in deg.C v=12.64;//potential drop in volts s=1;//specific heat of water in kj/kg-K i=4.35;//current through the heating element in amp //CALCULATIONS J=(v*i)/(r*s*(T2-T1));//the mechanical equivalent of heat in joule/calorie //OUTPUT mprintf('the mechanical equivalent of heat is %3.2f j/cal',J)
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errcatch(-1,"stop");mode(2);//Caption:Find the no load speed //Exa:2.45 ; ; V=220;//in volts R_a=2.5;//in ohms N_1=859;//in rpm I_ao=0; I_a=8;//in amperes E_b1=V-I_a*R_a; E_bo=V-I_ao*R_a; N_o=N_1*E_bo/E_b1; disp(N_o,'No Load Speed (in RPM)=') exit();
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hs.search.kate.sce
400 kate historysave_7.txt 409 sudo kate /opt/lampp/etc/extra/httpd-vhosts.conf 400 kate historysave_7.txt 409 sudo kate /opt/lampp/etc/extra/httpd-vhosts.conf 400 kate historysave_7.txt 409 sudo kate /opt/lampp/etc/extra/httpd-vhosts.conf 407 sudo kate /opt/lampp/etc/httpd.conf 409 sudo kate /opt/lampp/etc/httpd.conf 407 sudo kate /opt/lampp/etc/httpd.conf 409 sudo kate /opt/lampp/etc/httpd.conf 405 kate apt.conf.d/ 406 sudo kate apt.conf.d/ 240 sudo kate /etc/apt/apt.conf 403 sudo kate /etc/apt/apt.conf
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//Exa 3.2 clc; clear; close; //Given data ib=10;//in uA ic=1;//in mA ic=ic*10^3;//in uA vi=0.02;//in Volt RC=5;//in kohm RL=10;//in kohm //Part (i) Ai=-ic/ib;//unitless Beta=Ai;//unitless disp(Ai,"Current gain : "); //Part (ii) Rie=vi/(ib*10^-6);//in Ohm disp(Rie*10^-3,"Input impedence in kohm :"); //Part (iii) Rac=RC*RL/(RC+RL);//in kohm disp(Rac,"AC load in kohm : "); //Part (iv) Av=-Rac*10^3*Beta/Rie;//unitless disp(Av,"Voltage gain : "); //Part (v) PowerGain=Av*Ai;//unitless disp(PowerGain,"Power Gain is : "); //Note : Ans of Av and Power gain is wrong in the book.
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clear clc //to find energy,period,semimajor axis of B before and after burn // GIVEN: //refer to figure 14-19 from page no. 315 //mass of spacecraft m = 3250//in Kg //height above Earth h = 270//in Km //radius of earth RE = 6370//in Km //mass of earth ME = 5.98e24//in Kg //decrease in velocity after burn d = 0.95//in percent //Gravitational constant G = 6.67e-11//in N.m^2/Kg^2 // SOLUTION: //before burn //semimajor axis before burn a = RE+h//in Km //energy before burn E = -(G*m*ME)/(2*a*(1000))//in J //period before burn //applying Krpler's law of peroids T = ((4*(%pi^2)*((a*1000)^3))/(G*ME))^(1/2)//in seconds //kinetic energy before burn K = -(E)//in J //velocity before burn v = sqrt((2*K)/m)//in m/s //after burn //velocity after burn v_dash = (1-(d*0.01))*v//in m/s //kinetic energy after burn K_dash = 1/2*(m)*(v_dash)^2//in J //potential energy after burn U_dash = -(K)//in J //total energy after burn E_dash = K_dash+(2*U_dash)//in J //semimajor axis after burn a_dash = -((G*m*ME)/(2*E_dash))//in meters //period after burn T_dash = ((4*(%pi^2)*((a_dash)^3))/(G*ME))^(1/2)//in seconds T = nearfloat("pred",5381) E_dash = nearfloat("succ",-9.94e10) T_dash = nearfloat("succ",5240) printf ("\n\n Semimajor axis before burn a = \n\n %4i Km",a) printf ("\n\n Energy before burn E = \n\n %.2e J",E) printf ("\n\n Period before burn T = \n\n %4i s",T) printf ("\n\n Kinetic energy before burn K = \n\n %.2e J",K) printf ("\n\n Velocity before burn v = \n\n %.2e m/s",v) printf ("\n\n Velocity after burn v_dash = \n\n %.2e m/s",v_dash) printf ("\n\n Kinetic energy after burn K_dash = \n\n %.2e J",K_dash) printf ("\n\n Total energy after burn E_dash = \n\n %.2e J",E_dash) printf ("\n\n Semimajor axis after burn a_dash = \n\n %.2e m",a_dash) printf ("\n\n Period after burn T_dash = \n\n %4i s",T_dash)
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clear// // //Variable Declaration E_st=200 //Youngs Modulus of Steel in GPa sigma_st_yp=290 //Yielding Stress in MPa E_al=70 //Youngs Modulus of Aluminium in GPa sigma_al_yp=330 //Yielding Stresss of Aluminium in MPa A_st=900 //Area of steel rod in mm^2 A_al=600 //Area of Aluminium rod in mm^2 L_st=350 //Length of the steel rod in mm L_al=250 //Length of the aluminium rod in mm //Calculations //Limit Load P_st=sigma_st_yp*A_st*10**-3 //Load in limiting condition in kN P_al=sigma_al_yp*A_al*10**-3 //Load in limiting condition in kN P_L=P_st+2*P_al //Total Loading in kN //Elastic Unloading //Solving for Pst and Pal using matri approach A=([[1,2;L_st*(E_st*A_st)**-1,-L_al*(E_al*A_al)**-1]]) B=([P_L;0]) C=linsolve(A,B) //Loading in kN //Residual Stresses P_res_st=-C(1)-P_st //Residual Load in kN P_res_al=-C(2)-P_al //Residual Load in kN sigma_st=P_res_st/A_st //residual Stress in Steel in MPa sigma_al=P_res_al/A_al //residual Stress in Aluminium in MPa //Result printf("\n The Residual stresses are as follows") printf("\n Sigma_st= %0.1f MPa and sigma_al= %0.1f MPa",sigma_st*10**3,sigma_al*10**3)
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clc clear m=input("input the number of rows") n=input("input the number of column") disp("Enter elements of first matrix:") for i=1:m for j=1:n A(i,j)=input("") end end disp(A); p=input("input the number of rows") q=input("input the number of column") disp("Enter elements of second matrix:") for i=1:p for j=1:q B(i,j)=input("") end end disp(B); if n==p then for i=1:m for j=1:q C(i,j)=0 for k=1:p C(i,j)=C(i,j)+(A(i,k)*B(k,j)) end end end disp(C);;; else disp("matrix multiplication not possible") ;; end
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//Example 1_17 page no:34 clc; Va=1;//here Va is assumed to be one hence it will canceled out in calculation R=1;//here R is assumed to be one it will be assigned correct value on the flow of calculation V10=Va*(10/15); Vr=Va*R/(20+R); R=(10/15)*(20*3);//here 3 is included to show that R is canceled in calculation //hence 3R-2R=R for simplicity we introduced 3 in calculation disp(R,"the resistance R in the circuit is(in ohm)");
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function [m, A, Eigenfaces] = EigenfaceCore(T) // Use Principle Component Analysis (PCA) to determine the most // discriminating features between images of faces. // // Description: This function gets a 2D matrix, containing all training image vectors // and returns 3 outputs which are extracted from training database. // // Argument: T - A 2D matrix, containing all 1D image vectors. // Suppose all P images in the training database // have the same size of MxN. So the length of 1D // column vectors is M*N and 'T' will be a MNxP 2D matrix. // // Returns: m - (M*Nx1) Mean of the training database // Eigenfaces - (M*Nx(P-1)) Eigen vectors of the covariance matrix of the training database // A - (M*NxP) Matrix of centered image vectors // // // Calculating the mean image S=uint16(T); for i=1:36000 su=sum(S(i,:)); m(i)=su/80;// Computing the average face image m = (1/P)*sum(Tj's) (j = 1 : P) end Train_Number = size(T,2); // Calculating the deviation of each image from mean image A = []; for i = 1 : Train_Number temp = uint16(T(:,i)) - m; // Computing the difference image for each image in the training set Ai = Ti - m A = [A temp]; // Merging all centered images end // Snapshot method of Eigenface methos // We know from linear algebra theory that for a PxQ matrix, the maximum // number of non-zero eigenvalues that the matrix can have is min(P-1,Q-1). // Since the number of training images (P) is usually less than the number // of pixels (M*N), the most non-zero eigenvalues that can be found are equal // to P-1. So we can calculate eigenvalues of A'*A (a PxP matrix) instead of // A*A' (a M*NxM*N matrix). It is clear that the dimensions of A*A' is much // larger that A'*A. So the dimensionality will decrease. L = A'*A; // L is the surrogate of covariance matrix C=A*A'. [R,diagevals]=spec(L) // Diagonal elements of D are the eigenvalues for both L=A'*A and C=A*A'. // Sorting and eliminating eigenvalues // All eigenvalues of matrix L are sorted and those who are less than a // specified threshold, are eliminated. So the number of non-zero // eigenvectors may be less than (P-1). L_eig_vec = []; for i = 1 : size(V,2) if( S(i,i)>1 ) L_eig_vec = [L_eig_vec V(:,i)]; end end // Calculating the eigenvectors of covariance matrix 'C' // Eigenvectors of covariance matrix C (or so-called "Eigenfaces") // can be recovered from L's eiegnvectors. Eigenfaces = A * L_eig_vec; // A: centered image vectors endfunction
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// Example 9.7 // Calculation of the (a) the total data rate and (b) the spectral efficiency. // Page no 413 clc; clear; close; //Given data M=16; np=2; // No of polarization nc=24; // No of channels bs=28*10^9; // Symbol rate per polarization // (a) The total data rate B=bs*log2(M); T=B*np*nc; // (b) The spectral efficiency N=bs*nc; s=T/N; //Displaying results in the command window printf("\n The total data rate = %0.3f Tb/s ",T*10^-12); printf("\n The spectral efficiency = %0.1f b/s/Hz ",s);
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m=.05; //m=%pi.*a.^2.*I/c ring current I radius a len=0.1; b0=1.0; wid=1.0; shift=0.5; x=-1.0:0.05:1.0; y=0.1:0.1:2.0; [X1,Y1]=meshgrid(x-shift,y); [X2,Y2]=meshgrid(x+shift,y); //bx1=-0.1*(X1./sqrt(X1.^2))-2.0.*b0*X1.*exp(-wid.*(X1.^2)./len); bx1=-2.0.*b0*X1.*exp(-wid.*(X1.^2)./len); by1=+b0.*exp(-wid.*(X1.^2)./len); //bx2=0.1*(X2./sqrt(X2.^2))+2.0.*b0*X2.*exp(-wid.*(X2.^2)./len); bx2=+2.0.*b0*X2.*exp(-wid.*(X2.^2)./len); by2=-b0.*exp(-wid.*(X2.^2)./len); bx=bx1+bx2; by=by1+by2; bmag=sqrt(bx.^2+by.^2); contour(x,y,bmag',[0.005 0.006 0.007 0.008 0.009 0.01 0.05 0.1 0.15 0.2 0.25 0.3 .35 .4 .45 2]); //hold on //quiver(X(8:20,:),Y(8:20,:),bx(8:20,:),by(8:20,:),3); //hold off
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\ set time slow \rele print CROUTPUT: \ \SET CACH ON \ THIS TAKES SEVERAL HOURS ON A VAX 11/750 \ IT TAKES SEVERAL SECONDS ON A PENTIUM III \ \TITLE LARGE TEST JOB FOR CYBER \SET TIME SLOW \DISK EXTEND SIZE=0 END \LIST 1 REAL a = 14.5430 b = 15.6710 c = 18.7790 CONTINUE alpha = 69.2700 beta = 68.3900 gamma = 78.4800 END \SPACE GROUP SYMBOL P -1 END \LIST 3 READ NSCATTER = 7 SCATT IR -2.066 7.990 27.3049 1.59279 16.7296 8.86553 15.6115 CONT 0.417916 5.83377 45.0011 11.4722 SCATT AU -2.688 8.798 16.8819 0.461100 18.5913 8.62160 25.5582 CONT 1.48260 5.86000 36.3956 12.0658 SCATT P 0.090 0.095 6.43450 1.90670 4.17910 27.1570 1.78000 CONT 0.526000 1.49080 68.1645 1.11490 SCATT F 0.014 0.010 3.53920 10.2825 2.64120 4.29440 1.51700 CONT 0.261500 1.02430 26.1476 0.277600 SCATT O 0.008 0.006 3.04850 13.2771 2.28680 5.70110 1.54630 CONT 0.323900 0.867000 32.9089 0.250800 SCATT C 0.002 0.002 2.31000 20.8439 1.02000 10.2075 1.58860 CONT 0.568700 0.865000 51.6512 0.215600 SCATT H 0.0 0.0 0.493002 10.5109 0.322912 26.1257 0.140191 CONT 3.14236 0.040810 57.7997 0.003038 END \LIST 4 END \LIST 16 PLANAR C(111) UNTIL C(116) DISTANCES 1.395 , 0.02= C(111) TO C(112) , C(112) TO C(113) CONT C(113) TO C(114) , C(114) TO C(115) , C(115) TO C(116) , C(116) TO C(111) ANGLES 120.0 , 3.0= C(116) TO C(111) TO C(112) , C(111) TO C(112) TO C(113) CONT C(112) TO C(113) TO C(114) , C(113) TO C(114) TO C(115) CONT C(114) TO C(115) TO C(116) , C(115) TO C(116) TO C(111) PLANAR C(121) UNTIL C(126) DISTANCES 1.395 , 0.02= C(121) TO C(122) , C(122) TO C(123) CONT C(123) TO C(124) , C(124) TO C(125) , C(125) TO C(126) , C(126) TO C(121) ANGLES 120.0 , 3.0= C(126) TO C(121) TO C(122) , C(121) TO C(122) TO C(123) CONT C(122) TO C(123) TO C(124) , C(123) TO C(124) TO C(125) CONT C(124) TO C(125) TO C(126) , C(125) TO C(126) TO C(121) PLANAR C(131) UNTIL C(136) DISTANCES 1.395 , 0.02= C(131) TO C(132) , C(132) TO C(133) CONT C(133) TO C(134) , C(134) TO C(135) , C(135) TO C(136) , C(136) TO C(131) ANGLES 120.0 , 3.0= C(136) TO C(131) TO C(132) , C(131) TO C(132) TO C(133) CONT C(132) TO C(133) TO C(134) , C(133) TO C(134) TO C(135) CONT C(134) TO C(135) TO C(136) , C(135) TO C(136) TO C(131) PLANAR C(211) UNTIL C(216) DISTANCES 1.395 , 0.02= C(211) TO C(212) , C(212) TO C(213) CONT C(213) TO C(214) , C(214) TO C(215) , C(215) TO C(216) , C(216) TO C(211) ANGLES 120.0 , 3.0= C(216) TO C(211) TO C(212) , C(211) TO C(212) TO C(213) CONT C(212) TO C(213) TO C(214) , C(213) TO C(214) TO C(215) CONT C(214) TO C(215) TO C(216) , C(215) TO C(216) TO C(211) PLANAR C(221) UNTIL C(226) DISTANCES 1.395 , 0.02= C(221) TO C(222) , C(222) TO C(223) CONT C(223) TO C(224) , C(224) TO C(225) , C(225) TO C(226) , C(226) TO C(221) ANGLES 120.0 , 3.0= C(226) TO C(221) TO C(222) , C(221) TO C(222) TO C(223) CONT C(222) TO C(223) TO C(224) , C(223) TO C(224) TO C(225) CONT C(224) TO C(225) TO C(226) , C(225) TO C(226) TO C(221) PLANAR C(231) UNTIL C(236) DISTANCES 1.395 , 0.02= C(231) TO C(232) , C(232) TO C(233) CONT C(233) TO C(234) , C(234) TO C(235) , C(235) TO C(236) , C(236) TO C(231) ANGLES 120.0 , 3.0= C(236) TO C(231) TO C(232) , C(231) TO C(232) TO C(233) CONT C(232) TO C(233) TO C(234) , C(233) TO C(234) TO C(235) CONT C(234) TO C(235) TO C(236) , C(235) TO C(236) TO C(231) PLANAR C(311) UNTIL C(316) DISTANCES 1.395 , 0.02= C(311) TO C(312) , C(312) TO C(313) CONT C(313) TO C(314) , C(314) TO C(315) , C(315) TO C(316) , C(316) TO C(311) ANGLES 120.0 , 3.0= C(316) TO C(311) TO C(312) , C(311) TO C(312) TO C(313) CONT C(312) TO C(313) TO C(314) , C(313) TO C(314) TO C(315) CONT C(314) TO C(315) TO C(316) , C(315) TO C(316) TO C(311) PLANAR C(321) UNTIL C(326) DISTANCES 1.395 , 0.02= C(321) TO C(322) , C(322) TO C(323) CONT C(323) TO C(324) , C(324) TO C(325) , C(325) TO C(326) , C(326) TO C(321) ANGLES 120.0 , 3.0= C(326) TO C(321) TO C(322) , C(321) TO C(322) TO C(323) CONT C(322) TO C(323) TO C(324) , C(323) TO C(324) TO C(325) CONT C(324) TO C(325) TO C(326) , C(325) TO C(326) TO C(321) PLANAR C(331) UNTIL C(336) DISTANCES 1.395 , 0.02= C(331) TO C(332) , C(332) TO C(333) CONT C(333) TO C(334) , C(334) TO C(335) , C(335) TO C(336) , C(336) TO C(331) ANGLES 120.0 , 3.0= C(336) TO C(331) TO C(332) , C(331) TO C(332) TO C(333) CONT C(332) TO C(333) TO C(334) , C(333) TO C(334) TO C(335) CONT C(334) TO C(335) TO C(336) , C(335) TO C(336) TO C(331) PLANAR C(411) UNTIL C(416) DISTANCES 1.395 , 0.02= C(411) TO C(412) , C(412) TO C(413) CONT C(413) TO C(414) , C(414) TO C(415) , C(415) TO C(416) , C(416) TO C(411) ANGLES 120.0 , 3.0= C(416) TO C(411) TO C(412) , C(411) TO C(412) TO C(413) CONT C(412) TO C(413) TO C(414) , C(413) TO C(414) TO C(415) CONT C(414) TO C(415) TO C(416) , C(415) TO C(416) TO C(411) PLANAR C(421) UNTIL C(426) DISTANCES 1.395 , 0.02= C(421) TO C(422) , C(422) TO C(423) CONT C(423) TO C(424) , C(424) TO C(425) , C(425) TO C(426) , C(426) TO C(421) ANGLES 120.0 , 3.0= C(426) TO C(421) TO C(422) , C(421) TO C(422) TO C(423) CONT C(422) TO C(423) TO C(424) , C(423) TO C(424) TO C(425) CONT C(424) TO C(425) TO C(426) , C(425) TO C(426) TO C(421) PLANAR C(431) UNTIL C(436) DISTANCES 1.395 , 0.02= C(431) TO C(432) , C(432) TO C(433) CONT C(433) TO C(434) , C(434) TO C(435) , C(435) TO C(436) , C(436) TO C(431) ANGLES 120.0 , 3.0= C(436) TO C(431) TO C(432) , C(431) TO C(432) TO C(433) CONT C(432) TO C(433) TO C(434) , C(433) TO C(434) TO C(435) CONT C(434) TO C(435) TO C(436) , C(435) TO C(436) TO C(431) END \LIST 23 MODIFY ANOM=YES EXTINCT=YES MINIM REFL=YES REST=YES END \LIST 29 READ NELEM=12 ELEM PT 1.5000 1.5000 0.6000 0.000 0.0 0.0000 ELEM IR 1.5000 1.5000 0.6000 0.000 0.0 0.0000 ELEM AU 1.4000 1.5000 0.6000 0.000 0.0 0.0000 ELEM P 1.2000 1.5000 0.6000 0.000 0.0 0.0000 ELEM CL 1.2000 1.5000 0.6000 0.000 0.0 0.0000 ELEM S 1.2000 1.5000 0.6000 0.000 0.0 0.0000 ELEM C 0.8000 1.5000 0.6000 0.000 0.0 0.0000 ELEM N 0.7000 1.5000 0.6000 0.000 0.0 0.0000 ELEM O 0.6600 1.5000 0.6000 0.000 0.0 0.0000 ELEM F 0.6600 1.5000 0.6000 0.000 0.0 0.0000 ELEM H 0.2800 1.5000 0.6000 0.000 0.0 0.0000 ELEM PEAK 1.5000 1.5000 0.6000 0.000 0.0 0.0000 END # # Punched on 16-JAN87 at 15:59:05 # # Punched on 28/01/11 at 14:14:55 # #LIST 5 READ NATOM = 148, NLAYER = 0, NELEMENT = 0, NBATCH = 0 OVERALL 0.909262 0.021674 0.050000 1.000000 0.000000 113.1696625 ATOM IR 1.000000 1.000000 0.000000 0.251079 0.374585 0.300281 CON U[11]= 0.024021 0.027206 0.027862 -0.008651 -0.006840 -0.004387 CON SPARE= 0.00 0 0 0 ATOM AU 1.000000 1.000000 0.000000 0.079894 0.354308 0.289144 CON U[11]= 0.029608 0.036157 0.043692 -0.009513 -0.015078 -0.005667 CON SPARE= 0.00 0 0 0 ATOM P 1.000000 1.000000 0.000000 0.421568 0.385630 0.282991 CON U[11]= 0.025998 0.035642 0.030611 -0.012456 -0.007545 -0.003987 CON SPARE= 0.00 0 0 0 ATOM P 2.000000 1.000000 0.000000 0.190673 0.528069 0.268263 CON U[11]= 0.029327 0.030435 0.035618 -0.010690 -0.009860 -0.002318 CON SPARE= 0.00 0 0 0 ATOM P 3.000000 1.000000 0.000000 0.225418 0.220830 0.378478 CON U[11]= 0.034424 0.028668 0.036202 -0.009383 -0.009969 -0.004448 CON SPARE= 0.00 0 0 0 ATOM P 4.000000 1.000000 0.000000 -0.041663 0.326871 0.251422 CON U[11]= 0.035022 0.040772 0.052489 -0.008817 -0.021112 -0.007330 CON SPARE= 0.00 0 0 0 ATOM P 5.000000 1.000000 0.000000 0.604783 -0.174116 0.238618 CON U[11]= 0.106712 0.108646 0.114879 -0.066825 -0.056100 0.020168 CON SPARE= 0.00 0 0 0 ATOM F 1.000000 1.000000 0.000000 0.574748 -0.279289 0.269088 CON U[11]= 0.158394 0.135425 0.201293 -0.088815 -0.029709 -0.012361 CON SPARE= 0.00 0 0 0 ATOM F 2.000000 1.000000 0.000000 0.515551 -0.146724 0.204580 CON U[11]= 0.136944 0.220001 0.149104 -0.072522 -0.076943 0.013224 CON SPARE= 0.00 0 0 0 ATOM F 3.000000 1.000000 0.000000 0.677275 -0.191561 0.158970 CON U[11]= 0.162684 0.158070 0.102940 -0.054046 -0.002408 -0.009180 CON SPARE= 0.00 0 0 0 ATOM F 4.000000 1.000000 0.000000 0.528012 -0.165303 0.322413 CON U[11]= 0.149954 0.209662 0.165304 -0.133294 -0.059517 0.038554 CON SPARE= 0.00 0 0 0 ATOM F 5.000000 1.000000 0.000000 0.687711 -0.214308 0.279138 CON U[11]= 0.121006 0.185670 0.167397 -0.077929 -0.077840 0.025672 CON SPARE= 0.00 0 0 0 ATOM F 6.000000 1.000000 0.000000 0.629407 -0.078821 0.214369 CON U[11]= 0.216064 0.090403 0.362878 -0.084910 -0.010716 -0.051003 CON SPARE= 0.00 0 0 0 ATOM C 1.000000 1.000000 0.000000 0.285888 0.371724 0.192210 CON U[11]= 0.036051 0.044682 0.039122 -0.017600 -0.006604 -0.012701 CON SPARE= 0.00 0 0 0 ATOM O 1.000000 1.000000 0.000000 0.306096 0.375252 0.127090 CON U[11]= 0.055864 0.077965 0.035536 -0.020863 -0.006959 -0.018525 CON SPARE= 0.00 0 0 0 ATOM C 111.000000 1.000000 1.000000 0.477884 0.483307 0.197125 CON U[11]= 0.033403 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 112.000000 1.000000 1.000000 0.481503 0.568182 0.205361 CON U[11]= 0.039816 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 113.000000 1.000000 1.000000 0.521858 0.639563 0.136530 CON U[11]= 0.045756 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 114.000000 1.000000 1.000000 0.557510 0.628064 0.062171 CON U[11]= 0.050761 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 115.000000 1.000000 1.000000 0.553957 0.545608 0.053410 CON U[11]= 0.048402 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 116.000000 1.000000 1.000000 0.514767 0.473901 0.120234 CON U[11]= 0.040372 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 121.000000 1.000000 1.000000 0.507946 0.290520 0.253490 CON U[11]= 0.035931 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 122.000000 1.000000 1.000000 0.483905 0.238576 0.217353 CON U[11]= 0.048056 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 123.000000 1.000000 1.000000 0.547747 0.166135 0.196721 CON U[11]= 0.061756 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 124.000000 1.000000 1.000000 0.635272 0.143093 0.212579 CON U[11]= 0.071979 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 125.000000 1.000000 1.000000 0.661318 0.195448 0.247910 CON U[11]= 0.070071 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 126.000000 1.000000 1.000000 0.598526 0.268134 0.268392 CON U[11]= 0.052742 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 131.000000 1.000000 1.000000 0.454332 0.392727 0.366144 CON U[11]= 0.034885 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 132.000000 1.000000 1.000000 0.539669 0.431460 0.354301 CON U[11]= 0.043036 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 133.000000 1.000000 1.000000 0.562360 0.426837 0.422053 CON U[11]= 0.053991 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 134.000000 1.000000 1.000000 0.504389 0.385303 0.499056 CON U[11]= 0.056414 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 135.000000 1.000000 1.000000 0.419395 0.347886 0.511607 CON U[11]= 0.048721 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 136.000000 1.000000 1.000000 0.394391 0.352224 0.444745 CON U[11]= 0.038978 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 211.000000 1.000000 1.000000 0.246770 0.603455 0.294023 CON U[11]= 0.035867 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 212.000000 1.000000 1.000000 0.269732 0.567121 0.365390 CON U[11]= 0.039848 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 213.000000 1.000000 1.000000 0.309250 0.620515 0.390152 CON U[11]= 0.053371 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 214.000000 1.000000 1.000000 0.329033 0.709393 0.343240 CON U[11]= 0.060933 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 215.000000 1.000000 1.000000 0.305486 0.746720 0.274140 CON U[11]= 0.065844 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 216.000000 1.000000 1.000000 0.261686 0.694581 0.249492 CON U[11]= 0.050798 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 221.000000 1.000000 1.000000 0.060252 0.559101 0.319888 CON U[11]= 0.040715 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 222.000000 1.000000 1.000000 0.007436 0.500044 0.392372 CON U[11]= 0.053615 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 223.000000 1.000000 1.000000 -0.088776 0.524656 0.434194 CON U[11]= 0.076306 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 224.000000 1.000000 1.000000 -0.130350 0.610378 0.402780 CON U[11]= 0.072287 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 225.000000 1.000000 1.000000 -0.081849 0.669812 0.333209 CON U[11]= 0.079659 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 226.000000 1.000000 1.000000 0.014388 0.645003 0.292279 CON U[11]= 0.062633 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 231.000000 1.000000 1.000000 0.202222 0.579107 0.162394 CON U[11]= 0.039074 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 232.000000 1.000000 1.000000 0.290627 0.613283 0.105100 CON U[11]= 0.048558 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 233.000000 1.000000 1.000000 0.300542 0.648667 0.023572 CON U[11]= 0.065653 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 234.000000 1.000000 1.000000 0.226949 0.642796 -0.002056 CON U[11]= 0.077032 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 235.000000 1.000000 1.000000 0.138541 0.606091 0.053599 CON U[11]= 0.075786 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 236.000000 1.000000 1.000000 0.126543 0.575349 0.135391 CON U[11]= 0.057494 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 311.000000 1.000000 1.000000 0.294795 0.167253 0.451068 CON U[11]= 0.041138 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 312.000000 1.000000 1.000000 0.395496 0.142470 0.423285 CON U[11]= 0.050814 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 313.000000 1.000000 1.000000 0.450963 0.110175 0.474845 CON U[11]= 0.063788 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 314.000000 1.000000 1.000000 0.405314 0.101997 0.555541 CON U[11]= 0.072971 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 315.000000 1.000000 1.000000 0.304898 0.124311 0.585330 CON U[11]= 0.067946 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 316.000000 1.000000 1.000000 0.249641 0.157636 0.532809 CON U[11]= 0.055051 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 321.000000 1.000000 1.000000 0.097610 0.204117 0.446634 CON U[11]= 0.040110 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 322.000000 1.000000 1.000000 0.049919 0.261747 0.494237 CON U[11]= 0.050358 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 323.000000 1.000000 1.000000 -0.045731 0.247979 0.548032 CON U[11]= 0.064642 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 324.000000 1.000000 1.000000 -0.094704 0.175812 0.555667 CON U[11]= 0.069454 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 325.000000 1.000000 1.000000 -0.049695 0.119668 0.508976 CON U[11]= 0.067405 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 326.000000 1.000000 1.000000 0.046459 0.133047 0.454412 CON U[11]= 0.051639 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 331.000000 1.000000 1.000000 0.250891 0.137492 0.323816 CON U[11]= 0.042306 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 332.000000 1.000000 1.000000 0.294432 0.050317 0.349223 CON U[11]= 0.061409 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 333.000000 1.000000 1.000000 0.317383 -0.010561 0.304813 CON U[11]= 0.073241 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 334.000000 1.000000 1.000000 0.296365 0.017211 0.234025 CON U[11]= 0.088745 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 335.000000 1.000000 1.000000 0.249896 0.102407 0.209132 CON U[11]= 0.076940 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 336.000000 1.000000 1.000000 0.229030 0.162042 0.252374 CON U[11]= 0.056289 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 411.000000 1.000000 1.000000 -0.126378 0.426660 0.225783 CON U[11]= 0.043426 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 412.000000 1.000000 1.000000 -0.206412 0.571697 0.240622 CON U[11]= 0.069015 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 413.000000 1.000000 1.000000 -0.256722 0.576928 0.189865 CON U[11]= 0.064918 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 414.000000 1.000000 1.000000 -0.141678 0.496228 0.258097 CON U[11]= 0.056284 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 415.000000 1.000000 1.000000 -0.243070 0.507474 0.157509 CON U[11]= 0.064844 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 416.000000 1.000000 1.000000 -0.178801 0.431846 0.174705 CON U[11]= 0.059754 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 421.000000 1.000000 1.000000 0.015063 0.293774 0.160018 CON U[11]= 0.050373 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 422.000000 1.000000 1.000000 0.103145 0.330734 0.106184 CON U[11]= 0.065357 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 423.000000 1.000000 1.000000 0.148973 0.310793 0.035376 CON U[11]= 0.091406 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 424.000000 1.000000 1.000000 0.108697 0.254274 0.016536 CON U[11]= 0.101787 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 425.000000 1.000000 1.000000 0.021549 0.217031 0.067367 CON U[11]= 0.092210 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 426.000000 1.000000 1.000000 -0.026492 0.237453 0.140319 CON U[11]= 0.069390 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 431.000000 1.000000 1.000000 -0.122564 0.237294 0.322750 CON U[11]= 0.047647 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 432.000000 1.000000 1.000000 -0.216736 0.259281 0.369897 CON U[11]= 0.062324 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 433.000000 1.000000 1.000000 -0.280225 0.190645 0.424204 CON U[11]= 0.076923 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 434.000000 1.000000 1.000000 -0.246944 0.100742 0.428814 CON U[11]= 0.078984 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 435.000000 1.000000 1.000000 -0.153479 0.077866 0.383898 CON U[11]= 0.078071 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM C 436.000000 1.000000 1.000000 -0.089755 0.145575 0.332551 CON U[11]= 0.067507 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 1.000000 1.000000 1.000000 0.213716 0.397889 0.377500 CON U[11]= 0.051673 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 116.000000 1.000000 1.000000 0.513466 0.412883 0.114365 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 115.000000 1.000000 1.000000 0.579459 0.536282 -0.000454 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 114.000000 1.000000 1.000000 0.586380 0.680645 0.013332 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 113.000000 1.000000 1.000000 0.523898 0.699865 0.143049 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 112.000000 1.000000 1.000000 0.455636 0.575997 0.259534 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 126.000000 1.000000 1.000000 0.617775 0.304447 0.293826 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 125.000000 1.000000 1.000000 0.725568 0.178754 0.258779 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 124.000000 1.000000 1.000000 0.681780 0.089668 0.198916 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 123.000000 1.000000 1.000000 0.528682 0.128368 0.172046 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 122.000000 1.000000 1.000000 0.420582 0.254118 0.205175 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 136.000000 1.000000 1.000000 0.333151 0.326757 0.453393 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 135.000000 1.000000 1.000000 0.376818 0.318319 0.566167 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 134.000000 1.000000 1.000000 0.522346 0.382284 0.545416 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 133.000000 1.000000 1.000000 0.622992 0.455539 0.413559 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 132.000000 1.000000 1.000000 0.582432 0.460900 0.299755 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 216.000000 1.000000 1.000000 0.241683 0.723098 0.199929 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 215.000000 1.000000 1.000000 0.316144 0.811438 0.242218 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 214.000000 1.000000 1.000000 0.358737 0.747795 0.360275 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 213.000000 1.000000 1.000000 0.324181 0.595079 0.441489 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 212.000000 1.000000 1.000000 0.258477 0.502650 0.397883 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 226.000000 1.000000 1.000000 0.053170 0.688885 0.240487 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 225.000000 1.000000 1.000000 -0.115494 0.731284 0.311727 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 224.000000 1.000000 1.000000 -0.199764 0.629432 0.433423 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 223.000000 1.000000 1.000000 -0.129246 0.481729 0.485413 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 222.000000 1.000000 1.000000 0.040255 0.438699 0.413786 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 236.000000 1.000000 1.000000 0.062106 0.553914 0.174351 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 235.000000 1.000000 1.000000 0.086691 0.604250 0.031538 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 234.000000 1.000000 1.000000 0.236386 0.666437 -0.060506 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 233.000000 1.000000 1.000000 0.363305 0.677595 -0.016343 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 232.000000 1.000000 1.000000 0.346538 0.614719 0.122708 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 316.000000 1.000000 1.000000 0.177161 0.174572 0.553995 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 315.000000 1.000000 1.000000 0.272955 0.116577 0.643185 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 314.000000 1.000000 1.000000 0.445634 0.078796 0.593329 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 313.000000 1.000000 1.000000 0.522852 0.090860 0.455778 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 312.000000 1.000000 1.000000 0.427890 0.147983 0.365017 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 326.000000 1.000000 1.000000 0.079214 0.092033 0.420731 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 325.000000 1.000000 1.000000 -0.086431 0.070100 0.513899 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 324.000000 1.000000 1.000000 -0.164159 0.168330 0.593644 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 323.000000 1.000000 1.000000 -0.077983 0.288459 0.582669 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 322.000000 1.000000 1.000000 0.085293 0.312832 0.488593 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 336.000000 1.000000 1.000000 0.196966 0.223867 0.233692 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 335.000000 1.000000 1.000000 0.232662 0.119211 0.158761 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 334.000000 1.000000 1.000000 0.314000 -0.026904 0.202207 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 333.000000 1.000000 1.000000 0.350348 -0.072505 0.323197 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 332.000000 1.000000 1.000000 0.310161 0.030948 0.400130 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 413.000000 1.000000 1.000000 -0.299680 0.597212 0.154967 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 415.000000 1.000000 1.000000 -0.291210 0.543126 0.127940 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 416.000000 1.000000 1.000000 -0.170444 0.381441 0.152232 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 412.000000 1.000000 1.000000 -0.205964 0.612068 0.271098 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 414.000000 1.000000 1.000000 -0.097459 0.475394 0.292459 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 426.000000 1.000000 1.000000 -0.090409 0.209233 0.178672 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 425.000000 1.000000 1.000000 -0.008573 0.171709 0.054735 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 424.000000 1.000000 1.000000 0.145082 0.232935 -0.033150 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 423.000000 1.000000 1.000000 0.212288 0.335375 -0.003008 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 422.000000 1.000000 1.000000 0.133904 0.371798 0.119448 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 436.000000 1.000000 1.000000 -0.020386 0.128078 0.300480 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 435.000000 1.000000 1.000000 -0.131634 0.010345 0.391555 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 434.000000 1.000000 1.000000 -0.292280 0.051126 0.465970 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 433.000000 1.000000 1.000000 -0.346494 0.204701 0.461669 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 ATOM H 432.000000 1.000000 1.000000 -0.241059 0.326195 0.363940 CON U[11]= 0.075000 0.000000 0.000000 0.000000 0.000000 0.000000 CON SPARE= 0.00 0 0 0 END \DISK RETAIN 5 END # # Punched on 16-JAN87 at 15:59:13 # #LIST 6 READ NCOEFFICIENT = 5, TYPE = COMPRESSED, UNIT = DATAFILE INPUT H K L /FO/ RATIO MULTIPLIERS 1.0 1.0 1.0 2.843942642 3.768115520 END 0 0 1 189 584 2 99 176 3 36 44 4 449 699 5 421 571 6 677 854 7 189 176 8 57 42 9 55 35 10 100 72 11 83 57 12 292 196 13 83 47 16 89 40 18 151 57 512 1 0 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147 -11 159 87 -9 46 21 -8 184 135 -7 76 65 -6 514 533 -5 219 212 -4 115 93 -3 239 258 -2 361 430 -1 39 28 0 884 262 1 106 84 2 63 65 3 373 430 4 292 311 5 250 244 6 699 716 7 127 80 9 224 158 10 343 257 11 68 35 12 335 221 13 96 57 15 64 21 16 163 83 512 5 0 -17 127 63 -16 49 12 -13 110 68 -12 142 89 -11 198 113 -10 96 72 -9 141 79 -8 214 157 -7 286 238 -6 214 174 -5 445 447 -4 53 40 -3 152 124 -2 533 586 -1 632 712 0 370 400 1 452 500 2 147 119 3 148 121 4 306 300 5 221 190 6 285 246 7 223 168 10 302 205 11 225 133 12 100 64 13 175 80 16 160 69 17 147 59 512 6 0 -13 202 95 -12 85 44 -11 112 81 -9 43 15 -8 176 107 -7 398 332 -6 115 86 -5 211 164 -3 68 55 -2 271 247 -1 678 697 0 211 183 1 338 328 3 168 132 4 175 133 5 579 534 6 193 135 7 89 72 9 82 51 10 193 108 11 339 213 12 130 63 13 75 31 16 69 20 17 189 90 512 7 0 -15 64 20 -13 160 71 -12 243 130 -9 128 80 -7 211 134 -6 313 240 -3 99 75 -2 125 90 -1 449 413 0 474 442 1 92 66 3 228 176 4 160 104 5 407 338 6 388 305 7 106 70 9 150 83 10 64 28 11 212 107 12 198 95 13 58 18 14 54 14 15 98 43 17 111 45 512 8 0 -14 117 59 -12 229 111 -11 96 50 -9 100 67 -8 298 194 -7 82 49 -6 270 182 -5 189 119 -4 39 14 -3 183 121 -2 322 252 -1 69 46 0 458 390 1 178 121 3 267 198 4 409 327 6 372 271 7 176 97 8 99 63 9 151 79 10 253 139 11 68 28 12 156 79 13 93 43 15 112 51 16 183 92 512 9 0 -14 92 38 -13 133 75 -12 104 50 -11 154 69 -8 247 141 -7 308 194 -5 251 158 -3 52 23 -2 329 239 -1 475 378 0 90 67 1 103 78 2 76 50 3 54 26 4 336 240 5 370 267 6 123 66 7 72 37 8 77 41 10 236 121 11 237 113 13 61 18 16 142 58 512 10 0 -13 158 80 -12 70 23 -9 68 28 -8 51 17 -7 308 187 -6 181 90 -5 120 66 -2 121 78 -1 395 284 0 199 118 2 147 88 3 68 36 4 157 89 5 418 287 6 141 70 8 165 77 9 209 100 10 79 34 11 258 121 12 65 20 14 78 26 15 113 46 512 11 0 -13 68 18 -12 150 76 -10 63 21 -9 119 67 -8 80 37 -7 124 79 -6 247 133 -4 51 18 -3 130 86 -2 143 73 -1 135 81 0 275 170 1 61 28 3 183 95 4 150 77 5 242 132 6 192 97 8 82 40 9 230 109 10 158 82 11 152 82 12 159 75 15 122 48 512 12 0 -12 94 34 -9 96 43 -8 158 81 -7 56 17 -6 167 79 -5 65 27 -3 150 73 -2 328 195 -1 105 64 0 173 88 3 172 77 4 345 209 5 67 28 6 135 85 9 118 64 10 249 115 11 55 13 12 131 66 512 13 0 -8 140 80 -7 158 65 -6 51 14 -5 70 27 -4 81 37 -2 282 150 -1 317 176 1 85 46 2 86 47 3 73 34 4 248 129 5 294 161 8 96 44 10 141 69 11 168 76 512 14 0 -9 94 34 -7 185 78 -6 72 23 -4 87 37 -3 171 76 -1 262 131 0 133 77 2 66 26 3 192 86 5 240 113 6 128 75 9 121 59 11 146 73 512 15 0 -9 93 31 -8 131 61 -6 145 73 -3 149 75 -2 176 78 0 147 75 3 153 80 4 220 93 5 66 21 6 78 29 9 113 49 10 127 57 512 16 0 -8 121 47 -7 77 23 -6 75 23 -2 167 88 -1 90 37 0 60 17 3 90 36 4 223 89 5 61 17 7 56 14 8 77 25 9 62 15 10 195 89 512 17 0 -7 131 56 -4 64 17 -3 75 23 -2 97 37 -1 109 49 2 101 44 4 131 67 5 135 68 8 106 42 9 79 22 10 114 40 512 18 0 -4 57 12 -3 143 67 -1 122 54 3 148 77 5 104 39 512 19 0 -3 133 55 -2 132 54 3 119 47 4 142 64 512 -19 1 -3 123 49 -2 62 14 1 127 52 512 -18 1 -5 80 22 -4 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67 -11 104 49 -10 291 148 -9 79 37 -8 86 47 -7 81 41 -6 174 83 -5 78 41 -4 407 273 -3 86 52 0 144 80 1 195 109 2 335 224 3 136 69 5 193 96 6 169 89 7 129 80 8 194 90 9 90 47 11 119 66 12 140 80 14 83 28 512 -9 1 -16 121 49 -15 135 65 -13 51 12 -12 182 84 -11 84 36 -10 199 93 -9 185 87 -7 124 82 -6 310 200 -5 218 130 -4 196 115 -3 227 146 -1 85 61 0 403 310 1 128 71 2 188 111 3 157 84 5 131 87 6 367 243 7 89 52 8 193 94 9 53 18 11 49 13 12 226 99 13 78 28 512 -8 1 -15 112 49 -12 136 78 -11 195 88 -9 162 88 -8 46 15 -7 66 33 -6 254 167 -5 428 329 -3 160 95 -2 104 78 -1 98 67 0 358 291 1 578 486 2 43 17 3 110 85 4 68 41 5 126 83 6 259 164 7 304 196 9 76 39 10 81 43 11 120 74 12 140 74 13 187 76 512 -7 1 -17 137 61 -16 147 77 -11 235 126 -10 219 124 -8 72 41 -7 186 112 -6 57 29 -5 452 372 -4 251 191 -3 57 35 -1 202 153 0 133 83 1 527 474 2 351 292 3 83 63 4 75 53 5 249 179 6 104 82 7 316 222 8 193 110 10 61 27 11 180 90 13 166 76 14 120 66 512 -6 1 -16 183 81 -13 98 50 -12 194 93 -11 85 46 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137 78 -1 143 70 2 212 126 3 86 54 4 193 113 5 185 102 8 148 85 9 98 65 10 167 83 11 184 91 12 72 32 14 121 73 15 55 16 16 103 48 17 153 81 512 7 17 -7 105 46 -6 75 26 -3 162 79 -1 130 78 0 74 38 2 169 90 3 233 142 5 161 85 6 67 35 8 107 76 9 257 155 10 95 58 11 124 73 12 116 78 13 63 23 14 77 32 15 142 63 16 54 14 17 94 38 512 8 17 -6 93 40 -3 129 69 -2 177 80 0 109 71 3 214 125 4 210 122 6 125 84 7 108 80 9 219 122 10 231 127 12 102 60 13 77 33 15 122 67 16 155 73 17 57 14 512 9 17 -7 62 17 -6 71 23 -4 108 57 -2 215 105 -1 121 78 0 85 45 1 53 21 2 192 105 4 223 130 5 134 79 6 114 64 7 63 29 8 194 99 9 103 66 10 197 101 11 148 72 13 55 17 14 116 60 16 171 84 17 118 52 512 10 17 -7 106 44 -5 53 14 -4 130 79 -3 106 56 -2 99 49 -1 204 99 2 182 93 3 153 82 4 53 20 5 116 74 6 63 28 8 183 90 9 94 49 10 63 24 11 159 79 14 164 80 15 84 31 16 83 28 17 109 44 512 11 17 -6 60 16 -5 64 19 -3 141 63 -1 115 67 2 95 54 3 222 119 4 86 45 5 52 19 6 87 51 8 126 87 9 169 76 10 122 78 14 107 51 15 164 61 16 69 19 17 57 12 512 12 17 -3 84 34 -2 122 70 1 96 52 3 164 84 4 186 90 6 46 13 7 103 61 9 136 69 10 199 91 13 71 24 15 134 65 16 127 57 512 13 17 -4 80 28 -2 120 65 -1 87 38 1 102 54 2 160 84 4 168 86 5 83 39 6 79 36 7 122 77 8 213 102 10 146 66 11 109 55 12 50 12 14 149 63 16 92 30 512 14 17 -4 78 25 -3 94 37 -1 119 62 2 165 84 3 116 64 4 58 18 5 126 79 8 230 107 9 176 75 11 109 52 14 137 61 15 148 69 512 15 17 -3 130 61 -2 65 18 -1 76 26 1 114 59 3 157 72 4 85 37 7 91 39 8 69 22 9 169 66 10 101 43 13 97 36 15 154 72 512 16 17 -3 87 28 -2 119 52 1 103 45 2 96 41 3 63 18 4 127 70 5 56 15 7 100 46 8 76 27 10 94 37 13 124 54 512 17 17 2 138 73 3 66 19 4 91 35 5 63 17 8 131 64 13 85 24 512 18 17 2 116 49 3 101 38 8 120 50 9 113 44 512 19 17 3 104 37 5 57 12 7 122 49 9 117 44 512 -8 18 1 93 31 7 99 34 512 -7 18 -1 98 34 1 104 40 4 116 50 5 113 46 7 80 24 512 -6 18 -1 106 43 0 70 20 3 67 19 5 155 67 6 106 46 11 127 52 512 -5 18 0 125 65 3 89 36 4 84 31 5 51 12 6 152 82 8 54 13 9 74 24 10 94 36 12 139 62 512 -4 18 -2 127 61 0 81 29 1 127 72 4 154 72 5 83 33 6 63 20 7 77 29 10 138 63 11 69 21 13 83 27 512 -3 18 -5 81 24 -3 74 24 -2 95 40 -1 169 76 0 49 12 1 151 85 3 60 19 4 96 45 5 175 84 6 70 25 7 49 13 10 129 73 11 111 52 512 -2 18 -6 113 47 -3 99 44 -1 127 72 0 152 64 3 121 74 5 132 80 6 151 66 9 87 39 11 103 50 12 123 68 15 86 29 512 -1 18 -6 97 37 -5 78 25 -3 80 31 -2 90 40 0 124 73 3 143 73 4 167 84 6 134 77 7 67 27 9 131 65 10 108 56 12 104 51 15 95 36 512 0 18 -5 89 35 -2 139 85 -1 110 61 1 58 20 2 67 28 3 55 18 4 258 144 5 113 64 6 81 40 7 81 39 8 89 46 9 53 17 10 200 90 11 144 76 16 121 58 512 1 18 -7 114 49 -3 77 29 -2 82 36 -1 159 76 0 55 18 1 61 23 2 64 26 3 108 67 4 129 64 5 189 95 7 114 77 8 110 67 9 101 58 10 110 64 11 233 118 12 108 58 13 54 17 15 66 20 512 2 18 -7 78 24 -6 102 42 -3 172 82 -2 57 18 -1 119 73 0 175 79 3 215 118 4 68 31 5 89 52 6 158 76 9 210 109 10 83 40 11 109 62 12 158 74 15 123 69 17 56 13 512 3 18 -6 96 40 -4 94 44 -3 99 49 -2 145 70 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14 51 12 15 94 39 16 158 78 17 68 18 512 10 19 -4 112 51 -2 158 82 -1 119 68 0 59 19 2 175 77 4 156 77 5 103 61 8 193 92 10 105 55 11 79 34 13 65 21 14 140 83 16 113 50 512 11 19 -4 94 36 -3 94 37 -1 102 48 1 62 21 2 106 57 3 180 89 5 120 71 8 170 84 9 146 76 11 54 15 14 143 69 15 107 46 512 12 19 -3 127 65 -2 55 14 3 163 74 4 95 46 5 47 13 7 62 21 9 157 66 10 111 58 14 66 19 15 145 73 16 76 22 512 13 19 -2 106 46 1 95 43 2 82 32 3 110 58 4 132 78 7 117 66 8 81 32 9 94 42 10 148 78 13 96 39 14 61 15 15 57 12 512 14 19 -2 75 23 -1 80 28 2 138 67 4 122 68 5 66 23 6 77 31 7 65 21 8 234 106 10 82 29 11 77 26 14 144 70 512 15 19 2 102 45 3 135 75 6 50 12 8 172 86 9 145 68 11 91 35 14 120 49 512 16 19 1 99 39 3 126 64 4 93 38 7 98 39 9 128 63 10 70 19 13 98 34 512 17 19 2 107 43 4 111 47 5 58 14 7 90 31 8 88 29 10 76 22 512 18 19 5 55 12 8 119 48 9 60 12 512 -6 20 4 90 29 5 111 43 512 -5 20 3 74 22 5 111 46 6 88 30 9 63 15 512 -4 20 0 99 37 1 57 14 3 58 14 4 112 50 6 107 46 9 77 23 10 84 26 512 -3 20 -2 110 44 -1 78 24 1 101 43 4 127 66 5 115 57 7 70 22 10 132 63 11 99 38 512 -2 20 -3 54 11 -1 129 66 1 81 30 3 76 27 5 126 53 6 84 32 10 78 28 11 126 61 512 -1 20 -3 75 23 -1 75 25 0 124 66 3 115 63 4 63 20 5 78 31 6 129 73 9 84 34 11 66 20 12 83 30 512 0 20 -2 80 28 0 103 49 1 51 14 3 95 44 4 170 77 6 110 61 9 101 48 10 140 84 512 1 20 -2 96 42 -1 107 52 4 177 84 5 116 67 7 66 24 8 128 80 10 164 73 11 145 71 14 71 22 512 2 20 -3 65 19 -1 132 70 0 78 31 2 76 32 3 112 63 5 131 60 6 65 25 8 93 46 9 175 82 11 163 91 13 63 20 15 102 43 512 3 20 -3 125 67 -2 71 23 -1 74 28 0 140 68 3 162 79 4 128 83 5 70 28 6 117 75 9 215 103 10 99 50 12 88 40 15 124 64 16 96 37 512 4 20 -4 68 20 -3 55 14 -2 157 63 0 111 60 2 103 55 3 55 17 4 214 106 5 85 41 6 76 34 8 66 26 9 107 59 10 155 71 11 85 39 15 66 20 16 124 60 512 5 20 -4 76 26 -3 60 18 -2 128 72 -1 117 64 2 124 66 3 65 23 4 130 68 5 166 87 7 52 16 8 100 57 10 104 57 11 121 66 14 95 43 16 88 33 512 6 20 -3 83 31 -1 107 57 0 94 45 2 96 50 3 159 78 5 113 70 6 89 46 7 71 32 8 102 59 9 143 79 11 82 37 14 110 58 15 122 61 512 7 20 -3 93 40 -2 76 27 0 68 25 3 172 84 4 91 45 6 108 67 7 53 17 9 214 102 10 148 86 13 56 16 15 154 78 16 110 49 512 8 20 -4 84 31 -2 108 53 -1 68 23 2 106 57 3 66 24 4 170 87 5 63 24 6 62 23 7 46 12 8 137 71 9 96 47 10 210 97 11 85 37 12 58 18 14 89 37 16 144 80 512 9 20 -4 100 39 -3 53 13 -2 82 31 -1 121 66 2 155 78 3 101 52 4 98 51 5 126 83 8 196 91 9 106 55 10 91 43 11 135 66 14 139 73 15 83 29 512 10 20 -3 124 60 -1 108 53 1 81 35 2 67 23 3 183 79 5 83 38 6 59 20 8 133 86 9 183 90 10 69 25 11 78 32 13 67 21 14 101 45 15 136 71 16 70 19 512 11 20 -3 101 40 -2 105 46 0 65 21 1 73 27 2 69 24 3 118 69 4 146 76 6 82 37 7 96 50 9 139 84 10 99 49 13 102 46 15 116 52 16 116 50 512 12 20 -2 101 41 -1 83 31 2 148 75 4 125 75 5 99 50 8 164 74 10 87 37 11 64 20 13 86 33 14 105 44 512 13 20 -1 66 19 2 142 79 3 85 35 4 68 23 5 92 42 8 173 78 9 116 60 11 92 38 14 139 69 15 105 40 512 14 20 2 58 15 3 140 73 5 60 18 7 97 42 8 81 29 9 162 76 10 63 18 11 75 25 13 71 20 14 81 25 512 15 20 1 103 43 3 99 41 4 109 51 7 146 79 8 69 21 9 114 52 10 100 40 13 112 45 512 16 20 2 119 52 4 94 36 7 60 15 8 163 63 512 17 20 3 96 34 5 53 12 8 115 47 9 111 46 512 -4 21 4 106 41 5 89 31 7 63 16 512 -3 21 3 95 37 5 96 37 6 96 37 9 82 26 512 -2 21 0 98 38 3 68 20 4 110 49 6 114 55 9 96 37 10 94 35 512 -1 21 -2 93 33 1 78 27 4 147 80 5 87 34 7 89 38 -512 \DISK RESET 5 1 \LIST 12 BLOCK IR(1,U'S) UNTIL O(1) H(1,X'S,U[ISO]) CONT IR(1,X'S) UNTIL P(4) O(1,X'S) SCALE GROUP P(5) UNTIL F(6) GROUP C(111) UNTIL C(116) H(116) UNTIL H(112) RIDE C(111,U[ISO]) UNTIL C(116) H(116,U[ISO]) UNTIL H(112) GROUP C(121) UNTIL C(126) H(126) UNTIL H(122) RIDE C(121,U[ISO]) UNTIL C(126) H(126,U[ISO]) UNTIL H(122) GROUP C(131) UNTIL C(136) H(136) UNTIL H(132) RIDE C(131,U[ISO]) UNTIL C(136) H(136,U[ISO]) UNTIL H(132) GROUP C(211) UNTIL C(216) H(216) UNTIL H(212) RIDE C(211,U[ISO]) UNTIL C(216) H(216,U[ISO]) UNTIL H(212) GROUP C(221) UNTIL C(226) H(226) UNTIL H(222) RIDE C(221,U[ISO]) UNTIL C(226) H(226,U[ISO]) UNTIL H(222) GROUP C(231) UNTIL C(236) H(236) UNTIL H(232) RIDE C(231,U[ISO]) UNTIL C(236) H(236,U[ISO]) UNTIL H(232) GROUP C(311) UNTIL C(316) H(316) UNTIL H(312) RIDE C(311,U[ISO]) UNTIL C(316) H(316,U[ISO]) UNTIL H(312) GROUP C(321) UNTIL C(326) H(326) UNTIL H(322) RIDE C(321,U[ISO]) UNTIL C(326) H(326,U[ISO]) UNTIL H(322) GROUP C(331) UNTIL C(336) H(336) UNTIL H(332) RIDE C(331,U[ISO]) UNTIL C(336) H(336,U[ISO]) UNTIL H(332) GROUP C(411) UNTIL C(416) H(413) UNTIL H(414) RIDE C(411,U[ISO]) UNTIL C(416) H(413,U[ISO]) UNTIL H(414) GROUP C(421) UNTIL C(426) H(426) UNTIL H(422) RIDE C(421,U[ISO]) UNTIL C(426) H(426,U[ISO]) UNTIL H(422) GROUP C(431) UNTIL C(436) H(436) UNTIL H(432) RIDE C(431,U[ISO]) UNTIL C(436) H(436,U[ISO]) UNTIL H(432) END \LIST 22 END \PRINT 22 \PURGE end \ add CHECK to locate failing restraint (Restraint no 28) \check end \SFLS REFINE END \DISK RESET 5 1 DELETE 11 DELETE 22 \LIST 12 BLOCK GROUP IR(1) UNTIL H(1) \LIST 22 END \PURGE \SFLS REFINE END \DISK RESET 5 1 DELETE 22 DELETE 11 END \PURGE \DISK EXTEND FREE = 200 \LIST 12 BLOCK X Y Z \SFLS REFINE END \SFLS REFINE MATRIX=OLD END \DISK RESET 5 1 DELETE 22 DELETE 11 END \PURGE \SFLS CALC END \FINISH
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/1358/CH6/EX6.7/Example67.sce
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no_license
FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
2018-02-03T05:31:52
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Example67.sce
// Display mode mode(0); // Display warning for floating point exception ieee(1); clear; clc; disp("Turbomachinery Design and Theory,Rama S. R. Gorla and Aijaz A. Khan, Chapter 6, Example 7") disp("Blade speed U is given by: in m/s") D = 1050; N = 2800; U1 = %pi*D*N/(60*1000) disp("The velocity diagram is shown in Fig. Ex67. Applying the cosine rule to the triangle ABC,") C1 = 590; alpha1 = 20; V1 =(U1^2+C1^2-2*U1*C1*cos(alpha1*%pi/180))^0.5 disp("Applying the sine rule to the triangle ABC, C1sin (ACB) = V1/sin (alpha1)") disp("but sin(ACB) = sin(180-beta1) = sin(beta1)") beta1 = asin(C1*sin(alpha1*%pi/180)/V1)*180/%pi beta2 = beta1; disp("From Triangle ABD") Cw1 = C1*cos(alpha1*%pi/180) disp("From triangle CEF") disp("Ca2/(U + Cw2) = tan(beta2) = tan(beta1) = tan(26.75) = 0.504") Ca2 =155; Cw2 = Ca2/tan(beta1*%pi/180) -U1 DeltaCw = Cw1+Cw2 disp("Relative velocity at the rotor outlet is:") V2 = Ca2/sin(beta2*%pi/180) disp("Blade velocity coefficient is:") k = V2/V1 disp("Work done on the blades per kg/s: in kW") W = DeltaCw *U1/1000 disp("Diagram efficiency") etad = 2*W/(C1^2) *100000
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/system/kiks_arena_subroundobj.sci
cef56137923b2fd0c4a11f7eb3f6334bd7896d2f
[]
no_license
manasdas17/kiks-scilab
4f4064ed7619cad9e2117a6c0040a51056c938ee
37dc68914547c9d0f423008d44e973ba296de67b
refs/heads/master
2021-01-15T14:18:21.918789
2009-05-11T05:43:11
2009-05-11T05:43:11
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sci
kiks_arena_subroundobj.sci
function [] = kiks_arena_subroundobj(id,xpos,ypos) // Display mode mode(0); // Display warning for floating point exception ieee(1); // ----------------------------------------------------- // (c) 2000-2004 Theodor Storm <theodor@tstorm.se> // http://www.tstorm.se // ----------------------------------------------------- global("KIKS_MMPERPIXEL","KIKS_COLOR_CYLINDER","KIKS_ROUNDOBJMASK","KIKS_ROUNDOBJMASK_COL","KIKS_ARENA_MASK","KIKS_ARENA_COLORMASK","KIKS_ROUNDOBJECT_RADIUS"); [rows,cols] = size(mtlb_double(KIKS_ROUNDOBJMASK)); minx = mtlb_s(floor(mtlb_double(xpos)/mtlb_double(KIKS_MMPERPIXEL)),floor(mtlb_double(KIKS_ROUNDOBJECT_RADIUS)/mtlb_double(KIKS_MMPERPIXEL)));// xpos - object radius miny = mtlb_s(floor(mtlb_double(ypos)/mtlb_double(KIKS_MMPERPIXEL)),floor(mtlb_double(KIKS_ROUNDOBJECT_RADIUS)/mtlb_double(KIKS_MMPERPIXEL)));// ypos - object radius maxx = mtlb_a(floor(mtlb_double(xpos)/mtlb_double(KIKS_MMPERPIXEL)),floor(mtlb_double(KIKS_ROUNDOBJECT_RADIUS)/mtlb_double(KIKS_MMPERPIXEL))); maxy = mtlb_a(floor(mtlb_double(ypos)/mtlb_double(KIKS_MMPERPIXEL)),floor(mtlb_double(KIKS_ROUNDOBJECT_RADIUS)/mtlb_double(KIKS_MMPERPIXEL))); KIKS_ARENA_MASK(mtlb_imp(miny,maxy),mtlb_imp(minx,maxx)) = mtlb_s(mtlb_double(KIKS_ARENA_MASK(mtlb_imp(miny,maxy),mtlb_imp(minx,maxx))),mtlb_double(KIKS_ROUNDOBJMASK)); KIKS_ARENA_COLORMASK(mtlb_imp(miny,maxy),mtlb_imp(minx,maxx)) = mtlb_s(mtlb_double(KIKS_ARENA_COLORMASK(mtlb_imp(miny,maxy),mtlb_imp(minx,maxx))),mtlb_double(KIKS_ROUNDOBJMASK_COL)); endfunction
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/1382/CH6/EX6.11/EX_6_11.sce
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[]
no_license
FOSSEE/Scilab-TBC-Uploads
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2020-04-09T02:43:26.499817
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EX_6_11.sce
// Example 6.11;// feedback factor and Change in gain clc; clear; close; Zi=1;//input impedance without feedback in kiilo ohms Zo=10;//output impedance without feedback in kiilo ohms Zof=1;//output impedance with feedback in killo ohms A= 1000;// open loop voltage gain Beta=( (Zo/Zof)-1)/A;// feedback ratio BetaA= Beta*A;//feedback factor A1= (1-0.1)*A;//new open loop voltage gain Af=100;//FEEDBACK Af1= (A1/(1+(Beta*A1)));//GAIN WITH FEEDBACL dA=((Af-Af1)/Af)*100;// Change in overall gain in percentage disp(BetaA,"feedback factor is") disp(dA,"Change in overall gain in percentage is")
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/Toolbox Test/corrmtx/corrmtx8.sce
fa33f025c364f20182c80921f9a22dbcfd9f7b3b
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no_license
deecube/fosseetesting
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e353f1c03b0c0ef43abf44873e5e477b6adb6c7e
refs/heads/master
2021-01-20T11:34:43.535019
2016-09-27T05:12:48
2016-09-27T05:12:48
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corrmtx8.sce
//i/p args are x and m and the method is specified x=[1 2 3 4 5 7 4 62]; m=3; X = corrmtx(x,m,'modified'); disp(X); //output //. 4 3. 2. 1. // 5. 4. 3. 2. // 7. 5. 4. 3. // 4. 7. 5. 4. // 62. 4. 7. 5. // 1. 2. 3. 4. // 2. 3. 4. 5. // 3. 4. 5. 7. // 4. 5. 7. 4. // 5. 7. 4. 62. //matlab // 1.2649 0.9487 0.6325 0.3162 // 1.5811 1.2649 0.9487 0.6325 // 2.2136 1.5811 1.2649 0.9487 // 1.2649 2.2136 1.5811 1.2649 // 19.6061 1.2649 2.2136 1.5811 // 0.3162 0.6325 0.9487 1.2649 // 0.6325 0.9487 1.2649 1.5811 // 0.9487 1.2649 1.5811 2.2136 // 1.2649 1.5811 2.2136 1.2649 // 1.5811 2.2136 1.2649 19.6061
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449d555969bfd7befe906877abab098c6e63a0e8
/1586/CH5/EX5.8/EXP5_8.sce
c744c2dcf08b57c54374c4abb509e63c79bb1677
[]
no_license
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clc;funcprot(0);//EXAMPLE 5.8 // Initialisation of Variables H=10;.......//Required time to successfully carburize a batch of 500 steel gears t1=1173;......//Temperature at carburizing a batch of 500 steel gears in K t2=1273;.......//Temperature at carburizing a batch of 500 steel gears in K Q=32900;.........//The activation energy for diffusion of BCC steel R=1.987;.........//Gas constant in cal/mol.K c1=1000;......//cost per hour to operate the carburizing furnace at 900degree centigrades c2=1500;......//Cost per hour to operate the carburizing furnace at 1000 degree centigrade H2=(exp(-Q /(R*t1))*H*3600)/exp(-Q /(R*t2));.......// Time requried to successfully carburize a batch of 500 steel gears at 1000 degree centigrade Cp1=c1*H/500;.......//The cost per Part of steel rods at 900 degree centigrade Cv=(c2*3.299)/500;.......//The cost per Part of steel rods at 1000 degree centigrade disp(H2/3600,"Time requried to successfully carburize a batch of 500 steel gears at 1000 degree centigrade:") disp(Cp1,"The cost of carburizing per Part of steel rods at 900 degree centigrade") disp(Cv,"The cost of carburizing per Part of steel rods at 1000 degree centigrade")
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//Determine fourier transform of Given Signal and sketch magnitude and phase spectrum clc; clear; t=0:0.1:15; a=1; x=exp(-a*t).*(t>=0); X=dft(x,-1); Xmag=abs(X); subplot(1,2,1) plot(t,Xmag); xphase=atan(imag(X),real(X)); subplot(1,2,2) plot(t,xphase)
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clc;funcprot(0);//Example 1.2 //Initilisation of Variables A=2;...........//Area of ironplate in m^2 Q=100*10^3;.........//Conduction in W delt=70;.........//Temparature diffrence in degree celsius L=0.05;............//Thickness of plate in m //Calculations K=(Q*L)/(A*delt);...........//Thermal conductivity in W/(m*K) disp(K,"Thermal conductivity in W/(m*K):")
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//Scilab Code for Example 1.13 of Signals and systems by //P.Ramakrishna Rao clc; clear; //Discrete-time sequence plot clc A=10; t=0:1/1000:1; x=A*sin(2*%pi*100*t); q=plot2d3(t,x); disp('displaying a function plot on discrete time scale that has a sampling frequency of 1000 samples ps');
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//Transport Processes and Seperation Process Principles //Chapter 1 //Example 1.6-4 //Introduction to engineering principles and units //given data //heat of combustion for carbon to carbon dioxide is -393x10^3 kJ/kg mol or -94.0518 kCal/g mol //heat of combustion for carbon to carbon monoxide is -110x10^3 kJ/kg mol or -26.4157 kCal/g mol //basis: 10 g bol of carbon where 90% converts to carbon dioxide and rest to carbon monoxide HkJ=(90/100)*10*(-393.513)+(10/100)*10*(-110.523);//change in enthalpy= sum of heat of combustion of products(as reactant is a plain element) HkCal=(90/100)*10*(-94.0518)+(10/100)*10*(-26.4157); mprintf("change in enthalpy %f kJ",HkJ) mprintf("change in enthalpy %f kCal",HkCal) //end
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//Chapter 6 //Example 6_16 //Page 120 clear;clc; p=200; pf=0.8; fc=100; rc=0.05; pae=500; id=0.1; h=5000; x=fc; y=pae*id; ec_pf=sqrt(1-(y/x)^2); cap=p*(tan(acos(pf))-tan(acos(ec_pf))); uc=h*p; ec=uc*rc; cpae=y*cap; dc=x*p/ec_pf; ab=ec+cpae+dc; printf("Max demand charges = %.0f kW \n", x); printf("Expenditure on phase advnacing equipement = Rs. %.2f /kVAR/annnum \n\n", y); printf("(i) Most economical power factor at which factory should operate = %.3f lag \n\n", ec_pf); printf("(ii)Capacity of phase advancing equipment = %.2f kVAR \n\n", cap); printf("(iii) Units consumed per year = %.0f kWh \n", uc); printf("Annual energy charges = Rs. %.0f \n", ec); printf("Annual cost of phase advancing equipment = Rs. %.0f \n", cpae); printf("Max demand charges = Rs. %.0f \n", dc); printf("Annual bill for energy = Rs. %.0f \n", ab);
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clear; clc; funcprot(0); //Example - 15.11 //Page number - 528 printf("Example - 15.11 and Page number - 528\n\n"); //Given P = 12.25*101325*10^(-3);//[kPa] z_1 = 0.8; z_2 = 1 - z_1; V = 0.4; // log(P_1_sat) = 13.7713 - 2892.47/(T + 248.82) // log(P_2_sat) = 13.7224 - 2151.63/(T + 236.91) // P_1_sat = exp(13.7713 - 21892.47/(T + 248.82)); // P_2_sat = exp(13.7224 - 2151.63/(T + 236.91)); // Let the total mixture be 1 mol // We have to assume a temperature such that, // y_1 + y_2 = (K_1*z_1)/(1-V-K_1*V) + (K_2*z_2)/(1-V-K_2*V) = 1 // To assume a temperature we have to determine the BPT and DPT and take a temperature in between the range BPT to DPT // At the bubble point the whole feed lies in the liquid phase and an infinitesimal amount of vapour is formed, therefore x_1 = z_1; x_2 = z_2; // The bubble point pressure is given by // P = x_1*(exp(13.7713 - 21892.47/(T + 248.82))) + x_2*(exp(13.7224 - 2151.63/(T + 236.91))); deff('[y]=f(T)','y=x_1*(exp(13.7713 - 1892.47/(T + 248.82))) + x_2*(exp(13.7224 - 2151.63/(T + 236.91))) - P'); T_1 = fsolve(0.1,f); BPT = T_1; // At the dew point the whole feed lies in the vapour phase and a drop of liquid is formed, therefore y_1 = z_1; y_2 = z_2; // The dew point equation is given by // 1/P = y_1/P_1_sat + y_2/P_2_sat deff('[y]=f1(T)','y=1/(y_1/(exp(13.7713 - 1892.47/(T + 248.82))) + y_2/(exp(13.7224 - 2151.63/(T + 236.91)))) - P'); T_2 = fsolve(0.1,f1); DPT = T_2; // Now the assumed temperature should be in the range of BPT and DPT // Let the assumed temperature be 47 C T = 47;//[C] error = 10; while(error>0.001) P_1_sat = exp(13.7713 - 1892.47/(T + 248.82)); P_2_sat = exp(13.7224 - 2151.63/(T + 236.91)); K_1 = P_1_sat/P; K_2 = P_2_sat/P; y1 = (K_1*z_1)/(1-V+K_1*V); y2 = (K_2*z_2)/(1-V+K_2*V); y = y1 + y2; error=abs(y - 1); T = T - 0.0001; end printf(" The temperature when 40 mol %% of mixture is in the vapour is %f C",T);
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// Exa 2.1 clc; clear; close; // Given data lembda = 11000;// in Å lembda = lembda * 10^-10; h = 6.625*10^-34; c = 3*10^8; q = 1.6*10^-19;// in C E_g = h*c/lembda;// in J E_g= E_g/q;// in eV disp(E_g,"The energy gap in Si in eV is"); // Note: The answer in the book is not correct
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//Page Number: 5.42 //Example 5.35 clc; //Given, n=24; f=3.4D+3; //Hz ts=1D-6; //Second //(a) Spacing between succesive multiplexed pulses fs=8000; //Samples per second t1=1/fs; t2=n+1; //One synchronizing bit Tb=t1/t2; //Actual Tb, as actual duration of each pulse is 1us ATb=Tb-ts; disp('Seconds',ATb,'Spacing between succesive multiplexed pulses'); //(b) Nyquist Rate of Sampling f1=2*f; T=1/f1; //Seconds Tb1=T/t2; ATb1=Tb1-ts; disp('Seconds',ATb1,'Spacing between succesive multiplexed pulses using Nyquist rate of sampling');
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function [value] = kRadio_read(ref) // Ouput variables initialisation (not found in input variables) value=[]; // Display mode mode(0); // Display warning for floating point exception ieee(1); reply = kTurret(ref,4,"R"); // !! L.4: Matlab function sscanf not yet converted, original calling sequence used [value,count,errmsg] = sscanf(mtlb_e(reply,3:$),"%d,%d,%d,%d,%d,%d,%d,%d,%d,%d,%d,%d,%d,%d,%d,%d,%d,%d"); endfunction
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clc //Chapter9 //Example9.8, page no 400 //Given D1=1,D2=1.5*D1 // diameters of the new reflectors D1=1assumed for ease of calculation G_dbs=10*log10((D2/D1)^2)//Gain in dBs mprintf('Overall Gain is %f dBs',round(1000*G_dbs)/1000)
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// Ex3_12 clc; // Given: C=0.3;// in MeV^-1 a=2.0;// in MeV E=8; // in MeV // Solution: d=C*(exp(2*((2*8)^(0.5))));// excited level density s=(1/d)*1000;// level spacing nT=(E/a)^(0.5);// nuclear temperature printf("\n The excited level density is = %f MeV",d) printf("\n The level spacing is = %f keV",s) printf("\n The nuclear temperature is = %f MeV",nT)
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s=poly(0,'s'); H=[2/s,(s+1)/(s^2-5)]; Sys=tf2ss(H) clean(ss2tf(Sys))
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//to calculate the generator current and its pf clc; j=sqrt(-1); X=.24; r=400; //rating in MVA rr=600; //rating in MVA Pe=r/rr; Vt=1; Vth=1; dl=asind(Pe*X/(Vt*Vth)); Ia=2*sind(dl/2)/X; V=24000; IaB=(rr/3)*10^6/(V/sqrt(3)); Iaa=Ia*IaB;disp(Iaa,'generating current(A)'); phi=dl/2; pf= cosd(phi);disp(pf,'power factor'); Pe=1; dl1=asind(Pe*X/(Vt*Vth)); Ia=2*sind(dl1/2)/X; Iaa=Ia*IaB;disp(Iaa,'generating current(A)'); phi=dl1/2; pf= cosd(phi);disp(pf,'power factor'); Ef=Vt+j*Ia*(complex(cosd(-phi),sind(-phi)))*X; Eff=abs(Ef)*V; dl2=atand(imag(Ef)/real(Ef)); Xth=.24; Pe=abs(Ef)*Vth*sind(dl1+dl2)/(X+Xth);disp(Pe,'Pe(pu)');
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// chapter 9 // example 9.5 // find the equilibrium hole concentration and conductivity // page 273-274 clear; clc; // given ni=1.5E16; // in /m^3 (intrinsic carrier density) ue=0.135; // in m^2/(V-s) (electron mobilities) uh=0.048; // in m^2/(V-s) (hole mobilities) e=1.6E-19; // in C (charge of electron) ND=1E23; // in atom/m^3 (doping concentration) // calculate sigma_i=ni*e*(ue+uh); // calculation of intrinsic conductivity printf('\nThe intrinsic conductivity for silicon is %1.2E S',sigma_i); sigma=ND*ue*e; // calculation of conductivity after doping printf('\n\nThe conductivity after doping with phosphorus atoms is %1.2E S',sigma); rho=ni^2/ND; // calculation of equilibrium hole concentration printf('\n\nThe equilibrium hole concentration is %1.2E /m^3',rho);
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// chapter28 // example28.7 //page606 printf("Y = A . B + A . ( B + C ) + B . ( B + C ) \n") printf("By thoerem 14 \n") printf("Y = A . B + A . B + A . C + B . B + B .C \n") printf("By theorem 6 \n") printf("Y= A . B + A . B + A . C + B + B .C \n") printf("By theorem 5 \n") printf("Y = A . B + A . C + B + B . C \n") printf("Factor B out of last 2 terms \n") printf("Y = A . B + A . C + B . ( 1 + C ) \n") printf("Apply cummulative law and theorem 7 \n") printf("Y = A . B + A . C + B . 1 \n") printf("Apply theorem 2 \n") printf("Y = A . B + A . C + B \n") printf("Factor B out of first and third terms \n") printf("Y = B . ( A + 1 ) + A . C \n") printf("Apply theorem 7 \n") printf("Y = B . 1 + A . C \n") printf("Apply theorem 2 \n") printf("Y = B + A . C \n")
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// Exa 6.14 clc; clear; close; format('v',6) // Given data R1 = 100;// in ohm R2 = R1;// in ohm R3 = 3.9;// in k ohm R3 = R3 * 10^3;// in ohm R_F = R3;// in ohm Vx = -3.2;// in V Vy = -3;// in V // output voltage due to Vx, Vox = -(R_F/R1)*Vx and due to Vy, Voy = (R3/(R2+R3)) * (1+(R_F/R1))*Vy // Vo = Vox + Voy = -(R_F/R1)*Vx + (R_F/R1)*Vy (as R1=R2 and R3=Rf) //So, Aod = Vo/(Vx-Vy) = -R_F/R1; Aod = -R_F/R1; disp(Aod,"The closed loop differential gain is"); Vo = (-R_F/R1)*(Vx-Vy);// in V disp(Vo,"The output voltage in V is");
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-- Fuzzy Logix, LLC: Functional Testing Script for DB Lytix functions on Teradata -- -- Copyright (c): 2014 Fuzzy Logix, LLC -- -- NOTICE: All information contained herein is, and remains the property of Fuzzy Logix, LLC. -- The intellectual and technical concepts contained herein are proprietary to Fuzzy Logix, LLC. -- and may be covered by U.S. and Foreign Patents, patents in process, and are protected by trade -- secret or copyright law. Dissemination of this information or reproduction of this material is -- strictly forbidden unless prior written permission is obtained from Fuzzy Logix, LLC. -- Functional Test Specifications: -- -- Test Category: Math Functions -- -- Test Unit Number: FLMod-TD-01 -- -- Name(s): FLMod -- -- Description: Scalar function which returns the remainder after a number (dividend) is divided by another number (divisor) -- -- Applications: -- -- Signature: FLMod(x BIGINT, n BIGINT) -- -- Parameters: See Documentation -- -- Return value: BIGINT -- -- Last Updated: 01-29-2014 -- -- Author: <Zhi.Wang@fuzzyl.com> -- -- BEGIN: TEST SCRIPT -- .run file=../PulsarLogOn.sql -- .set width 2500 -- BEGIN: POSITIVE TEST(s) ---- Positive Test 1: Manual Example --- Same Output, Good SELECT FLMod(12,5) AS Modulo; ---- Positive Test 2: Dividend < Divisor --- Return expected results, Good SELECT FLMod(5,12) AS Modulo; SELECT FLMod(0,12) AS Modulo; ---- Positive Test 3: Negative Dividend or Divisor, --- Return expected results, Good SELECT FLMod(-12,5) AS Modulo; SELECT FLMod(12,-5) AS Modulo; SELECT FLMod(-12,-5) AS Modulo; ---- Positive Test 4: Should Output 0 --- Return expected results, Good SELECT FLMod(12,1) AS Modulo; -- END: POSITIVE TEST(s) -- BEGIN: NEGATIVE TEST(s) ---- Negative Test 1: Input Out of Boundary Values --- Return expected results, Good SELECT FLMod(CAST (2 ** 63 AS BIGINT),1) AS Modulo; ---- Negative Test 2: Divisor = 0 --- Return expected error, Good SELECT FLMod(12,0) AS Modulo; ---- Negative Test 3: Invalid Data Type --- Return expected error, Good SELECT FLMod(12,1.0) AS Modulo; SELECT FLMod(NULL,1) AS Modulo; SELECT FLMod(12,NULL) AS Modulo; -- END: NEGATIVE TEST(s) -- END: TEST SCRIPT
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function result = run(data, particles, iterations) ploty = zeros(iterations) [r, c] = size(data) distances = zeros(r, r) for i=1:r for j=1:r distx = (data(i,2) - data(j,2))^2 disty = (data(i,3) - data(j,3))^2 distances(i,j) = sqrt(distx + disty) end end f = zeros(particles) //objective function v = zeros(particles, r) //particle's velocity x = zeros(particles, r) //solutions, particles //weights c1 = [0.9:-(0.8/iterations):0.1] c2 = [0.05:(0.75/iterations):0.8] x = grand(particles, "prm", (1:r)) //random initial swarm for p=1:particles //x(p,:) = removecrossings(x(p,:), data) f(p) = objectivefn(x(p, :), distances) end pbestx = zeros(particles, r) //best route found by the particle gbestx = zeros(1, r) //best route found by the swarm pbestf = zeros(particles, 1) //best fitness reached by the particle pbestx = x //first route is the best so far pbestf = f //first fitness is the best so far [i, j] = min(pbestf) //index of smallest fitness (smaller is better) gbestx = pbestx(j, :) //best route found by all particles gbestf = pbestf(j) //best fitness found by all particles for i=1:iterations c3 = 1-(c1(i)+c2(i)) for p=1:particles // x = busca local na particula (hill climbing/delete crossings/2-opt) x(p,:) = neighborhoodinversion(x(p,:), c1(i)) //neighborhoodinversion - local search // pathrelinking entre pbest e x x(p,:) = pathrelinking(x(p,:), pbestx(p,:), c2(i)) // pathrelinking entre gbest e x x(p,:) = pathrelinking(x(p,:), gbestx(1,:), c3) // atualiza o f(p) f(p) = objectivefn(x(p, :), distances) if(f(p) < pbestf(p)) x(p,:) = removecrossings(x(p,:), c1(i)) pbestx(p,:) = x(p,:) pbestf(p) = f(p) if(f(p) < gbestf) gbestx = x(p,:) gbestf = f(p) end end end ploty(i) = gbestf disp("i:" + string(i) + "--gbest:" + string(gbestf) + "--weights:" + string(c1(i)) + ',' + string(c2(i)) + ',' + string(c3)) end plot2d(ploty) result = gbestf endfunction
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clc(); clear; //Given : V1 = 250; // potential in V V2 = 500;// potential in V theta1 = 45;// angle in degrees //Law of electron refraction = sin(theta1)/sin(theta2) = (V2/V1)^0.5 theta2 = asind(((V1/V2)^(1/2))*sind(45)); printf("theta2 = %d degrees",theta2);
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//Caption: Probability //Example 2.3 //page no 43 //find the probability clc; clear; total_cards=52; ways_of_drawingtwocards=52*51/(2*1);//ways of drawing 2cards from a deck of 52cards diamonds=13; Hearts=13; waysof_diamonds_Hearts=diamonds*Hearts;//ways of drawing a Diamond and a Heart probability=waysof_diamonds_Hearts/ways_of_drawingtwocards; disp(probability,"Probability that one card is Diamond and Othercard is Heart");
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a = 55 ; // Angle made by helix with longitudinal axis in degree r = 1.8 ; // Inner radius of vessel in m t = 0.02 ; // thickness of vessel in m E = 200e09 ; // Modulus of ealsticity of steel in Pa v = 0.3 ; // Poission's ratio of steel P = 800e03 ; // Pressure inside the tank in Pa // Part (a) s1 = (P*r)/t ; // Circumferential stress in Pa s2 = (P*r)/(2*t) ; // Longitudinal stress in Pa // Part (b) t_max_z = (s1-s2)/2 ; // Maximum inplane shear stress in Pa t_max = s1/2 ; // Maximum out of plane shear stress in Pa // Part (c) e1 = (s1/(2*E))*(2-v) ; // Strain in circumferential direction e2 = (s2/E)*(1-(2*v)); // Strain in longitudinal direction // Part (d) // x1 is the direction along the helix theta = 90 - a ; sx1 = ((P*r)/(4*t))*(3-cosd(2*theta)); // Stress along x1 direction tx1y1 = ((P*r)/(4*t))*(sind(2*theta)); // Shear stress in x1y1 plane sy1 = s1+s2-sx1 ; // Stress along y1 direction // Mohr Circle Method savg = (s1+s2)/2 ; // Average stress in Pa R = (s1 - s2 )/2 ; // Radius of Mohr's Circle in Pa sx1_ = savg - R*cosd(2*theta) ; // Stress along x1 direction tx1y1_ = R*sind(2*theta); // Shear stress in x1y1 plane
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// problem 10.3 d2=0.6 Q=20/60 N=1400/60 V1=2.8 g=9.81 y2=30 w=9810 Vf1=V1 Vf2=V1 u2=3.142*d2*N x=Vf2/tand(y2) Vw2=u2-x Hm=Vw2*u2/g P=(w*Q*Hm)/1000 disp(P,Hm,"head developed, pump power")
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disp('To find a basis for the eigenspace') disp('Matrix A=') a=[4 0 1;-2 1 0;-2 0 1] disp(a) disp('for lambda=1') disp('A-1I=') b=a-eye(3,3) disp(b) disp('solving (A-I)x=0, we get') disp('-2*x1=0 and 3*x1+x3=0') disp('therefore, x1=x3=0') disp('which leaves x2 as a free variable') disp('Hence a basis for the eigen space is:') disp([0;1;0]) disp('for lambda=2') disp('A-2I=') b=a-2*eye(3,3) disp(b) disp('performing row operations on the augmented matrix') c=[b [0;0;0]] disp(c) c(2,:)=c(2,:)+c(1,:) c(3,:)=c(3,:)+c(1,:) disp(c) c(1,:)=c(1,:)/c(2,2) disp(c) disp('We can see that x3 is a free variable') disp('x2=x3 and x1=-.05*x3') disp('Hence, a basis for the eigenspace is:') disp([-.5;1;1]) disp('for lambda=3') disp('A-3I=') b=a-3*eye(3,3) disp(b) disp('performing row operations on the augmented matrix') c=[b [0;0;0]] disp(c) c(2,:)=c(2,:)+2*c(1,:) c(3,:)=c(3,:)+2*c(1,:) disp(c) c(2,:)=c(2,:)/2 disp(c) disp('Again x3 is a free variable') disp('x1=-x3 and x2=x3') disp('Hence, a basis for the eigenspace is:') disp([-1;1;1])
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//scilab 5.4.1 clear; clc; printf("\t\t\tProblem Number 10.2\n\n\n"); // Chapter 10 : Refrigeration // Problem 10.2 (page no. 504) // Solution T1=20+273; //20C=20+273 R //Energy flows into the system at reservoir at constant temperature T1(unit:R) T2=-5+273; //-5C=-5+273 R //Heat is rejected to the constant temperature T2(Unit:R) printf("Solution for (a),\n"); COP=T2/(T1-T2); //Coefficient of performance printf("Coefficient of performance(COP) of the cycle is %f\n\n",COP); printf("Solution for (b),\n"); Qremoved=30; //Unit:kW //heat removal W=Qremoved/COP; //power required //unit:kW printf("The power required is %f kW \n\n",W); printf("Solution for (c),\n"); Qrej=Qremoved+W; //The rate of heat rejected to the room //Unit:kW printf("The rate of heat rejected to the room is %f kW",Qrej);
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//signals and systems //Inverse Z Transform:ROC |z|>2 z = %z; syms n z1;//To find out Inverse z transform z must be linear z = z1 X =-z*(z+0.4)/((z-0.8)*(z-2)) X1 = denom(X); zp = roots(X1); X1 = -z1*(z1+0.4)/((z1-0.8)*(z1-2)) F1 = X1*(z1^(n-1))*(z1-zp(1)); F2 = X1*(z1^(n-1))*(z1-zp(2)); h1 = limit(F1,z1,zp(1)); disp(h1,'h1[n]=') h2 = limit(F2,z1,zp(2)); disp(h2,'h2[n]=') h = h1+h2; disp(h,'h[n]=') //Inverse Z Transform:ROC 0.8<|z|<2 z = %z; syms n z1; X =-z*(z+0.4)/((z-0.8)*(z-2)) X1 = denom(X); zp = roots(X1); X1 = -z1*(z1+0.4)/((z1-0.8)*(z1-2)) F1 = X1*(z1^(n-1))*(z1-zp(1)); F2 = X1*(z1^(n-1))*(z1-zp(2)); h1 = limit(F1,z1,zp(1)); disp(h1*'u(n)','h1[n]=') h2 = limit(F2,z1,zp(2)); disp((h2)*'u(-n-1)','h2[n]=') disp((h1)*'u(n)'-(h2)*'u(n-1)','h[n]=') //Inverse Z Transform:ROC |z|<0.8 z = %z; syms n z1; X =-z*(z+0.4)/((z-0.8)*(z-2)) X1 = denom(X); zp = roots(X1); X1 = -z1*(z1+0.4)/((z1-0.8)*(z1-2)) F1 = X1*(z1^(n-1))*(z1-zp(1)); F2 = X1*(z1^(n-1))*(z1-zp(2)); h1 = limit(F1,z1,zp(1)); disp(h1*'u(-n-1)','h1[n]=') h2 = limit(F2,z1,zp(2)); disp((h2)*'u(-n-1)','h2[n]=') disp(-(h1)*'u(-n-1)'-(h2)*'u(-n-1)','h[n]=')
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function [intervalA, intervalB] = GetNewInterval(f, a, b) C0 = ( a + b ) / 2; if ( f( a ) * f( C0 ) < 0 ) then intervalA = a; intervalB = C0; elseif( f( b ) * f( C0 ) < 0) then intervalA = C0; intervalB = b; else disp( "Invalid interval specified" ) end endfunction function x = BisectionSolve( f, a, b, density ) it = 1; while %T [ a, b ] = GetNewInterval( f, a, b ); if(abs( a - b ) < density) x = ( a + b ) / 2; break; end it = it + 1; end mprintf( "\nSolved on iteration number %d\n", it ) endfunction
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//Eg-4.2 //pg-143 clear clc xl=0; xu=1; for i=1:20 fl=xl-cos(xl); fu=xu-cos(xu); rt=(xl+xu)/2; fr=rt-cos(rt); if fl*fr<0 then xu=(xl+xu)/2; elseif fr*fu<0 then xl=(xl+xu)/2; else rt=(xl+xu)/2; end end printf('The solution after 20 iterations is %f',rt)
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v=24; r1=2.2; r2=1; r3=4.7; disp("Part a"); i1=v/r1; disp("the current drawn (in mA) by R1 is"); disp(i1); i2=v/r2; disp("the current drawn (in mA) by R2 is"); disp(i2); i3=v/r3; disp("the current drawn (in mA) by R3 is"); disp(i3); disp("Part b"); i=i1+i2+i3; disp("the total current drawn (in mA) from the source is"); disp(i); disp("Part c"); r=v/i; disp("the combined resistance (in Ω) is"); disp(r); disp("Part d"); r=1/(1/r1+1/r2+1/r3); disp("the combined resistance (in Ω) using Eq. 6.4 is"); disp(r); disp("Part e"); i=v/r; disp("the total current drawn (in mA) using the combine resistance is"); disp(i); disp("Part f"); disp("the reading of the ammeter (in mA) between R1 and R2 is"); disp(i2+i3); disp("Part g"); p1=(v^2)/r1; disp("Power dissipated (in mW) by R1 is"); disp(p1); p2=(v^2)/r2; disp("Power dissipated (in mW) by R2 is"); disp(p2); p3=(v^2)/r3; disp("Power dissipated (in mW) by R3 is"); disp(p3); disp("Part h"); p=p1+p2+p3; disp("the total power dissipated (in mW) by the source is"); disp(p); disp("Part i"); disp("the voltage across R3 will remain 24 V");
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//Variable declaration f=50*10**3. //OPAMP freequency(Hz) Vm=0.02 //maximum value of signal voltage(V) S=.5*10**6 //slew rate(V/s) //Calculations Kvf=S/(2*(%pi)*f*Vm) //closed loop gain of amplifier //Results printf ("closed loop gain of amplifier is %.f",Kvf)
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clc; clear; //clears the console and all previously stored variables function V_0 = UpOutPut_BinMod(S_0, r, sigma, T, K, M) delta_t = T/M; //calculation of delta_t Beta = (exp(-r*delta_t)+exp((r+sigma^2)*delta_t))/2; //calculation of beta for CRR u=Beta+sqrt((Beta^2)-1); //so u>d is true d=u^-1; //because ud=1 q=(exp(r*delta_t)-d)/(u-d); //calculation of succes probability (u) S=zeros(M+1,M+1); //creation stock price matrix S(1,1)=S_0; //Setting stock price at t=0 as initial price in the stock matrix for i=2:M+1; //Initializing algo for computation of stock price for j=1:i; S(j,i)=S(1,1)*u^(j-1)*d^(i-j); //with j upwards and i-j downwards movements end; end; V=-ones(M+1,M+1); //creating option value matrix V(:,M+1)=max((K-S(:,M+1)), 0); //calculation of option values for last column for i=M:-1:1 //Initializing algo for computation of option price //for j=1:i (it is faster to use matrix operation than to include a second "for loop") //calculation of option values for rest of the matrix until V_0 V(1:i,i)=max(max((K-S(1:i,i)),0), exp(-r*delta_t)*(q*V(2:i+1,i+1)+(1-q)*V(1:i,i+1))); //end (not needed as second "for loop" is not used) end V_0 = V(1,1); //setting of first element of the option value matrix as option price at time t=0 endfunction S_0=100; r=0.05; sigma=0.2; T=1; , K=95, M=1000; V_0 = UpOutPut_BinMod(S_0, r, sigma, T, K, M); disp("Option price at time t=0 for an American put option is "+string(V_0));
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//Page Number: 298 //Example 5.13 clc; //Given f=9D+9;//hz v0=250;//V l=0.5;//cm l1=l/100;//m //Bandwidth n=3; df=(n+(3/4))/(6.774D-6*l1*sqrt(v0));//hz disp('Mhz',df/10^6,'Bandwidth:');
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function [t,x]=beuler(f,x0,ti,tf,h) //metodo de Backward Euler con iteracion de Newton //exec('jacobiant.sci') t=[ti:h:tf]; x=zeros(length(x0),length(t)); x(:,1)=x0; k=0; I=eye(length(x0),length(x0))//matriz identidad for tk=ti:h:tf-h k=k+1; //armamos la iteracion de Newton xprev=x(:,k); J=jacobiant(f,xprev,t(k+1));//Jacobiano del Sistema invH=pinv(I-h*J);//inversa del Hessiano x(:,k+1)=xprev-invH*(xprev-h*f(xprev,t(k+1))-x(:,k));//iteracion de Newton l=0; while norm(x(:,k+1)-xprev)>1e-6*(norm(xprev)+1e-3)&l<20 l=l+1; xprev=x(:,k+1); J=jacobiant(f,xprev,t(k+1));//Jacobiano del Sistema invH=pinv(I-h*J);//inversa del Hessiano x(:,k+1)=xprev-invH*(xprev-h*f(xprev,t(k+1))-x(:,k));//iteracion de Newton end end endfunction
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clc //Chapter3 //Ex_16 //Given h=6.6*10^-34 //in J s e=1.6*10^-19 // in coulombs E1=13.6 //in eV E1=E1*e //in J Z=1 n1=109 n2=110 ao=52.918*10^-12 // in m v=Z^2*E1*((1/n1^2)-(1/n2^2))/h disp(v*10^-6,"Frequency of radiation in MHz is") disp("The frequency of radiation in the transition from n1=109 to n2=110 is same as that of the detected frequency .Hence, the radiation comes from excited hydrogen atoms in the give transition") x=2*n2^2*ao disp(x*10^6,"The sie of the atom in micro meter is") //slight difference in the answer is due to approximations
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AJOUT dolly CompteEpargne 1234 100
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// Calculate the range of readings specified interms of f.s.d. and true value clc; disp('Range when specified interms of f.s.d.') Error_fsd=1*1000/100' Range_lower_value=100-Error_fsd; disp(Range_lower_value,'Lower value of range (kN/m2)') Range_upper_value=100+Error_fsd; disp(Range_upper_value,'Upper value of range (kN/m2)') disp('Range when specified interms of True value') Error_true=1*100/100' Range_lower_value=100-Error_true; disp(Range_lower_value,'Lower value of range (kN/m2)') Range_upper_value=100+Error_true; disp(Range_upper_value,'Upper value of range (kN/m2)')
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clc clear Ma=18000; //in kg/hr P=10; //in bar x=0.97; //Dryness Fraction Tfw=40; //in C Mf=2050; //in kg/hr CV=28000; //kJ/kg //At 10 bar Hf1=762.8; Hfg1=2015.3; H=Hf1+(x*Hfg1); Hfw=167.6; Eff=(Ma*100*(H-Hfw))/(Mf*CV); printf('Boiler efficiency: %3.2f Percent',Eff); printf('\n'); EA=((Ma/Mf)*(H-Hfw))/2257; printf('Equivalent Evaporation: %3.2f kg/kg of coal',EA); printf('\n');
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errcatch(-1,"stop");mode(2);//14.2; ; T=3*10^-3; f=1/T; printf("frequency of the voltage applied=%.2f m",f) exit();
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function SetTarget_() //** INRIA / SCILAB / Roberto Bucher / Simone Mannori / Paolo Gai //** 16 Jan 2008 //** Note: this code SHOULD be rewritten because respect the organization //** and style now obsolete. Future compatibility is not garantee. //** ------------- Preliminary I/O section ___________________________________________________________________________ k = [] ; //** index of the CodeGen source superbloc candidate xc = %pt(1); //** last valid click position yc = %pt(2); %pt = [] ; Cmenu = [] ; k = getobj(scs_m,[xc;yc]) ; //** look for a block //** check if we have clicked near an object if k==[] then return //** check if we have clicked near a block elseif typeof(scs_m.objs(k))<>"Block" then return end //** If the clicked/selected block is really a superblock //** <k> if scs_m.objs(k).model.sim(1)=="super" then disablemenus() lab = scs_m.objs(k).model.rpar.props.void3; //** Mark the super-block with a specific propriety if lab==[] then lab = ['dspic','ode4','10']; end ode_x = ['ode1';'ode2';'ode4']; //** Open a dialog box and wait user interaction while %t [ok, target, odefun, stp] = getvalue(.. "Embedded Code Generation ",.. ["Toolchain : "; "ODE cont. function solver: "; "Step between sampling: "],.. list('str',1,'str',1,'str',1),lab); if ~ok then break ; //** the the case of "cancel" exit end TARGETDIR = SCI+"/contrib/RT_templates"; // if exists("TARGET_DIR") then // [fd,ierr]=mopen(TARGET_DIR+'/'+target+'.gen','r'); // if ierr==0 then // TARGETDIR = TARGET_DIR; // mclose(fd); // end // end [fd,ierr] = mopen(TARGETDIR+'/'+target+'.gen','r'); if ierr==0 then mclose(fd); else x_message("Target not valid "+target+".gen"); ok = %f ; end if grep(odefun,ode_x) == [] then x_message("Ode function not valid"); ok = %f; end if ok then lab = [target,odefun,stp]; scs_m.objs(k).model.rpar.props.void3 = lab; break ; //** EXIT end end edited = %t ; enablemenus() else message("Generation Code only work for a Super Block ! "); end endfunction
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clc m=9.11*10^-31// kg*m/s v=10^5//m/s h=6.625*10^-34//js p=m*v disp(p,"momentum is") lambda=h/p disp(lambda,"de broglie wavelength in meter is")
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4_2_Theoretical_Problem.sce
clear; clc; printf('FUNDAMENTALS OF HEAT AND MASS TRANSFER \n Incropera / Dewitt / Bergman / Lavine \n EXAMPLE 4.2 Page 218 \n')// Example 4.2 //Theoretical Problem printf('\n The given example is theoretical and does not involve any numerical computation') //End
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//Problem 8.07: An electron in a television tube has a charge of 1.6 ð 1019 coulombs and travels at 3 ð 107 m/s perpendicular to a field of flux density 18.5 μT. Determine the force exerted on the electron in the field. //initializing the variables: Q = 1.6E-19; // in Coulomb v = 3E7; // in m/s B = 18.5E-6; // in Tesla u0 = 4*%pi*1E-7; //calculation: F = Q*v*B printf("\n\nResult\n\n") printf("\n Force exerted on the electron in the field. = %.2E N",F)
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//chapter6 //page no 140 //example 6-3 //given clear; clc; //data insufficient Rth=17.70; // Rth assumed minimum Rthc_H=0.65; //k/w Rthj_a=33; //k/w Rthj_c=3; //k/w RthH_a=1/(1/Rth-1/Rthj_a)-Rthj_c-Rthc_H; printf("RthH-a <= %0.1f K/W",RthH_a); //disp(RthH_a,"heat sink thermal resistance");
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//Example 4.14 clear; clc; //Given Cpw=75.42;//heat capacity of water in J K^-1 mol^-1 T=363; //temperature of water in K P=1;//pressure in atm Cpi=37.20;//heat capacity of ice in J K^-1 mol^-1 delHf=5980;// latent heat of fusion in J mol^-1 mp=273;//melting point of water in K n=10/18;//moles of ice taken //To calculate the entropy change T2=306;//since q=0 q1=n*delHf;//heat in J q2=n*Cpw*(T2-mp);//heat in J q3=n*2*Cpi*(T2-T);//heat in J delS1=q1/mp;//entropy change during 1st step in J K^-1 delS2=n*Cpw*log(T2/mp);//entropy change during 2nd step in J K^-1 delS3=2*n*Cpw*log(T2/T);//entropy change during final step in J K^-1 delS=delS1+delS2+delS3;//total entropy change in J K^-1 mprintf('Entropy change = %f J K^-1',delS); //end
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[fd,err] = mopen("verre2d","r") verre2d = read("verre2d",10100,101) mclose(fd) x=[1:1:101] y=[1:1:101] for t=0:99 drawlater(); clf() surf(verre2d(x+(t*101),y)) drawnow(); end
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//Example 1_6 clc; clear; //find the distance between the slits lamda=500 //units in nm lamda=500*10^-9 D=2 //units in mts f=100 d1=5 //units in cm d1=5*10^-2 //units in mts betaa=d1/f //unitd in mts //the distance between the slits d=(lamda*D)/betaa //units in mts d=d*10^3 //units in mm printf("distance between slits is %dmm",d)
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clear ; clc; // Example 5.6 printf('Example 5.6\n\n'); printf('Page No. 120\n\n'); // given x = 0.90;// dryness fraction m = 0.25;// Mass flow rate in kg/s P = 0.7;// pressure in bar T1 = 10;// in degree celcius //from steam table h_10= 42*10^3;// Specific enthalpy of water at 10 degree celcius in J/kg h_25 = 105*10^3;// Specific enthalpy of water at 25 degree celcius in J/kg h_30 = 126*10^3;// Specific enthalpy of water at 30 degree celcius in J/kg h_s = 2432*10^3;// Specific enthalpy of steam in J/kg //(a)T2 = 25; T2 = 25;// in degree celcius // By heat balance, heat transfered at 10 degree celcius = heat gained at 25 degree celcius; "(m*h_s)+(h_10*y)= (m*h_25)+(h_25*y)"; where 'y' is the quqntity of water to be used at 25 degree celcius in kg/s y = (m*(h_s-h_25)/(h_25-h_10)); printf('the quantity of water to be used at 25 degree celcius is %.2f kg/s \n',y) //(b)T2 = 30; T2 = 30;// in degree celcius // By heat balance, heat transfered at 10 degree celcius = heat gained at 30 degree celcius; "(m*h_s)+(h_10*y)= (m*h_30)+(h_30*y)"; where 'z' is the quqntity of water to be used at 30 degree celcius in kg/s z = (m*(h_s-h_30)/(h_30-h_10)); printf('the quantity of water to be used at 30 degree celcius is %.2f kg/s \n',z)
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clc; clf; clear all; n=-2:1; x=[1,-2,3,6]; subplot(221); a=gca(); a.x_location='origin'; b=gca(); b.y_location='origin'; plot2d3(n,x,4); title('x(n)'); xlabel('n'); ylabel('x(n)'); n=-1:2; y1=[6,3,-2,1]; subplot(222); a=gca(); a.x_location='origin'; b=gca(); b.y_location='origin'; plot2d3(n,y1,4); title('y1(n)'); xlabel('n'); ylabel('y1(n)'); n=-5:0; y2=[1,-2,3,6,0,0]; subplot(223); a=gca(); a.x_location='origin'; b=gca(); b.y_location='origin'; plot2d3(n,y2,4); title('y2(n)'); xlabel('n'); ylabel('y2(n)'); n=-3:0; y3=[12,6,-4,2]; subplot(224); a=gca(); a.x_location='origin'; b=gca(); b.y_location='origin'; plot2d3(n,y3,4); title('y3(n)'); xlabel('n'); ylabel('y3(n)');
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clc mo = 2 // mass of oxygen in kg mn = 6 // mass of nitrogen in kg muo = 32 // molecular mass of oxygen mun = 28 // molecular mass of nitrogen o = mo/muo // mass fraction of oxygen n = mn/mun // mass fraction of nitrogen xo = o/(n+o) // mole fraction of oxygen xn = n/(n+o) // mole fraction of nitrogen R = 8.314 // Universal gas constant Ro = R/muo // Gas constant for oxygen Rn = R/mun // Gas constant for nitrogen dS = -mo*Ro*log(xo)-mn*Rn*log(xn) // Increase in entropy printf("\n Example 10.9") printf("\n Increase in entropy is %f kJ/kg K",dS) //The answers vary due to round off error
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//Example 5.3 clear; clc; T0=25; IBT0=1*10^(-12); T=100; IBT=IBT0*2^((T-T0)/10); printf("IB(100degC)=%.2f nA",IBT*10^9);
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//Ideal Gas Equation clear; clc; printf("\t Example 5.5\n"); V1=0.55;//volume, L P1=1;//pressure at sea level, atm P2=0.4;//pressurea at 6.5km height, atm //n1=n2 and T1=T2 given hence P1V1=P2V2 V2=P1*V1/P2; printf("\t the volume of He balloon at height 6.5km above sea level is : %4.1f L\n",V2); //End
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; @Harness: disassembler ; @Result: PASS section .text size=0x00000080 vma=0x00000000 lma=0x00000000 offset=0x00000034 ;2**0 section .data size=0x00000000 vma=0x00000000 lma=0x00000000 offset=0x000000b4 ;2**0 start .text: label 0x00000000 ".text": 0x0: 0x00 0x04 cpc r0, r0 0x2: 0x10 0x04 cpc r1, r0 0x4: 0x20 0x04 cpc r2, r0 0x6: 0x30 0x04 cpc r3, r0 0x8: 0x40 0x04 cpc r4, r0 0xa: 0x50 0x04 cpc r5, r0 0xc: 0x60 0x04 cpc r6, r0 0xe: 0x70 0x04 cpc r7, r0 0x10: 0x80 0x04 cpc r8, r0 0x12: 0x90 0x04 cpc r9, r0 0x14: 0xa0 0x04 cpc r10, r0 0x16: 0xb0 0x04 cpc r11, r0 0x18: 0xc0 0x04 cpc r12, r0 0x1a: 0xd0 0x04 cpc r13, r0 0x1c: 0xe0 0x04 cpc r14, r0 0x1e: 0xf0 0x04 cpc r15, r0 0x20: 0x00 0x05 cpc r16, r0 0x22: 0x10 0x05 cpc r17, r0 0x24: 0x20 0x05 cpc r18, r0 0x26: 0x30 0x05 cpc r19, r0 0x28: 0x40 0x05 cpc r20, r0 0x2a: 0x50 0x05 cpc r21, r0 0x2c: 0x60 0x05 cpc r22, r0 0x2e: 0x70 0x05 cpc r23, r0 0x30: 0x80 0x05 cpc r24, r0 0x32: 0x90 0x05 cpc r25, r0 0x34: 0xa0 0x05 cpc r26, r0 0x36: 0xb0 0x05 cpc r27, r0 0x38: 0xc0 0x05 cpc r28, r0 0x3a: 0xd0 0x05 cpc r29, r0 0x3c: 0xe0 0x05 cpc r30, r0 0x3e: 0xf0 0x05 cpc r31, r0 0x40: 0x00 0x04 cpc r0, r0 0x42: 0x01 0x04 cpc r0, r1 0x44: 0x02 0x04 cpc r0, r2 0x46: 0x03 0x04 cpc r0, r3 0x48: 0x04 0x04 cpc r0, r4 0x4a: 0x05 0x04 cpc r0, r5 0x4c: 0x06 0x04 cpc r0, r6 0x4e: 0x07 0x04 cpc r0, r7 0x50: 0x08 0x04 cpc r0, r8 0x52: 0x09 0x04 cpc r0, r9 0x54: 0x0a 0x04 cpc r0, r10 0x56: 0x0b 0x04 cpc r0, r11 0x58: 0x0c 0x04 cpc r0, r12 0x5a: 0x0d 0x04 cpc r0, r13 0x5c: 0x0e 0x04 cpc r0, r14 0x5e: 0x0f 0x04 cpc r0, r15 0x60: 0x00 0x06 cpc r0, r16 0x62: 0x01 0x06 cpc r0, r17 0x64: 0x02 0x06 cpc r0, r18 0x66: 0x03 0x06 cpc r0, r19 0x68: 0x04 0x06 cpc r0, r20 0x6a: 0x05 0x06 cpc r0, r21 0x6c: 0x06 0x06 cpc r0, r22 0x6e: 0x07 0x06 cpc r0, r23 0x70: 0x08 0x06 cpc r0, r24 0x72: 0x09 0x06 cpc r0, r25 0x74: 0x0a 0x06 cpc r0, r26 0x76: 0x0b 0x06 cpc r0, r27 0x78: 0x0c 0x06 cpc r0, r28 0x7a: 0x0d 0x06 cpc r0, r29 0x7c: 0x0e 0x06 cpc r0, r30 0x7e: 0x0f 0x06 cpc r0, r31 start .data:
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//Variable Declaration p = 0.05 // probability of any device to show excessive drift //Calculation p1 = (1-p)^5*(p^1) // required probability //Results printf ( "probability of sixth measuring device to be the first to show excessive drift: %.3f",p1)
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Ex10_2.sce
//Chapter 10 : Crystallography and Crystal Imperfections clear; //Variable declaration rho=7.86*10**3 //density of material n=2 //No. of atoms/cell A=55.85 //Atomic weigth No=6.023*10**26 //Avagadro's No. //Calculations a=((n*A)/(No*rho))**(1/3)/10**-10 //Result mprintf("Lattice parameter a= %.5f*10**-10 m",a)
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Bf=1300//width of flange, in mm Df=80//thickness of flange, in mm d=600//effective depth, in mm sigma_cbc=7//in MPa sigma_st=140//in MPa m=13.33//modular ratio //to find critical depth of neutral axis Xc=d/(1+sigma_st/(m*sigma_cbc))//in mm Xc=240//round-off, in mm //to find Ast Ast=Bf*Df*(Xc-Df/2)/(m*(d-Xc))//in sq mm mprintf("Neutral axis depth=%d mm\nArea of steel=%f mm^2", Xc,Ast)
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// A Texbook on POWER SYSTEM ENGINEERING // A.Chakrabarti, M.L.Soni, P.V.Gupta, U.S.Bhatnagar // DHANPAT RAI & Co. // SECOND EDITION // PART II : TRANSMISSION AND DISTRIBUTION // CHAPTER 10: POWER SYSTEM STABILITY // EXAMPLE : 10.21 : // Page number 305-306 clear ; clc ; close ; // Clear the work space and console // Given data f = 50.0 // Frequency(Hz) P = 4.0 // Number of poles G = 20.0 // Rating of turbo-generator(MVA) V = 13.2 // Voltage(kV) H = 9.0 // Inertia constant(kW-sec/kVA) P_s = 20.0 // Input power less rotational loss(MW) P_e = 15.0 // Output power(MW) // Calculations KE = G*H // Kinetic energy stored(MJ) M = G*H/(180*f) // Angular momentum(MJ-sec/elect.degree) P_a = P_s-P_e // Accelerating power(MW) alpha = P_a/M // Acceleration(elect.degree/sec^2) alpha_deg = alpha/2.0 // Acceleration(degree/sec^2) alpha_rpm = 60.0*alpha_deg/360 // Acceleration(rpm/sec) // Results disp("PART II - EXAMPLE : 10.21 : SOLUTION :-") printf("\nCase(a): Kinetic energy stored by rotor at synchronous speed, GH = %.f MJ", KE) printf("\nCase(b): Acceleration, α = %.f degree/sec^2", alpha_deg) printf("\n Acceleration, α = %.2f rpm/sec", alpha_rpm)
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clc clear //Initialization of variables l=6 //ft d1=0.55 //in d2=0.75 //in h1=280 //Btu/hr ft^2 F h2=2000 //Btu/fr ft^2 F k=220 //Btu/hr ft F t2=212 //F t1=60 //F //calculations A2=%pi*d1*l/12 A3=%pi*d2*l/12 Rt=1/(h1*A2) + 1/(h2*A3) +log(d2/d1) /(2*%pi*k*l) U3=1/(A3*Rt) //results printf("Overall Heat transfer coefficient = %.1f Btu/hr ft^2 F",U3) disp("The answer in the textbook is a bit different due to rounding off error in textbook.")
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clear; clc; ZR=300;s=9;d=0.1 r=d/2; Zof=276*log10(s/r); Zoq=sqrt(ZR*Zof); do=(s*2)/10^(Zoq/276); printf("Diameter of wire used = %f cm",fix(do*10)/10);
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// 4.2 clc; t=600; C=2.5*10^-12; E=500; e=300; a=log10(E/e) R=(0.4343*t)/(C*a); printf("Insulation resistance=%.2f mega-ohm",R)
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5_3.sce
//ques-5.3 //Finding specific and equivalent conductance of acid clc R1=225;//resistance of KCl (in ohms) k1=0.00141;//specific conductance of KCl (in mho/cm) R2=80;//resistance of acid solution (in ohms) N=0.02;//normality of acid c=k1*R1;//cell constant (in /cm) k2=c/R2;//specific conductance of acid solution (in mho/cm) e=1000*(k2/N);////equivalent conductance of acid solution (in cm^2 mho/eq) printf("The equivalent conductance of acid is %.2f cm^2 mho/eq and specific conductance is %.6f mho/cm.",e,k2);
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Example2_5.sce
//clear// //Caption: Program to calculate Fiber Birefringence BETA_f //Example2.5 //page 65 clear; close; clc; Lambda = input('Enter the wavelength of Optical Signal'); Lp = input('Beat Length'); BETA_f_FORMULA1 = 2*%pi/Lp; disp(BETA_f_FORMULA1,"The fiber birefriengence using formula 1"); BETA_f_FORMULA2 = Lambda/Lp; disp(BETA_f_FORMULA2,"The fiber birefriengence using formula 2"); //Result //Enter the wavelength of Optical Signal 1300e-09 //Beat Length 8e-02 //The fiber birefriengence using formula 1 78.539816 //The fiber birefriengence using formula 2 0.0000162
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lines(0); ilib_verbose(0); ierr = exec('loader.sce', 'errcatch'); if ierr <> 0 then disp(lasterror()); exit(ierr); end // Call our gcd() function x = 42; y = 105; g = gcd(x,y); printf("The gcd of %d and %d is %d\n",x,y,g); // Manipulate the Foo global variable // Get its default value (see in example.c) defaultValue = Foo_get() if defaultValue <> 3 then pause; end // Change its value Foo_set(3.1415926) // See if the change took effect if Foo_get() <> 3.1415926 then pause,end exit
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ex7_4.sci
//Chapter 7,Ex7.4,Pg7.15 clc; B=100 Icbo=4 //current in microamperes Ib=40 //Current in microamperes Ic=B*Ib+(B+1)*Icbo printf("\n Ic=%.1f mA \n",Ic*10^-3)
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ex4_2.sce
// Exa 4.2 clc; clear; close; // Given data // w = 2*g*h g = 9.81; m =(0.2+10/1000)*10^3 ;// in gm s = 1;// in cal/gm°C del_T = 2;// in °C H = m * s * del_T;// in cal H = H * 10^-3;// kcal J = 4.1868 * 1000; // W= 2*g*h= J*H h = J*H/(2 * g);// in m disp(h,"Height from which the mass should fall in meter is : ");