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Ex4_17.sce
//Chapter-4, Illustration 17, Page 148 //Title: Gears and Gear Drivers //============================================================================= clc clear //Input data Ta=20// no of teeth on pinion A Tb=25// no of teeth on wheel B Tc=50// no of teeth on gear C Td=60// no of teeth on gear D Te=60// no of teeth on gear E Na=200// SPEED of the gear A Nd=100// speed of the gear D //calculations //(i) //(5/6)x+y=0 //(5/4)x+y=200 A1=[(Tc/Td) 1 (Tb/Ta) 1]//Coefficient matrix B1=[0 Na]//Constant matrix X1=inv(A1)*B1//Variable matrix Ne1=X1(2)-(Tc/Td)*X1(1)// T1=(-Ne1/Na)// ratio of torques when D is fixed //(ii) //(5/4)x+y=200 //(5/6)x+y=100 A2=[(Tc/Td) 1 (Tb/Ta) 1]//Coefficient matrix B2=[Nd Na]//Constant matrix X2=inv(A2)*B2//Variable matrix Ne2=X2(2)-(Tc/Td)*X2(1) T2=(-Ne2/Na)// ratio of torques when D ratates at 100 rpm //Output printf('speed of E= %.2f rpm in clockwise direction\n speed of E in 2nd case(when D rotates at 100 rpm)= %d rpm in clockwise direction\n ratio of torques when D is fixed= %d \n ratio of torques when D ratates at 100 rpm= %d',Ne1,Ne2,T1,T2)
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exec('put.sci') r=0.03 sigma=0.1 K=100 s=[1:10]*20 t=[1/12,1/6,1/4,1/3,1/2,1] p=zeros(10,6) for i=[1:10] for j=[1:6] p(i,j)=put(s(i),r,sigma,T,K) end end plot3d(s,t,p)
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ex14_1.sce
// Example 14.1 format('v',6) clc; clear; close; // given data V1=15;// in V V2=1;// in V R= 100;// in Ω // The load current I= (V1-V2)/R;// in A I= I*10^3;// in mA disp(I,"The load current in mA is : ")
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function changeModeSciMtlb() //vtVar=fscanfMat(nomearq) endfunction
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example_7_1.sce
//example 7.1 clear; clc; //for 50 kHz clock clk_frq1 = 50000; c_t_500 = 1000/clk_frq1; //for 8-MHz clock clk_frq2 = 8000000; c_t_8 = 10000000/clk_frq2; printf('Cycle time for 500-kHz clock is %f milliseconds \n',c_t_500);//displaying results printf(' Cycle time for 8-MHz clock is %f micro seconds',c_t_8);
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//Example 4.4. clc format(6) disp("In an N-type material, the concentration of donor atoms is given by") disp("ND = NC*e^(-(EC - EF)/k*T)") disp("Let initially ND = ND0, EF = EF0 and EC - EF0 = 0.2 eV") disp("Therefore, ND0 = NC*e^(-0.2/0.025) = NC*e^-8") disp("(a) When ND = 4ND0 and EF = EF1, then") disp("4*ND0 = NC*e^(-(EC-EF1)/0.025) = NC*e^-40(EC - EF1)") disp("Therefore, 4*NC*e^-8 = NC*e^-40(EC - EF1)") disp("Therefore, 4 = e^(-40*(EC - EF1)+8)") disp("Taking natural logarithm on both sides, we get") disp("ln 4 = -40(EC - EF1) + 8") q1=(8-log(4))/40 disp(q1,"EC - EF1(in eV) = ") disp("(b) When ND=8*ND0 and EF = EF2, then") disp("ln 8 = -40*(EC - EF2) + 8") q2=(8-log(8))/40 disp(q2,"EC - EF2(in eV) = ")
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equalsMatrix.sci
function R = equalsMatrix(M, N) [h,w] = size(M) [h2,w2] = size(N) if w <> w2 | h <> h2 then R = %f else R = %t for i = 1:h for j = 1:w R = R & M(i,j) == N(i,j) end end end endfunction
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4_5.sce
clc //initialisation of variables H1= 10//ft H2=2 //ft d= 0.62 so= 3 //in w= 5 //ft g= 32.2 //ft/sec^2 b= 2.5 //ft b1= 7.5 //ft //CALCULATIONS A1= w*b A2= w*b1 a= so^2/144 T= (2*A1*(H1^0.5-H2^0.5))/(d*a*(1+(A1/A2))*sqrt(2*g)) //RESULTS printf (' Time required to lower the level of water = %.1f sec',T)
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//Chapter-4,Example4_15_13,pg 4-32 d=2650 //density Y=8*10^10 //Young's modulus n=2*10^6 //frequency of wave k=1 //consider 1st harmonic t=(k/(2*n))*sqrt(Y/d) //arranging formula of natural frequency printf("thickness =") disp(t) printf("meter")
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//Ex 2.7.1 clc;clear;close; format('v',6); //Given : Vgamma=0.6;//volt rf=12;//ohm V=5;//volts R=1;//kohm IF=(V-Vgamma)/(R*1000+rf);//A disp(IF*1000,"Diode current in mA :"); VF=Vgamma+IF*rf;//volts disp(VF,"Diode voltage in volts :");
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s=%s ; //create state equation of the following matrix TFcont=syslin ('c',(s^2+3*s+3)/(s^3+2*s^2+3*s-1)) SScont=tf2ss(TFcont ) [Ac ,Bc ,U, ind ]=canon( SScont ( 2 ) , SScont ( 3 ) ) disp(Ac,"MAtrix A=") disp(Bc,"MAtrix B=") s=%s; A =[0 0 1;1 0 -3;0 1 -2]; B =[3;3;1]; x =[0 0 1]; [r c]= size (A) p=s*eye(r,c)-A // s*I-A q=inv(p) c=x*q*B; disp(c,"required transfer function =")
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//radiation resistance of hertzian dipole //given clc lemda=1//as the radiation resistance is independent of lemda function[Rr]=rad_resistance(dl) for(lemda!=0) Rr=80*%pi^2*(dl/lemda)^2 Rr=round(Rr*1000)/1000///rounding off decimals end endfunction dl=lemda/20 [Rr1]=rad_resistance(dl) dl=lemda/30 [Rr2]=rad_resistance(dl) dl=lemda/40 [Rr3]=rad_resistance(dl) disp(Rr3,Rr2,Rr1,'the radiation resistance of hertzian dipole')
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DPSK Modulation.sce
clc; clear; xdel ( winsid () ) ; //Differential Phase shift keying b = [1 0 1 0 1 0 1 0]; //Diffreential Eccoding d = 1;// Initial bit dc=[]; for i = 1:length(b) dc = [dc d]; d=~(bitxor(d,b(i))); end dc=[dc d]; //Bit to symbol mapping for ii = 1:length(dc) if dc(ii)==1; nn(ii)=1; else nn(ii)=-1; end end // pulse shaping S = 100; i = 1; t=0:1/S:length(dc); for j = 1:length(t) if t(j)<=i; m(j)=nn(i); else m(j)=nn(i); i=i+1; end end //plotting subplot(411); plot2d2(t,m, style=[color("navy blue")]); xlabel('Time'); ylabel('Amplitude'); title('NRZ polar signal'); // Carrier Signal c=cos(2*%pi*2*t); subplot(412); plot2d2(t,c, style=[color("navy blue")]); xlabel('Time'); xlabel('Time'); ylabel('Amplitude'); title('Carrier Signal'); //BPSK Modulation x = m' .* c; subplot(413); plot2d2(t,x, style=[color("red")]); xlabel('Time'); xlabel('Time'); ylabel('Amplitude'); title('DPSK Modulated Signal'); //Coherent Detection and reconstruction y=x; y1=y.*c; // Product Modulator subplot(414); plot2d2(t,y1, style=[color("green")]); xlabel('Time'); xlabel('Time'); ylabel('Amplitude'); title('DPSK Demodulated signal'); //Integrator output //k=1/S:1/S:1; int_op=[]; for ii=0:S:length(y1)-S; int_o=(1/S)*inttrap(y1(ii+1:ii+S)); int_op=[int_op int_o]; end //Hard decision decoding for i = 1 : length(int_op); if int_op(i) >=0; detect(i) = 1; else detect(i)=0; end end disp('Input Bits:') disp (b) disp('DPSK Modulated Bits:') detect1 = detect(2:length(detect)); disp(detect1') //Differential detection for ii = 1:length(detect)-1; if detect(ii)==detect(ii+1); op(ii)=1; else op(ii)=0; end end disp('DPSK Demodulated Bits:') disp(op')
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first(2).sce
Vc=9; fc=100; fm=50; t=0:0.001:0.5; m=0.5; subplot(311); plot(Vc*(cos(2*3.14*fc*t)+m*(sin(2*3.14*fm*t)))); subplot(312); plot(Vc*(cos(2*3.14*fc*t)+1*(sin(2*3.14*fm*t)))); subplot(313); plot(Vc*(cos(2*3.14*fc*t)+2*(sin(2*3.14*fm*t))));
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java -ea make.Main -f make-tests/make04.mk -D make-tests/file04 A
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12_18.sce
clear; clc; close; Tj = 200; Ta = 40; Qjc = 0.5; Qcs = 0.6; Qsa = 1.5; Pd = (Tj-Ta)/(Qjc+Qcs+Qsa); disp(Pd,'Maximum power dissipated(Watts) = ');
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clc,clear //Example 6.13 //To determine the cube roots of i z=%i //given complex number //modulii for cuberoots r1=abs(z)^(1/3) r2=abs(z)^(1/3) r3=abs(z)^(1/3) //arguements for cuberoots theta1= (phasemag(z)+360*0)/3 theta2= (phasemag(z)+360*1)/3 theta3= (phasemag(z)+360*2)/3 cube_root_1 = r1 *(cosd(theta1)+ %i*sind(theta1)) cube_root_2 = r2 *(cosd(theta2)+ %i*sind(theta2)) cube_root_3 = r3 *(cosd(theta3)+ %i*sind(theta3)) printf('cuberoot 1: %f + %f*i\n',real(cube_root_1),imag(cube_root_1)) printf('cuberoot 2: %f + %f*i\n',real(cube_root_2),imag(cube_root_2)) printf('cuberoot 3: %f + %f*i\n',real(cube_root_3),imag(cube_root_3))
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//CHAPTER 8- DIRECT CURRENT MACHINES //Example 31 disp("CHAPTER 8"); disp("EXAMPLE 31"); //series motor //VARIABLE INITIALIZATION r_a=0.1; //combined resistance of armature & field resistance in Ohms v_t=230; //in Volts I_a1=100; //in Amperes N1=1000; //in rpm I_a2=200; //in Amperes ratio=1.2; //ratio of Φ2:Φ1=1.2 //SOLUTION //Eb1 dir prop phi1.N1 //Eb1=Vt-Ia1.Ra //=> (Vt-Ia1.Ra) dir prop ph1.N1 //and //=> (Vt-Ia2.Ra) dir prop ph1.N2 //=> (Vt-Ia1.Ra)/ (Vt-Ia1.Ra) = phi1.N1/phi2.N2 //given Phi2=1.2 Phi1 as flux is increased by 20% E_b1=v_t-(I_a1*r_a); //numerator of LHS according to the book E_b2=v_t-(I_a2*r_a); //denominator of LHS according to the book N2=(E_b2/E_b1)*(1/ratio)*N1; N2=round(N2); //to round off the value disp(sprintf("The new speed of the armature is %d rpm",N2)); //END
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// to find if diode will get destroyed // Electronic Principles // By Albert Malvino , David Bates // Seventh Edition // The McGraw-Hill Companies // Example 3-2, page 63 clear;clc; close; // Given data v=1.2; // diode voltage in volts i=1.75; // diode current in amperes P(1)=5;// power rating in watts // Calculations P(2)=v*i; // power dissipation disp("Watts",P(2),"Power dissipation") // Result // As power dissipation is lower than power rating the diode will not get destroyed.
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errcatch(-1,"stop");mode(2);//Caption:Find the frequency of voltage generated //Exa:13.1 ; ; p=16//Number of poles n=375//Speed of alternator(in r.p.m) f=(p*n)/120 disp(f,'Frequency of voltage generated(in c/s)=') exit();
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clc; clear all; Vp=50;//given peak to peak envelope voltages Vr=1;//given voltage of envelope ripple in volts Sc=20*log10(Vp/Vr);//carrier supression in db disp(Sc,'carrier supression in dB is=');
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Checking that a simple switch to single is working. In this case, upon encountering the single block, the Single is for Single spacing Verbatim allows text that matches the Itemize uses ticks to indicate items Center allows a block to be centered Notice that all of the whitepace should be removed and at this point, we should return to whatever the spacing had been
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A=[4,-1,1;1,1,1;-2,0,-6;] disp(A) printf('Eigen values are:') disp(spec(A)) printf('Display of Shifting in Power Method:') printf('Shifted Matrix (Shifted by -6)is') A1=A-(-6)*eye(3,3) disp(A1) printf('Inverse of Shifted Matrix is' ) A=inv(A1) disp(A) U=[1,1,1]' for i=1:4 B=A*U a=abs(B(1,1)) b=abs(B(2,1)) c=abs(B(3,1)) if ((a>b)&(a>c)) then T= (B(1,1)) elseif ((b>a)&(b>c)) then T=(B(2,1)) else T=(B(3,1)) end printf('After %d iteration eigenvalue of Inverse Shifted Matrix is ',i) disp(T) printf(' corresponding eigenvector of Inverse Shifted Matrix is ') U=B/T disp(U) end T1=1/T T2=-6+T1 printf('Largest eigen value of Shifted Matrix' ) disp(T1) printf('Largest eigen value of Matrix is' ) disp(T2)
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//valores Linealizados analiticamente caso del pendulo paper // Load the parameters exec('edsonjParametersPap.sce', -1); Aa=[0 1 0 0;... 0 -((b*(I+m*l^2))/((M+m)*(I+m*l^2)-m^2*l^2)) ((m^2*l^2*g)/((M+m)*(I+m*l^2)-m^2*l^2)) 0;... 0 0 0 1;... 0 -((b*m*l)/((M+m)*(I+m*l^2)-m^2*l^2)) ((m*g*l*(M+m))/((M+m)*(I+m*l^2)-m^2*l^2)) 0]; Ba=[0;... ((I+m*l^2)/((M+m)*(I+m*l^2)-m^2*l^2));... 0;... ((m*l)/((M+m)*(I+m*l^2)-m^2*l^2))]; Ca=[1 0 0 0; 0 0 1 0]; Da=[0; 0]; sysa=syslin('c', Aa, Ba, Ca, Da); // save the data save("edsonjLTIanaliticoPap.sod","sysa")
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//Two cars //refer fig.12.13 //Let A and B be the positions of cars when the drivers see each other and apply brakes //Let they meet at C //1.car A au=12 //m/sec av=0 //s=x //a1 be acceleration //using equation of motion //a1=(-12)/t //x=6*t //2.car B bu=9 //m/sec bv=0 //a=a2 //time=t //s=100-x //using equation of motion //a2=-9/t //100-x=4.5*t //solving t=100/10.5 //sec a1=-12/t //m/sec^2 a2=-9/t //m/sec^2 x=57.14 //m //distance traveled by second car bx=100-x //m printf("\nt=%.2f sec\na1=%.2f m/sec^2\na2=%.2f m/sec^2\nDistance travelled by first car=%.2f m\nDistance travelled by second car=%.2f m",t,a1,a2,x,bx)
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epsilonr=4.6; f=2*10^9; z0=50; //line impedance mu0=4*%pi*10^-7; epsilon0=8.85*10^-12; zf=sqrt(mu0/epsilon0); //free space impedance temp=((epsilonr-1)/(epsilonr+1))*(0.23+(0.11/epsilonr)); temp1=2*%pi*(z0/zf)*sqrt((epsilonr+1)/2); A=temp+temp1; wtoh=(8*%e^A)/((%e^2*A)-2); Eff=(epsilonr+1)/2+(epsilonr-1)/2*1/(sqrt(1+12*(1/(wtoh)))); vp=3*10^8/sqrt(Eff); lambda=vp/f; disp("metre/second",vp,"Phase velocity"); disp("metre",lambda,"Wavelength");
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//Section-1,Example-2,Page no.AC-343 //To calculate viscosiy index of the oil sample under test. L=774 H=414 U=564 VI=((L-U)/(L-H))*100 disp (VI,'Viscosity index of the oil sample under test')
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//example 8.7 clc; clear; close; printf("For input J and K = 0 otput Qn+1 = Qn i.e output does not change its state And for J = K = 1, The Output Qn+1 = Qn` i.e output toggles " );
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//============================================================================================================ // chapter 10 example 7 clc clear // Variable declaration n1 = 1.33; //refractive index of water n2 = 1; // refractive index of air // Calculations theta_c = asin((n2/n1)) theta_c_deg = theta_c*(180/%pi); // radian to degree conversion // Result mprintf('For angles above %3.2f degrees , there will be total internal reflection in water',theta_c_deg ); //================================================================================================================
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clc;funcprot(0);//EXAMPLE 3.28 // Initialisation of Variables t1=373;.............//Initial temperature in K p1=1;...............//Initial pressure in bar p3=65;..............//Maximum pressure in bar R=287;.................//Gas constant in kJ/kg p4=p3; ga=1.41;.................//Ratio of specific heats Vs=0.0085;............//Swept volume in m^3 afr=21;...............//Air fuel ratio r=15;.................//Compression ratio C=43890;..............//Calorific value of fuel in kJ/kg cp=1;................//Specific heat at constant pressure in kJ/kgK cv=0.71;..............//Specific heat at constant volume in kJ/kgK //Calculations Vc=Vs/(r-1);...............//Clearance volume in m^3 v2=Vc;v1=Vs+v2; v3=Vc;v5=v1; p2=p1*(r^ga);.....................//Pressure at the end of adiabatic compression in bar t2=t1*(r^(ga-1));................//Temperature at the end of adiabatic compression in K t3=(t2*p3)/p2;...................//Temperature at the end of isochoric compression in K m=(p1*v1*10^5)/(R*t1);............//Mass of air in the cycle in kg Qv=m*cv*(t3-t2);.....................//Heat added during constant volume process in kJ fv=Qv/C;.............................//Fuel added during constant volume process in kg mf=m/afr;..................//Total amount of fuel added in kg mfib=mf-fv;....................//Total amount of fuel added in isobaric process in kg Qib=mfib*C;....................//Total amount of heat added in isobaric process in kJ t4=(Qib/((m+mf)*cp))+t3;........//Temperature at the end of isobaric process in K v4=(v3*t4)/t3;..................//Volume at the end of isobaric process in m^3 t5=t4/((v5/v4)^(ga-1));.........//Temperature at the end of isochoric expansion in K Qrv=(m+mf)*cv*(t5-t1);...............//Heat rejected during constant volume process in kJ W=(Qib+Qv)-Qrv;................//Work done in kJ etath=W/(Qib+Qv);..................//Thermal efficiency disp(etath*100,"Thermal efficiency in %:")
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//Function to round-up a value such that it is divisible by 5 function[v] = round_five(w) v = ceil(w) rem = pmodulo(v,5) if (rem ~= 0) v = v + (5 - rem) end endfunction function[] = plot_format() //Get the handle of current axes g = gca() //Give labels and set label properties g.labels_font_color=5 g.font_size=3 g.grid=[1,1] g.box="off" endfunction //Obtain path of solution file path = get_absolute_file_path('solution4_11.sce') //Obtain path of data file datapath = path + filesep() + 'data4_11.sci' //Clear all clc //Execute the data file exec(datapath) //Calculate permissible bending stress sigmab (N/mm2) sigmab = Sut/fs //Distance of B l (mm) l = pdist //Increment length by 20mm and plot the bending moment variation over cantilever //Infinite for loop for i = 1:1:%inf Mb(i) = (P * 1000)*(l) len(i) = l if(l == dist) break end l = l + 20 end plot(len,Mb) plot_format() title('Variation of bending moment against cantilever length') xlabel('Cantilever Length(mm)') ylabel('Bending Moment (Hogging) (N-mm)') //Calculate maximum bending moment at A Mbmax (N-mm) from the plot Mbmax = max(Mb) //Assume the width of the cross-section to be 1mm w w = 1 //Calculate the value of y (mm) y = w //Calculate second moment of area I (mm4) I = (w * ((ratio * w)^3))/12 //Calculate the width of the cross-section (mm) w = ((Mbmax * y)/(I * sigmab))^(1/3) w = round_five(w) //Calculate the depth of the cross-section d (mm) d = 2 * w //Print results printf('\nWidth of the cross-section(w) = %f mm\n',w) printf('\nDepth of the cross-section(d) = %f mm\n',d)
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; asin.tst ; ; Copyright 2009-2023, Arm Limited. ; SPDX-License-Identifier: MIT OR Apache-2.0 WITH LLVM-exception func=asin op1=7ff80000.00000001 result=7ff80000.00000001 errno=0 func=asin op1=fff80000.00000001 result=7ff80000.00000001 errno=0 func=asin op1=7ff00000.00000001 result=7ff80000.00000001 errno=0 status=i func=asin op1=fff00000.00000001 result=7ff80000.00000001 errno=0 status=i func=asin op1=7ff00000.00000000 result=7ff80000.00000001 errno=EDOM status=i func=asin op1=fff00000.00000000 result=7ff80000.00000001 errno=EDOM status=i func=asin op1=00000000.00000000 result=00000000.00000000 errno=0 func=asin op1=80000000.00000000 result=80000000.00000000 errno=0 ; Inconsistent behavior was detected for the following 2 cases. ; No exception is raised with certain versions of glibc. Functions ; approximated by x near zero may not generate/implement flops and ; thus may not raise exceptions. func=asin op1=00000000.00000001 result=00000000.00000001 errno=0 maybestatus=ux func=asin op1=80000000.00000001 result=80000000.00000001 errno=0 maybestatus=ux func=asin op1=3ff00000.00000000 result=3ff921fb.54442d18.469 errno=0 func=asin op1=bff00000.00000000 result=bff921fb.54442d18.469 errno=0 func=asin op1=3ff00000.00000001 result=7ff80000.00000001 errno=EDOM status=i func=asin op1=bff00000.00000001 result=7ff80000.00000001 errno=EDOM status=i
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clc disp("Example 4.29") printf("\n") disp("Calculate suitable values of R1,Rp,R2 for SCR in circuit Fig 4.12") printf("Given\n") printf("Resistance are in ohms \nCurrent are in Ampere \n Voltage sources are in volt\n") //gate current Ig=600*10^-6 //gate trigger voltage Vg=0.7 Vd=0.7 //supply voltage Vs=230 //peak value of supply voltage Vm=sqrt(2)*Vs //supply voltage at angle 8deg Vs1=Vm*sin(8*%pi/180) //supply voltage at angle 90deg Vs2=Vm*sin(90*%pi/180) //to trigger SCR at 10deg moving contact of Rp is at top //from circuit VR1=Vs1-Vg //choose I1min>>Ig I1min=6*10^-3 R1=VR1/I1min //since Ig<<I1min, current through Rp & R2 is I1min RpPLUSR2=Vg/I1min //to trigger SCR at 90deg moving contact of Rp is at bottom VR2=Vt I1=Vs2/(R1+RpPLUSR2) R2=Vg/I1 Rp=RpPLUSR2-R2 printf("Resistance R1 is %f ohm \n",R1) printf("Resistance R2 is %f ohm \n",R2) printf("Resistance Rp is %f ohm \n",Rp)
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clc clear //DATA GIVEN V1=0.216; //gas consumption in m^3/min P1=75; //gas temperature in mm of water T1=17+273; //gas tempertaure in K m=2.84; //air consumption in kg/min Ta=17+273; //air tempertaure in K br=745; //barometer reading in mm of Hg D=0.25; //bore of engine cylinder in m L=0.475; //stroke length in m N=240; //engine speed in R.P.M. R=287; //gas constant for air in J/kgK n=1; //no. of cylinders k=1; //for 2-stroke cylinder P1=br+P1/13.6; //pressure of the gas //at NTP P2=760; //mm of Hg T2=0+273; //in K //P1*V1/T1=P2*V2/T2 V2=P1*V1*T2/(P2*T1); //volume of gas used at NTP in m^3 Vg=V2/(N/2); //gas used per stroke in m^3 //PV=mRT P2=1.0132*10^5; V=m*R*T2/P2; //volume occupied by air in m^3/min Va=V/(N/2); //air used per stroke in m Vmix=Vg+Va; //mixture of gas and air in m^3 //ETAvol=(actual volume of mixture drawn per stroke at NTP)/(swept volume of system) ETAvol=Vmix/((%pi/4)*D^2*L); printf(' The Volumetric efficiency is: %3.3f or %3.1f percent. \n',ETAvol,(ETAvol*100));
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// Example no 4.7 // To compute diffraction loss and identify Fresnel zone within which tip of obstruction lies for a)h=25m b)h=0 c)h=-25m // Page no. 132 clc; clear; // Given data lambda=1/3; // Wavelength in meter d1=1*10^3; // Distance between transmitter and obstructing screen in m d2=1*10^3; // Distance between receiver and obstructing screen in m // a) For h=25m h=25; // Effective heigth of obstruction screen in m v=h*sqrt((2*(d1+d2))/(lambda*d1*d2)); // Fresnel diffraction parameter printf('\n a) For h=25m Fresnel diffraction parameter v = %0.2f',v); printf('\n From the plot of Knife-edge diffraction gain as a function of Fresnel diffraction parameter, diffraction loss is 22dB.'); Gd=-20*log10(0.225/v); // Diffraction loss for v>2.4 in dB printf('\n Using numerical approximation, diffraction loss for v > 2.4 = %0.1f dB',Gd); delta=(h^2/2)*((d1+d2)/(d1*d2)); // Path length difference between direct and diffracted rays n=(2*delta)/lambda; // Number of Fresnel zones in which the obstruction lies printf('\n Fresnel zone within which tip of obstruction lies = %0.2f',n); printf('\n Therefore, the tip of obstruction completely blocks the first three Fresnel zones.'); // b) For h=0 h=0; // Effective heigth of obstruction screen in m v=h*sqrt((2*(d1+d2))/(lambda*d1*d2)); // Fresnel diffraction parameter printf('\n \n b) For h=0 Fresnel diffraction parameter v = %0.0f',v); printf('\n From the plot of Knife-edge diffraction gain as a function of Fresnel diffraction parameter, diffraction loss is 6dB.'); Gd=-20*log10(0.5-0.62*v); // Diffraction loss for v=0 in dB printf('\n Using numerical approximation, diffraction loss for v=0 = %0.0f dB',Gd); delta=(h^2/2)*((d1+d2)/(d1*d2)); // Path length difference between direct and diffracted rays n=(2*delta)/lambda; // Number of Fresnel zones in which the obstruction lies printf('\n Fresnel zone within which tip of obstruction lies = %0.0f',n); printf('\n Therefore, the tip of obstruction lies in middle of first Fresnel zone.'); // c) For h=-25m h=-25; // Effective heigth of obstruction screen in m v=h*sqrt((2*(d1+d2))/(lambda*d1*d2)); // Fresnel diffraction parameter printf('\n \n c) For h=-25m Fresnel diffraction parameter v = %0.2f',v); printf('\n From the plot of Knife-edge diffraction gain as a function of Fresnel diffraction parameter, diffraction loss is approximately 1dB.'); Gd=0; // Diffraction loss for v<-1 in dB printf('\n Using numerical approximation, diffraction loss for v < -1 = %0.0f in dB',Gd); delta=(h^2/2)*((d1+d2)/(d1*d2)); // Path length difference between direct and diffracted rays n=(2*delta)/lambda; // Number of Fresnel zones in which the obstruction lies printf('\n Fresnel zone within which tip of obstruction lies = %0.2f',n); printf('\n Therefore, the tip of obstruction completely blocks the first three Fresnel zones but diffraction loss is negligible.');
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//pathname=get_absolute_file_path('19.02.sce') //filename=pathname+filesep()+'19.02-data.sci' //exec(filename) T1=285 //K p1=1 //bar T3=773 //K p2=4 //bar r=1.4 Cpa=1.005 //kJ/kg.K CV=43100 //kJ/kg.K T3=273+500 //K //Temperature at state 2(in K): T2=T1*(p2/p1)^((r-1)/r) //Temperature at state 2'(in K): T2a=T1+1.1*(T2-T1) //Work required in compressor(in kJ/kg of air): Wc=Cpa*(T2a-T1) printf("\n RESULT \n") printf("\nPower required to drive compressor = %f kW/kg of air",Wc) //Heat added in combustion chamber(in kJ/kg of air): qa=Cpa*(T3-T2a) //Air fuel ratio: r1=CV/qa printf("\nAir-fuel ratio = %f",r1) //Temperature at state 5(in K): T5=T3*(p1/p2)^((r-1)/r) //Enthalpy drop in the nozzle(in kJ/kg of air): hd=Cpa*(T3-T5-T2a+T1) //Velocity of exit gas from nozzle(in m/s): Ce=sqrt(2*hd*10^3) //Thrust(in N/kg/s): T=(1+1/r)*Ce printf("\nThrust = %f N/kg of air/s",Ce)
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function[z]=fx(x,y) z=(x^2)+3*(y^2)-2*x+2*y endfunction x=[­2:0.1:1.5]; y=x; w=feval(x,y,fx); plot3d(x,x,w)
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ANALOG_READ_SB_help.tst
\name ANALOG_READ_SB \palette Arduino \smalldescription Permet de réaliser l'acquisition d'une grandeur analogique sur le port Analogique d'une carte Arduino. \description La carte Arduino UNO possède 6 ports d'entrées analogiques (de A0 à A5), la carte Arduino Mega possède 16 ports d'entrée analogique (de A0 à A15). Le bloc proposé permet de transmettre la valeur numérique codée sur 10 bits (de 0 à 1023) d'une grandeur analogique associée à un port d'entrée. On rappelle que l'échantillonnage est de 8 ms au minimum pour ce bloc. \dialogbox \image{ANALOG_READ_SB_dialogbox.png} Le numéro du port de 0 à 5 doit être spécifié pour la carte UNO, de 0 à 15 pour une carte MEGA. Le numéro de la carte ne peut pas être modifié pour l'instant. Il n'y a pas de vérification de la valeur donnée, veuillez vous reporter à la spécification de votre carte Arduino pour mettre une valeur correcte. \example1 L'exemple ci-dessous montre l'utilisation du bloc dans le cas d'un potentiomètre angulaire dont la broche de mesure est connectée au port 2. Les deux autres broches du potentiomètre sont reliées à la masse (GND) et le 5 Volt de la carte directement. \image{ANALOG_READ_example.png} \seealso ANALOG_WRITE_SB DIGITAL_READ_SB DIGITAL_WRITE_SB
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clear; //clc(); function y=z(x) y=sin(x) endfunction exact=-2.5432; pe=50; pm=100; p_inc=30; del1=asin(pe/pm); //at point b pb=80; del2=asin(pb/pm); a1=pb*(0.927-0.523)-100*intg(0.523,0.927,z); a2=100*intg(0.927,(3.14-0.927),z)-80*(3.14-2*del2); if a1<a2 then disp("the generator will remain stable"); else disp("the system is unstable"); end
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Reconstruction.sce
//Graphical// //Example 4.02.7 Sampling a Nonbandlimited Signal //Plotting Discrete Time Fourier Transform of //Discrete Time Signal x(nT)= exp(-A*T*abs(n)) clear; clc; close; // Analog Signal A =1; //Amplitude Dt = 0.005; t = -2:Dt:2; //Continuous Time Signal xa = exp(-A*abs(t)); //Discrete Time Signal Fs =input('Enter the Sampling Frequency in Hertz');//Fs = 1Hz(or)20Hz Ts = 1/Fs; n = -5:1:5; nTs = n*Ts; x = exp(-A*abs(nTs)); // Analog Signal reconstruction Dt = 0.005; t = -2:Dt:2; Xa = x *sinc_new(Fs*(ones(length(nTs),1)*t-nTs'*ones(1,length(t)))); // check error = max(abs(Xa - xa)) subplot(2,1,1); a =gca(); a.x_location = "origin"; a.y_location = "origin"; plot(t,xa); xlabel('t in msec.'); ylabel('xa(t)') title('Original Analog Signal') subplot(2,1,2); a =gca(); a.x_location = "origin"; a.y_location = "origin"; xlabel('t in msec.'); ylabel('xa(t)') title('Reconstructed Signal from x(n) using sinc function'); plot(t,Xa);
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Ex7_21.sce
clear // // //Initilization of Variables d=150 //mm //Diameter T=20*10**6 //N //Torque M=12*10**6 //N-mm //B.M F=200*10**3 //N //Axial Thrust //Calculations //M.I I=(%pi*64**-1*d**4) //Bending stress f_A=M*I**-1*(d*2**-1) //N/mm**2 f_B=-f_A //N/mm**2 //Axial thrust due to thrust sigma=F*(%pi*4**-1*d**2)**-1 //At A p_x=f_A-sigma //N/mm**2 //At B p_x2=f_B-sigma //N/mm**2 p_y=0 //At A and B //Polar Modulus J=%pi*32**-1*d**4 //mm**4 //Shearing stress at A and B q=T*J**-1*(d*2**-1) //N/mm**2 //Principal Stresses //At A P1=(p_x+p_y)*2**-1+(((p_x-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2 P2=(p_x+p_y)*2**-1-(((p_x-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2 //Max shear stress q_max1=(((p_x-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2 //At B P1_2=(p_x2+p_y)*2**-1+(((p_x2-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2 P2_2=(p_x2+p_y)*2**-1-(((p_x2-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2 //Max shear stress q_max2=(((p_x2-p_y)*2**-1)**2+q**2)**0.5 //N/mm**2 //Result printf("\n MAx Principal Stresses:P1 %0.2f N/mm**2",P1) printf("\n :P2 %0.2f N/mm**2",P2) printf("\n Min Principal Stresses:P1_2 %0.2f N/mm**2",P1_2) printf("\n :P2_2 %0.2f N/mm**2",P2_2)
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//Método de Taylor //Utiliza das expansões da série de taylor, onde os dois primeiros elementos são o método de Euler, o resto do somatório é o erro //Para obter um método melhor basta calcular mais termos da série //Método é explicito e possue uma boa zona de estabilidade //Problema: é necessário a f e a derivada de f /* EXEMPLO DE ORDEM 3 function y = f(t,u) y = u*t endfunction //Deriva em relação a u e em relação a t pois u depende de t //u'*t + t'*u -> Regra da multiplicação function y=ft(t,u) y = (u*t)*t + u endfunction //Para ordem 3 function y=ftt(t,u) y = ((u*t)*t + u)*t + 2*u*t endfunction */ function y = f(t,u) y = cos(u + t) endfunction function y = ft(t,u) y = -sin(u + t)*(cos(u + t) + 1) endfunction function [ultimo] = taylor(h) u(1) = 0.84 //Condição Inicial t(1) = 1 T = 2 //Valor de u(x) que se deseja calcular N = (T-t(1))/h for n=1:N t(n+1) = t(n) + h F = f(t(n),u(n)) Ft = ft(t(n),u(n)) u(n+1) = u(n) + h*F + (h^2/2)*Ft //Para ordem 3: + (h^3/3!)*Ftt ... end ultimo = u(N+1); endfunction
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sce
Ex4_21.sce
//Variable declaration gm = 2 //transconductance rd = 200*10^3 //dynamic drain resistance(ohms) Cgs = 10 //gate to source capacitance(pF) Cgd = 0 //gate to drain capacitance(pF) Rs = 1*10^3 //source resistance(ohms) Rg = 1*10^6 //Rg = R1||R2 Rd = 5*10^3 //drain resistance(ohms) Rs1 = 2 //resistance(k ohms) Cc1 = 0.1*10^-6 //coupling capacitors(F) Cc2 = Cc1 Co = 10*10^-12 //output capacitance(F) Vgs = 1 //gate to source voltage(V) //Calculations //Part a R = (Rd*rd)/(Rd+rd) //Rd||rd(k ohms) Avo = -Vgs*gm*R //voltage gain Vo = Avo //Part b w11 = 1/(Cc1*(Rs*Rg)) //corner freq(rad/s) wL = w11 //input circuit corner freq(rad/s) //Part c w22 = 10^12/((Cgs*R)*10^3) //output circuit corner frequency(rad/s) wH = w22/(2*%pi) //Part d G = -Avo*wH //gain bandwidth product //Part e Rd = 4*10^3 //drain resistance reduced(ohms) Rnew = (Rd*rd)/(Rd+rd) //new resistance(ohms) Avo1 = -Vgs*gm*Rnew //new voltage gain BWnew = (10^8/Rnew)/(2*%pi) //new bandwidth(Mrad/s) Gnew = -Avo1*BWnew //gain bandwidth product new //Results printf ("a)Avo is %.2f",Avo/1E+3) printf ("b)wL is %.2f rad/s",wL/1E-3) printf ("c)wH is %.1f MHz",wH/1E+3) printf ("d)G is %.2f MHz",G/1E+6) printf ("e)Gnew is %.1f MHz",Gnew/1E+6)
b11eb081cbdad3c407f746a57f5189064c65db31
931df7de6dffa2b03ac9771d79e06d88c24ab4ff
/Air VL Sparky.sce
0924f5f7c56056a73b0425b1c6f3157c3c001678
[]
no_license
MBHuman/Scenarios
be1a722825b3b960014b07cda2f12fa4f75c7fc8
1db6bfdec8cc42164ca9ff57dd9d3c82cfaf2137
refs/heads/master
2023-01-14T02:10:25.103083
2020-11-21T16:47:14
2020-11-21T16:47:14
null
0
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null
null
null
null
UTF-8
Scilab
false
false
107,015
sce
Air VL Sparky.sce
Name=Air VL Sparky PlayerCharacters=A BotCharacters=Bot Rotation air.rot IsChallenge=true Timelimit=1000.0 PlayerProfile=A AddedBots=Bot Rotation air.rot PlayerMaxLives=0 BotMaxLives=6 PlayerTeam=1 BotTeams=2 MapName=airvertlimited03b.map MapScale=6.0 BlockProjectilePredictors=false BlockCheats=true InvinciblePlayer=false InvincibleBots=false Timescale=1.0 BlockHealthbars=false TimeRefilledByKill=0.0 ScoreToWin=1000.0 ScorePerDamage=0.0 ScorePerKill=0.0 ScorePerMidairDirect=0.0 ScorePerAnyDirect=0.0 ScorePerTime=1.0 ScoreLossPerDamageTaken=0.0 ScoreLossPerDeath=0.0 ScoreLossPerMidairDirected=0.0 ScoreLossPerAnyDirected=0.0 ScoreMultAccuracy=false ScoreMultDamageEfficiency=false ScoreMultKillEfficiency=false GameTag=Air Vertical Limited Sparky WeaponHeroTag=Track Master 100 DifficultyTag=4 AuthorsTag=patys, Whisper, DeA, Tammas BlockHitMarkers=false BlockHitSounds=false BlockMissSounds=true BlockFCT=false Description=Air nuns vertical limited with revamped map and bot physics, the bots are also faster smaller and have less health. GameVersion=2.0.2.0 ScorePerDistance=0.0 MBSEnable=false MBSTime1=0.25 MBSTime2=0.5 MBSTime3=0.75 MBSTime1Mult=1.0 MBSTime2Mult=2.0 MBSTime3Mult=3.0 MBSFBInstead=false MBSRequireEnemyAlive=false LockFOVRange=false LockedFOVMin=60.0 LockedFOVMax=120.0 LockedFOVScale=Clamped Horizontal [Aim Profile] Name=Default MinReactionTime=0.3 MaxReactionTime=0.4 MinSelfMovementCorrectionTime=0.001 MaxSelfMovementCorrectionTime=0.05 FlickFOV=30.0 FlickSpeed=1.5 FlickError=15.0 TrackSpeed=3.5 TrackError=3.5 MaxTurnAngleFromPadCenter=75.0 MinRecenterTime=0.3 MaxRecenterTime=0.5 OptimalAimFOV=30.0 OuterAimPenalty=1.0 MaxError=40.0 ShootFOV=15.0 VerticalAimOffset=0.0 MaxTolerableSpread=5.0 MinTolerableSpread=1.0 TolerableSpreadDist=2000.0 MaxSpreadDistFactor=2.0 AimingStyle=Original ScanSpeedMultiplier=1.0 MaxSeekPitch=30.0 MaxSeekYaw=30.0 AimingSpeed=5.0 MinShootDelay=0.3 MaxShootDelay=0.6 [Bot Profile] Name=air1F_far_short DodgeProfileNames=Short Strafes Jumping DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=air1_fast SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=air1F_close_short DodgeProfileNames=Short Strafes Close DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=air1_fast SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=air1F_far_long DodgeProfileNames=Long Strafes Jumping DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=air1_fast SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=air1F_close_long DodgeProfileNames=Long Strafes Close DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=air1_fast SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=air1_far_short DodgeProfileNames=Short Strafes Jumping DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=air1 SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Profile] Name=air_close_short DodgeProfileNames=Short Strafes Close DodgeProfileWeights=1.0 DodgeProfileMaxChangeTime=5.0 DodgeProfileMinChangeTime=1.0 WeaponProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0;1.0;1.0 AimingProfileNames=Default;Default;Default;Default;Default;Default;Default;Default WeaponSwitchTime=3.0 UseWeapons=true CharacterProfile=air1 SeeThroughWalls=false NoDodging=false NoAiming=false AbilityUseTimer=0.1 UseAbilityFrequency=1.0 UseAbilityFreqMinTime=0.3 UseAbilityFreqMaxTime=0.6 ShowLaser=false LaserRGB=X=1.000 Y=0.300 Z=0.000 LaserAlpha=1.0 [Bot Rotation Profile] Name=Bot Rotation air ProfileNames=air1F_far_short;air1F_close_short;air1F_far_long;air1F_close_long;air1_far_short;air_close_short ProfileWeights=1.0;1.0;1.0;1.0;1.0;1.0 Randomized=false [Character Profile] Name=A MaxHealth=100.0 WeaponProfileNames=Track Master 100;;;;;;; MinRespawnDelay=1.0 MaxRespawnDelay=5.0 StepUpHeight=75.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=0.0 MaxCrouchSpeed=500.0 Acceleration=10000.0 AirAcceleration=16000.0 Friction=8.0 BrakingFrictionFactor=2.0 JumpVelocity=800.0 Gravity=0.0 AirControl=0.25 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=230.0 MainBBRadius=55.0 MainBBHasHead=false MainBBHeadRadius=1.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=false JetpackActivationDelay=0.2 JetpackFullFuelTime=4.0 JetpackFuelIncPerSec=1.0 JetpackFuelRegensInAir=false JetpackThrust=6000.0 JetpackMaxZVelocity=400.0 JetpackAirControlWithThrust=0.25 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.0 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=60.0 BlockSpawnDistance=9001.0 RespawnAnimationDuration=0.5 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=600.0 TPSOffset=X=0.000 Y=0.000 Z=0.000 BrakingDeceleration=2048.0 VerticalSpawnOffset=0.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=true ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=air1_fast MaxHealth=1000.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=1.5 MaxRespawnDelay=1.5 StepUpHeight=0.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=1600.0 MaxCrouchSpeed=500.0 Acceleration=6000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=500.0 Gravity=2.0 AirControl=1.0 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=160.0 MainBBRadius=70.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=true JetpackActivationDelay=0.01 JetpackFullFuelTime=3.0 JetpackFuelIncPerSec=1.25 JetpackFuelRegensInAir=true JetpackThrust=2500.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=1.0 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.5 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2000.0 VerticalSpawnOffset=25.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Character Profile] Name=air1 MaxHealth=1000.0 WeaponProfileNames=;;;;;;; MinRespawnDelay=1.5 MaxRespawnDelay=1.5 StepUpHeight=0.0 CrouchHeightModifier=0.5 CrouchAnimationSpeed=1.0 CameraOffset=X=0.000 Y=0.000 Z=0.000 HeadshotOnly=false DamageKnockbackFactor=8.0 MovementType=Base MaxSpeed=1200.0 MaxCrouchSpeed=500.0 Acceleration=7000.0 AirAcceleration=16000.0 Friction=4.0 BrakingFrictionFactor=2.0 JumpVelocity=500.0 Gravity=2.0 AirControl=1.0 CanCrouch=false CanPogoJump=false CanCrouchInAir=false CanJumpFromCrouch=false EnemyBodyColor=X=255.000 Y=0.000 Z=0.000 EnemyHeadColor=X=255.000 Y=255.000 Z=255.000 TeamBodyColor=X=0.000 Y=0.000 Z=255.000 TeamHeadColor=X=255.000 Y=255.000 Z=255.000 BlockSelfDamage=false InvinciblePlayer=false InvincibleBots=false BlockTeamDamage=false AirJumpCount=0 AirJumpVelocity=800.0 MainBBType=Cylindrical MainBBHeight=160.0 MainBBRadius=70.0 MainBBHasHead=false MainBBHeadRadius=45.0 MainBBHeadOffset=0.0 MainBBHide=false ProjBBType=Cylindrical ProjBBHeight=230.0 ProjBBRadius=55.0 ProjBBHasHead=true ProjBBHeadRadius=45.0 ProjBBHeadOffset=0.0 ProjBBHide=true HasJetpack=true JetpackActivationDelay=0.01 JetpackFullFuelTime=3.0 JetpackFuelIncPerSec=1.25 JetpackFuelRegensInAir=true JetpackThrust=2500.0 JetpackMaxZVelocity=600.0 JetpackAirControlWithThrust=1.0 AbilityProfileNames=;;; HideWeapon=false AerialFriction=0.35 StrafeSpeedMult=1.0 BackSpeedMult=1.0 RespawnInvulnTime=0.0 BlockedSpawnRadius=0.0 BlockSpawnFOV=0.0 BlockSpawnDistance=0.0 RespawnAnimationDuration=0.0 AllowBufferedJumps=true BounceOffWalls=false LeanAngle=0.0 LeanDisplacement=0.0 AirJumpExtraControl=0.0 ForwardSpeedBias=1.0 HealthRegainedonkill=0.0 HealthRegenPerSec=0.0 HealthRegenDelay=0.0 JumpSpeedPenaltyDuration=0.0 JumpSpeedPenaltyPercent=0.0 ThirdPersonCamera=false TPSArmLength=300.0 TPSOffset=X=0.000 Y=150.000 Z=150.000 BrakingDeceleration=2000.0 VerticalSpawnOffset=25.0 TerminalVelocity=0.0 CharacterModel=None CharacterSkin=Default SpawnXOffset=0.0 SpawnYOffset=0.0 InvertBlockedSpawn=false ViewBobTime=0.0 ViewBobAngleAdjustment=0.0 ViewBobCameraZOffset=0.0 ViewBobAffectsShots=false IsFlyer=false FlightObeysPitch=false FlightVelocityUp=800.0 FlightVelocityDown=800.0 [Dodge Profile] Name=Short Strafes Jumping MaxTargetDistance=2500.0 MinTargetDistance=1750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.25 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.6 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.1 MaxJumpTime=0.5 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.0 BlockedMovementReactionMin=0.0 BlockedMovementReactionMax=0.0 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Dodge Profile] Name=Short Strafes Close MaxTargetDistance=1000.0 MinTargetDistance=700.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.25 MaxLRTimeChange=0.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.05 MaxJumpTime=0.3 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.0 BlockedMovementReactionMin=0.0 BlockedMovementReactionMax=0.0 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Dodge Profile] Name=Long Strafes Jumping MaxTargetDistance=2500.0 MinTargetDistance=1750.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.5 MaxLRTimeChange=1.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.6 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.1 MaxJumpTime=0.5 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.0 BlockedMovementReactionMin=0.0 BlockedMovementReactionMax=0.0 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Dodge Profile] Name=Long Strafes Close MaxTargetDistance=1000.0 MinTargetDistance=700.0 ToggleLeftRight=true ToggleForwardBack=false MinLRTimeChange=0.5 MaxLRTimeChange=1.5 MinFBTimeChange=0.2 MaxFBTimeChange=0.5 DamageReactionChangesDirection=false DamageReactionChanceToIgnore=0.5 DamageReactionMinimumDelay=0.125 DamageReactionMaximumDelay=0.25 DamageReactionCooldown=1.0 DamageReactionThreshold=0.0 DamageReactionResetTimer=0.1 JumpFrequency=0.5 CrouchInAirFrequency=0.0 CrouchOnGroundFrequency=0.0 TargetStrafeOverride=Ignore TargetStrafeMinDelay=0.125 TargetStrafeMaxDelay=0.25 MinProfileChangeTime=0.0 MaxProfileChangeTime=0.0 MinCrouchTime=0.3 MaxCrouchTime=0.6 MinJumpTime=0.05 MaxJumpTime=0.3 LeftStrafeTimeMult=1.0 RightStrafeTimeMult=1.0 StrafeSwapMinPause=0.0 StrafeSwapMaxPause=0.0 BlockedMovementPercent=0.0 BlockedMovementReactionMin=0.0 BlockedMovementReactionMax=0.0 WaypointLogic=Ignore WaypointTurnRate=200.0 MinTimeBeforeShot=0.15 MaxTimeBeforeShot=0.25 IgnoreShotChance=0.0 ForwardTimeMult=1.0 BackTimeMult=1.0 DamageReactionChangesFB=false [Weapon Profile] Name=Track Master 100 Type=Hitscan ShotsPerClick=1 DamagePerShot=1.0 KnockbackFactor=0.0 TimeBetweenShots=0.01 Pierces=false Category=FullyAuto BurstShotCount=1 TimeBetweenBursts=0.5 ChargeStartDamage=10.0 ChargeStartVelocity=X=500.000 Y=0.000 Z=0.000 ChargeTimeToAutoRelease=2.0 ChargeTimeToCap=1.0 ChargeMoveSpeedModifier=1.0 MuzzleVelocityMin=X=2000.000 Y=0.000 Z=0.000 MuzzleVelocityMax=X=2000.000 Y=0.000 Z=0.000 InheritOwnerVelocity=0.0 OriginOffset=X=0.000 Y=0.000 Z=0.000 MaxTravelTime=5.0 MaxHitscanRange=1000000.0 GravityScale=1.0 HeadshotCapable=false HeadshotMultiplier=2.0 MagazineMax=0 AmmoPerShot=1 ReloadTimeFromEmpty=0.5 ReloadTimeFromPartial=0.5 DamageFalloffStartDistance=100000.0 DamageFalloffStopDistance=100000.0 DamageAtMaxRange=25.0 DelayBeforeShot=0.0 ProjectileGraphic=Ball VisualLifetime=0.1 BounceOffWorld=false BounceFactor=0.5 BounceCount=0 HomingProjectileAcceleration=0.0 ProjectileEnemyHitRadius=1.0 CanAimDownSight=false ADSZoomDelay=0.0 ADSZoomSensFactor=0.7 ADSMoveFactor=1.0 ADSStartDelay=0.0 ShootSoundCooldown=0.01 HitSoundCooldown=0.01 HitscanVisualOffset=X=0.000 Y=0.000 Z=-50.000 ADSBlocksShooting=false ShootingBlocksADS=false KnockbackFactorAir=0.0 RecoilNegatable=false DecalType=1 DecalSize=30.0 DelayAfterShooting=0.0 BeamTracksCrosshair=false AlsoShoot= ADSShoot= StunDuration=0.0 CircularSpread=true SpreadStationaryVelocity=300.0 PassiveCharging=false BurstFullyAuto=true FlatKnockbackHorizontal=0.0 FlatKnockbackVertical=0.0 HitscanRadius=0.0 HitscanVisualRadius=6.0 TaggingDuration=0.0 TaggingMaxFactor=0.0 TaggingHitFactor=0.0 RecoilCrouchScale=1.0 RecoilADSScale=1.0 PSRCrouchScale=1.0 PSRADSScale=1.0 ProjectileAcceleration=0.0 AccelIncludeVertical=true AimPunchAmount=0.0 AimPunchResetTime=0.05 AimPunchCooldown=0.5 AimPunchHeadshotOnly=false AimPunchCosmeticOnly=true MinimumDecelVelocity=0.0 PSRManualNegation=false PSRAutoReset=true AimPunchUpTime=0.05 AmmoReloadedOnKill=0 CancelReloadOnKill=false FlatKnockbackHorizontalMin=0.0 FlatKnockbackVerticalMin=0.0 ADSScope=No Scope ADSFOVOverride=72.099998 ADSFOVScale=Horizontal (16:9) ADSAllowUserOverrideFOV=true IsBurstWeapon=false ForceFirstPersonInADS=true ZoomBlockedInAir=false ADSCameraOffsetX=0.0 ADSCameraOffsetY=0.0 ADSCameraOffsetZ=0.0 QuickSwitchTime=0.0 WeaponModel=Heavy Surge Rifle WeaponAnimation=Primary UseIncReload=false IncReloadStartupTime=0.0 IncReloadLoopTime=0.0 IncReloadAmmoPerLoop=1 IncReloadEndTime=0.0 IncReloadCancelWithShoot=true WeaponSkin=Default ProjectileVisualOffset=X=0.000 Y=0.000 Z=0.000 SpreadDecayDelay=0.0 ReloadBeforeRecovery=true 3rdPersonWeaponModel=Pistol 3rdPersonWeaponSkin=Default ParticleMuzzleFlash=None ParticleWallImpact=None ParticleBodyImpact=None ParticleProjectileTrail=None ParticleHitscanTrace=None ParticleMuzzleFlashScale=1.0 ParticleWallImpactScale=1.0 ParticleBodyImpactScale=1.0 ParticleProjectileTrailScale=1.0 Explosive=false Radius=500.0 DamageAtCenter=100.0 DamageAtEdge=100.0 SelfDamageMultiplier=0.5 ExplodesOnContactWithEnemy=false DelayAfterEnemyContact=0.0 ExplodesOnContactWithWorld=false DelayAfterWorldContact=0.0 ExplodesOnNextAttack=false DelayAfterSpawn=0.0 BlockedByWorld=false SpreadSSA=1.0,1.0,-1.0,5.0 SpreadSCA=1.0,1.0,-1.0,5.0 SpreadMSA=1.0,1.0,-1.0,5.0 SpreadMCA=1.0,1.0,-1.0,5.0 SpreadSSH=0.0,0.1,0.0,0.0 SpreadSCH=1.0,1.0,-1.0,5.0 SpreadMSH=0.0,0.1,0.0,0.0 SpreadMCH=1.0,1.0,-1.0,5.0 MaxRecoilUp=0.0 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//Example 8.6 //current clc; clear; close; V=220;// in volts I=60;// in amperes rpm=728;//turns Ts=150;//shaft torque in N-m nc=80;//commercial efficiency in percentge I=((Ts*2*%pi*rpm*746)/(60*746*(nc/100)*V));// CURRENT TAKEN IN AMPERES disp(round(I),"current taken in amperes is")
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clear;lines(0); besselj(0.5:3,1:4)
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//Example 1.14<c> // Find wheather the following signal is periodic or not x3(n)=e^(i*7*pi*n) clc; n=-21:21; x=exp(%i *7* %pi *n); f=(7*%pi)/(2*%pi); N=1/f; disp(N,'the given signal is periodic');
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//effect of moving pole near jw axis s=%s sys1=syslin('c',(s+1)/(s^2*(s+10))) //a=10 b=1 evans(sys1) sys2=syslin('c',(s+1)/(s^2*(s+9))) //a=9 evans(sys2) sys3=syslin('c',(s+1)/(s^2*(s+8))) //a=8 evans(sys3) sys4=syslin('c',(s+1)/(s^2*(s+3))) //a=3 evans(sys4) sys5=syslin('c',(s+1)/(s^2*(s+1))) //a=1 evans(sys5) printf("as pole is moved towards jw axis RL also moves towards jw axis")
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//Graphical// //Example 8.3.5 Sigle pole analog filter //Bilinear Transformation //To convert analog filter into digital filter clear; clc; close; s = poly(0,'s'); Omegac = 0.2*%pi; H = Omegac/(s+Omegac); T =1;//Sampling period T = 1 Second z = poly(0,'z'); Hz = horner(H,(2/T)*((z-1)/(z+1))) disp(Hz,'Hz =') HW =frmag(Hz(2),Hz(3),512); W = 0:%pi/511:%pi; plot(W/%pi,HW) a=gca(); a.thickness = 3; a.foreground = 1; a.font_style = 9; xgrid(1) xtitle('Magnitude Response of Single pole LPF Filter Cutoff frequency = 0.2*pi','Digital Frequency--->','Magnitude'); //Result //Hz = // // 0.6283185 + 0.6283185z // ---------------------- // - 1.3716815 + 2.6283185z // //-->Hz(3)=Hz(3)/2.6283185 // Hz = // // 0.6283185 + 0.6283185z // ---------------------- // - 0.5218856 + z // //-->Hz(2)=Hz(2)/2.6283185 // Hz = // // 0.2390572 + 0.2390572z // ---------------------- // - 0.5218856 + z // // which is equivalent to //Hz = // // 0.2390572(1 + z^-1) // ---------------------- // 1 - 0.5218856*z^-1
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// Given:- EfFdot = 100.00 // exergy rate of fuel entering the boiler in MW cF = 1.44 // unit cost of fuel in cents per kw.h Zbdot = 1080.00 // the cost of owning and operating boiler in dollars per hour Ef1dot = 35.00 // exergy rate of exiting steam from the boiler in MW p1 = 50.00 // pressure of exiting steam from the boiler in bar T1 = 466.00 // temperature of exiting steam from the boiler in degree celcius Ztdot = 92.00 // the cost of owning and operating turbine in dollars per hour p2 = 5.00 // pressure of exiting steam from the turbine in bars T2 = 205.00 // temperature of exiting steam from the turbine in degree celcius m2dot = 26.15 // mass flow rate of exiting steam from the turbine in kg/s T0 = 298.00 // in kelvin // Part(a) // From table A-4, h1 = 3353.54 // in kj/kg h2 = 2865.96 // in kj/kg s1 = 6.8773 // in kj/kg.k s2 = 7.0806 // in kj/kg.k // Calculations // From assumption,For each control volume,Qcvdot = 0 and kinetic and potential energy effects are negligible,the mass and energy rate // balances for a control volume enclosing the turbine reduce at steady state to give Wedot = m2dot *(h1-h2)/1000 // power in MW Ef2dot = Ef1dot+m2dot*(h2-h1-T0*(s2-s1))/1000 // the rate exergy exits with the steam in MW // Results printf( ' For the turbine,the power is %.2f MW.',Wedot) printf( ' For the turbine,the rate exergy exits with the steam is %.2f MW.',Ef2dot) // Part(b) // Calculations c1 = cF*(EfFdot/Ef1dot) + ((Zbdot/Ef1dot)/10**3)*100 // unit cost of exiting steam from boiler in cents/Kw.h c2 = c1 // Assigning the same unit cost to the steam entering and exiting the turbine ce = c1*((Ef1dot-Ef2dot)/Wedot) + ((Ztdot/Wedot)/10**3)*100 // unit cost of power in cents/kw.h // Results printf('The unit costs of the steam exiting the boiler of exergy is: %.2f cents per kw.h.',c1) printf('The unit costs of the steam exiting the turbine of exergy is: %.2f cents per kw.h.',c2) printf('Unit cost of power is: %f cents per kw.h.',ce) // Part(c) C2dot = (c2*Ef2dot*10**3)/100 // cost rate for low-pressure steam in dollars per hour Cedot = (ce*Wedot*10**3)/100 // cost rate for power in dollars per hour // Results printf( ' The cost rate of the steam exiting the turbine is: %.2f dollars per hour.',C2dot) printf( ' The cost rate of the power is: %.2f dollars per hour.',Cedot)
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// 21 janvier 2013 // construction du modele du bonhomme // modelisation 2 D 5 segments pour le bonhomme et // le deambulateur est un objet rigide a trois branches // On ajoute un PI pour vrifier que la pose est telle que les pieds touchent le sol. // read qualysis data path = '/home/dune/Documents/data/AnalysisQualisys/MADN/'; pathres = 'results/essai1-'; pathMatFile = path+ 'KBM-essai1.mat'; loadmatfile(pathMatFile); [P1x,P1y,P1z,... P2x,P2y,P2z,... P3x,P3y,P3z,... P4x,P4y,P4z,... P5x,P5y,P5z,... P6x,P6y,P6z,... P7x,P7y,P7z,... P8x,P8y,P8z,... P9x,P9y,P9z,... P10x,P10y,P10z,... P11x,P11y,P11z,... P12x,P12y,P12z] = mocapData(essai1); index=100; //jeu de données de test global Ptest ; Ptest = [ P2x(index),P2y(index),P2z(index),1000; P3x(index),P3y(index),P3z(index),1000; P4x(index),P4y(index),P4z(index),1000; P5x(index),P5y(index),P5z(index),1000; P6x(index),P6y(index),P6z(index),1000; P8x(index),P8y(index),P8z(index),1000; P9x(index),P9y(index),P9z(index),1000; P10x(index),P10y(index),P10z(index),1000; P11x(index),P11y(index),P11z(index),1000; P12x(index),P12y(index),P12z(index),1000]; Ptest = Ptest'/1000; //tout mettre en metre //Ptest = Ptest-[Ptest(1:3,6);0]*ones(1,12); // pour que le repère soit celui du premier pied xset("window",10); humanMocapPlot(Ptest); show_pixmap(); // le robot est un robot plan sur xy // simuInit //q1 = 0 ; // angle plante du pied/sol G q2 = 0.72546 ; // cheville G q3 = -0.7 ; // genou G q4 = 0.4; // hanche gauche q5 = %pi-.3; // hanche droite q6 = 0.2; // genou D q7 = 0.3926745 ; // cheville D //q8 = 0; // pied D q9 = 3.3 ; // epaule gauche q10 = -0.8 ; // coude G //q11 = -1.89 ; // poignet G q12 = 3; // epaule droite q13 = -0.4; // coude droit ////q14 = 0.6577 ; // poignet D // nouveau modele q0 = [q2,q3,q4,q5,q6, q7, q9, q10, q12, q13]; global d0; d0 = H2LWSagSeg(); d0(1)=d0(1)+0.1; d0(5)=d0(1); d0(2)=d0(2)+0.1; d0(4)=d0(2); d0(3)=d0(3)+0.15; tx0 = 0;//.0864232;//;Ptest(2,6); // position du pied dans le plan sagital tz0 = 0;//-0.0976375 ;//Ptest(3,6); // elevation du pied au sol x0 = [d0,q0,tx0,tz0]; P2 = computePest(x0);// le robot est un robot plan sur xy // display //plotHuman14dof(P2) plotHuman10dots(P2); show_pixmap(); disp('Pause avant optimisation') pause //simplex nelder&mead //x = fminsearch ( costfunction , x0 ); // moindre carre [fopt,x]=leastsq(costfunction, x0); P3 = computePest(x); plotHuman10dots(P3);
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type newType = array 20 of short; void sym1 (int a, short b, newType c) { var e : array 10 of short; var d : array 10 of newType; PRINT SYMBOL TABLE }
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clc clear //Input data d=6;//Diameter of the bore in cm l=9;//Length of the stroke in cm m=0.00025;//Mass of charge admitted in each suction stroke R=29.27;//Gas constant Kgfm/kg K p=1;//Normal pressure in kgf/cm^2 T=273;//Temperature in K //Calculations V=(m*R*T)*10^6/(p*10^4);//Volume of charge admitted in each cycle in m^3 Vs=(3.14*d^2*l)/4;//Swept volume of the cylinder nv=(V/Vs)*100;//Volumetric efficiency in percentage //Output printf('The volumetric efficiency is %3.1f percent',nv)
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clc //initialization of variables l1=2886 //cm^-1 l2=5668 //cm^-1 //calculations wave=2*l1-l2 wave2= wave+l1 x=wave/(2*wave2) //results printf("anharmonicity constant = %.4f ",x)
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//Function migration (image list to matrix) for: filter2D //Generated by migrate.cpp //Author: Anirudh Katoch function res = filter2D(varargin) select length(varargin) case 06 then res = il2mat(raw_filter2D(mat2il(varargin(01)), varargin(02), varargin(03), varargin(04), varargin(05), varargin(06))) else error(39) end endfunction
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//Example 9.5 clc disp("V_CC = +15 V") vsat=0.9*15 format(5) disp(vsat,"Therefore, V_sat(in V) = 0.9 V_CC =") disp(" R1 = 51 k-ohm, R2 = 120 ohm") vut=(13.5*120)/((51*10^3)+120) format(8) disp(vut,"V_UT(in V) = +V_sat*R2 / R1+R2 =") vlt=(-13.5*120)/((51*10^3)+120) disp(vlt,"V_LT(in V) = -V_sat*R2 / R1+R2 =") h=(0.03169*2)*10^3 format(6) disp(h,"H(in mV) = V_UT - V_LT =")
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clc //initialisation of variables Qt= 150000 //cuses i= 1/10000 n1= 1 n2= 2/3 d1= 30 //ft C1= 100 C2= 75 b1= 600 //ft b2= 2000 //ft r= 2 A1= (b1+d1)*d1 P1= b1+(2*d1*sqrt(2)) m1= A1/P1 v1= C1*sqrt(m1*i) Q1= A1*v1 Q2= Qt-Q1 v2= v1/2 A2= Q2/v2 d2= (-b2+sqrt(b2^2+4*1.5*A2))/(2*1.5) //RESULTS printf ('depth of water = %.f ft ',d2)
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clc; //Example 12.7 //Page No 526 //Solution c=3*10^8; disp("Substituting into equation 12-48"); d=((0.8)*c*(1*10^-6))/2; disp('m',d,'d = ');
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// //Implementation of Matlab function compand() in Scilab. // //Name:Pooja Mahadev Soundalgekar //2nd Year Information Technology //National Institute of Technology Karnataka //Email: pooja27ms@gmail.com // //Function:compand() // //Function argument types: // //1. out = compand(in,param,v) same behaviour as of out = compand(in,Mu,v,'mu/compressor') //Input arguments: //data = 2:2:12 //compressed = compand(data,255,max(data)) //Output arguments: //compressed = //8.1644 9.6394 10.5084 11.1268 11.6071 12. // //2. out = compand(in,Mu,v,'mu/compressor') //Input arguments: //data = 2:2:12 //compressed = compand(data,255,max(data),'mu/compressor') //Output arguments: //compressed = //8.1644 9.6394 10.5084 11.1268 11.6071 12. // //3. out = compand(in,Mu,v,'mu/expander') //Input arguments: //expanded = compand(compressed,255,max(data),'mu/expander') //Output arguments: //expanded = //2. 4. 6. 8. 10. 12. // //4. out = compand(in,A,v,'A/compressor') //Input arguments: //data = 1:5 //compressed = compand(data,87.6,max(data),'a/compressor') //Output arguments: //compressed = //3.5296 4.1629 4.5333 4.7961 5.O //5. out = compand(in,A,v,'A/expander') //Input arguments: //expanded = compand(compressed,87.6,max(data),'a/expander') //Output arguments details: //expanded = //1. 2. 3. 4. 5. //Resources: //For the documentation of compand(): http://in.mathworks.com/help/comm/functionlist.html //For understanding the syntax of Scilab, Scilab functions: http://spoken-tutorial.org/tutorial-search/?search_foss=Scilab&search_language=English // //Function definition: function[y]=compand(varargin) //varargin will store the input arguments [lhs,rhs] = argn()// lhs has the left side arguments in this case : y and rhs has right side arguments in this case: in,Mu/A,v,opt in=varargin(1) mu=varargin(2) v=varargin(3) if( rhs ==3 ) then //for out = compand(in,param,v) which does not take in the fourth parameter, it is set to "" opt="" end if(rhs == 4) then //if there are four argyments passed, fourth input argument is set to opt opt=varargin(4) end j=1 //index for y len = length(in) for i = in //loop through x if(opt == "mu/compressor") then //y=V*log(1+μ|x|/V)*sgn(x)/log(1+μ) temp = v*log(1+(mu*abs(i)/v))/log(1+mu) temp=temp*signm(i) y(1,j)=round(temp*10^6/10^2)/10^4 //round upto four decimal point end if(opt == "") then //y=V*log(1+μ|x|/V)*sgn(x)/log(1+μ) temp = v*log(1+(mu*abs(i)/v))/log(1+mu) temp=temp*signm(i) y(1,j)=round(temp*10^6/10^2)/10^4 //round upto four decimal point end if(opt == "mu/expander") then //x=V(e^(|y|*log(1+μ)/V)−1)*sgn(y)/μ temp = v*(exp((abs(i)*log(1+mu))/v)-1)*signm(i) temp=temp/mu y(1,j)=round(round(temp*10^6/10^2)/10^4)//round upto four decimal point end if(opt == "A/compressor") then // for 0 <= |x| <= v/A here A is named as variable mu // y= A|x|*sgn(x)/(1+logA) if(abs(i) >= 0) then if(abs(i) <= v/mu) then temp=mu*abs(i)/(1+log(mu)) temp=temp*signm(i) y(1,j)=round(temp*10^6/10^2)/10^4 //round upto four decimal point end end if(abs(i)>v/mu) then // for v/A < |x| <= v //y= V*(1+log(A|x|/V))*sgn(x)/(1+logA) if(abs(i)<=v) then temp=v*(1+log(mu*abs(i)/v))/(1+log(mu)) temp=temp*signm(i) y(1,j)=round(temp*10^6/10^2)/10^4 //round upto four decimal point end end end if( opt == "A/expander") then //for 0≤ |y| ≤V/(1+logA) // x= y*(1+logA)/A if(abs(i)>=0) then if(abs(i)<=v/(1+log(mu))) then temp=(i*(1+log(mu)))/mu y(1,j)=round(round(temp*10^6/10^2)/10^4) //round upto four decimal point end end if(abs(i)>v/(1+log(mu))) then //for V/(1+logA) < |y| ≤ V //x= exp(|y|*(1+logA)/V−1)*V*sgn(y)/A if(abs(i)<=v) then temp=exp(abs(i)*(1+log(mu))/v-1)*v/mu temp=temp*signm(i) y(1,j)=round(round(temp*10^6/10^2)/10^4) //round upto four decimal point end end end j=j+1 end endfunction
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// Given :- clc; r = 18.00 // compression ratio T1 = 300.00 // temperature at the beginning of the compression process in kelvin p1 = 0.1 // pressure at the beginning of the compression process in MPa rc = 2.00 // cutoff ratio // Part(a) // With T1 = 300 K, Table A-22 gives u1 = 214.07 // in kj/kg vr1 = 621.2 // Interpolating in Table A-22, we get T2 = 898.3 // in kelvin h2 = 930.98 // in kj/kg // From Table A-22, h3 = 1999.1 // in kj/kg vr3 = 3.97 // Interpolating in Table A-22 with vr4, we get u4 = 664.3 // in kj/kg T4 = 887.7 // in kelvin // Calculations // Since Process 2–3 occurs at constant pressure, the ideal gas equation of state gives T3 = rc*T2 // in kelvin // With the ideal gas equation of state p2 = p1*(T2/T1)*(r) // in MPa p3 = p2 // For the isentropic compression process 1–2 vr2 = vr1/r // For the isentropic expansion process 3–4 vr4 = (r/rc)*vr3 // The ideal gas equation of state applied at states 1 and 4 gives p4 = p1*(T4/T1) // in MPa // Results printf( '\n At state1, the pressure is : %.2f bar.',p1) printf( '\n At state1, the temperature is %.2f kelvin.' ,T1) printf( '\n At state2, the pressure in bar is : %.2f bar.',p2) printf( '\n At state2, the temperature is %.2f kelvin.',T2) printf( '\n At state3, the pressure in bar is : %.2f bar.',p3) printf( '\n At state3, the temperature is %.2f kelvin.',T3) printf( '\n At state4, the pressure is: %.2f MPa.',p4) printf( '\n At state4, the temperature is %.2f kelvin.',T4) // Part(b) eta = 1- (u4-u1)/(h3-h2) printf( '\n The thermal efficiency is : %.2f ',eta) // Part(c) R = 8.314 // universal gas constant, in SI units M = 28.97 // molar mass of air in grams // Calculations wcycle = (h3-h2)-(u4-u1) // The net work of the cycle in kj/kg v1 = ((R/M)*T1/p1)/10**3 // The specific volume at state 1 in m^3/kg mep = (wcycle/(v1*(1-1/r)))*10**3*10**-6 // in MPa // Results printf( '\n The mean effective pressure, is : %.2f MPa.',mep)
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result postfix=[1, 1, x, -, x, y, *, -, /] A007318 tria 0 1 1,-1,-1,0,0,0 x,y result postfix=[1, 1, x, -, 1, x, y, *, -, *, 1, x, 2, ^, y, *, -, *, /] A003983 tria 1 1 1,-1,-1,0,0,0,0,1,1,0,0,0,-1,0,0,0,0,0,0,0,0,0,0,0,0,0,0,0 x,y result postfix=[1, 1, x, -, 2, ^, 1, x, y, *, -, *, /] A004736 tria 1 1 1,-2,-1,1,2,0,0,-1,0,0,0,0,0,0,0 x,y result postfix=[0, 1, -, 2, x, *, y, *, +, 0, 1, -, 3, x, *, y, *, +, x, +, /] A038763 tria 0 1,0,-2,0,0,0 1,-1,-3,0,0,0 x,y result postfix=[x, 1, y, x, 2, ^, 4, x, *, +, 3, +, *, -, /] A299989 tria 0 0,1,0 1,0,-4,0,-1,0,0,0,0,0 x,y result postfix=[y, 1, x, y, 2, ^, 4, y, *, +, 3, +, *, -, /] A299989 tria 0 0,0,0 1,-3,-4,0,0,0,0,0,0,0 x,y
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//Harriot P.,2003,Chemical Reactor Design (I-Edition) Marcel Dekker,Inc. USA,pp 436. //Chapter-7 Ex7.2 Pg No.270 //Title:The gradient for B in the liquid film //=========================================================================================================== clear clc //INPUT C_B0_by_C_Ai=40; D_A_by_D_B=1.2; sqrt_M=10; phi=sqrt_M;//Assume the gradient for A is the same as when the gradient for B is negligible eff_diff_distA_by_xL=(1/phi); //CALCULATION eff_diff_distB_by_xL=(1-eff_diff_distA_by_xL); CB0_minus_CBbar_by_CB0=D_A_by_D_B*(1/C_B0_by_C_Ai)*(eff_diff_distB_by_xL/eff_diff_distA_by_xL); C_Bbar_by_C_B0=(1-CB0_minus_CBbar_by_CB0); sqrt_kC_B=sqrt(C_Bbar_by_C_B0); phi_corrected=phi*sqrt_kC_B; Percent_change=((phi-phi_corrected)/(phi))*100; //OUTPUT mprintf('\n Percentage Decrease in Rate :%0.0f%% ',Percent_change); mprintf('\n The decrease in rate is significant ,hence the gradient for B is significant in liquid film'); fid= mopen('.\Chapter7-Ex2-Output.txt','w'); mfprintf(fid,'\n Percentage Decrease in Rate :%0.0f%% ',Percent_change); mfprintf(fid,'\n The decrease in rate is significant ,hence the gradient for B is significant in liquid film'); mclose(fid); //================================================END OF PROGRAM==========================================================
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//Page Number: 5.43 //Example 5.37 clc; //Given, bw=3.5D+3; //Hz //Roll off factor a=0.25; Rb=(2*bw)/(1+a); disp('b/s',Rb,'Data Rate');
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clc; //page 86 // Given data P=30; // lb, Force applied to shift lever alpha=20;// degree, angle made by force P with -ve X axis Q=P*sind(alpha)//in degree d=3//in ft M_o=Q*d//N.m , here negative signs are taken as each component creates moment clockwise printf("The moment of force P about B is %.2f lb-ft . -ve sign \n shows its acting clockwise\n",M_o);
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clear; s=loadwave("son.wav"); fs=44100; plot(s); halt(); xbasc(); analyze(s,fmin=100,fmax=3000,rate=fs); halt(); xbasc(); mapsound(s,dt=0.1,simpl=1,fmin=100,fmax=3000,rate=fs); //playsnd(s);
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pathname=get_absolute_file_path('5_12.sce') filename=pathname+filesep()+'5_12data.sci' exec(filename) v1= (L1/L0)*V(3); v2= (L2/L0)*V(4); v3= v1+v2; theta=atan(v3/(D(9)-D(6))); printf("\nθB: %f rad",theta);
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//Example_a_5_5 page no:204 clc; Vmag=100; Vang=0; f=50; L1=3+(%i*31.41); L2=5-(31.83*%i); L3=10+(%i*150.73); R1=3; R2=5; R3=10; L1mag=sqrt(real(L1)^2+imag(L1)^2); L1ang=atand(imag(L1)/real(L1)); I1mag=Vmag/L1mag; I1ang=Vang-L1ang; I1real=I1mag*cosd(I1ang); I1img=I1mag*sind(I1ang)*%i; I1=I1real+I1img; disp(I1,"the current passing thorugh 3+31.41i ohm is (in A)"); L2mag=sqrt(real(L2)^2+imag(L2)^2); L2ang=atand(imag(L2)/real(L2)); I2mag=Vmag/L2mag; I2ang=Vang-L2ang; I2real=I2mag*cosd(I2ang); I2img=I2mag*sind(I2ang)*%i; I2=I2real+I2img; disp(I2,"the current passing through 5-31.83i ohm is (in A)"); L3mag=sqrt(real(L3)^2+imag(L3)^2); L3ang=atand(imag(L3)/real(L3)); I3mag=Vmag/L3mag; I3ang=Vang-L3ang; I3real=I3mag*cosd(I3ang); I3img=I3mag*sind(I3ang)*%i; I3=I3real+I3img; disp(I3,"the current passing through 10+150.73i ohm is (in A)"); It=I1+I2+I3; disp(It,"the total current is (in A)"); V1=R1*I1; V2=R2*I2; V3=R3*I3; V1mag=sqrt(real(V1)^2+imag(V1)^2); V1ang=atand(imag(V1)/real(V1)); V2mag=sqrt(real(V2)^2+imag(V2)^2); V2ang=atand(imag(V2)/real(V2)); V3mag=sqrt(real(V3)^2+imag(V3)^2); V3ang=atand(imag(V3)/real(V3)); disp(V1mag,"the magnitude of voltage across 3 ohm resistor is (in V)"); disp(V1ang,"the angle of voltage across 3 ohm resistor is (in degree)"); disp(V2mag,"the magnitude of voltage across 5 ohm resistor is (in V)"); disp(V2ang,"the angle of voltage across 5 ohm resistor is (in degree)"); disp(V3mag,"the magnitude of voltage across 10 ohm resistor is (in V)"); disp(V3ang,"the angle of voltage across 10 ohm resistor is (in degree)"); V0_1h=(I1*(31.41*%i)); V0_1hmag=sqrt(real(V0_1h)^2+imag(V0_1h)^2); V0_1hang=atand(imag(V0_1h)/real(V0_1h)); V100h=(I2*(-31.83*%i)); V100hmag=sqrt(real(V100h)^2+imag(V100h)^2); V100hang=atand(imag(V100h)/real(V100h)); V0_5h=(I3*(157.81*%i)); V0_5hmag=sqrt(real(V0_5h)^2+imag(V0_5h)^2); V0_5hang=atand(imag(V0_5h)/real(V0_5h)); V500h=(I3*(-6.37*%i)); V500hmag=sqrt(real(V500h)^2+imag(V500h)^2); V500hang=atand(imag(V500h)/real(V500h)); V500hang=V500hang-180; disp(V0_1hmag,"the magnitude of voltage across 0.1 henry inductance is (in V)"); disp(V0_1hang,"the angle of voltage across 0.1 henry inductance is (in V)"); disp(V100hmag,"the magnitude of voltage across 100 milli henry inductance is (in V)"); disp(V100hang,"the angle of voltage across 100 milli henry inductance is (in V)"); disp(V0_5hmag,"the magnitude of voltage across 0.5 henry inductance is (in V)"); disp(V0_5hang,"the angle of voltage across 0.5 henry inductance is (in V)"); disp(V500hmag,"the magnitude of voltage across 500 milli henry inductance is (in V)"); disp(V500hang,"the angle of voltage across 50 milli henry inductance is (in V)");//the angle is added with 180 degree to give positive value hence both value i.e in text book and scilab result are same mathematically //here angle values varies a little here more accurate values are used for calcultaion hence values are not altered in any variable but in text book values are rounded off and they produce approximate results
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// This file is part of the materials accompanying the book // "The Elements of Computing Systems" by Nisan and Schocken, // MIT Press. Book site: www.idc.ac.il/tecs // File name: projects/08/FunctionCalls/StaticsTest/StaticsTest.tst load StaticsTest.asm, output-file StaticsTest.out, compare-to StaticsTest.cmp, output-list RAM[0]%D1.6.1 RAM[261]%D1.6.1 RAM[262]%D1.6.1; set RAM[0] 256, repeat 2500 { ticktock; } output;
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@relation pima-5 @attribute 'preg' real [0.0, 17.0] @attribute 'plas' real [0.0, 199.0] @attribute 'pres' real [0.0, 122.0] @attribute 'skin' real [0.0, 99.0] @attribute 'insu' real [0.0, 846.0] @attribute 'mass' real [0.0, 67.1] @attribute 'pedi' real [0.078, 2.42] @attribute 'age' real [21.0, 81.0] @attribute 'class' {tested_negative, tested_positive} @inputs 'preg', 'plas', 'pres', 'skin', 'insu', 'mass', 'pedi', 'age' @outputs 'class' tested_positive tested_positive tested_positive tested_positive tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_positive tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_negative tested_positive tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_positive tested_positive tested_positive tested_positive tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_positive tested_positive tested_positive tested_positive tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_negative tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_positive tested_positive tested_positive tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_positive tested_negative tested_positive tested_negative tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_positive tested_positive tested_positive tested_negative tested_positive tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_positive tested_negative tested_negative tested_positive tested_negative tested_positive tested_negative tested_positive tested_positive tested_positive tested_positive tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative tested_negative
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//Example 3.3.5 page 3.33 clc; clear; n= 3.6; BETA= 21*10^-3; alpha= 10; L= 250*10^-4; r= (n-1)^2/(n+1)^2; Jth= 1/BETA *( alpha + (log(1/r)/L)); Jth=Jth/1000; //converting for displaying... printf("The threshold current density is %.2fx10^3",Jth); Jth=Jth*1000; Ith =Jth*250*100*10^-8; Ith=Ith*1000; //converting into mA... printf("\n\nThe threshold current is %.1f mA",Ith);
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// Example 6.3.2 page 6.12 clc; clear; n=1.7; //refractive index L=5d-2; //distance between mirror c=3d8; //speed of light lamda=0.45d-6; //wavelength k=2*n*L/lamda; //computing number of modes delf=c/(2*n*L); //computing mode separation delf=delf*10^-9; printf("\nNumber of modes are %.2e.\nFrequency separation is %.2f GHz.",k,delf);
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//Example 2.7.13;//design clc; clear; close; format('v',6) vs=30;//in volts n=0.51;// vd=0.7;//in volts vp=(n*vs+vd);//in volts c=0.1;//in micro farads vv=3.5;//in volts x=log(vv/(vp-vd));// t2=50;//in micro seconds r3=-((t2*10^-6)/(x*c*10^-6));//in ohms f=50;//in Hz t=(1/f)*10^3;//in ms t1=(t-(t2*10^-6));//inms x1=log(1-((vp-vv)/(vs)));// y1=(-t1*10^-3)/(c*10^-6);// r1=y1/x1;//in ohms r2=(10^4)/(n*vs);//in ohms disp(r1*10^-3,"R1 in ohm is") disp(r2,"R2 in ohm is") disp(round(r3),"R3 in ohm is") disp(c,"capaictance in micro Farad is") //R3 is wrong in the textbook
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//practical interpolation //example 3.12 //page 99 clc;clear;close; x=[1.72 1.73 1.74 1.75 1.76 1.77 1.78]; y=[0.1790661479 0.1772844100 0.1755204006 0.1737739435 0.1720448638 0.1703329888 0.1686381473]; h=0.01//interval between values of x c=1; for i=1:6 d1(c)=y(i+1)-y(i); c=c+1; end c=1; for i=1:5 d2(c)=d1(i+1)-d1(i); c=c+1 end c=1; for i=1:4 d3(c)=d2(i+1)-d2(i); c=c+1; end c=1; for i=1:3 d4(c)=d3(i+1)-d3(i); c=c+1; end x0=1.7475; y_x=y(3); p=(x0-x(3))/h; y_x=y_x+p*d1(3)+p*(p-1)*((d2(2)+d2(3))/2)/2; printf(' the value at %f by bessels formula is : %0.10f\n\n',x0,y_x); y_x=y(4); q=1-p; y_x=q*y(3)+q*(q^2-1)*d2(2)/6+p*y(4)+p*(p^2-1)*d2(2)/6; printf(' the value at %f by everrets formula is : %0.10f\n\n',x0,y_x);
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function x=msign(a) // msign - computes the matrix sign function. //%CALLING SEQUENCE // x=msign(a) //%PARAMETERS // a : square hermitian matrix // x : square hermitian matrix //%DESCRIPTION // This macro is called by the function sign to compute square matrix // sign function. //! [m,n]=size(a) if m<>n then error(20,1),end flag=or(a<>a'); if flag then error('msign: non hermitian matrix'),end [u,s]=schur(a) x=u'*diag(sign(real(diag(s))))*u
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clear; clc; //Example - 18.5 //Page number - 652 printf("Example - 18.5 and Page number - 652\n\n"); // Given // N2 + 3H2 - 2NH3 T_1 = 700;//[K] - Reaction temperature Max_adia_rise = 100;///[K] - Maximum adiabatic rise in temperature T_2 = T_1 + Max_adia_rise;//[K] - delta_H_rkn_700 = -94.2;//[kJ] - Standard enthalpy of reaction at 700 K delta_H_rkn_700 = delta_H_rkn_700*10^(3);//[J] // The mean standard heat capacity of various components over the temperature range from 700 to 800 K is Cp_N2 = 30.0;//[cal/mol-K] Cp_H2 = 28.9;//[cal/mol-K] Cp_NH3 = 49.2;//[cal/mol-K] // The energy balance equation is // X*delta_H_rkn_700 + integrate('(sum_ni_Cpi_exit)*dT','T',T_1,T_2) //At exit, let moles of NH3 = (1-X), moles of H2 = (3-3X), moles of NH3 = 2X . Therefore we have, // delta_H_rkn_700*X + {(1-X)*Cp_N2 + (3-3X)*Cp_H2 + (2X)*Cp_NH3}*(T_2 - T_1) // On simplification we get, 960.3*X = 116.7 X = 116.7/960.3; printf(" The maximum allowable conversion fraction in the reactor is given by, X = %f \n",X);
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// Example 2.10.a;Core Readius clc; clear; close; n1=1.450;//Waveguide Refractive Index n2=1.447;//Cladding Refractive Index h= 1.3;// Wavelenght in micrometers NA=sqrt(n1^2-n2^2);// Numerical Aperture a= (2.405*h)/(2*%pi*NA);// Core radius disp(a,"Core radius in micro meter")
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//check o/p when the length of impulse response is smaller than the largest order impr=[1 2 3]; num_ord=4; den_ord=4; [num,den]=prony(impr,num_ord,den_ord); disp(num); disp(den); //output // 1. 2. 3. 0. 0. // // 1. 0. 0. 0. 0.
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//Example 3.18 //Program to Compute output responce of following sequences //x[n]=[1,2,3,1] //h[n]=[1,1,1] //(1)Linear Convolution //(2)Circular Convolution //(3)Circular Convolution with zero padding clear; clc ; close ; x=[1,2,3,1]; h=[1,1,1]; //(1)Linear Convolution Computation ylinear=convol (x,h); //Display Linear Convoluted Sequence y[n] in command window disp(ylinear,"ylinear[n]="); //(2)Circular Convolution Computation //Now zero padding in h[n] sequence to make length of x[n] and h[n] equal h1=[h,zeros(1,1)]; //Now Performing Circular Convolution by DFT method X=fft(x,-1); H=fft(h1,-1); Y=X.*H; ycircular=fft(Y,1); //Display Circular Convoluted Sequence y[n] in command window disp(ycircular,"ycircular[n]="); //(3)Circular Convolution Computation with zero Padding x2=[x,zeros(1,2)]; h2=[h,zeros(1,3)]; //Now Performing Circular Convolution by DFT method X2=fft(x2,-1); H2=fft(h2,-1); Y2=X2.*H2; ycircularp=fft(Y2,1); //Display Circular Convoluted Sequence with zero Padding y[n] in command window disp(ycircularp,"ycircularp[n]=");
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clc(); clear; // to calculate the maximum temperature inside the coil when current was 2.5 amp // the ratio of radii 12/13.5 is so great that the curvature may be neglected Di= 10/12; // inside diameter of the coil in ft x=7/48; // thickness of coil in ft ts=70.5; // Initial temp. of coil in degF Rm=12.1; // Resistance of coil e=0.0024; // Temperature coefficient of coil in degF i=0.009; // Initial current in amp V=0.1; // Initial Voltage in volts Rs=V/i; // Initial resistance in ohms Thm=(Rm/Rs-1)/e; // Mean temperature in degF Th0=1.5*Thm; // Increase in temperature in degF to=ts+Th0; // Maximum temperature in degF printf("The maximum temperature of the coil was %.1f degF",to);
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//page 39 clear; close; clc; A=[1 1 1;1 1 3;2 5 8]; disp(A,'A='); [L,U,P]=lu(A); disp(L,'L='); disp(U,'U='); disp(P,'P='); disp(P*A,'PA=') disp(L*U,'LU=') disp('This shows that PA is the same as LU') //end
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clear; clc; //Example10.1[Nucleate Boiling of Water in a Pan] Ts=108;//Temp of surface of bottom of pan[degree Celcius] Tsat=100;//Saturation temp of water[degree Celcius] D=0.3;//Diameter[m] //Properties of water at the saturation temp rho_l=957.9;//Density of liquid[kg/m^3] rho_v=0.6;//Density of vapour[kg/m^3] Pr_l=1.75;//Prandtl no of liquid mu_l=0.282*10^(-3);//Viscosity of liquid[kg/m.s] Cp_l=4217;//Specific Heat of liquid[J/kg.degree Celcius] h_fg=2257*10^3;//[J/kg] sigma=0.0589;//[N/m] g=9.81;//Acc due to gravity[m/s^2] Csf=0.0130,n=1.0; //Solution(a):- q_nuc=mu_l*h_fg*((g*(rho_l-rho_v)/sigma)^(1/2))*((Cp_l*(Ts-Tsat)/(Csf*h_fg*(Pr_l^n)))^3);//[W/m^2] A=%pi*(D^2)/4;//Surface Area of bottom of the pan[m^2] Q_boiling=A*q_nuc;//[W] disp("W",Q_boiling,"(a) The rate of heat transfer during nucleate boiling becomes ") //Solution(b):- m=Q_boiling/h_fg;//[kg/s] disp("kg/s",m,"The rate of Evaporation of water is")
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clc; KE=1/2*(800*1000/3600)^2/1000; T0=-50+273; cp=1.005; T0_=T0+[24.7/cp]; Ieff=0.9; T0_s=Ieff*(T0_-T0)+T0; y=1.4; pa=0.24; p0_=[(T0_s/T0)^[y/(y-1)]]*pa; p0_2!p0_=10; T0_2s=T0_*[p0_2!p0_^([y-1]/y)]; T0_2=T0_+(T0_2s-T0_)/Ieff; p0_2=10*p0_; p0_3=p0_2-(0.14); T0_3=820+273; meff=0.98; cp2=1.15; T0_4=T0_3-[cp*(T0_2-T0_)/(cp2*meff)]; T0_4s=T0_3-[cp*(T0_2-T0_)/(cp2*meff)]/0.92; y2=1.333; p0_4=3.24/[(T0_3/T0_4s)^{(y2/(y2-1))}] pc=p0_4*([2/(y2+1)]^{y2/(y2-1)}); T0_5=[2/(y2+1)]*T0_4; T0_5s=T0_4-{(T0_4-T0_5)/0.92}; p5=p0_4/[(T0_4/T0_5s)^(y2/{y2-1})]; R=cp2*(y2-1)/y2; v5=R*T0_5*1000/10^5/p5; T5=741.3//K Cj=(y2*R*1000*T5)^0.5; A=0.08; m=A*Cj/v5; Cg=222.2; mt=m*(Cj-Cg) pt=(p5-pa)*A*10^5; Tt=pt+mt; Q=m*cp2*(T0_3-T0_2) C=43300; mf=Q/meff/C; SFC=mf*10^3/6453 disp("kg/kNs",SFC,"specific fuel consumption is")
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//pathname=get_absolute_file_path('1.07.sce') //filename=pathname+filesep()+'1.07-data.sci' //exec(filename) //Weight of object at standard gravitational acceleration(in N): w=100 //Standard acceleration due to gravity(in m/s^2): g=9.81 //Gravitation acceleration at given location(in m/s^2): g1=8.5 //Mass of object(in kg): m=w/g //Spring balance reading(in N): s=m*g1 printf("\n\n RESULT \n\n") printf("\n\n The spring balance reading = %f N \n\n",s)
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v1 = 1; v2 = v1; v3 = v2; v4 = v2; e = 0.56; // Degree of reaction P = 1; // Dummy T = 1200; R = 8.3143; x1 = (1-e)/2; x2 = (1-e)/2; x3 = e/2; x4 = e/2; K = (((x3^v3)*(x4^v4))/((x1^v1)*(x2^v2)))*P^(v3+v4-v1-v2); // Equillibrium constant dG = -R*T*log(K); disp(K,"Equillibrium constant is") disp("J/gmol",dG,"Gibbs function change is")
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//clc() Pas = 71.2;//kPa Pbs = 48.9;//kPa P = 65;//kPa //P=(Pas-Pbs)*xa+Pbs,xa=mole fraction of n-heptane,liq. condition,therefore xa = (P - Pbs)/(Pas - Pbs); //ya = Pa / P , Vapour condition ya = Pas * xa / P; P1 = xa * 100; P2 = ya * 100; disp("%",P1,"Percentage of hepatne in liquid = ") disp("%",P2,"Percentage of hepatne in vapour = ")
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4_1exam.sce
//Engineering and Chemical Thermodynamics //Example 4.1 //Page no :175 clear ; clc ; //Let H2O = 1 ; NH3 = 2 ; CH4 = 3 ; CH3Cl = 4 ; CCl4 = 5 ; M_11 = 1.85 ; alp_12 = 14.80 ; I_13 = 12.62 ; M_12 = 1.47 ; alp_22 = 22.20 ; I_23 = 10.07 ; M_31 = 0.00 ; alp_32 = 26.00 ; I_33 = 12.61 ; M_41 = 1.87 ; alp_42 = 45.30 ; I_43 = 11.26 ; M_51 = 0.00 ; alp_52 = 105.0 ; I_53 = 11.47 ; k =1.38 * 10^-16 ; //[ J/K] T = 298 ; //[K] A =[M_11 , alp_12 , I_13; M_12 , alp_22 , I_23 ; M_31 , alp_32 , I_33 ; M_41 , alp_42 , I_43 ; M_51 , alp_52 , I_53 ;] ; disp(" Example: 4.1 Page no : 175") ; disp(" Molecule M alp*10^25 I C*10^60 Cd_d Cind Cdis") ; for i=1:5 A(i,5) = ceil( 2/3 * A(i,1)^4 / (k * T) * 10^-12) ; A(i,6) = ceil(2 * A(i,2) * A(i,1)^2 * 10^-1) ; A(i,7) = ceil(3/4 * A(i,2)^2 * A(i,3) * 1.6 * 10^-2) ; A(i,4) = ceil(A(i,5) + A(i,6) + A(i,7)) ; // ....E4.1D end ; printf(" H2O %.2f %.1f %.2f %d %d %d %d ",A(1,1),A(1,2),A(1,3),A(1,4),A(1,5),A(1,6),A(1,7)) ; printf("\n NH3 %.2f %.1f %.2f %d %d %d %d ",A(2,1),A(2,2),A(2,3),A(2,4),A(2,5),A(2,6),A(2,7)) ; printf("\n CH4 %.2f %.1f %.2f %d %d %d %d ",A(3,1),A(3,2),A(3,3),A(1,4),A(3,5),A(3,6),A(3,7)) ; printf("\n CH3Cl %.2f %.1f %.2f %d %d %d %d ",A(4,1),A(4,2),A(4,3),A(4,4),A(4,5),A(4,6),A(4,7)) ; printf("\n CCl4 %.2f %.1f %.2f %d %d %d %d \n",A(5,1),A(5,2),A(5,3),A(5,4),A(5,5),A(5,6),A(5,7)) ; disp(" Even though it is non polar , CCl4 exhibit the largest intermolecular forces . It is due to the large polarizability accociated with the four Cl atom in CCl4 .") ;
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//i/p arg k is of type char k=['char','v']; [num,den] = latc2tf(k,'allpass'); disp(num); disp(den); //output //!--error 53 //latc2tf: Wrong type for argument #1 (k); Real or complex vector expected //at line 78 of function latc2tf called by : //[num,den] = latc2tf(k,'allpass');
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//pathname=get_absolute_file_path('19.05.sce') //filename=pathname+filesep()+'19.05-data.sci' //exec(filename) //Pressures(in bar): p1=2.2 //Temperatures(in K): T1=220 T4=1273 //Velocities(in m/s): C1=260 //Nozzle efficiency: nn=0.85 //Turbine efficiency: nt=0.88 //Diffuser efficiency: nd=0.90 //Specific heat(in kJ/kg.K): Cp=1.005 //Adiabatic index of compression: r=1.4 //Pressure ratio: r1=12 //Temperature at state 2(in K): T2=T1+C1^2/(2*Cp*10^3) //Pressure at state 2(in bar): p2=p1*(T2/T1)^(r/(r-1)) p3=p2*r1 p4=p3 //Temperature at state 3(in K): T3=T2*(p3/p2)^((r-1)/r) //Temperature at state 3'(in K): T3a=T2+(T3-T2)/nn //Temperature at state 5'(in K): T5a=T4-(T3a-T2) //Temperature of state 5(in K): T5=T4-(T4-T5a)/nt //Pressure at state 5(in bar): p5=p4*(T5/T4)^(r/(r-1)) //Temperature at state 2(in K): T2=C1+(200)^2/(2*Cp*10^3) //Temperature at state 2'(in K): T2a=T1+(T2-T1)/nd T3a=568.635 T4=1000 p6=2.2 T6=542.83 //Velocity at exit of nozzle(in m/s): C6=sqrt(2*(T5-T6)*Cp*10^3) printf("\n RESULT \n") printf("\nVelocity of exit of nozzle = %f m/s",C6)
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a a r o n s o h n א ר ו נ ס ו ן a b d o u ע ב ד ו a b e d i ע ב י ד י a b i g a i l א ב י ג י י ל a b r a h a m א ב ר ה ם a b u d ע ב ع ד a d l e r א ד ל ר a d n a n ע ד נ א ן a d o r n o א ד ו ר נ ו a d r i a n a א ד ר י א נ א a h e r n א ה י ר ן a i m a r א י מ א ר a j a m i ע ' ג מ י a k i א ק י a l a l w a n i א ל ע ל ו א נ י a l a s s a d א ל א ס ד a l b a y r a k א ל ב א י ר ק a l b i n א ל ב י ן a l f o n s o א ל פ ו נ ס ו a l i a k s a n d r א ל י א ק ס א נ ד ר a l l o u d i ע ל ו ד י a l l y s o n א ל י ס ו ן a l m a i m a n i א ל מ א י מ נ י a l m e y d a א ל מ י ד א a m e r i c a n a א מ ר י ק א נ א a m n o n א מ נ ו ן a n a h e i m א נ א ה א י ם a n d r e a s א נ ד ר י א ס a n n o א נ ו a n t o n א נ ט ו ן a n t o n i u s א נ ט ו נ י ו ס a p o c a l y p t i c a א פ ו ק א ל י פ ט י ק א a p o l l i n a i r e א פ ו ל י נ י י ר a q u i t a i n e א ק ו י ט י י ן a r b i l א ר ב י ל a r d a s h i r א ר ד ש י ר a r m a n d א ר מ א נ ד a r n e א ר נ י a r t z i א ר צ י a s a h a r a א ס א ה א ר א a s a m o a h א ס א מ ו א a s c i i א ס ק י a s c o l i א ס ק ו ל י a s t u r i a s א ס ט ו ר י א ס a t l e t i c o א ט ל ט י ק ו a u b r e y א ו ב ר י a u d o א ו ד ו a u s t i n א ו ס ט י ן a v r a h a m א ב ר ה ם a z a l i א ז א ל י b a b y l o n ב א ב י ל ו ן b a d o u ב א ד ו b a d u ב ד ו b a e y e r ב א י ר b a h j a t ב ה ג ' ט b a h n i n i ב ח נ י נ י b a j e r ב א י ר b a k r ב ק ר b a r d o n ב א ר ד ו ן b a r d s l e y ב א ר ד ס ל י b a r n a r d ב ר נ א ר b a r r a g a n ב ר א ג א ן b a r u s s o ב א ר ו ס ו b a s s e m ב א ס ם b a s s i m ב א ס י ם b a s t i a n ב א ס ט י א ן b a t a y s k ב א ט א י ס ק b a t r o u n ב ט ר ו ן b a t t i s t o n ב א ט י ס ט ו ן b a u h a u s ב א ו ה א ו ס b a u h i n ב ו ה י ן b e c k e t t ב י ק י ט b e e r ב י ר b e g i n ב ג י ן b e h r a m i ב ה ר א מ י b e l g r a d e ב ל ג ר א ד b e n a g l i o ב י נ א ג ל י ו b e n i n ב נ י ן b e n n i s ב נ י ס b e r c e l l i n o ב ר צ ' ל י נ ו b e r l u s c o n i ב ר ל ס ק ו נ 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א ן c l a r e ק ל י י ר c l e a r y ק ל י ר י c o c o ק ו ק ו c o l e t t e ק ו ל י ט c o l o m b o ק ו ל ו מ ב ו c o m b i n ק ו מ ב י ן c o n a n ק ו נ א ן c o n c e i c a o ק ו נ ס י ס א ו c o n n e r y ק ו נ ר י c o n t i ק ו נ ט י c o o l s ק ו ל ז c o p e l a n d ק ו פ ל א נ ד c o r e l l i ק ו ר י ל י c o r i n ק ו ר י ן c o r n w a l l ק ו ר נ ו א ל c o s m i n ק ו ז מ י ן c o s t a n z o ק ו ס ט א נ ז ו c o t y ק ו ט י c o u r t e n e y ק ו ר ט נ י c r o t h e r s ק ר ו ת ר ס c u r l ק ו ר ל d a d a ד א ד א d a f n a ד פ נ א d a g e s t a n ד א ג ס ט א ן d a h a m ד ה א ם d a h l ד א ל d a l l a s ד א ל א ס d a l l i ד א ל י d a n a ד א נ א d a n i e l e ד נ י א ל d a n n i ד א נ י d a n t e ד א נ ט ה d a n y ד א נ י d a r o n ד א ר ו ן d a r u i ד א ר ו י d a u d e t ד ו ד ה d a v a l a ד א ו א ל א d a w a ד א ו ה d e c i u s ד ק י ו ס d e c k e r ד י ק ר d e h n ד ה ן d e i m o s ד י י מ ו ס d e l e ד י ל י d e l f i n o ד ל פ י נ ו d e l v e c c h i o ד ל ב י ק י ו d e m i r e l ד י מ י ר י ל d e m p s e y ד מ פ ס י d e n z i l ד י נ ז ל d e s a i ד ס א י d e s a i l l y ד י ס א י י d e v e r i c ד י ב י ר י ט ש d i l l o n ד י ל ו ן d i n d a n e ד נ ד א נ י d i o n ד י ו ן d o m i n g o ד ו מ י נ ג ו d o m i n i k a ד ו מ י נ י ק א d o m i t i a n ד ו מ י ט י א ן d o n s k o y ד ו נ ס ק ו י d o r i g o ד ו ר י ג ו d o t c h e v ד ו צ ' ב d r a g o s l a v ד ר א ג ו ס ל א ב d r e s d e n ד ר ס ד ן d r e t a r ד ר י ט א ר d r n o v s e k ד ר נ ו ב ס י ק d r u z e ד ר ו ז d u c o m m u n ד ו ק ו מ ו ן d u d u ד ו ד ו d u l c e ד ו ל ס י d u n n ד א ן d u n s t a p l e ד א נ ס ט א פ ל d z h o k h a r ג ' ו ח ר e b o l i א ב ו ל י e f r a t א פ ר ת e l i n א ל י ן e l i s h a א ל י ש ע e m a r א י מ א ר e m d e n א מ ד ן e m e k ע מ ק e n d l e s s א נ ד ל י ס e p h r a i m א פ ר י ם e r o s א י ר ו ס e s t a d i o א ס ט א ד י ו f a h i m a פ ה י מ ה f a n d e l פ א נ ד ל f a r g e o n פ א ר ג י ו ן f a r i d פ ר י ד f a r i s פ א ר י ס f a u r e פ ו ר י f e c h n e r פ כ נ ר f e r d o o s פ ר ד ו ס f i g h t i n g פ א י ט י נ ג f i n n פ י ן f l a h e r t y פ ל א ה י ר ט י f l a m i o n פ ל א מ י ו ן f l o r i a n o p o l i s פ ל ו ר י א נ ו פ ו ל י ס f o e k e פ ו ק י f r a n c i s c a n פ ר נ ס י ס ק ן f r a n c o פ ר א נ ק ו f r e d e r i c k s פ ר י ד ר י ק ס f r e d r i c פ ר י ד ר י ק f r e i פ ר י י f r e y פ ר י י f u l l e r פ ו ל ר f u n k e פ ו נ ק ה g a b r i e l ג ב ר י א ל g a b r i e l a ג א ב ר י א ל ה g a e t a n o ג א י ט א נ ו g a l a k o s ג א ל א ק ו ס g a l i m z y a n ג א ל י מ ז י א ן g a l i n o v i c ג א ל י נ ו ב י ט ש g a l l e r ג א ל ר g a l s w o r t h y ג א ל ז ו ו ר ת י g a m z a t o v ג מ ז ט ו ב g a n ג א ן g a n g n i h e s s o u ג א נ ג נ י ה י ס ו g a n z o u r i ג נ ז ו ר י g a r b o ג א ר ב ו g a r i s e b ג א ר י ס ב g a r n e r ג א ר נ ר g a r y ג א ר י g a t e s ג י י ט ס g a z z a n i g a ג א ז א נ י ג א g e o r g e s ג ' ו ר ג ' g e r h a r d ג ר ה א ר ד g e r i z i m ג ר י ז י ם g e r m a n ג ' ר מ א ן g e z a ג ז א g h a l y ג א ל י g h a z i ג א ז י g i a n c a r l o ג ' א נ ק א ר ל ו g i g i ג ' י ג ' י g i l a d ג ל ע א ד g i m m e ג י מ י g i o r g i o ג ' ו ר ג ' ו g i o v a n n a ג ' ו ב א נ א g i u l i a n i ג ' ו ל י א נ י g j i r o k a s t e r ג י ר ו ק א ס ט ר g l o v e r ג ל ו ב ר g o d f r e y ג ו ד פ ר י g o e t h a l s ג ו ת א ל ס g o h a r ג ו ה ר g r a z i a ג ר א ז י א g r i m a l d i ג ר י מ א ל ד י g r i m i ג ר י מ י g u e n o n ג ו י נ ו ן g u e r r e i r o ג ו י ר י ר ו g u e v a r a ג ו ו א ר א g u i m a r d ג י מ א ר g u l b e n k i a n ג ו ל ב נ ק י א ן g u y ג א י h a b r e ח ב ר י h a d i t h ח ד י ת h a f e e t ח פ י ט h a f i d ח פ י ד h a i d o n g ה א י ד ו נ ג h a i r u d d i n ה א י ר ו ד י ן h a j e r i ח ג ' ר י h a l e v i ה ל ו י h a l i l h o d z i c ח ל י ל ה ו ד ז י ט ש h a m b u r g ה א מ ב ו ר ג h a m d a n ח מ ד א ן h a m i t ח מ י ט h a n e s c u ה א נ י ס ק ו h a n n i b a l ה א נ י ב א ל h a r i t h ח א ר י ת h a r k u s ה א ר ק ו ס h a r o l d ה א ר ו ל ד h a t o y a m a ה א ט ו י א מ א h a y e s ה י י ז h a y m a n o t ה א י מ א נ ו ט h e a l e y ה י ל י h e b u t e r n e א ב ו ט א ר ן h e e n a n ה י נ א ן h e i d e l b e r g ה א י ד ל ב ר ג h e i o a r ה י י ו ר h e m e d ח מ ד h e n g ה י נ ג h e n m a n ה י נ מ א ן h e r a c l e s ה י ר א ק ל י ס h e r a c l i t u s ה י ר א ק ל י ט ס h e r s c h e l ה י ר ש י ל h e r u t ח י ר ו ת h e y l e n s ה י י ל נ ס h e y n e m a n n ה י י נ י מ א ן h e y s e ה י י ס h i c h a m ה י ש א ם h i c k ה י ק h i k m a t ח ק מ ט h i r o a k i ה י ר ו א ק י h i r z ח י ר ז h i t m a n ה י ט מ א ן h j a l m a r ה י א ל מ א ר h m a m ח מ א ם h m e d e ח מ י ד ה h o k o ה ו ק ו h o l c e r ה ו ל ק ר h o l l a n d ה ו ל א נ ד h o l o d o m o r ה ו ל ו ד ו מ ו ר h o r i k a w a ה ו ר י ק א ו א h o r i s o n ה ו ר י ס ו ן h o r s t ה ו ר ס ט h o r u s ח ו ר ו ס h o s s e i n i ח ו ס י י נ י h o w e ה א ו h r a w i ה ר א ו י h r b a t y ה ר ב א ט י h u b b e r t ה ו ב ר ט h u d d l e s t o n e ה א ד ל ס ט ו ן h u d h a y f a h ח ו ד י י פ ה h u l k ה ל ק h u m b o l d t ה א מ ב ו ל ט h u t c h i n s o n ה ו ט ש י נ ס ו ן h y d r o g r a p h y ה א י ג ' ר ו ג ר א פ י i b t i s a m א י ב ט י ס א ם i h a r a א י ה א ר א i i i א י י י i n d y k א י נ ד י ק i r a q i ע י ר א ק י i r n e א י ר ן i s h a k א י ס ח א ק i s h i h a r a א י ש י ה א ר א i s r a e l s א י ז ר י ל ז i s s t a א י ס ט א i s s y k א י ס י ק i t a l y א י ט א ל י i v a n h o e א י ב א נ ה ו i v e r s o n א י ב ר ס ו ן i z h a r א י ז ה א ר i z m i r א י ז מ י ר j a b a l ג ' ב ל j a c q u a r d ג ' א ק א ר j a c q u e s ז ' ק j a d ג ' א ד j a h a n g i r ג ' ה א נ ג י ר j a h n י א ן j a i m e ג ' י י מ י j a m e ג ' י י ם j a m i e s o n ג ' מ י ס ו ן j a m m e h ג ' א מ ע j a n e ג ' י י ן j a r e d ג ' א ר י ד j a v a d ג ' א ו ו א ד j a w d a t ג ' א ו ד א ט j e f f r e y ג ' פ ר י j e n c k s ג ' נ ק ס j e n s e n ג ' נ ס ן j e r z y י י ר ז י j e s p e r י ס פ ר j l l o y d ג ' ל ו י ד j o d y ג ' ו ד י j o h a n n e s b u r g ג ' ו ה א נ ס ב ר ג j o n b e n e t ג ' ו נ ב י נ י ט j o r d a o ח ו ר ד א ו j o s e ח ו ס ה j o s e p h i n e ג ' ו ז פ י ן j o s h u a ג ' ו ש ו א j o s p i n ג ' ו ס פ א ן j o u h a u x ג ' ו ה ו j u l i a ג ' ו ל י א k a l i n i c ק א ל י נ י ט ש k a l l o n ק א ל ו ן k a m a m o t o ק א מ א מ ו ט ו k a m e n ק א מ ן k a m i y a ק א מ י א k a r i m ק ר י ם k a r i o k k a ק א ר י ו ק א k a r i r i ק ר י ר י k a r p i n s k i ק א ר פ י נ ס ק י k a r r o u b i ק א ר ו ב י k a s h m i r ק ש מ י ר k a w a i ק א ו א י k e a c h ק י ט ש k e e s ק י ז k e i z o ק י י ז ו k e m p f f ק י מ פ ף k e n t a r o ק י נ ט א ר ו k f a r כ פ ר k h a l d u n ח ל ד ו ן k i b a k i ק י ב א ק י k i i c h i r o ק י ט ש י ר ו k i k u c h i ק י ק ו צ ' י k i l p i n ק י ל פ ן k i m i ק י מ י k i r b y ק י ר ב י k i r c h n e r ק י ר ש נ י ר k i r k i l a s ק י ר ק י ל א ס k i t t i s a k ק י ט י ס א ק k j a r ק י א ר k l i n g h o f f e r ק ל י נ ג ו פ ר k n e z נ י ז k o k o s c h k a ק ו ק ו ש ק א k o l l h o f f ק ו ל ה ו ף k o m a n ק ו מ א ן k o n d r a t i e v ק ו נ ד ר א ט י י ב k o n s t a n t i n o s ק ו נ ס ט א נ ט י נ ו ס k o p k e ק ו פ ק ה k o r b u t ק ו ר ב ט k o r e a n ק ו ר י א ן k o t a r o ק ו ט א ר ו k o u i s ק ו י ס k r a n k l ק ר א נ ק ל k r i s t i a n s a n d ק ר י ס ט י א נ ס א נ ד k r i s t o f ק ר י ס ט ו ף k u d r o w ק ו ד ר ו k u l ק ו ל k u l t h u m ק ל ת ו ם k u m a r a t u n g a ק מ א ר א ט ו נ ג א k u n d e r a ק ו נ ד י ר א k u r o k a w a ק ו ר ו ק א ו א k u t a i s i ק ו ט א י ס י k u z n e t s o v a ק ו ז נ ט ס ו ב א k v a s n a k ק ב א ס נ א ק k y r e n i a ק י ר י נ י א l a b a n ל ב ן l a b o n e ל א ב ו ן l a d y ל י י ד י l a m a ל א מ א l a m a r i ל א מ א ר י l a m a r t i n e ל א מ א ר ט י ן l a n d a u ל א נ ד א ו l a r s e n ל א ר ס ן l a t o u n d j i ל א ט ו נ ג ' י l a t u f f ל א ט ו ף l a w a l ל א ו א ל l e b e d ל י ב י ד l e c u o n a ל י ק ו נ א l e i d e n ל י ד י ן l e i g h ל י l e i l e i ל י י ל י י l e m ל ם l e n e v ל נ ב l e r d o r f ל ר ד ו ר ף l e t o ל י ט ו l e w a n d o w s k i ל י ב א נ ד ו ב ס ק י l i a k h o v ל י א ק ו ב l i b e r t a d o r e s ל י ב ר ט א ד ו ר י ס l i l ל י ל l i n g ל י נ ג l i p s t a d t ל י פ ס ט ד א ט l o c a r n o ל ו ק א ר נ ו l o d o v i c o ל ו ד ו ב י ק ו l o l a ל ו ל א l o o s ל ו ס l o r n a ל ו ר נ א l u g a n o ל ו ג א נ ו l u h a n s k ל ו ה א נ ס ק l u n g ל ו נ ג l y n n e ל י ן l y u d m i l a ל ו ד מ י ל א m a b r o u k מ ב ר ו ק m a c e i o מ א ס י ו m a c l a i n e מ א ק ל י י ן m a d e l e i n e מ א ד ל י ן m a g g i e מ א ג י m a g h r e b מ א ג ר ב m a g i d מ ג י ד m a h a l מ ח ל m a j o r מ י י ג ו ' ר m a j s t o r o v i c מ א י ס ט ר ו ב י ט ש m a k o n n e n מ א ק ו נ י ן m a k o t o מ א ק ו ט ו m a k r a m מ ק ר ם m a k s i m מ א ק ס י ם m a l d i v e s מ א ל ד א י ב ז m a l i k מ א ל י ק m a l o t מ א ל ו m a m e t מ א מ ט m a n o l e t e מ א נ ו ל י ט י m a n s f i e l d מ א נ ס פ י ל ד m a r c h e t t o מ א ר ק י ט ו m a r i a n מ א ר י א ן m a r i a n o מ א ר י א נ ו m a r i o t מ א ר י ו ט m a r i u s מ א ר י ו ס m a r k o v מ א ר ק ו ב m a r m a d u k e מ א ר מ א ד ו ק m a r u l a n d a מ א ר ו ל א נ ד א m a r x מ א ר ק ס m a s a k a z u מ א ס א ק א ז ו m a s a k o מ א ס א ק ו m a s e r a t i מ ס י ר א ט י m a s h e g o מ א ש י ג ו m a s h h a d מ ש ה ד m a s l o w מ א ס ל ו m a s n y מ א ס נ י m a t e r a z z i מ א ט י ר א צ י m a t t i מ א ט י m a t y a s מ א ט י א ס m a t z a מ צ ה m a u r i a c מ ו ר י א ק m a y a k o v s k y מ א י א ק ו ב ס ק י m a z u t מ א ז ו ט m b o m a מ ב ו מ א m c c a n n מ ק א ן m c c l a i r מ ק ל י ר m e g a l o d o n מ י ג א ל ו ד ו ן m e h a n n a מ ה נ א m e l מ ל m e l a m e d מ ל מ ד m e l a n i e מ י ל א נ י m e n a s s e מ י נ א ס ה m e n o מ י נ ו m e r k a z מ ר כ ז m e r n i s s i מ ר נ י ס י m e r o n מ י ר ו ן m e r s e n n e מ י ר ס י ן m e t r e v e l i מ י ט ר י ב י ל י m i c a h מ י ק ה m i c h a e l s מ א י ק ל ז m i g l i o r e מ י ג ל י ו ר י m i g r o n מ י ג ר ו ן m i n o t מ י נ ו ט m i r o מ י ר ו m i t s u a k i מ י ט ס ו א ק י m i z u s h i m a מ י ז ו ש י מ א m o c h i z u k i מ ו צ ' י ז ו ק י m o d i g l i a n i מ ו ד י ל י א נ י m o g l e n מ ו ג ל י ן m o h a m e d מ ו ח מ ד m o h a m m e d מ ו ח מ ד m o k h t a r i מ ו ח ט א ר י m o k o e n a מ ו ק ו י נ א m o n c a y o מ ו נ ק א י ו m o n r o v i a מ ו נ ר ו ב י א m o n t a n a מ ו נ ט א נ א m o n t a n d מ ו נ ט א ן m o n t e r r o s o מ ו נ ט י ר ו ס ו m o r a n מ ו ר א ן m o r i מ ו ר י m o r i e n t e s מ ו ר י א נ ט ס m o r i h i r o מ ו ר י ה י ר ו m o t e a b מ ו ט ע ב m o z a r t מ ו צ א ר ט m u d i מ ו ד י m u h a r r a m מ ו ח א ר ם m u l l i s מ ו ל י ס m u r a w s k i מ ו ר א ו ס ק י m u r t a l a מ ו ר ט א ל א n a d e r נ י י ד ר n a h u m נ ח ו ם n a k a c h e נ ק א ש n a k a m a t s u נ א ק א מ א צ ו n a k a t a נ א ק א ט א n a m b a r y n נ א מ ב א ר י ן n a m i k a w a נ א מ י ק א ו א n a n a נ א נ א n a n i נ א נ י n a s d a q נ א ס ד א ק n a s r i נ ס ר י n a t i v נ ת י ב n a y s m i t h נ י י ס מ י ת n e d a נ ד א n e f e r t i t i נ פ ר ט י ט י n e p a l נ פ א ל n e t z e r נ צ ר n i c k y נ י ק י n i i g a k i נ י ג א ק י n i k נ י ק n i k o l a y נ י ק ו ל א י n i m i t z נ י מ י ץ n i s h i k o r i נ י ש י ק ו ר י n i u e נ י ו n o d i a נ ו ד י א n o k i a נ ו ק י א n o l b e r t o נ ו ל ב י ר ט ו n o r i o נ ו ר י ו n o u נ ו n o v a r t i s נ ו ב א ר ט י ס n o v i n נ ו ב י ן n u n o נ ו נ ו n u r e n b e r g נ ו ר י נ ב י ר ג o b a m a א ו ב א מ א o k w u n w a n n e א ו ק ו ו נ ו א נ י o l y m p u s א ו ל י מ פ ו ס o m a r i ע ו מ א ר י o r h a n א ו ר ה א ן o r t e g a א ו ר ט י ג א o u s m a n e ע ו ס מ א ן o w e n א ו י ן o z e r ע ו ז י י ר p a g a n i פ א ג א נ י p a i n e פ י י ן p a k i t o פ א ק י ט ו p a l a u פ א ל א ו p a l e r m o פ א ל ר מ ו p a n t a n a l פ א נ ט א נ א ל p a r m a פ א ר מ א p a r r i s h פ א ר י ש p a s c a n i פ א ס ק א נ י p a s c u a l פ א ס ק ו א ל p a s q u a l פ א ס ק ו א ל p a s q u a l e t t i פ א ס ק ו א ל י ט י p a s t o n פ א ס ט ו ן p a t i e n c e פ י י ש א נ ס p a t t o n פ א ט ן p a u l i n a פ א ו ל י נ א p a u l u s פ א ו ל ו ס p a y t o n פ י י ט ו ן p e a r s o n פ י ר ס ו ן p e d e r s e n פ י ד ר ס ן p e d r o פ ד ר ו p e d r o s פ י ד ר ו ס p e l l e פ י ל י p e l l e g r i n i פ י ל י ג ר י נ י p e l l i פ י ל י p e l t o n פ י ל ט ו ן p e p i n פ פ י ן p e r e l m a n פ ר ל מ א ן p e r i פ ר י p e r l m u t t e r פ י ר ל מ ו ט ר p e t r i c פ ט ר י ט ש p h i l i p p i n e s פ י ל י פ י נ ז p h i l l i p s פ י ל י פ ס p i a f פ י א ף p i e n a a r פ י נ א ר p i e r o פ י י ר ו p i n i פ י נ י p i t u r a t פ י ט ו ר א ט p o i n c a r e פ ו א נ ק א ר ה p o l y e n e פ ו ל י י ן p o m p e u פ ו מ פ י ו p o p e s c u פ ו פ י ס ק ו p o p u l a r פ ו פ י ו ל א ר p o r p h y r i a פ ו ר פ י ר י א p o r t a s פ ו ר ט א ס p o s e y פ ו ז י p o t t e r פ ו ט ר p o z z o פ ו צ ו p r o g e r i a פ ר ו ג י ר י א p r y o r פ ר א י ו ר q a r u h ק א ר ו ה q u a n ק ו א ן q u i x o t e ק י ו ט י r a b a h ר א ב ח r a b i n ר ב י ן r a c h a d ר א צ ' א ד r a d i o ר א ד י ו r a d o j k o ר א ד ו י ק ו r a d o n ר י י ד ו ן r a d w a n s k a ר א ד ו א נ ס ק א r a f a e l ר פ א ל r a j o u b ר ' ג ו ב r a m p a l ר א מ פ א ל r a n d a l l ר א נ ד א ל r a p p ר א פ י r a s ר א ס r a s c h k e ר א ש ק י r a s p u t i n ר א ס פ י ו ט י ן r a z ר א ז r e a g a n ר י י ג ן r e i n h o l d ר א י נ ה ו ל ד r e m i ר י מ י r e n a u l t ר י נ ו ל ט r e n q u i n ר י נ ק ו י ן r e x ר ק ס r h o d e s i a ר ו ד י ס י א r i b b e c k ר י ב י ק r i g o b e r t a ר י ג ו ב י ר ט א r i m i t t i ר י מ י ט י r i s k i n ר י ס ק י ן r i t a ר י ט א r i y a d ר י א ד r o b e r t s ר ו ב ר ט ס r o c h e ר ו ש r o c h e l l e ר ו ש י ל r o d r i g u e z ר ו ד ר י ג י ז r o e n t g e n i u m ר ו נ ט ג נ י ו ם r o g g e v e e n ר ו ג י ב י ן r o g i e r ר ו ג ' י ר r o m n e y ר ו מ נ י r o n d o n i a ר ו נ ד ו נ י א r o o m ר ו ם r o s s i ר ו ס י r o s s i n i ר ו ס י נ י r o t h m a n ר ו ת מ א ן r o t t ר ו ט r o u a n i ר ו א נ י r o y a l ר ו י א ל r u b i n ר ו ב י ן r u d d ר ו ד r u f f a l o ר ו פ א ל ו r u i ר ו י r u s l a n ר ו ס ל א ן r u s s i a ר א ש א r u u d ר ו ד r u u t e l ר ו ט ל s a d e k ס א ד ק s a e z ס א י ז s a g a n o w s k i ס א ג א נ ו ו ס ק י s a h a ס א ה א s a i f ס א י ף s a l e n k o ס א ל י נ ק ו s a l e s ס י י ל ז s a l h a b ס ל ה ב s a l i ס א ל י s a l p i g i d i s ס א ל פ י ג י ד י ס s a l v a t o r e ס א ל ב א ט ו ר י s a m o s a ס א מ ו ס א s a m p r a s ס א מ פ ר א ס s a m u e l ס א מ ו א ל s a m y ס א מ י s a n d o r ס א נ ד ו ר s a n k a r a ס א נ ק א ר א s a n o g o ס א נ ו ג ו s a n o u ס א נ ו s a n t o n ס א נ ט ו ן s a r g s y a n ס ר ג ס י א ן s a r r i o n a n d i a ס א ר י ו נ א נ ד י א s c a r p a ס ק א ר פ א s c h l o s s b e r g ש ל ו ס ב ר ג s c h m i d t ש מ י ד ט s c h o p e n h a u e r ש ו פ נ ה א ו ר s c h r i j v e r s ש ר י ב ר ז s c h u s t e r ש ו ס ט ר s c o l a ס ק ו ל א s e b a s t i a n ס י ב א ס ט י א ן s e e d o r f ס י ד ו ר ף s e e h a w o n g ס י ה א ו ו נ ג s e i n f e l d ס י י נ פ י ל ד s e l k i r k ס י ל ק י ר ק s e m a n ס י מ א ן s e n j u r o ס י נ ג ' ו ר ו s e o u l ס י א ו ל s e r a f i n ס ר א פ י ן s e s t i c ס ס ט י ק s h a a r a w i ש ע ר א ו י s h a b t a i ש ב ת א י s h a k i b ש א ק י ב s h a l o m ש ל ו ם s h a m i l ש א מ י ל s h a n e ש י י ן s h a r i f ש ר י ף s h a w a r m a ש א ו ר מ א s h e e t r i t ש ט ר י ת s h e r i h a n ש ר י ה א ן s h i g e y o s h i ש י ג י ו ש י s h i k m a ש י ק מ א s h i l k a ש י ל ק א s h i l l a ש י ל א s h i p m a n ש י פ מ א ן s h k l o v s k y ש ק ל ו ב ס ק י s h l o m o ש ל מ ה s h r a g a ש ר ג א s i b e n i k ס י ב י נ י ק s i d o r e n k o ס א י ד ו ר נ י ק ו s i e n n a ס י א נ א s i h a n o u k ס י ה א נ ו ק s i m e o n ס י מ י א ן s i m o n s ס י מ ו נ ז s i n i b a l d i ס י נ י ב א ל ד י s i n n ס י ן s i t i ס י ט י s l i m ס ל י ם s l o v a k ס ל ו ב א ק s l o v a k i a ס ל ו ב א ק י א s o c h a ס ו כ א s o l e r ס ו ל ר s o r a i a ס ו ר א י א s o r b o n n e ס ו ר ב ו ן s o w e ס ו s o y u z ס ו י ו ז s p a r t a ס פ א ר ט א s p e r l ס פ א ר ל s p y c h e r ס פ א י ק ר s t a c y ס ט י י ס י s t a p l e t o n ס ט י י פ ל ט ו ן s t e f k a ס ט י פ ק א s t i r l i n g ס ט י ר ל י נ ג s t o o r ס ט ו ר s t u p a r ס ט ו פ א ר s u c h a ס ו ש א s u r ס ו ר s v i a t o s l a v ס ב י א ט ו ס ל א ב s y l v e s t e r ס י ל ב ס ט ר t a c c o n i ט א ק ו נ י t a i m ט א י ם t a j i k i s t a n ט א ג ' י ק ס ט א ן t a k a s h i ט א ק א ש י t a l a b a n i ט א ל ב א נ י t a l m u d ת ל מ ו ד t a m a r ת מ ר t a m m e t ט א מ י ט t a m r a ט א מ ר א t a r i n ט א ר י ן t a r y n ט א ר י ן t a s s o s ט א ס ו ס t a u b ט א ו ב t a y e b ט י י ב t c h a n g a i ט צ ' א נ ג א י t e f i l o ט פ י ל ו t e n j i ט י נ ג ' י t e n z i n g ט י נ ס י נ ג t e r r e n c e ט י ר י נ ס t e x ט י ק ס t h a b o ת א ב ו t h e o d o r a ת י ו ד ו ר א t h e r a v a d a ת י ר א ב א ד א t h e r d s a k ת ר ד ס א ק t h i e r i n g ת י ר י נ ג t h o m p s o n ט ו מ ס ו ן t h o u s a n d ת ו ס נ ד t i c h y ט י צ ' י t i c l e a n u ט י ק ל י א נ ו t i e r n e y ט י ר נ י t i t o ט י ט ו t o j o ט ו ג ' ו t o k i m u n e ט ו ק י מ ו נ ה t o m ט ו ם t o m m o t ט ו מ ו ט t o r r e ט ו ר י t o r t o l a ט ו ר ט ו ל א t o r t o s a ט ו ר ט ו ס א t o s h i k i ט ו ש י ק י t o s h i y u k i ט ו ש י ו ק י t o s i c ט ו ס י ט ש t o t o ט ו ט ו t o u m a n i ט ו מ א נ י t o u q a n ט ו ק א ן t o v ט ו ב t o y o t o m i ט ו י ו ט ו מ י t r a o u i ט ר א ו י t r o t t a ט ר ו ט א t u l l a m o r e ט ו ל א מ ו ר t u r a n d o t ט ו ר א נ ד ו ט t u r g u t ט ו ר ג ו ט t w a i n ט ו י י ן t y m o s c h u k ט י מ ו ש ו ק t y n a n ט י נ א ן u m a r u ע מ א ר ו u n i t e d י ו נ א י ט ד v a l e n t e ו א ל נ ט י v a l e n t i n ع א ל נ ט י ן v a l e n t i n e ו א ל נ ט י ן v a l e r a ב א ל י ר א v a l e r i y ו א ל י ר י v a l k e ו א ל ק v a n a h e i m r ו א נ א ה י מ ר v a n o n i ו א נ ו נ י v e d r a n ו ד ר א ן v e r d e ו ר ד י v i a l e ו י א ל י v i d u k a ו י ד ו ק א v i n s o n ו י נ ס ו ן v i o r e l ו י ו ר י ל v i s t u l a ו י ס ט ו ל א v i v o ב י ב ו v o j i s l a v ו ו י ס ל א ב v o j t a ב ו י ט א v o l o d y m y r ו ו ל ו ד י מ י ר v o l t a ו ו ל ט א v u k c e v i c ו ו ק ס י ב י ט ש v u k o t i c ו ו ק ו ט י ט ש w a s e i g e ו א ס י ג ' w a y n e ו י י ן w e n d y ו נ ד י w h e l a n ו י ל א ן w i l d e r ו א י ל ד ר w i l k i n s ו י ל ק י נ ז w i l l i a m s ו י ל י א מ ס w i m m e r ו י מ ר w o r t h i n g t o n ו ר ת י נ ג ט ן x i a n g ק ס י א נ ג x u r i ק ס ו ר י y a j i m a י א ג ' י מ א y a m i n י מ י ן y a m o u s s o u k r o י א מ ו ס ו ק ר ו y a n g י א נ ג y a n n i s י א נ י ס y a p i n g י א פ י נ ג y a z i d י ז י ד y e l l o w s t o n e י ל ו ס ט ו ן y o u n g י ו נ ג y u l i a n t o י ו ל י א נ ט ו z a c c h e r o n i ז א ק י ר ו נ י z a c k ז א ק z a m o r a ז א מ ו ר א z a p a t e r 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clc hfg = 2202.6 // Latent heat of fusion in kJ/kg Qh = 5.83 // Heat addition in MJ/s ws = Qh/hfg // steam flow rate eg = 0.9 // efficiency of generator P = 1000 // Power generation rate in kW Wnet = 1000/eg // Net output nbrake = 0.8 // brake thermal efficiency h1_2s = Wnet/(ws*nbrake) // Ideal heat addition n_internal = 0.85 // internal efficiency h12 = n_internal*h1_2s // Actual heat addition hg = 2706.3 // Enthalpy of gas in kJ/kg h2 = hg //Isenthalpic process h1 = h12+h2 // Total enthalpy h2s = h1-h1_2s // Enthalpy change hf = 503.71 // Enthalpy of fluid in kJ/kg x2s = (h2s-hf)/hfg // Quality of steam sf = 1.5276 // entropy of fluid in kJ/kgK sfg = 5.6020 // Entropy change due to vaporization in kJ/kgK s2s = sf+(x2s*sfg) // Entropy at state 2s s1 = s2s // Isentropic process P1 = 22.5 // Turbine inlet pressure in bar from Mollier chart t1 = 360 // Temperature of the steam in degree Celsius from Mollier chart printf("\n Example 12.9\n") printf("\n Temperature of the steam is %d degree celcius",t1) printf("\n Pressure of the steam is %f bar",P1) //The answers vary due to round off error
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function [x,y,typ]=TRASH_f(job,arg1,arg2) x=[];y=[];typ=[] select job case 'plot' then standard_draw(arg1) graphics=arg1(2); [orig,sz,label]=graphics([1:2 4]) xstringb(orig(1),orig(2),'Trash',sz(1),sz(2),'fill') case 'getinputs' then [x,y,typ]=standard_inputs(o) case 'getoutputs' then x=[];y=[];typ=[]; case 'getorigin' then [x,y]=standard_origin(arg1) case 'set' then x=arg1; graphics=arg1(2);label=graphics(4) model=arg1(3);nin=model(2) while %t do [ok,label,nin]=getvalue(.. 'Set Trash parameters',.. ['Block label'; 'Number of inputs'],.. list('str',1,'vec',1),.. ['Trash'; string(nin)]); if ~ok then break,end [model,graphics,ok]=check_io(model,graphics,nin,0,1,0) if ok then graphics(4)=label; x(2)=graphics;x(3)=model break end end case 'define' then nin=1 model=list('trash',1,0,1,0,[],[],[],[],'d',%f,[%f %f]) x=standard_define([2 2],model) end
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errcatch(-1,"stop");mode(2);//Example 1.5 ; ; //To find the refractive index of coil volume=0.2 //units in CC thickness=volume/(100*100) //units in cm n=1 lamda=5.5*10^-5 //units in cm r=0 u=(n*lamda)/(2*thickness*cos(r)) printf("Refractive index of oil is %.3f",u) exit();
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// Scilab Code Ex10.5: Page-224 (2010) N_A = 6.023e+023; // Avogadro's number k = 1.38e-023; // Boltzmann constant, J/K T = 293; // Temperature of sodium, K E_F = 3.24; // Fermi energy of sodium, eV e = 1.6e-019; // Energy equivalent of 1 eV, J/eV C_v = %pi^2*N_A*k^2*T/(2*E_F*e); // Molar specific heat of sodium, J/mole/K printf("\nThe molar specific heat of sodium = %4.2f J/mole/K", C_v); // Result // The molar specific heat of sodium = 0.32 J/mole/K
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function [chirp,waveform_distance] = chirp_generator(btproduct, start_frequency, bandwidth) end_time = btproduct/bandwidth; sample_rate = 5*bandwidth; samples = end_time*sample_rate; sample_step = end_time/samples; chirp_rate = bandwidth/end_time; time = [0:sample_step:end_time]; chirp = %e^(-%i*2*%pi*(start_frequency.*time+chirp_rate.*time.*time)); waveform_distance = end_time*3*10^8; endfunction
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clear //Depends on data22_7.sci file //Obtain path of solution file path = get_absolute_file_path('Ex22_7.sce') //Obtain path of data file datapath = path + filesep() + 'data22_7.sci' //Clear all clc //Execute the data file exec(datapath) //Calculate the shrinkage pressure P (N/mm2) P = sigmaMax * (D3^2 - D2^2)/(D3^2 + D2^2) //Calculate the radial and tangential stresses in the jacket //Store the results in arrays for plotting purposes sigmar1, sigmat1 (N/mm2) sigmar1 = []; sigmat1 = []; rad1 = []; count = 0; //Jacket radius varies from D2/2 to D3/2 for r = D2/2:2:D3/2 count = count + 1; rad1(1,count) = r; sigmar1(1,count) = ((-1 * P * D2^2)/(D3^2 - D2^2))*((D3^2/(4 * r^2)) - 1); sigmat1(1,count) = ((P * D2^2)/(D3^2 - D2^2))*((D3^2/(4 * r^2)) + 1); end //Calculate the radial and tangential stresses in the inner tube //Store the results in arrays for plotting purposes sigmar2, sigmat2 (N/mm2) sigmar2 = []; sigmat2 = []; rad2 = []; count = 0; //Inner tube radius varies from D1/2 to D2/2 for r = D1/2:2:D2/2 count = count + 1; rad2(1,count) = r; sigmar2(1,count) = ((-1 * P * D2^2)/(D2^2 - D1^2))*(1 - (D1^2/(4 * r^2))); sigmat2(1,count) = ((-1 * P * D2^2)/(D2^2 - D1^2))*(1 + (D1^2/(4 * r^2))); end //Calculate the radial and tangential stresses due to internal pressure //Store the results in arrays for plotting purposes sigmar3, sigmat3 (N/mm2) sigmar3 = []; sigmat3 = []; rad3 = []; count = 0; //Radius varies from D1/2 to D3/2 for r = D1/2:2:D3/2 count = count + 1; rad3(1,count) = r; sigmar3(1,count) = ((-1 * Pi * D1^2)/(D3^2 - D1^2))*((D3^2/(4 * r^2)) - 1); sigmat3(1,count) = ((Pi * D1^2)/(D3^2 - D1^2))*((D3^2/(4 * r^2)) + 1); end //Calculate the resultant stresses //Store the results in arrays for plotting purposes sigmar4, sigmat4 (N/mm2) //For inner tube sigmar4i = sigmar3(1,1:length(sigmar2)) + sigmar2(1,:); sigmat4i = sigmat3(1,1:length(sigmat2)) + sigmat2(1,:); //For jacket sigmar4j = sigmar3(1,length(sigmar2):length(sigmar3)) + sigmar1(1,:); sigmat4j = sigmat3(1,length(sigmat2):length(sigmat3)) + sigmat1(1,:); //Plot stresses due to internal pressure subplot(231) plot(rad3, sigmar3, '-o') title("Radial stress distribution due to internal pressure") xlabel("Radius(mm)") ylabel("Radial stress(N/mm2)") subplot(232) plot(rad3, sigmat3, '-o') title("Tangential stress distribution due to internal pressure") xlabel("Radius(mm)") ylabel("Tangential stress(N/mm2)") //Plot stresses due to shrink fit subplot(233) plot([rad2 rad1], [sigmar2,sigmar1], '-o') title("Radial stress distribution due to shrink fit") xlabel("Radius(mm)") ylabel("Radial stress(N/mm2)") subplot(234) plot([rad2 rad1], [sigmat2,sigmat1], '-o') title("Tangential stress distribution due to shrink fit") xlabel("Radius(mm)") ylabel("Tangential stress(N/mm2)") //Plot resultant stresses subplot(235) plot([rad2 rad1], [sigmar4i,sigmar4j], '-o') title("Resultant radial stress distribution") xlabel("Radius(mm)") ylabel("Radial stress(N/mm2)") subplot(236) plot([rad2 rad1], [sigmat4i,sigmat4j], '-o') title("Resultant tangential stress distribution") xlabel("Radius(mm)") ylabel("Tangential stress(N/mm2)")
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//Example number 12.4, Page number 264 clc;clear; close; //Variable declaration n1=1.563; //Core refractive index n2=1.498; //Cladding refractive index //Calculation NA=sqrt(n1**2-n2**2); //numerical aperture theta0=asin(NA); //acceptance angle(radian) theta0=theta0*180/%pi; //acceptance angle(degrees) //Resul" printf("acceptance angle is %.2f degree",theta0)