Code:
clc
clear
%% r = specific heat (gama)
%% M = Mach #
M = [0:0.1:2]';
r = 1.4;
A = ((r-1)/(2));
B = ((r)/(r-1));
C = (2*r/(3*r-1));
%% -----------------------------------
PR = (1./(sqrt(r).*M)); %% PR == P/P*
E = (1+(A.*(M.^2)));
PSR = (1./(sqrt(r).*M)).*((C*(E)).^B); %%PSR = P/P*o
TR = C.*(1+(A.*(M.^2))); %%TR = T/T*
Rou = (1./(sqrt(r).*M)); %%Rou = static density / static density*
F = (1-(r.*(M.^2)))./((r.*(M.^2))) + log((r.*(M.^2))); %%F = fLmax/D
disp(table(M, PR, PSR, TR, Rou, F))
Output:
MATLAB code is written below. please put and arrange all the output ( PR, PSR, TR,...
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