M = input("Enter the Mach number"); G = input("Enter y"); %%lsentropic Flow%%
Pressure_Ratio = (1 + (G-1)/2* M^2)^(-G/
(G-1));
Temp_Ratio = (1 + (G-1)/2 * M^2)^(-1); Density_Ratio = (1 + (G-1)/2 * M^2)^(-1/ (G-1));
Area_Ratio = (1/M)*((2/(G+1)*(1 + (G-1)/2 * M^2)))^((G+1)/(2*(G-1))); MFP = sqrt(G)*M*( 1 + (G-1)/2 * M^2)^(-1*(G+1)/(2*(G-1)));
%%Normal Shock%%
NM2 = sqrt((M^2+2/(G-1))/(2*G/ (G-1)*M^2-1))
NPt21 = (((G+1)/2*M^2)/(1+(G-1)/ 2*M^2))^(G/(G-1)) * (2*G/(G+1)*M^2 - (G-1)/(G+1))^((-1)/(G-1))
NP21 = (2*G*M^2/(G+1))-((G-1)/(G+1)) ((2*G/(G-1)*M^2-1)*(1+(G-1)/
NT21 =
DescriptionIn this final assignment, the students will demonstrate their ability to apply two ma
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