Question: Please create a MATLAB code that will give the Mach numbers (M 1 and M 2 ) in the equation below if the expansion ratio
Please create a MATLAB code that will give the Mach numbers (M1 and M2) in the equation below if the expansion ratio (A/A*) in the inlet and exit of a nozzle, and gamma (
) is given.
For example :
in both inlet and outlet A/A* = 1.2
gamma (
) = 1.45
What are M1 and M2 ?

AA=(2+1)2(y1)y+1M(1+21M2)2(y1)y+1
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