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Engineering Numerical Analysis (10626251)

Use C++ or python language to solve the problem :

Problem 1: Consider isentropic supersonic flow around a sharp expansion comer. The relationship between the Mach number before the comer (i.e., M₁) and after the comer (i.e., M₂), derived by Zucrow and Hoffman, is given by:

=b12tan-1M22-1b1/2-tan-1M12-1b1/2-tan-1M22-11/2- tan-1M12-11/2

b=+1-1

where is the specific heat ratio of the gas and equals to 1.4.

Use the false-position method to find the value of M₂ when M₁ = 1.5 and =10 degree.