Use any programming language to solve the following questions: Problem 1: Consider isentropic supersonic flow around a sharp expansion comer. The relationship between the Mach number before the comer (i.e., M) and after the comer (i.e., M), derived by Zucrow and Hoffman, is given by: where is the specific heat ratio of the gas and equals to 1.4. Use the false-position method to find the value of M, when M, = 1.5 and