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.c.. M2), derived by Zucrow and Hoffman, is given by: =>!(*n*(~4-4)" . -tan -|(41-4)") - (tan-(03 197) (tan*(03 1)*2) (y +1) (-1) where y 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 M, -1.5 and 8 = 10 degree. 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.c.. M2), derived by Zucrow and Hoffman, is given by: =>!(*n*(~4-4)" . -tan -|(41-4)") - (tan-(03 197) (tan*(03 1)*2) (y +1) (-1) where y 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 M, -1.5 and 8 = 10 degree