c++ preferable

: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., Mi) and after the comer (i.e., M2), derived by Zucrow and Hoffman, is given by: I 1/2 8 = b3|tan- -tan- tan (y +1) b= (7-1) 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