please i need the answer in c++ ,not math !!

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: 1/2 (M 6 = b2| tam-1 b -1 - tan (-4)*) - (een="(ma} 1)*2) ( tan-(w 1)*2)) (y +1) b= (-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 Mi = 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.e., M), derived by Zucrow and Hoffman, is given by: 1/2 (M 6 = b2| tam-1 b -1 - tan (-4)*) - (een="(ma} 1)*2) ( tan-(w 1)*2)) (y +1) b= (-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 Mi = 1.5 and 8 = 10 degree