Solve the below problem:
Q: For flow of air through a normal shock, the upstream conditions are V1 = 600 m/s, To1 = 500 K, and po1 = 700 kPa. Compute the downstream conditions Ma2, V2, T2, p2, and po2. The response must be typed, single spaced, must be in times new roman font (size 12) and must follow the APA format