A normal shock wave occurs in an air flow at a point where the velocity is 700 m/s, the static pressure is 80 kPa, and the static temperature is 60 degrees Celsius. Find the velocity, static pressure, and static temperature downstream of the shock. Also, find the stagnation temperature and stagnation pressure upstream and downstream of the shock.

Answer rating: 100% (QA)

Given data Upstream velocity before the shock V1 700 ms Upstream static pressure before the shock P1 80 kPa 80000 Pa Upstream static temperature befor... View the full answer