Flowing in a convergent nozzle. At a particular location within the nozzle the pressure is 280kPa, the stream temperature is 345K, and the velocity is 150 m/s. If the cross-section area at this location is 9.29 x 10^3m^2, find:
A) The Mach number at this location
B) The stagnation temperature and pressure
C) The area, pressure, and temperature at this exit where M = 1.0.
D) The Mass rate of flow for this nozzle.