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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.
in an air-standard otto cycle the air at the beginning of the compression stroke is at 95 kpa and 22 degrees c and the
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