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Air from a compressor discharges at a constant rate through a converging-diverging nozzle to the ambient. The inlet conditions to the nozzle are the following:
P=100kPa
T=300K
We also know:
P(ambient)=60kPa
The nozzle exit area is twice the throat area
Determine:
The throat pressure (kPa) and temperature (K), the shock location in terms of A/A*, and the Mach numbers immediately upstream and immeadiately downstream of the shock.
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