Consider the isentropic flow through a supersonic nozzle. If the test section conditions are given by T=250K, p=latm, and V-750m/s, calculate the reservoir pressure and temperature.

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Consider the isentropic flow through a supersonic nozzle.
If the test section conditions are given by T-250K, p=latm,
and V-750m/s, calculate the reservoir pressure and
6.
temperature.
Transcribed Image Text:Consider the isentropic flow through a supersonic nozzle. If the test section conditions are given by T-250K, p=latm, and V-750m/s, calculate the reservoir pressure and 6. temperature.
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