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Physics, 18.01.2021 21:20 lololol270

A rocket engine has a chamber pressure 4 MPa and a chamber temperature of 2000 K. Assuming isentropic expansion through the nozzle, and an exit Mach number of 3.2, what are the static pressure and temperature in the exit plane of the nozzle

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A rocket engine has a chamber pressure 4 MPa and a chamber temperature of 2000 K. Assuming isentropi...
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