jaxmoran2679 jaxmoran2679

28-02-2024
Engineering

contestada

Air enters a normal shock with the following conditions:
Pressure: 18kPa
Temperature: 205K
Velocity: 740m/s
Calculate the following properties:
a. Stagnation pressure and Mach number upstream of the shock.
b. Pressure, temperature, velocity, Mach number, and stagnation pressure downstream of the shock.

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