Determine the air velocity relative to a stationary observer

Reference no: EM131347008

A nuclear blast generates a normal shock wave that travels through still air with a Mach number of 5.00. The pressure and temperature in front of the shock (i.e., downstream) are 0.101 MPa and 20.0°C.

Determine the air velocity relative to a stationary observer (i.e., the wind velocity), the pressure, and the temperature immediately after the shock wave has passed.

Reference no: EM131347008

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