A normal shock wave was formed on the surface of a supersonic aircraft at a velocity of 1,600 m/s into still atmospheric air at standard seal level conditions. Calculate: a) M1, b) M2, c) P2, d) T2, e)V2

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A normal shock wave was formed on the surface of
a supersonic aircraft at a velocity of 1,600 m/s into still
atmospheric air at standard seal level conditions.
Calculate: a) M1, b) M2, c) P2, d) T2, e)V2
Transcribed Image Text:A normal shock wave was formed on the surface of a supersonic aircraft at a velocity of 1,600 m/s into still atmospheric air at standard seal level conditions. Calculate: a) M1, b) M2, c) P2, d) T2, e)V2
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