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Posted: **Thu May 26, 2022 11:25 am**

: 8 Points Supersonic Air Flow At M 3 0 Is Slowed Down To M 0 5 Via A Normal Shock In A Diverging Channel With A A 2 1 (24.92 KiB) Viewed 16 times

[8 points] Supersonic air flow at M-3.0 is slowed down to M-0.5 via a normal shock in a diverging channel with A./A; -2.50. From this information, determine: a) the static pressure ratio Pe/Pi, b) the static pressure ratio P₂/P₁. Exit Inlet M₁-3.0 Me -0.5 2