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Posted: **Fri May 27, 2022 6:49 am**

: Moving At True Or False 8 Points Supersonic Air Flow At M 3 0 Is Slowed Down To Me 0 5 Via A Normal Shock In A Divergi 1 (15.63 KiB) Viewed 15 times

moving at True or False [8 points] Supersonic air flow at M-3.0 is slowed down to Me-0.5 via a normal shock in a diverging channel with A./ A. -2.50. From this information, determine: Exit a) the static pressure ratio P./Pi, b) the static pressure ratio P₂/P1. Intet Me -0.5 M-3.0 12