A supersonic flow at Mach 3.0 and y = 1.4 is to be slowed down via...

 

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A supersonic flow at Mach 3.0 and y = 1.4 is to be slowed down via a normal shock in a diverging channel. For the conditions shown in the Figure below, find p2/pı and pe/pi. Exit Inlet M, = 0.4 M = 3.0 Ai A = 2A; A supersonic flow at Mach 3.0 and y = 1.4 is to be slowed down via a normal shock in a diverging channel. For the conditions shown in the Figure below, find p2/pı and pe/pi. Exit Inlet M, = 0.4 M = 3.0 Ai A = 2A;