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2. (10 Points) The shock wave at the nose of the wedge shown below is a region in which viscous d...


2. (10 Points) The shock wave at the nose of the wedge shown below is a region in which viscous dissipation results in a chan
Shock wave V2 Wedge
2. (10 Points) The shock wave at the nose of the wedge shown below is a region in which viscous dissipation results in a change of flow properties. If the wedge is traveling through sea level air (T-298 K & p 14.7 psia) at a supersonic speed of 654 m/s, and temperature of the air behind the shock is 412 K, what is the speed of the air behind the shock measured relative to the shock?
Shock wave V2 Wedge
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レ wedko 2t m2 (-1) 4-1) 1.9 +2 8.444 Cs 3 44

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