Question: Consider a supersonic airflow at Mach number M = 5 over a double-wedge surface, as depicted in the Figure Q3. The wedge angles are
Consider a supersonic airflow at Mach number M = 5 over a double-wedge surface, as depicted in the Figure Q3. The wedge angles are = 8 and 8 = 30. Determine: (i) The Mach number of the flow over the second wedge. 15 mark (ii) The pressure ratio between the flow over the second wedge and the 5 marks freestream. 2 82 Figure Q3: A double-wedge surface.
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