Question: 4 . 1 4 Consider a supersonic flow past a compression corner with = 2 0 . The upstream properties are M 1 = 3

4.14 Consider a supersonic flow past a compression corner with =20. The upstream properties are M1=3 and p1=2116lbft2. A Pitot tube is inserted in the flow downstream of the corner. Calculate the value of pressure measured
4 . 1 4 Consider a supersonic flow past a

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