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Posted: **Mon Jul 11, 2022 10:06 am**

: 4 14 Consider A Supersonic Flow Past A Compression Corner With 20 The Upstream Properties Are M 3 And P 2116 L 1 (161.87 KiB) Viewed 18 times

4.14 Consider a supersonic flow past a compression corner with = 20°. The upstream properties are M₁ = 3 and p₁ = 2116 lb/ft². A Pitot tube is inserted in the flow downstream of the corner. Calculate the value of pressure measured by the Pitot tube.