Question: 3 . Consider an infinitely thin flat plate at an angle of attack of ( 2 0 ^ { prime prime }

3. Consider an infinitely thin flat plate at an angle of attack of \(20^{\prime \prime}\) in a Mach 3 free stream. Calculate the magnitude of the flow direction angle \(\boldsymbol{\phi}\), downstream of the trailing edge, as sketched in Fig below.
3 . Consider an infinitely thin flat plate at an

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