Consider an infinitely thin flat plate at an angle of attack of (20^{circ}) in a Mach 3
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Consider an infinitely thin flat plate at an angle of attack of \(20^{\circ}\) in a Mach 3 free stream. Calculate the magnitude of the flow direction angle \(\Phi\) downstream of the trailing edge, as sketched in Fig. 4.37.
Figure 4.37:
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