Consider a (15^{circ}) half-angle wedge at zero angle of attack in a Mach 3 flow of air.

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Consider a $15^{\circ}$ half-angle wedge at zero angle of attack in a Mach 3 flow of air. Calculate the drag coefficient. Assume that the pressure exerted over the base of the wedge, the base pressure, is equal to the free-stream pressure.

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Modern Compressible Flow With Historical

ISBN: 9781260570823

4th Edition

Authors: John Anderson

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Question Posted: Apr 16, 2024 07:00 AM

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Consider a (15^{circ}) half-angle wedge at zero angle of attack in a Mach 3 flow of air.

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The physical picture is sketched in Fig 412 The drag is the net force in the x direction p2 i...View the full answer

Modern Compressible Flow With Historical

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