Consider an infinitely thin flat plate at a (5^{circ}) angle of attack in a Mach 2.6 free

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Consider an infinitely thin flat plate at a $5^{\circ}$ angle of attack in a Mach 2.6 free stream. Calculate the lift and drag coefficients.

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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 an infinitely thin flat plate at a (5^{circ}) angle of attack in a Mach 2.6 free

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Modern Compressible Flow With Historical

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