The low-speed lift coefficient for an NACA 2412 airfoil at an angle of attack of (4^{circ}) is

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The low-speed lift coefficient for an NACA 2412 airfoil at an angle of attack of $4^{\circ}$ is 0.65 . Using the Prandtl-Glauert rule, calculate the lift coefficient for $M_{\infty}=0.7$.

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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 11:00 AM

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The low-speed lift coefficient for an NACA 2412 airfoil at an angle of attack of (4^{circ}) is

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Modern Compressible Flow With Historical

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