The front section of an airfoil is a flat plate, and the rear section is a flat

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The front section of an airfoil is a flat plate, and the rear section is a flat plate flap with a downward deviation of 15°, as shown in the fellow figure, try to calculate the CL at angle of attack of 5°.

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Aerodynamics

ISBN: 9789811945861

1st Edition

Authors: Peiqing Liu

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Question Posted: Apr 29, 2024 06:00 AM

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The front section of an airfoil is a flat plate, and the rear section is a flat

Question:

-- a=5% 213 15

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Aerodynamics

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