NACA 2412 airfoil with chord length of 0.64 m in the air flow under standard sea-level conditions

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NACA 2412 airfoil with chord length of 0.64 m in the air flow under standard sea-level conditions is considered. The free flow velocity is 70 m/s, and the lift per unit chord is 1254 N/m. Try to calculate the angle of attack and drag per unit chord.

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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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NACA 2412 airfoil with chord length of 0.64 m in the air flow under standard sea-level conditions

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Aerodynamics

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