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Kutta-Joukowski Theorem, Aerospace Engineering Lecture 25
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Aerospace Engineering Lectures - Kutta-Joukowski Theorem, Aerospace Engineering Lecture 25

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The concept of circulation around an airfoil and the Kutta condition are explained. A simple intuitive proof of the Kutta-Joukowski theorem which relates lift per unit span on a wing to circulation. #aerospaceengineering #gateaerospaceengineering #aerodynamics #fluidmechanics

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