Kutta-Joukowski Theorem, Aerospace Engineering Lecture 25

Описание к видео Kutta-Joukowski Theorem, Aerospace Engineering Lecture 25

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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