proof ch:14-fluid-dynamics@prooflink-4

open in the book · parts/03-classical-mechanics/14-fluid-dynamics.tex:2244

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proof : ch:14-fluid-dynamics@prooflink-4proofproposition 31.70: The lift-curve slope of a thin aerofoil31.70proposition 31.28: Potential flow reduces to Laplace's equation31.28theorem 31.68: Kutta–Joukowski31.68

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proves The lift-curve slope of a thin aerofoil declared parts/03-classical-mechanics/14-fluid-dynamics.tex:2244