proposition 31.70 The lift-curve slope of a thin aerofoil

open in the book · parts/03-classical-mechanics/14-fluid-dynamics.tex:2225 · p. 1067

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proposition 31.70: The lift-curve slope of a thin aerofoil31.70proposition 31.28: Potential flow reduces to Laplace's equation31.28theorem 31.68: Kutta–Joukowski31.68proof : ch:14-fluid-dynamics@prooflink-4proofcorollary 31.13: Incompressible flow31.13equation 10.24: eq:pde-poisson-equation10.24proposition 7.136: Properties of conservative fields7.136example 31.29: Flow past a sphere31.29lemma A.777: The tangential field above a bending plateA.777lemma A.733: The circle with incidence and circulationA.733proposition A.797: The outer limit loses a boundary conditionA.797theorem A.707: D'Alembert's paradoxA.707theorem 31.74: The interface dispersion relation31.74proof : ch:14-fluid-dynamics@proof-14prooflemma 31.67: Blasius' force formula31.67theorem 8.24: Residue theorem8.24remark 31.69: The Kutta condition, and where the circulation comes from31.69theorem A.737: The lift-curve slope of the flat plateA.737proof : ch:14-fluid-dynamics@proof-32proof

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typedirectionnode provenancewhere
depends_on Potential flow reduces to Laplace's equation declared parts/03-classical-mechanics/14-fluid-dynamics.tex:2241
depends_on Kutta–Joukowski declared parts/03-classical-mechanics/14-fluid-dynamics.tex:2241
proves ch:14-fluid-dynamics@prooflink-4 declared parts/03-classical-mechanics/14-fluid-dynamics.tex:2244