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升力線理論 · Vinony

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Aerodynamics
升力線理論

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EntityQ13582551· pop 5· linked from 20 articles

升力線理論

mathematical model to quantify lift

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Cambridge University Press

Theodore von Kármán

angle of attack

integral equation

Euler equations

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What links here20 pages

wingtip vortices

John Joseph Montgomery

Kutta–Joukowski theorem

lift coefficient

Irmgard Flügge-Lotz

Lift-induced drag

elliptical wing

Prandtl–Glauert transformation

Horseshoe vortex

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