Prediction of leading-edge vortex behaviour to supplement the suction analogy

DOI10.1007/BF00042738zbMath0585.76027OpenAlexW1970545313MaRDI QIDQ1070923

B. George

Publication date: 1985

Published in: Journal of Engineering Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00042738

zbMATH Keywords

linearized approximationlow-speed flowslender-body theoryleading-edge suction analogypath of leading-edge vorticesplane wingssingle line- vortexthin wings of delta-like planformthree-dimensional lifting-surface theory

Mathematics Subject Classification ID

Vortex flows for incompressible inviscid fluids (76B47) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (2)

Inviscid separated flow over a non-slender delta wing ⋮ A vortex model for forces and moments on low-aspect-ratio wings in side-slip with experimental validation

Cites Work

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