A vortex model for forces and moments on low-aspect-ratio wings in side-slip with experimental validation

DOI10.1098/rspa.2016.0760zbMath1404.76150OpenAlexW2589860301WikidataQ55048875 ScholiaQ55048875MaRDI QIDQ4647133

Adam C. Devoria, Kamran Mohseni

Publication date: 4 January 2019

Published in: Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1098/rspa.2016.0760

zbMATH Keywords

high angle of attacklow-aspect-ratio wingsroll stall

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) General aerodynamics and subsonic flows (76G25) Flow control and optimization for compressible fluids and gas dynamics (76N25)

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Instability and the post-critical behaviour of two-dimensional inverted flags in axial flow

Cites Work

• Prediction of leading-edge vortex behaviour to supplement the suction analogy
• A theory of the flow past a slender delta wing with leading edge separation
• Three-dimensional flows around low-aspect-ratio flat-plate wings at low Reynolds numbers
• Topology of flow patterns in vortex motions and turbulence
• On the mechanism of high-incidence lift generation for steadily translating low-aspect-ratio wings
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