Inviscid separated flow over a non-slender delta wing

DOI10.1017/S0022112095004642zbMath0865.76008MaRDI QIDQ4892845

No author found.

Publication date: 1 September 1996

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

Newton's methodLaplace equationnonlinear eigenvalue problemsimilarity solutionGreen functionvelocity potentialsteady flowlimit of small apex anglesymmetrical conical vortex sheets

Mathematics Subject Classification ID

Boundary element methods applied to problems in fluid mechanics (76M15) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Cites Work

• Prediction of leading-edge vortex behaviour to supplement the suction analogy
• Secondary separation from a slender wing

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