Nonaxisymmetric compressible swirling flow in turbomachine annuli

DOI10.2514/3.9227zbMath0594.76014OpenAlexW1968424361MaRDI QIDQ5903153

No author found.

Publication date: 1986

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.9227

zbMATH Keywords

ground effectlifting-line solutionsteady, inviscid incompressible flowsymmetrical thin wing

Mathematics Subject Classification ID

Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (4)

A numerical solution for the equation of the lifting surface in ground effects ⋮ Lifting line theory for wing-in-ground effect in proximity to a free surface ⋮ A subsonic lifting surface theory for wing-in-ground effect ⋮ Subsonic flow past thick wing in ground effect, lifting line theory

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