Secondary separation from a slender wing

DOI10.1007/BF00037465zbMath0747.76046OpenAlexW2061112505MaRDI QIDQ1189827

S. Singh

Publication date: 27 September 1992

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

Full work available at URL: https://doi.org/10.1007/bf00037465

zbMATH Keywords

laminar flowincompressible fluidsuctioninteractive viscous-inviscid calculationprimary separationpurely inviscid calculations

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) 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 ⋮ Optimal control of diffuser shapes for non-uniform flow

Cites Work

• Separation from a smooth surface in a slender conical flow
• The laminar separation of an incompressible fluid streaming past a smooth surface
• Singularities associated with separating boundary layers
• Improved calculations of leading-edge separation from slender, thin, delta wings

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