The physical interpretation of the lift discrepancy in Lanchester–Prandtl lifting wing theory for Euler flow, leading to the proposal of an alternative model in Oseen flow

DOI10.1098/rspa.2007.1870zbMath1187.76630OpenAlexW1998169208MaRDI QIDQ5438421

Ali Hatam, Edmund A. Chadwick

Publication date: 23 January 2008

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.2007.1870

zbMATH Keywords

Oseen flowEuler flowwing theory

Mathematics Subject Classification ID

Incompressible viscous fluids (76D99) General aerodynamics and subsonic flows (76G25) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Related Items (2)

A coupled far-field formulation for time-periodic numerical problems in fluid dynamics ⋮ A further note on the force discrepancy for wing theory in Euler flow

Cites Work

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• Low-Speed Aerodynamics
• The vortex line in steady, incompressible Oseen flow
• The far–field Oseen velocity expansion
• Motion and expansion of a viscous vortex ring. Part 1. A higher-order asymptotic formula for the velocity
• A slender–body theory in Oseen flow
• Vortex Dynamics
• A slender–wing theory in potential flow
• On the flow near the trailing edge of a flat plate II
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate

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