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A nonlinear hybrid vortex method for wings at large angle of attack - MaRDI portal

A nonlinear hybrid vortex method for wings at large angle of attack

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DOI10.2514/3.8396zbMath0538.76010OpenAlexW2167955920MaRDI QIDQ3325266

Thomas F. Tureaud, Lichuan Chu, Osama A. Kandil

Publication date: 1984

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

Full work available at URL: https://doi.org/10.2514/3.8396

zbMATH Keywords

closed-form expressions Biot-Savart law near field far field aerodynamic loads large angles of attack concentrated vortex lines induced velocity low aspect ratio wings panels with linear vorticity distribution quadratic doublet distribution rectangular wings in steady and unsteady flows steady and unsteady nonlinear hybrid vortex method

Mathematics Subject Classification ID

Vortex flows for incompressible inviscid fluids (76B47) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10) Basic methods in fluid mechanics (76M99)

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