Simulation of leading-edge vortex flows

descriptionPublicationkeyboard_double_arrow_right Article 01 Jan 1990 English Publisher:Springer Science and Business Media LLCJournal:Theoretical and Computational Fluid Dynamics, volume 1, pages 379-390 (issn: 0935-4964, eissn: 1432-2250,

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Authors: Hsu, C.-H.; Liu, C. H.;

doi: 10.1007/bf00271797

Simulation of leading-edge vortex flows

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Abstract

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Related Organizations

Langley Research Center
United States
Hampton University
United States
National Aeronautics and Space Administration
United States

Keywords

incompressible Navier-Stokes equations, Transonic flows, implicit upwind-relaxation finite-difference algorithm, three round-edged low-aspect-ratio wings, low-speed, three-dimensional, laminar, leading- edge vortex flows, General aerodynamics and subsonic flows, Finite difference methods applied to problems in fluid mechanics

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