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NASA NTRS · 19890057889

Studies of vortex flow aerodynamics using CFD flow visualizations

Abstract

Navier-Stokes computations of three-dimensional vortical flows over a round-edged double-delta wing and a tangent-ogive forebody are performed using an implicit upwind finite-difference scheme. Computed particle traces are compared with experimental oil-flow streaks.

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BibTeXRIS

Hsu, C.-H., Hartwich, P.-M., Liu, C. H.. 1989-08-01. Studies of vortex flow aerodynamics using CFD flow visualizations. https://ntrs.nasa.gov/citations/19890057889

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