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Navier-Stokes computations of separated vortical flows past prolate spheroid at incidenceThe problem of steady incompressible viscous flow past prolate spheroids at incidence is formulated using the unsteady incompressible and compressible thin-layer Navier-Stokes equations. The two sets of Navier-Stokes equations are solved using a pseudotime stepping of the implicit flux-difference splitting scheme on a curvilinear grid, which is generated by a transfinite grid generator. The Baldwin and Lomax (1978) algebraic eddy-viscosity model is used to model the turbulent flow. The computational applications cover a 6:1 prolate spheroid at different angles of attack and Reynolds numbers. The results are compared with experimental data.
Document ID
19890038072
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wong, Tin-Chee
(Old Dominion Univ. Norfolk, VA, United States)
Kandil, Osama A.
(Old Dominion University Norfolk, VA, United States)
Liu, C. H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 89-0553
Accession Number
89A25443
Funding Number(s)
CONTRACT_GRANT: NAS1-18584
Distribution Limits
Public
Copyright
Other

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