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The effect of turbulence models on the numerical prediction of the flowfield about a prolate spheroid at high angle of attackThe F3D thin-layer Navier-Stokes code presently used to numerically investigate the three-dimensional separated flow about a prolate spheroid at high incidence analyzes the effect of different turbulence models on the flowfield solution and the characteristics of the predicted flow. The Johnson-King (1984) model is applied in order to evaluate the importance of modeling nonequilibrium effects in predicting flow about a slender body at high incidence; the computations in question are for steady-state, fully turbulent flow. Insight is gained into the effects of turbulence models on flow characteristics, and model effects on the accurate prediction of highly separated and vortical flows about a slender body are demonstrated.
Document ID
19900058800
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gee, Ken
(NASA Ames Research Center Moffett Field, CA, United States)
Cummings, Russell M.
(NASA Ames Research Center Moffett Field, CA, United States)
Schiff, Lewis B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 90-3106
Report Number: AIAA PAPER 90-3106
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Portland, OR
Country: United States
Start Date: August 20, 1990
End Date: August 22, 1990
Accession Number
90A45855
Funding Number(s)
CONTRACT_GRANT: NCC2-564
Distribution Limits
Public
Copyright
Other

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