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Turbulence model effects on separated flow about a prolate spheroid

Authors :
Ken Gee
Russell M. Cummings
Lewis B. Schiff
Source :
AIAA Journal. 30:655-664
Publication Year :
1992
Publisher :
American Institute of Aeronautics and Astronautics (AIAA), 1992.

Abstract

The three-dimensional separated flow about a prolate spheroid at high incidence is numerically investigated using the F3D thin-layer Navier-Stokes code. The effect of different turbulence models on the flowfield solution and the characteristics of the predicted flow are analyzed. The models used in this study are the Baldvvin-Lomax algebraic model, the Baldvvin-Lomax model as modified for crossflow separation by Degani and Schiff, and a modified version of the Johnson-King model with and without the Degani-Schiff crossflow modifications applied. The Johnson-King model is applied to assess the importance of modeling nonequilibrium effects in predicting flow about a slender body at high incidence. The computations are made for steady-state, fully turbulent flow. The results are compared with experimental pressure data and with computational results obtained by Panaras and Steger, using the identical code and grid, but with their own modifications to the Baldwin-Lomax model. In addition, the computed solutions are analyzed using surface flow patterns, helicity density contours, and turbulent eddy-viscosity profiles. The results of this analysis provide insight into the effects of the turbulence models on flow characteristics and demonstrate the effect of the models on the accurate prediction of highly separated and vortical flows about a slender body.

Details

ISSN :
1533385X and 00011452
Volume :
30
Database :
OpenAIRE
Journal :
AIAA Journal
Accession number :
edsair.doi...........11842d92ccc4b70fe49d81ae2f8b4569