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Turbulence modeling for impinging jet flowsThe objective of the present work is to improve the accuracy of the k-epsilon turbulence model for flows involving one or more jets impinging on a plate in a crossflow which generate a horseshoe vortex. The k-epsilon model is modified by adding source terms to the epsilon equation, which enables it to more accurately predict the shear stress in flows subject to streamline curvature and vortex stretching (or lateral divergence). Calculations with the modified model predict the ground vortex core to be about 15 percent upstream of its experimental location. This is a significant improvement over the standard model which yields higher errors for calculation of the vortex-core location.
Document ID
19920062903
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Childs, Robert E.
(NASA Ames Research Center Moffett Field, CA, United States)
Rodman, Laura C.
(Nielsen Engineering & Research, Inc. Mountain View, CA, United States)
Bradshaw, Peter
(NASA Ames Research Center Moffett Field, CA, United States)
Bott, Donald M.
(NASA Ames Research Center Moffett Field, CA, United States)
Shoemaker, William C.
(Stanford University CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-2672
Report Number: AIAA PAPER 92-2672
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Palo Alto, CA
Country: United States
Start Date: June 22, 1992
End Date: June 24, 1992
Accession Number
92A45527
Funding Number(s)
CONTRACT_GRANT: F33615-90-C-3002
Distribution Limits
Public
Copyright
Other

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