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Budget of Turbulent Kinetic Energy in a Shock Wave Boundary-Layer InteractionImplicit large-eddy simulation (ILES) of a shock wave/boundary-layer interaction (SBLI) was performed. Quantities present in the exact equation of the turbulent kinetic energy transport were accumulated and used to calculate terms like production, dissipation, molecular diffusion, and turbulent transport. The present results for a turbulent boundary layer were validated by comparison with direct numerical simulation data. It was found that a longer development domain was necessary for the boundary layer to reach an equilibrium state and a finer mesh resolution would improve the predictions. In spite of these findings, trends of the present budget match closely with that of the direct numerical simulation. Budgets for the SBLI region are presented at key axial stations. These budgets showed interesting dynamics as the incoming boundary layer transforms and the terms of the turbulent kinetic energy budget change behavior within the interaction region.
Document ID
20170000245
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Vyas, Manan A.
(NASA Glenn Research Center Cleveland, OH United States)
Waindim, Mbu
(Ohio State Univ. Columbus, OH, United States)
Gaitonde, Datta V.
(Ohio State Univ. Columbus, OH, United States)
Date Acquired
January 4, 2017
Publication Date
June 13, 2016
Subject Category
Aerodynamics
Fluid Mechanics And Thermodynamics
Report/Patent Number
GRC-E-DAA-TN32149
Report Number: GRC-E-DAA-TN32149
Meeting Information
Meeting: AIAA Aviation 2016
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 109492.02.03.01.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
shock wave/boundary-layer interaction
large-eddy simulation
turbulence modeling
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