NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Reynolds-Stress Budgets in an Impinging Shock Wave/Boundary-Layer InteractionImplicit large-eddy simulation (ILES) of a shock wave/boundary-layer interaction (SBLI) was performed. Comparisons with experimental data showed a sensitivity of the current prediction to the modeling of the sidewalls. This was found to be common among various computational studies in the literature where periodic boundary conditions were used in the spanwise direction, as was the case in the present work. Thus, although the experiment was quasi-two-dimensional, the present simulation was determined to be two-dimensional. Quantities present in the exact equation of the Reynolds-stress transport, i.e., production, molecular diffusion, turbulent transport, pressure diffusion, pressure strain, dissipation, and turbulent mass flux were calculated. Reynolds-stress budgets were compared with past large-eddy simulation and direct numerical simulation datasets in the undisturbed portion of the turbulent boundary layer to validate the current approach. The budgets in SBLI showed the growth in the production term for the primary normal stress and energy transfer mechanism was led by the pressure strain term in the secondary normal stresses. The pressure diffusion term, commonly assumed as negligible by turbulence model developers, was shown to be small but non-zero in the normal stress budgets, however it played a key role in the primary shear stress budget.
Document ID
20180001494
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Vyas, Manan A.
(NASA Glenn Research Center Cleveland, OH, United States)
Yoder, Dennis A.
(NASA Glenn Research Center Cleveland, OH, United States)
Gaitonde, Datta V.
(Ohio State Univ. Columbus, OH, United States)
Date Acquired
February 27, 2018
Publication Date
January 8, 2018
Subject Category
Fluid Mechanics And Thermodynamics
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN50199
Meeting Information
Meeting: AIAA SciTech Forum
Location: Kissimmee, FL
Country: United States
Start Date: January 8, 2018
End Date: January 12, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 109492.02.03.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
shock wave/boundary-layer interactio
No Preview Available