NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Modeling Shock-Separated Flow with the Active Model SplitThe predictive accuracy of typical hybrid RANS/LES models is limited by several shortcomings, such as modeled-stress depletion and a dependence on scalar grid measures. The "active model-split" (AMS) hybrid RANS/LES model was developed by Haering, Oliver, and Moser to address these shortcomings. In this model, the mean and fluctuating portions of the stress are modeled separately; this allows for a consistent treatment of the mean flow even in the presence of resolved fluctuations. Part of this hybrid model is an active forcing, which generates turbulent fluctuations in regions that support LES-type fluctuations. In this presentation, some recent results are shown using the active model-split for shock-separated flows. The effects of the active forcing are examined, including the effects on anisotropy and acoustics. Superior predictive accuracy over RANS is shown for some quantities of interest, such as the shock location.
Document ID
20210024231
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
C Pederson
(Langley Research Center Hampton, Virginia, United States)
T Oliver
(The University of Texas at Austin Austin, Texas, United States)
R D Moser
(The University of Texas at Austin Austin, Texas, United States)
Date Acquired
November 10, 2021
Subject Category
Aerodynamics
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 74th Annual Meeting of the American Physical Society Division of Fluid Dynamics
Location: Phoenix, AZ
Country: US
Start Date: November 21, 2021
End Date: November 23, 2021
Sponsors: American Physical Society
Funding Number(s)
OTHER: NSF Grant No. 1610403
CONTRACT_GRANT: SPEC5732
CONTRACT_GRANT: NNN12AA01C
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
RANS
LES
hybrid RANS/LES
CFD
SBLI
No Preview Available