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A New Formulation for Hybrid LES-RANS ComputationsIdeally, a hybrid LES-RANS computation would employ LES only where necessary to make up for the failure of the RANS model to provide sufficient accuracy or to provide time-dependent information. Current approaches are fairly restrictive in the placement of LES and RANS regions; an LES-RANS transition in a boundary layer, for example, yields an unphysical log-layer shift. A hybrid computation is formulated here to allow greater control over the placement of LES and RANS regions and the transitions between them. The concept of model invariance is introduced, which provides a basis for interpreting hybrid results within an LES-RANS transition zone. Consequences of imposing model invariance include the addition of terms to the governing equations that compensate for unphysical gradients created as the model changes between RANS and LES. Computational results illustrate the increased accuracy of the approach and its insensitivity to the location of the transition and to the blending function employed.
Document ID
20140000464
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Woodruff, Stephen L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
January 29, 2014
Publication Date
June 24, 2013
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-15665
Report Number: NF1676L-15665
Meeting Information
Meeting: AIAA Fluid Dynamics Conference and Exhibit
Location: San Diego, CA
Country: United States
Start Date: June 24, 2013
End Date: June 27, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 699959.02.08.07.11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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