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Entropy Stable Wall Boundary Conditions for the Compressible Navier-Stokes EquationsNon-linear entropy stability and a summation-by-parts framework are used to derive entropy stable wall boundary conditions for the compressible Navier-Stokes equations. A semi-discrete entropy estimate for the entire domain is achieved when the new boundary conditions are coupled with an entropy stable discrete interior operator. The data at the boundary are weakly imposed using a penalty flux approach and a simultaneous-approximation-term penalty technique. Although discontinuous spectral collocation operators are used herein for the purpose of demonstrating their robustness and efficacy, the new boundary conditions are compatible with any diagonal norm summation-by-parts spatial operator, including finite element, finite volume, finite difference, discontinuous Galerkin, and flux reconstruction schemes. The proposed boundary treatment is tested for three-dimensional subsonic and supersonic flows. The numerical computations corroborate the non-linear stability (entropy stability) and accuracy of the boundary conditions.
Document ID
20140010085
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Parsani, Matteo
(Oak Ridge Associated Universities, Inc. Hampton, VA, United States)
Carpenter, Mark H.
(NASA Langley Research Center Hampton, VA, United States)
Nielsen, Eric J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
July 24, 2014
Publication Date
June 1, 2014
Subject Category
Aeronautics (General)
Report/Patent Number
NF1676L-19188
NASA/TM-2014-218282
L-20431
Funding Number(s)
WBS: WBS 794072.02.07.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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