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Using Adaptive Mesh Refinement to Study Grid Resolution Effects for Shock/Boundary-Layer InteractionsAdaptive Mesh Refinement (AMR) promises a much more computationally efficient meansto obtain a discrete approximation to a continuous boundary value problem of a specifiedaccuracy than classic isotropic grid refinement. The AMR capability of OVERFLOW is utilizedto provide estimates of the exact analytical solutions to problems of interest to turbulencemodeling. Predictions of surface pressure and skin friction, essentially the state of stress at thesurface, shows little difference with grids believed to be "grid resolved." Velocity profiles, on theother hand, show marked differences in flows with shocks. The AMR method, as implementedin OVERFLOW2.2k, appears to provide the ability to produce arbitrarily accurate solutionsat a predictable cost much smaller than classic uniform mesh refinement.
Document ID
20190026978
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Olsen, Michael E.
(NASA Ames Research Center Moffett Field, CA, United States)
Lillard, Randolph P.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
July 3, 2019
Publication Date
June 25, 2018
Subject Category
Aerodynamics
Report/Patent Number
ARC-E-DAA-TN58039
Report Number: ARC-E-DAA-TN58039
Meeting Information
Meeting: 2018 AIAA AVIATION Forum
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Adaptive Mesh Refinement
CFD
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