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Economical Third-Order Methods for Accurate Surface Heating Predictions on Simplex Element MeshesA node-centered edge-based finite volume discretization of the compressible Navier-Stokes equations is presented with the heat flux reformulated as a first order system. A dissipation vector is derived for the reformulated system, such that the heat flux can be upgraded to O(h^3) on
simplex element meshes in the same fashion as the inviscid fluxes. The method of manufactured solutions is used to demonstrate this uniform order property in heat flux. This new system is shown to efficiently produce accurate surface heating predictions on hypersonic hemisphere
flow using an anisotropic simplex element mesh, achieving O(h^3) accuracy at relatively low computational cost compared to similar methods.
Document ID
20220017904
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Kyle B Thompson
(Langley Research Center Hampton, Virginia, United States)
Hiroaki Nishikawa
(National Institute of Aerospace Hampton, Virginia, United States)
Emmett Padway
(National Institute of Aerospace Hampton, Virginia, United States)
Matthew D O'Connell
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
November 28, 2022
Subject Category
Numerical Analysis
Fluid Mechanics And Thermodynamics
Aerodynamics
Meeting Information
Meeting: AIAA SciTech Forum
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 335803.04.22.23.10.01
CONTRACT_GRANT: USARO-W911NF-19-1-0429
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Professional Review
Keywords
Computational Fluid Dynamics
Hyperbolic
HyperSolve
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