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F-ANG+: A 3-D Augmented-Stencil Face-Averaged Nodal-Gradient Cell-Centered Finite-Volume Method for Hypersonic Flows
Document ID
20210024787
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Jeffery A White (Langley Research Center Hampton, Virginia, United States)
Hiroaki Nishikawa (National Institute of Aerospace Hampton, Virginia, United States)
Matthew D. O’Connell (Langley Research Center Hampton, Virginia, United States)
Date Acquired
November 22, 2021
Subject Category
Aeronautics (General)
Meeting Information
Meeting: AIAA SciTech 2022
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 725017.02.07.01
CONTRACT_GRANT: NNL09AA00A
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
Weighted Least-Squares
Computational Fluid Dynamics
Hypersonic Flow
Gradient Limiters
Unstructured Grids
Adapted Grids

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