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Toward Adaptive Mixed-Element Unstructured Grids for Simulations of Viscous FlowsAccurate prediction of surface skin friction and heat transfer for viscous flow applications using computational fluid dynamics tools necessitates thin wall-normal elements in the boundary layer. A tetrahedral adaptation process is extended to incorporate the advancing front local reconnection procedure. Thin boundary-layer grids are adapted from the solution, which governs the boundary-layer grid parameters such as first cell height off the wall. The process enables grid-converged steady-state results from a CAD file. Results are presented across the speed range from low subsonic flow over an airfoil to high-speed flows over blunt bodies and a rocket.
Document ID
20240014149
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Gabriel Nastac
(Langley Research Center Hampton, United States)
Forrest Miller
(Langley Research Center Hampton, United States)
Dominic Schneider
(Langley Research Center Hampton, United States)
Kevin Jacobson
(Langley Research Center Hampton, United States)
William T Jones
(Langley Research Center Hampton, United States)
Matthew Opgenorth
(Sierra Space)
Date Acquired
November 7, 2024
Subject Category
Computer Programming and Software
Aerodynamics
Fluid Mechanics and Thermodynamics
Meeting Information
Meeting: AIAA SciTech Forum
Location: Orlando, FL
Country: US
Start Date: January 6, 2025
End Date: January 10, 2025
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.07.09.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
CFD
unstructured grids
hypersonic
chemically reacting flow
rocket engines
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