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Boundary Representation Tolerance Impacts on Mesh Generation and AdaptationThe control of discretization error is critical to obtaining reliable simulation results. Re-cent progress has matured anisotropic mesh adaptation, which automates discretization error control for complex geometries. However, the meshing process can fail when geometric model Boundary REPresentation (BREP) tolerances are larger than boundary layer surface nor-mal and tangential spacing requirements. Geometry sources are often created in Mechanical Computer-Aided Design (MCAD) systems, which are designed to produce models for manufacturing and not the stricter requirements of viscous flow analysis. BREP tolerances are strained by three factors: the inherent complexity of the model (e.g., large range of scales and complex topology), the numerical difficulties arising from surface/surface intersections, and the omission of crucial data during export and translation. Manual preparation of geometry is commonly employed to enable expert-guided mesh generation, which severely inhibits work-flow automation. Accommodation of loose BREP tolerances is required for automated mesh processes, because barrier issues may not be detected until well into the solution process. To raise awareness of this class of geometry issues and their impact on simulation, a survey of these barrier issues is presented with example mitigation techniques. This awareness may also impact geometry creation workflows to prevent the introduction of these artifacts.
Document ID
20210016359
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Michael A Park
(Langley Research Center Hampton, Virginia, United States)
Robert Haimes
(Massachusetts Institute of Technology Cambridge, Massachusetts, United States)
Nicholas J Wyman
(Cadence Design Systems (United States) San Jose, California, United States)
Patrick A Baker
(Cadence Design Systems (United States) San Jose, California, United States)
Adrien Loseille
(French Institute for Research in Computer Science and Automation Le Chesnay, France)
Todd Michal
(Boeing (United States) Chicago, Illinois, United States)
Joshua A Krakos
(Boeing (United States) Chicago, Illinois, United States)
Date Acquired
May 26, 2021
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 2021 AIAA Aviation Forum
Location: Virtual
Country: US
Start Date: August 2, 2021
End Date: August 6, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 110076.02.07.03.31
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
CAD
BREP
Tolerance
CFD
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