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Geometry Modeling for Unstructured Mesh AdaptationThe quantification and control of discretization error is critical to obtaining reliable simulation results. Adaptive mesh techniques have the potential to automate discretization error control, but have made limited impact on production analysis workflow. Recent progress has matured a number of independent implementations of flow solvers, error estimation methods, and anisotropic mesh adaptation mechanics. However, the poor integration of initial mesh generation and adaptive mesh mechanics to typical sources of geometry has hindered adoption of adaptive mesh techniques, where these geometries are often created in Mechanical Computer- Aided Design (MCAD) systems. The difficulty of this coupling is compounded by two factors: the inherent complexity of the model (e.g., large range of scales, bodies in proximity, details not required for analysis) and unintended geometry construction artifacts (e.g., translation, uneven parameterization, degeneracy, self-intersection, sliver faces, gaps, large tolerances be- tween topological elements, local high curvature to enforce continuity). Manual preparation of geometry is commonly employed to enable fixed-grid and adaptive-grid workflows by reducing the severity and negative impacts of these construction artifacts, but manual process interaction inhibits workflow automation. Techniques to permit the use of complex geometry models and reduce the impact of geometry construction artifacts on unstructured grid workflows are models from the AIAA Sonic Boom and High Lift Prediction are shown to demonstrate the utility of the current approach.
Document ID
20200002617
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Park, Michael A.
(NASA Langley Research Center Hampton, VA, United States)
Kleb, Bill
(NASA Langley Research Center Hampton, VA, United States)
Jones, William T.
(NASA Langley Research Center Hampton, VA, United States)
Krakos, Joshua A.
(Boeing Company Saint Louis, MO, United States)
Michal, Todd
(Boeing Company Saint Louis, MO, United States)
Loseille, Adrien
(Institut National de Recherche d'Informatique et d'Automatique Le Chesnay, France)
Haimes, Robert
(Massachusetts Institute of Technology (MIT) Cambridge, MA, United States)
Dannenhoffer, John F., III
(Syracuse Univ. Syracuse, NY, United States)
Date Acquired
April 17, 2020
Publication Date
June 17, 2019
Subject Category
Aerodynamics
Mathematical And Computer Sciences (General)
Report/Patent Number
NF1676L-31515
Report Number: NF1676L-31515
Meeting Information
Meeting: 2019 AIAA Aviation
Location: Dallas, TX
Country: United States
Start Date: June 17, 2019
End Date: June 21, 2019
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 109492.02.07.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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