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Accuracy, Scalability, and Efficiency of Mixed-Element USM3D for Benchmark Three-Dimensional FlowsThe unstructured, mixed-element, cell-centered, finite-volume flow solver USM3D is enhanced with new capabilities including parallelization, line generation for general unstructured grids, improved discretization scheme, and optimized iterative solver. The paper reports on the new developments to the flow solver and assesses the accuracy, scalability, and efficiency. The USM3D assessments are conducted using a baseline method and the recent hierarchical adaptive nonlinear iteration method framework. Two benchmark turbulent flows, namely, a subsonic separated flow around a three-dimensional hemisphere-cylinder configuration and a transonic flow around the ONERA M6 wing are considered.


Document ID
20200002362
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Pandya, Mohagna J.
(NASA Langley Research Center Hampton, VA, United States)
Jespersen, Dennis C.
(NASA Ames Research Center Moffett Field, CA, United States)
Diskin, Boris
(National Inst. of Aerospace Hampton, VA, United States)
Thomas, James L.
(NASA Langley Research Center Hampton, VA, United States)
Frink, Neal T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 14, 2020
Publication Date
January 7, 2019
Subject Category
Mathematical And Computer Sciences (General)
Report/Patent Number
NF1676L-30141
Meeting Information
Meeting: 2019 AIAA SciTech Forum and Exposition
Location: San Diego, CA
Country: United States
Start Date: January 7, 2019
End Date: January 11, 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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