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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 such as line generation for general unstructured grids and optimization of the iterative solver. The efficiency of the new developments is assessed in a massively parallel environment. The assessments are conducted using a baseline method and the recent hierarchical adaptive nonlinear iteration method framework. Three benchmark turbulent flows, namely, a subsonic separated flow around a three-dimensional hemisphere cylinder configuration, a transonic flow around the ONERA M6 wing, and a supersonic flow through a square duct are considered.
Document ID
20210011392
Acquisition Source
Langley Research Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Mohagna J Pandya
(Langley Research Center Hampton, Virginia, United States)
Dennis C Jaspersen
(Ames Research Center Mountain View, California, United States)
Boris Diskin
(National Institute of Aerospace Hampton, Virginia, United States)
James L Thomas
(Langley Research Center Hampton, Virginia, United States)
Neal T Frink
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
March 16, 2021
Publication Date
June 21, 2021
Publication Information
Publication: AIAA Journal
Publisher: AIAA
Volume: 59
Issue: 8
Issue Publication Date: August 1, 2021
ISSN: 0001-1452
e-ISSN: 1533-385X
Subject Category
Aerodynamics
Funding Number(s)
WBS: 109492.02.07.09.01
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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