NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Improved Convergence and Robustness of USM3D Solutions on Mixed-Element GridsSeveral improvements to the mixed-elementUSM3Ddiscretization and defect-correction schemes have been made. A new methodology for nonlinear iterations, called the Hierarchical Adaptive Nonlinear Iteration Method, has been developed and implemented. The Hierarchical Adaptive Nonlinear Iteration Method provides two additional hierarchies around a simple and approximate preconditioner of USM3D. The hierarchies are a matrix-free linear solver for the exact linearization of Reynolds-averaged Navier-Stokes equations and a nonlinear control of the solution update. Two variants of the Hierarchical Adaptive Nonlinear Iteration Method are assessed on four benchmark cases, namely, a zero-pressure-gradient flat plate, a bump-in-channel configuration, the NACA 0012 airfoil, and a NASA Common Research Model configuration. The new methodology provides a convergence acceleration factor of 1.4 to 13 over the preconditioner-alone method representing the baseline solver technology.
Document ID
20170007694
Acquisition Source
Langley Research Center
Document Type
Conference Paper
External Source(s)
Authors
Pandya, Mohagna J.
(NASA Langley Research Center Hampton, VA, United States)
Diskin, Boris
(National Inst. of Aerospace Hampton, VA, United States)
Thomas, James L.
(NASA Langley Research Center Hampton, VA, United States)
Frinks, Neal T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2017
Publication Date
June 20, 2016
Publication Information
Publication: AIAA Journal
Volume: 54
Issue: 9
ISSN: 0001-1452
e-ISSN: 1533-385X
Subject Category
Fluid Mechanics And Thermodynamics
Numerical Analysis
Report/Patent Number
AIAA Paper 2015-1747
NF1676L-23409
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 109492.02.07.01.01
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available