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Re-evaluation of an Optimized Second Order Backward Difference (BDF2OPT) Scheme for Unsteady Flow ApplicationsRecent experience in the application of an optimized, second-order, backward-difference (BDF2OPT) temporal scheme is reported. The primary focus of the work is on obtaining accurate solutions of the unsteady Reynolds-averaged Navier-Stokes equations over long periods of time for aerodynamic problems of interest. The baseline flow solver under consideration uses a particular BDF2OPT temporal scheme with a dual-time-stepping algorithm for advancing the flow solutions in time. Numerical difficulties are encountered with this scheme when the flow code is run for a large number of time steps, a behavior not seen with the standard second-order, backward-difference, temporal scheme. Based on a stability analysis, slight modifications to the BDF2OPT scheme are suggested. The performance and accuracy of this modified scheme is assessed by comparing the computational results with other numerical schemes and experimental data.
Document ID
20100002944
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Vatsa, Veer N.
(NASA Langley Research Center Hampton, VA, United States)
Carpenter, Mark H.
(NASA Langley Research Center Hampton, VA, United States)
Lockard, David P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
December 18, 2009
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2010-0122
LF99-8943
Report Number: AIAA Paper 2010-0122
Report Number: LF99-8943
Meeting Information
Meeting: 48th AIAA Aerospace Sciences Meeting
Location: Orlando, FL
Country: United States
Start Date: January 4, 2010
End Date: January 7, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.08.07.18.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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