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Upwind relaxation methods for the Navier-Stokes equations using inner iterationsA supersonic and subsonic test problem is solved using an upwind line relaxation algorithm for the Navier-Stokes equations which employs inner iterations. In the supersonic test case, the inner iteration method was found to require only about 65 percent of the CPU time which was required by the most efficient line relaxation method without inner iterations. In the subsonic test case, poor matrix conditioning resulted in less efficiency than line relaxation methods employing a more conventional CPU-saving strategy.
Document ID
19890054430
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Taylor, Arthur C., III
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Hg, Wing-Fai
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Walters, Robert W.
(Virginia Polytechnic Institute and State University Blacksburg, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 89-1954
Meeting Information
Meeting: AIAA Computational Fluid Dynamics Conference
Location: Buffalo, NY
Country: United States
Start Date: June 13, 1989
End Date: June 15, 1989
Accession Number
89A41801
Distribution Limits
Public
Copyright
Other

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