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A coarse-grid correction/nonlinear relaxation algorithm for the three-dimensional, compressible Navier-Stokes equationsA combined coarse-grid correction/upwind relaxation strategy to provide rapid convergence for 3D high-speed viscous flowfields is discussed an evaluated. The construction and analysis of a simple two-grid acceleration procedure based on 'hyperbolic' multigrid concepts is presented. Numerical simulations of a 2D compression-corner flowfield, a 3D crossing shock/turbulent boundary layer interaction, and a 3D scramjet inlet flowfield are presented to illustrate the benefits of the approach. Results indicate that the procedure generally converges two or more times faster than the baseline algorithm.
Document ID
19930061016
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Edwards, Jack R.
(NASA Headquarters Washington, DC United States)
Mcrae, D. S.
(North Carolina State Univ. Raleigh, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Computational Fluid Dynamics Conference, 11th, Orlando, FL, July 6-9, 1993, Technical Papers. Pt. 1 (A93-44994 18-34)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-3317
Report Number: AIAA PAPER 93-3317
Accession Number
93A45013
Funding Number(s)
CONTRACT_GRANT: NAGW-1072
Distribution Limits
Public
Copyright
Other

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