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Convergence acceleration for a three-dimensional Euler/Navier-Stokes zonal approachA fast diagonal algorithm is coupled with a zonal approach to solve the three-dimensional Euler/Navier-Stokes equations. Transonic viscous solutions are obtained on a 150,000 point mesh for a NACA 0012 wing. The new computational approach yields a speedup by as much as a factor of 40 over the standard Beam-Warming algorithm/zonal method originally coded. A three-order-of-magnitude drop in the L2-norm of the residual requires approximately 500 iterations, which takes about 45 min of CPU time on a Cray-XMP. The numerically computed solutions are in good agreement with experimental results. Effects on convergence rate owing to increasing the zonal boundary overlap regions, different stretching distributions in the viscous regions, and different CFL values are also explored.
Document ID
19850058783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Flores, J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-1495
Meeting Information
Meeting: Computational Fluid Dynamics Conference
Location: Cincinnati, OH
Start Date: July 15, 1985
End Date: July 17, 1985
Accession Number
85A40934
Distribution Limits
Public
Copyright
Other

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