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Simple numerical method for predicting steady compressible flowsThe present numerical method for the solution of the isenthalpic form of the governing equations for compressible viscous and inviscid flows has its basis in the concept of flux vector splitting in its implicit form, and has been tested in the cases of several difficult viscous and inviscid configurations. An acceleration of time-marching to steady state is accomplished by implementing a multigrid procedure which effectively increases the convergence rate. The steady state results obtained are largely of good quality, and required only short computational times.
Document ID
19870061806
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Von Lavante, E.
(Old Dominion University Norfolk, VA, United States)
Melson, N. Duane
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 87-2409
Accession Number
87A49080
Funding Number(s)
CONTRACT_GRANT: NAG1-633
Distribution Limits
Public
Copyright
Other

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