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Calculations of three-dimensional flows using the isenthalpic Euler equations with implicit flux-vector splittingA numerical method for solving the isenthalpic form of the Euler equations is developed. The method is based on the concept of flux vector splitting in its implicit form applied to a cell centered finite volume scheme. Approximate factorization is implemented in solving the implicit part of the governing equations. Time marching to a steady state solution requires short computational times due to the relative efficiency of the basic method. Computational times are further reduced by the implementation of multigrid. Results for several basic cases are shown.
Document ID
19880053535
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cannizzaro, Frank E.
(Old Dominion Univ. Norfolk, VA, United States)
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, 1988
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 88-2516
Meeting Information
Meeting: AIAA Applied Aerodynamics Conference
Location: Williamsburg, VA
Country: United States
Start Date: June 6, 1988
End Date: June 8, 1988
Accession Number
88A40762
Funding Number(s)
CONTRACT_GRANT: NAG1-633
Distribution Limits
Public
Copyright
Other

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