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Accelerated finite-volume calculation of transonic potential flowsA fully conservative finite-volume algorithm is used to calculate transonic potential flows past isolated airfoils and through two-dimensional channels. The difference equations are solved by a multigrid technique which uses an alternating direction implicit method as a smoothing algorithm. The finite-volume formulation provides a framework within which to treat flows past complicated geometries, while the multigrid/alternating direction scheme provides rapid convergence of the solution to very small residuals.
Document ID
19820029068
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Authors
Jameson, A.
(New York Univ. New York, NY, United States)
Pelz, R.
(New York University New York, NY, United States)
Caughey, D. A.
(Cornell University Ithaca, NY, United States)
Jou, W. H.
(Flow Research, Inc. Kent, WA, United States)
Steinhoff, J.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Subject Category
Aerodynamics
Accession Number
82A12603
Funding Number(s)
CONTRACT_GRANT: EY-76-C-02-3077
CONTRACT_GRANT: N00014-78-C-0079
CONTRACT_GRANT: NGR-33-016-201
CONTRACT_GRANT: NSG-1579
CONTRACT_GRANT: N00014-77-C-0032
CONTRACT_GRANT: N00014-77-C-0033
Distribution Limits
Public
Copyright
Other

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