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Applications of the multigrid method to calculations of transonic potential flow about wing fuselage combinationsThe multigrid method is applied to the calculation of transonic, potential flow fields about arbitrary three dimensional wing-body combinations. Numerical results for iterative convergence rate are in good agreement with those predicted by a local mode analysis and show substantial improvement over conventional relaxation algorithms.
Document ID
19810025342
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shmikovich, A. (Cornell Univ. New York, NY, United States)
Caughey, D. A. (Cornell Univ. New York, NY, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1981
Publication Information
Publication: NASA. Ames Research Center Multigrid Methods
Subject Category
Numerical Analysis
Accession Number
81N33885
Funding Number(s)
CONTRACT_GRANT: N00014-77-C-0033
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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