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Implicit approximate-factorization schemes for the efficient solution of steady transonic flow problemsImplicit approximate-factorization algorithms (AF) are developed for the solution of steady-state transonic flow problems. The performance of the AF solution method is evaluated relative to that of the standard solution method for transonic flow problems, successive line over-relaxation (SLOR). Both methods are applied to the solution of the nonlinear, two-dimensional transonic small-disturbance equation. Results indicate that the AF method requires substantially less computer time than SLOR to solve the nonlinear finite-difference matrix equation for a transonic flow field. This increase in computational efficiency is achieved with no appreciable increase in computer storage or coding complexity.
Document ID
19770011867
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ballhaus, W. F.
(NASA Ames Research Center Moffett Field, CA, United States)
Jameson, A.
(N. Y. Univ. Moffett Field, CA, United States)
Albert, J.
(NASA Ames Research Center)
Date Acquired
September 3, 2013
Publication Date
January 1, 1977
Subject Category
Numerical Analysis
Report/Patent Number
A-6898
NASA-TM-X-73202
Report Number: A-6898
Report Number: NASA-TM-X-73202
Accession Number
77N18811
Funding Number(s)
PROJECT: RTOP 505-06-12-05
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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