NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
New approach to the solution of large, full matrix equationsA new approach to the solution of matrix equations resulting from integral equations is presented and applied to the solution of two-dimensional Neumann problems describing the inviscid, incompressible flow past an airfoil. The problem is reformulated in terms of a preselected set of mode functions giving an equivalent matrix equation to be solved for the mode-function expansion coefficients. Because of the inherent smoothness of the original problem, the coefficient problem can be solved approximately without significantly affecting the accuracy of the final solution. Very promising two-dimensional results are obtained and the extension of the method to three-dimensional problems is investigated. On the basis of these results it is shown that the computing time for the matrix solution for a large three-dimensional panel method calculation could be reduced by an order of magnitude compared with that required for a direct solution.
Document ID
19810037148
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Clark, R. W.
(Douglas Aircraft Co. Long Beach, Calif., United States)
James, R. M.
(Boeing Co. Seattle, Wash., United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1981
Publication Information
Publication: AIAA Journal
Volume: 19
Subject Category
Aerodynamics
Accession Number
81A21552
Funding Number(s)
CONTRACT_GRANT: NAS1-14892
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available