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Observations on computational methodologies for use in large-scale, gradient-based, multidisciplinary designVarious computational methodologies relevant to large-scale multidisciplinary gradient-based optimization for engineering systems design problems are examined with emphasis on the situation where one or more discipline responses required by the optimized design procedure involve the solution of a system of nonlinear partial differential equations. Such situations occur when advanced CFD codes are applied in a multidisciplinary procedure for optimizing an aerospace vehicle design. A technique for satisfying the multidisciplinary design requirements for gradient information is presented. The technique is shown to permit some leeway in the CFD algorithms which can be used, an expansion to 3D problems, and straightforward use of other computational methodologies.
Document ID
19930036354
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Newman, P. A.
(NASA Langley Research Center Hampton, VA, United States)
Hou, G. J.-W.
(Old Dominion Univ. Norfolk, VA, United States)
Jones, J. E.
(U.S. Army, Aviation Systems Command, Hampton VA, United States)
Taylor, A. C., III
(NASA Langley Research Center Hampton, VA, United States)
Korivi, V. M.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Publication Information
Publication: In: AIAA(USAF)NASA/OAI Symposium on Multidisciplinary Analysis and Optimization, 4th, Cleveland, OH, Sept. 21-23, 1992, Technical Papers. Pt. 1 (A93-20301 06-66)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Numerical Analysis
Report/Patent Number
AIAA PAPER 92-4753
Accession Number
93A20351
Distribution Limits
Public
Copyright
Other

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