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Observations on computational methodologies for use in large-scale, gradient-based, multidisciplinary design incorporating advanced CFD codesHow a combination of various computational methodologies could reduce the enormous computational costs envisioned in using advanced CFD codes in gradient based optimized multidisciplinary design (MdD) procedures is briefly outlined. Implications of these MdD requirements upon advanced CFD codes are somewhat different than those imposed by a single discipline design. A means for satisfying these MdD requirements for gradient information is presented which appear to permit: (1) some leeway in the CFD solution algorithms which can be used; (2) an extension to 3-D problems; and (3) straightforward use of other computational methodologies. Many of these observations have previously been discussed as possibilities for doing parts of the problem more efficiently; the contribution here is observing how they fit together in a mutually beneficial way.
Document ID
19920015713
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Newman, P. A.
(NASA Langley Research Center Hampton, VA, United States)
Hou, G. J.-W.
(NASA Langley Research Center Hampton, VA, United States)
Jones, H. E.
(NASA Langley Research Center 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
September 6, 2013
Publication Date
February 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-104206
NAS 1.15:104206
AVSCOM-TR-92-B-007
Report Number: NASA-TM-104206
Report Number: NAS 1.15:104206
Report Number: AVSCOM-TR-92-B-007
Accession Number
92N24956
Funding Number(s)
PROJECT: RTOP 505-59-53-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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