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Combining analysis with optimization at Langley Research Center. An evolutionary processThe evolutionary process of combining analysis and optimization codes was traced with a view toward providing insight into the long term goal of developing the methodology for an integrated, multidisciplinary software system for the concurrent analysis and optimization of aerospace structures. It was traced along the lines of strength sizing, concurrent strength and flutter sizing, and general optimization to define a near-term goal for combining analysis and optimization codes. Development of a modular software system combining general-purpose, state-of-the-art, production-level analysis computer programs for structures, aerodynamics, and aeroelasticity with a state-of-the-art optimization program is required. Incorporation of a modular and flexible structural optimization software system into a state-of-the-art finite element analysis computer program will facilitate this effort. This effort results in the software system used that is controlled with a special-purpose language, communicates with a data management system, and is easily modified for adding new programs and capabilities. A 337 degree-of-freedom finite element model is used in verifying the accuracy of this system.
Document ID
19820016970
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rogers, J. L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1982
Subject Category
Computer Programming And Software
Report/Patent Number
NAS 1.15:84472
NASA-TM-84472
Report Number: NAS 1.15:84472
Report Number: NASA-TM-84472
Accession Number
82N24846
Funding Number(s)
PROJECT: RTOP 505-33-63-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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