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A programing system for research and applications in structural optimizationThe flexibility necessary for such diverse utilizations is achieved by combining, in a modular manner, a state-of-the-art optimization program, a production level structural analysis program, and user supplied and problem dependent interface programs. Standard utility capabilities in modern computer operating systems are used to integrate these programs. This approach results in flexibility of the optimization procedure organization and versatility in the formulation of constraints and design variables. Features shown in numerical examples include: variability of structural layout and overall shape geometry, static strength and stiffness constraints, local buckling failure, and vibration constraints.
Document ID
19810024646
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Sobieszczanski-Sobieski, J.
(NASA Langley Research Center Hampton, VA, United States)
Rogers, J. L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-83191
Report Number: NASA-TM-83191
Accession Number
81N33189
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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