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ATLAS, an integrated structural analysis and design system. Volume 6: Design module theoryThe automated design theory underlying the operation of the ATLAS Design Module is decribed. The methods, applications and limitations associated with the fully stressed design, the thermal fully stressed design and a regional optimization algorithm are presented. A discussion of the convergence characteristics of the fully stressed design is also included. Derivations and concepts specific to the ATLAS design theory are shown, while conventional terminology and established methods are identified by references.
Document ID
19790023454
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Backman, B. F.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1979
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-159046
D6-25400-0006-VOL-6
Report Number: NASA-CR-159046
Report Number: D6-25400-0006-VOL-6
Accession Number
79N31625
Funding Number(s)
CONTRACT_GRANT: DAAG46-75-C-0072
CONTRACT_GRANT: NAS1-12911
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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