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DESAP 2: A structural design program with stress and buckling constraints. Volume 1: Theoretical and user's manualDESAP 2 is described as a finite element program for computer-automated, minimum weight design of elastic structures with constraints on stresses (including local instability criteria) and buckling loads. No limits are placed on the number of load conditions for stress-constrained design, but only one of these load conditions can be chosen as the potential buckling load. A substantial portion of DESAP 2, particularly the analysis of the prebuckling state, is derived from the SOLID SAP finite element program. The stress-constrained design is based on the classical stress ratio method, which drives the design towards a fully stressed state. The constraints on the buckling load are handled by solving the appropriate optimality criterion by successive iterations. During each iteration, the element sizes determined by the stress ratio method are used as the minimum size constraints. The element subroutines are organized in a manner that permits the user to make additions and changes with a minimal programming effort. Consequently, DESAP 2 can readily be changed into a special-purpose program to handle the user's specific design requirements and failure criteria.
Document ID
19770011528
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kiusalaas, J.
(Pennsylvania State Univ. University Park, PA, United States)
Reddy, G. B.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1977
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
M-205
NASA-CR-2797
Report Number: M-205
Report Number: NASA-CR-2797
Accession Number
77N18472
Funding Number(s)
CONTRACT_GRANT: NCA-8-71/72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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