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Alternative approximation concepts for space frame synthesisA structural synthesis methodology for the minimum mass design of 3-dimensionall frame-truss structures under multiple static loading conditions and subject to limits on displacements, rotations, stresses, local buckling, and element cross-sectional dimensions is presented. A variety of approximation concept options are employed to yield near optimum designs after no more than 10 structural analyses. Available options include: (A) formulation of the nonlinear mathematcal programming problem in either reciprocal section property (RSP) or cross-sectional dimension (CSD) space; (B) two alternative approximate problem structures in each design space; and (C) three distinct assumptions about element end-force variations. Fixed element, design element linking, and temporary constraint deletion features are also included. The solution of each approximate problem, in either its primal or dual form, is obtained using CONMIN, a feasible directions program. The frame-truss synthesis methodology is implemented in the COMPASS computer program and is used to solve a variety of problems. These problems were chosen so that, in addition to exercising the various approximation concepts options, the results could be compared with previously published work.
Document ID
19850012840
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lust, R. V.
(California Univ. Los Angeles, CA, United States)
Schmit, L. A.
(California Univ. Los Angeles, CA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:172526
NASA-CR-172526
Report Number: NAS 1.26:172526
Report Number: NASA-CR-172526
Accession Number
85N21150
Funding Number(s)
PROJECT: RTOP 506-53-53
CONTRACT_GRANT: NSG-1490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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