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Static and dynamic structural-sensitivity derivative calculations in the finite-element-based Engineering Analysis Language (EAL) systemThe implementation of static and dynamic structural-sensitivity derivative calculations in a general purpose, finite-element computer program denoted the Engineering Analysis Language (EAL) System is described. Derivatives are calculated with respect to structural parameters, specifically, member sectional properties including thicknesses, cross-sectional areas, and moments of inertia. Derivatives are obtained for displacements, stresses, vibration frequencies and mode shapes, and buckling loads and mode shapes. Three methods for calculating derivatives are implemented (analytical, semianalytical, and finite differences), and comparisons of computer time and accuracy are made. Results are presented for four examples: a swept wing, a box beam, a stiffened cylinder with a cutout, and a space radiometer-antenna truss.
Document ID
19840012812
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Camarda, C. J.
(NASA Langley Research Center Hampton, VA, United States)
Adelman, H. M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1984
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-85743
NAS 1.15:85743
L-15659
Report Number: NASA-TM-85743
Report Number: NAS 1.15:85743
Report Number: L-15659
Accession Number
84N20880
Funding Number(s)
PROJECT: RTOP 506-53-53-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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