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Implementation of structural response sensitivity calculations in a large-scale finite-element analysis systemThe implementation includes a generalized method for specifying element cross-sectional dimensions as design variables that can be used in analytically calculating derivatives of output quantities from static stress, vibration, and buckling analyses for both membrane and bending elements. Limited sample results for static displacements and stresses are presented to indicate the advantages of analytically calclating response derivatives compared to finite difference methods. Continuing developments to implement these procedures into an enhanced version of the system are also discussed.
Document ID
19820015676
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Giles, G. L.
(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
March 1, 1982
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:83293
NASA-TM-83293
AIAA PAPER 82-0714
Report Number: NAS 1.15:83293
Report Number: NASA-TM-83293
Report Number: AIAA PAPER 82-0714
Meeting Information
Meeting: AIAA/ASME/ASCH/AHS Struct., Structural Dyn. and Mater. conf.,
Location: New Orleans, LA
Country: United States
Start Date: May 10, 1982
End Date: May 12, 1982
Accession Number
82N23550
Funding Number(s)
PROJECT: RTOP 505-33-63-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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