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Sensitivity and optimization of composite structures using MSC/NASTRANDesign sensitivity analysis for composites will soon be available in MSC/NASTRAN. The design variables for composites can be lamina thicknesses, orientation angles, material properties or a combination of all three. With the increasing use of composites in aerospace and automotive industries, this general capability can be used in its own right for carrying out sensitivity analysis of complicated real-life structures. As part of a research effort, the sensitivity analysis was coupled with a general purpose optimizer. This preliminary version of the optimizer is capable of dealing with minimum weight structural design with a rather general design variable linking capability at the element level or system level. Only sizing type of design variables (i.e., lamina thicknesses) can be handled by the optimizer. Test cases were run and validated by comparison with independent finite element packages. The linking of design sensitivity capability for composites in MSC/NASTRAN with an optimizer would give designers a powerful automated tool to carry out practical opitmization design of real-life complicated composite structures.
Document ID
19870009432
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Nagendra, Gopal K.
(MacNeal-Schwendler Corp. Los Angeles, CA, United States)
Fleury, Claude
(California Univ. Los Angeles, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1987
Publication Information
Publication: NASA. Langley Research Center Sensitivity Analysis in Engineering
Subject Category
Structural Mechanics
Accession Number
87N18865
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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