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Composite laminate tailoring with probabilistic constraints and loadsA reliability-based structural synthesis procedure was developed to tailor laminates to meet reliability-based (ply) strength requirements and achieve desirable laminate responses. The main thrust is to demonstrate how to integrate the optimization technique in the composite laminate tailoring process to meet reliability design requirements. The question of reliability arises in fiber composite analysis and design because of the inherent scatter that is observed in the constituent (fiber and matrix) material properties during experimentation. Symmetric and asymmetric composite laminates subject to mechanical loadings are considered as application examples. These application examples illustrate the effectiveness and ease with which reliability considerations can be integrated in the design optimization model for composite laminate tailoring.
Document ID
19900010822
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Thanedar, P. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-102515
E-5182
NAS 1.15:102515
Report Number: NASA-TM-102515
Report Number: E-5182
Report Number: NAS 1.15:102515
Meeting Information
Meeting: Energy Technology Conference and Exhibition
Location: New Orleans, LA
Country: United States
Start Date: January 14, 1990
End Date: January 18, 1990
Sponsors: ASME
Accession Number
90N20138
Funding Number(s)
PROJECT: RTOP 505-63-1B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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