NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
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
19910054131
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
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Structural Mechanics
Meeting Information
Meeting: ASME Annual Energy-Sources 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
91A38754
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available