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Environmental effects and viscoelastic behavior of laminated graphite/epoxy composites

Authors :
Dillard, D. A
Morris, D. H
Brinson, H. F
Publication Year :
1983
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1983.

Abstract

Primarily because of the polymeric matrix, graphite/epoxy composites are viscoelastic materials which exhibit creep and delayed failures. Guided by the time-temperature superposition principle, the authors are developing accelerated characterization techniques to predict the long term compliance behavior and creep rupture strength of composite materials based on short term tests at elevated temperatures. The effect of a post-cure cycle on the compliance and creep rupture strength of composite materials is discussed. The Zhurkov type failure law is applied to experimental creep rupture data of a typical laminate and is shown to correlate the data. A beneficial mechanical strengthening effect is described which significantly affects the failure strengths of specimens which have been under creep loading for a period of time. This aging effect is reversible if the specimen is allowed to recover before being loaded to failure. Other environmental aspects of composite materials are also reviewed.

Subjects

Subjects :
Composite Materials

Details

Language :
English
Database :
NASA Technical Reports
Notes :
NCC2-71
Publication Type :
Report
Accession number :
edsnas.19840040727
Document Type :
Report