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Transverse flexural tests as a tool for assessing damage to PMR-15 composites from isothermal aging in air at elevated temperaturesTo date, the effect of thermo-oxidative aging on unidirectional composite mechanical properties has been monitored by the measurement of interlaminar shear strength (ILSS) and either three or four point longitudinal flexural strength (LFS) of the composites being tested. Both results are affected by the fiber-to-matrix bonding, the former being dependent on the shear resistance of the interface and the latter on the degree of load sharing by the fibers through the fiber/matrix interface. Recently, fiber/matrix interfacial bond strengths have been monitored using a transverse flexural strength (TFS) test method. This test method was used to evaluate the effect of fiber surface treatment on the fiber/matrix bond. The interface bonding was varied in these tests using Hercules A-fibers with three-types of surfaces that produce bonds of poor, better, and good quality. The TFS was found not only to be sensitive to the bonding, but also to the aging time of unidirectional A-fiber/PMR-15 composites. This relationship reflects the mechanism by which the PMR-15 degrades during thermal aging.
Document ID
19930003549
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bowles, Kenneth J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1992
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-105848
E-7293
NAS 1.15:105848
Report Number: NASA-TM-105848
Report Number: E-7293
Report Number: NAS 1.15:105848
Accession Number
93N12737
Funding Number(s)
PROJECT: RTOP 510-01-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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