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Effects of method of loading and specimen configuration on compressive strength of graphite/epoxy composite materialsThree test schemes were examined for testing graphite/epoxy (Narmco T300/5208) composite material specimens to failure in compression, including an adaptation of the IITRI "wedge grip" compression fixture, a face-supported-compression fixture, and an end-loaded-coupon fixture. The effects of specimen size, specimen support arrangement and method of load transfer on compressive behavior of graphite/epoxy were investigated. Compressive stress strain, strength, and modulus data obtained with the three fixtures are presented with evaluations showing the effects of all test parameters, including fiber orientation. The IITRI fixture has the potential to provide good stress/strain data to failure for unidirectional and quasi-isotropic laminates. The face supported fixture was found to be the most desirable for testing + or - 45 s laminates.
Document ID
19800013919
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Clark, R. K.
(NASA Langley Research Center Hampton, VA, United States)
Lisagor, W. B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1980
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-81796
Report Number: NASA-TM-81796
Accession Number
80N22406
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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