NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Compression testing of graphite/epoxy composite materialsThree methods for compression testing coupons of filament-reinforced polymer-matrix composite materials are evaluated, to identify the sensitivity of the test techniques to laminate, specimen, and test parameters. A 'wedge-grip' compression fixture, a face-supported compression fixture, and an end-loaded coupon fixture are described. Specimens of 12.5-, 25-, and 50-mm widths, 8-, 16-, and 24-ply thicknesses, and of various fiber orientations were used to test the 'wedge-grip' compression fixture and the face-supported fixture; the end-loaded coupon fixture was tested using 16-ply specimens. Compressive strain-stress, strength, and modulus data obtained with the fixtures and evaluations showing the effects of all the test parameters are presented. One of the conclusions asserts that the 'wedge-grip' compression fixture provides good stress-strain data to failure for unidirectional and quasi-isotropic laminates.
Document ID
19810063400
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
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
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Composite Materials
Meeting Information
Meeting: Symposium on Test methods and design allowables for fibrous composites
Location: Dearborn, MI
Start Date: October 2, 1979
End Date: October 3, 1979
Accession Number
81A47804
Distribution Limits
Public
Copyright
Other

Available Downloads

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