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Compression behavior of unidirectional fibrous compositeThe longitudinal compression behavior of unidirectional fiber composites is investigated using a modified Celanese test method with thick and thin test specimens. The test data obtained are interpreted using the stress/strain curves from back-to-back strain gages, examination of fracture surfaces by scanning electron microscope, and predictive equations for distinct failure modes including fiber compression failure, Euler buckling, delamination, and flexure. The results show that the longitudinal compression fracture is induced by a combination of delamination, flexure, and fiber tier breaks. No distinct fracture surface characteristics can be associated with unique failure modes. An equation is described which can be used to extract the longitudinal compression strength knowing the longitudinal tensile and flexural strengths of the same composite system.
Document ID
19820014439
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sinclair, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:82833
E-1145
NASA-TM-82833
Report Number: NAS 1.15:82833
Report Number: E-1145
Report Number: NASA-TM-82833
Meeting Information
Meeting: Symp. on Compression Testing of Homogeneous Mater. and Composites
Location: Williamsburg, VA
Country: United States
Start Date: March 10, 1982
End Date: March 11, 1982
Sponsors: Am. Soc. for Testing and Materials
Accession Number
82N22313
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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