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Fracture characteristics of angleplied laminates fabricated from overaged graphite/epoxy prepregA series of angleplied graphite/epoxy laminates was fabricated from overaged prepreg and tested in tension to investigate the effects of overaged or advanced cure material on the degradation of laminate strength. Results, which include fracture stresses, indicate a severe degradation in strength. In addition, the fracture surfaces and microstructural characteristics are distinctly unlike any features observed in previous tests of this prepreg and laminate configuration. Photographs of the surfaces and microstructures reveal flat morphologies consisting of alternate rows of fibers and hackles. These fracture surface characteristics are independent of the laminate configurations. The photomicrographs are presented and compared with data from similar studies to show the unique characteristics produced by the overage prepreg. Analytical studies produced results which agreed with those from the experimental investigations.
Document ID
19860015945
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ginty, C. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-87266
NAS 1.15:87266
E-2968
Report Number: NASA-TM-87266
Report Number: NAS 1.15:87266
Report Number: E-2968
Meeting Information
Meeting: Symposium on Fractography of Modern Engineering Materials
Location: Nashville, TN
Country: United States
Start Date: November 18, 1985
End Date: November 19, 1985
Accession Number
86N25417
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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