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Mode II Interlaminar Fracture Toughness and Fatigue Characterization of a Graphite Epoxy Composite MaterialMode II interlaminar fracture toughness and delamination onset and growth characterization data were generated for IM7/8552 graphite epoxy composite materials from two suppliers for use in fracture mechanics analyses. Both the fracture toughness testing and the fatigue testing were conducted using the End-notched Flexure (ENF) test. The ENF test for mode II fracture toughness is currently under review by ASTM as a potential standard test method. This current draft ASTM protocol was used as a guide to conduct the tests on the IM7/8552 material. This report summarizes the test approach, methods, procedures and results of this characterization effort.
Document ID
20100031113
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
O'Brien, T. Kevin
(NASA Langley Research Center Hampton, VA, United States)
Johnston, William M.
(Lockheed Martin Corp. Hampton, VA, United States)
Toland, Gregory J.
(California Univ. Santa Barbara, CA, United States)
Date Acquired
August 25, 2013
Publication Date
August 1, 2010
Subject Category
Composite Materials
Report/Patent Number
NF1676L-10105
NASA/TM-2010-216838
L-19898
Report Number: NF1676L-10105
Report Number: NASA/TM-2010-216838
Report Number: L-19898
Funding Number(s)
WBS: WBS 698259.02.07.07.03.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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