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Fatigue degradation in compressively loaded composite laminatesThe effect of imbedded delaminations on the compression fatigue behavior of quasi-isotropic, T300/5208, graphite/epoxy laminates was investigated. Teflon imbedments were introduced during panel layup to create delaminations. Static and constant amplitude (R=10, omega = 10 Hz) fatigue tests were conducted. S-N data and half life residual strength data were obtained. During static compression loading, the maximum deflection of the buckled delaminated region was recorded. Under compression fatigue, growth of the imbedded delamination was identified as the predominant failure mode in most of the test cases. Specimens that exhibited others failures had a single low stiffness ply above the Teflon imbedment. Delamination growth during fatigue was monitored using DIB enhanced radiography. In specimens with buried delaminations, the dye penetrant (DIB) was introduced into the delaminated region through a minute laser drilled hole, using a hypodermic needle. A low kV, microfocus, X-ray unit was mounted near the test equipment to efficiently record the cyclic growth of buried delaminations on Polaroid film.
Document ID
19810014659
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ramkumar, R. L.
(Northrop Corp. Hawthorne, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1981
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-165681
NOR-81-79
Report Number: NASA-CR-165681
Report Number: NOR-81-79
Accession Number
81N23192
Funding Number(s)
CONTRACT_GRANT: NAS1-15956
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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