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A study of the effects of long-term exposure to fuels and fluids on the behavior of advanced composite materialsThe periodic testing and evaluation of graphite/epoxy and Kevlar/epoxy material systems after subjecting test specimens to prolonged exposure to several laboratory-controlled environments deemed typical of normal aircraft operations is discussed. It is noted that specimen immersion in water or water-based fluids resulted in the greatest effect on the mechanical properties tested. Also, the environmental fluids showed a tendency to affect Kevlar/epoxy systems at an earlier exposure period than the graphite/epoxy systems. Results also indicate mechanical property strength retention generally being lower for the Kevlar/epoxy systems when compared to the corresponding graphite/epoxy systems in similar environments, after prolonged exposure.
Document ID
19820010453
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tanimoto, E. Y.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1981
Subject Category
Composite Materials
Report/Patent Number
D6-41185-9
NASA-CR-165763
Report Number: D6-41185-9
Report Number: NASA-CR-165763
Accession Number
82N18327
Funding Number(s)
CONTRACT_GRANT: NAS1-12428
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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