Lamb Wave Stiffness Characterization of Composites Undergoing Thermal-Mechanical Aging Seale, Michael Madaras, Eric 2018-02-14T09:21:18.000 2020-06-30T06:50:44Z 2020-06-30T06:50:44Z Fri Jan 01 00:00:00 UTC 1999 1999
dc.description.abstract <p>The introduction of new, advanced composite materials into aviation systems requires a thorough understanding of the long term effects of combined thermal and mechanical loading upon those materials. Analytical methods investigating the effects of intense thermal heating combined with mechanical loading have been investigated by Griffis, et al. [1] and Chen, et al. [2]. Schubbe and Mall [3] and Castelli, et al. [4] have experimentally investigated both in-phase (maximum temperature at maximum load) and out-of-phase (maximum temperature at minimum load) thermal-mechanical cycling on composites. Both authors found that the damage mechanisms and fatigue lives were dependent on test parameters as well as stress levels. Castelli, et al. [4] identified matrix dominated failure modes for out-of-phase cycling and fiber dominated damage modes for in-phase cycling.</p>
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dc.identifier archive/
dc.identifier.articleid 4165
dc.identifier.contextkey 5824045
dc.identifier.s3bucket isulib-bepress-aws-west
dc.identifier.submissionpath qnde/1999/allcontent/157
dc.language.iso en
dc.source.bitstream archive/|||Fri Jan 14 20:45:04 UTC 2022
dc.source.uri 10.1007/978-1-4615-4791-4_158
dc.title Lamb Wave Stiffness Characterization of Composites Undergoing Thermal-Mechanical Aging
dc.type event
dc.type.genre article
dspace.entity.type Publication
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