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Temperature and deflection data from the asymmetric heating of cross-ply composite tubesData generated while heating several cross-ply graphite-epoxy tubes on one side, along their lengths, and cooling them on the other side are presented. This heating arrangement produces a circumferential temperature gradient, and the data show that the gradient can be represented by a cosinusoidal temperature distribution. The thermally induced bending deflections caused by the temperature gradient are also presented.
Document ID
19870050875
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hyer, Michael W.
(Maryland, University College Park, United States)
Cooper, David E.
(Boeing Aerospace Co. Seattle, WA, United States)
Tompkins, S. S.
(NASA Langley Research Center Hampton, VA, United States)
Cohen, David
(Maryland Univ. College Park, MD, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Publication Information
Publication: Journal of Composites Technology and Research
Volume: 9
ISSN: 0885-6804
Subject Category
Composite Materials
Accession Number
87A38149
Funding Number(s)
CONTRACT_GRANT: NAG1-343
Distribution Limits
Public
Copyright
Other

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