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Analytical study of graphite-epoxy tube response to thermal loadsThe thermally-induced stresses and deformations in graphite-epoxy tubes with aluminum foil bonded to both inner and outer surfaces, and to the outer surface only are computed. Tubes fabricated from three material systems, T300/934, P75s/934, and P75s/BP907, and having a 1 inch inner radius and a lamination sequence of (+15/0 + or - 10/0)sub s are studied. Radial, axial, and circumferential stresses in the various layers of the tube, in the foil, and in the adhesive bonding the foil to the tubes are computed using an elasticity solution. The results indicate that the coatings have no detrimental effect on the stress state in the tube, particularly those stresses that lead to microcracking. The addition of the aluminum foil does, however, significantly influence the axial expansion of the T300/934 tube, the tube with the softer graphite fibers. The addition of foil can change the sign of the axial coefficient of thermal expansion. Twist tendencies of the tubes are only slightly affected by the addition of the coatings, but are of second order compared to the axial response.
Document ID
19880020500
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Knott, Tamara W.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Hyer, M. W.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1988
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-183215
CCMS-88-16
VPI-E-88-25
PB89-104160
NAS 1.26:183215
Report Number: NASA-CR-183215
Report Number: CCMS-88-16
Report Number: VPI-E-88-25
Report Number: PB89-104160
Report Number: NAS 1.26:183215
Accession Number
88N29884
Funding Number(s)
CONTRACT_GRANT: NAG1-343
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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