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Manufacturing Distortions of Curved Composite PanelsThis papa briefly discusses the influences of through-thickness thermal expansion, a misaligned ply, and a resin-rich slightly thicker ply on the deformations of a curved composite laminate during cool down from tbc cure temperature. Both two-dimensional and three-dimensional level finite-element analyses are used. The deformations are categorized as to radial and tangential deformations and twist, and for each of the three influences, these deformations are quantified. An additional outcome of the study is an indication of the level of analysis needed to study each of these three influences.
Document ID
20040084808
Acquisition Source
Headquarters
Document Type
Reprint (Version printed in journal)
Authors
Starnes, James H., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Ochinero, T. T.
(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
August 21, 2013
Publication Date
March 1, 2002
Publication Information
Publication: Journal of Thermoplastic Composite Materials
Publisher: Sage Publications
Volume: 15
ISSN: 0892-7057
Subject Category
Composite Materials
Funding Number(s)
CONTRACT_GRANT: NAG1-1895
Distribution Limits
Public
Copyright
Other

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