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Structural design criteria for filament-wound composite shellsAdvanced composite cylinders, manufactured by filament winding, provide a cost effective solution to many present structural applications; however, the compressive performance of filament-wound cylinders is lower than comparable shells fabricated from unidirectional tape. The objective of this study was to determine the cause of this reduction in thin filament-wound cylinders by relating the manufacturing procedures to the quality of the cylinder and to its compressive performance. The experiments on cylinder buckling were complemented by eigenvalue buckling analysis using a detailed geometric model in a finite element analysis. The applicability of classical buckling analyses was also investigated as a design tool.
Document ID
19940019929
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hahn, H. T.
(Pennsylvania State Univ. University Park, PA, United States)
Jensen, D. W.
(Pennsylvania State Univ. University Park, PA, United States)
Claus, S. J.
(Pennsylvania State Univ. University Park, PA, United States)
Pai, S. P.
(Pennsylvania State Univ. University Park, PA, United States)
Hipp, P. A.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-195125
NAS 1.26:195125
Report Number: NASA-CR-195125
Report Number: NAS 1.26:195125
Accession Number
94N24402
Funding Number(s)
CONTRACT_GRANT: NAG1-982
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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