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Discontinuously Stiffened Composite Panel under Compressive LoadingThe design of composite structures requires an evaluation of their safety and durability under service loads and possible overload conditions. This paper presents a computational tool that has been developed to examine the response of stiffened composite panels via the simulation of damage initiation, growth, accumulation, progression, and propagation to structural fracture or collapse. The structural durability of a composite panel with a discontinuous stiffener is investigated under compressive loading induced by the gradual displacement of an end support. Results indicate damage initiation and progression to have significant effects on structural behavior under loading. Utilization of an integrated computer code for structural durability assessment is demonstrated.
Document ID
19970003424
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Minnetyan, Levon
(Clarkson Univ. Potsdam, NY United States)
Rivers, James M.
(Clarkson Univ. Potsdam, NY United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH United States)
Murthy, Pappu L. N.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: Journal of Reinforced Plastics and Composites
Volume: 14
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:202685
NASA-CR-202685
Report Number: NAS 1.26:202685
Report Number: NASA-CR-202685
Accession Number
97N12159
Funding Number(s)
CONTRACT_GRANT: NAG3-1101
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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