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Structural Durability of Damaged Metallic Panel Repaired with Composite PatchesStructural durability/damage tolerance characteristics of an aluminum tension specimen possessing a short crack and repaired by applying a fiber composite surface patch is investigated via computational simulation. The composite patch is made of graphite/epoxy plies with various layups. An integrated computer code that accounts for all possible failure modes is utilized for the simulation of combined fiber-composite/aluminum structural degradation under loading. Damage initiation, growth, accumulation, and propagation to structural fracture are included in the simulation. Results show the structural degradation stages due to tensile loading and illustrate the use of computational simulation for the investigation of a composite patch repaired cracked metallic panel.
Document ID
19970026583
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Minnetyan, Levon
(Clarkson Univ. Potsdam, NY United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Publication Information
Publication: Journal of Reinforced Plastics and Composites
Publisher: Technomic
Volume: 16
Issue: 3
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-112530
NAS 1.15:112530
Report Number: NASA-TM-112530
Report Number: NAS 1.15:112530
Accession Number
97N25832
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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