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Damage Progression in Bolted CompositesStructural durability, damage tolerance, and progressive fracture characteristics of bolted graphite/epoxy composite laminates are evaluated via computational simulation. Constituent material properties and stress and strain limits are scaled up to the structure level to evaluate the overall damage and fracture propagation for bolted composites. Single and double bolted composite specimens with various widths and bolt spacings are evaluated. The effect of bolt spacing is investigated with regard to the structural durability of a bolted joint. Damage initiation, growth, accumulation, and propagation to fracture are included in the simulations. Results show the damage progression sequence and structural fracture resistance during different degradation stages. A procedure is outlined for the use of computational simulation data in the assessment of damage tolerance, determination of sensitive parameters affecting fracture, and interpretation of experimental results with insight for design decisions.
Document ID
20000033690
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)
Gotsis, Pascal K.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
August 19, 2013
Publication Date
May 1, 1998
Publication Information
Publication: Journal of Thermoplastic Composite Materials
Volume: 2
Subject Category
Composite Materials
Distribution Limits
Public
Copyright
Other

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