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Progressive Fracture of Fiber Composite Build-Up StructuresDamage progression and fracture of built-up composite structures is evaluated by using computational simulation. The objective is to examine the behavior and response of a stiffened composite (0 +/-45/90)(sub s6) laminate panel by simulating the damage initiation, growth, accumulation, progression and propagation to structural collapse. An integrated computer code CODSTRAN was augmented for the simulation of the progressive damage and fracture of built-up composite structures under mechanical loading. Results show that damage initiation and progression to have significant effect on the structural response. Influence of the type of loading is investigated on the damage initiation, propagation and final fracture of the build-up composite panel.
Document ID
19970026605
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Minnetyan, Levon
(Clarkson Univ. Potsdam, NY United States)
Gotsis, Pascal K.
(NASA Lewis Research Center Cleveland, OH United States)
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1997
Publication Information
Publication: Reinforced Plastics and Composites
Volume: 16
Issue: 2
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-112529
NAS 1.15:112529
Report Number: NASA-TM-112529
Report Number: NAS 1.15:112529
Accession Number
97N25854
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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