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Progressive fracture of polymer matrix composite structures: A new approachA new approach independent of stress intensity factors and fracture toughness parameters has been developed and is described for the computational simulation of progressive fracture of polymer matrix composite structures. The damage stages are quantified based on physics via composite mechanics while the degradation of the structural behavior is quantified via the finite element method. The approach account for all types of composite behavior, structures, load conditions, and fracture processes starting from damage initiation, to unstable propagation and to global structural collapse. Results of structural fracture in composite beams, panels, plates, and shells are presented to demonstrate the effectiveness and versatility of this new approach. Parameters and guidelines are identified which can be used as criteria for structural fracture, inspection intervals, and retirement for cause. Generalization to structures made of monolithic metallic materials are outlined and lessons learned in undertaking the development of new approaches, in general, are summarized.
Document ID
19920013951
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Murthy, P. L. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Minnetyan, L.
(Clarkson Univ. Potsdam, NY., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-105574
E-6900
NAS 1.15:105574
Report Number: NASA-TM-105574
Report Number: E-6900
Report Number: NAS 1.15:105574
Meeting Information
Meeting: Annual Energy-Sources Technology Conference and Exhibition
Location: Houston, TX
Country: United States
Start Date: January 26, 1992
End Date: January 29, 1992
Sponsors: ASME
Accession Number
92N23194
Funding Number(s)
PROJECT: RTOP 505-63-53
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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