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Progressive Fracture of Composite StructuresA new approach is described for evaluating fracture in composite structures. This approach is independent of classical fracture mechanics parameters like fracture toughness. It relies on computational simulation and is programmed in a stand-alone integrated computer code. It is multiscale, multifunctional because it includes composite mechanics for the composite behavior and finite element analysis for predicting the structural response. It contains seven modules; layered composite mechanics (micro, macro, laminate), finite element, updating scheme, local fracture, global fracture, stress based failure modes, and fracture progression. The computer code is called CODSTRAN (Composite Durability Structural ANalysis). It is used in the present paper to evaluate the global fracture of four composite shell problems and one composite built-up structure. Results show that the composite shells and the built-up composite structure global fracture are enhanced when internal pressure is combined with shear loads.
Document ID
20080018612
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH, United States)
Minnetyan, Levon
(Clarkson Univ. Potsdam, NY, United States)
Date Acquired
August 24, 2013
Publication Date
April 7, 2008
Subject Category
Structural Mechanics
Meeting Information
Meeting: 49th SDM/AIAA Conference
Location: Schaumburg, IL
Country: United States
Start Date: April 7, 2008
End Date: April 10, 2008
Sponsors: Structural Dynamics and Materials, American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.10.03.23
WBS: WBS 659877.02.03.0573.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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