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Multiscale Multifunctional 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. Global fracture is enhanced when internal pressure is combined with shear loads. The old reference denotes that nothing has been added to this comprehensive report since then.
Document ID
20120015254
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Chamis, C. C.
(NASA Glenn Research Center Cleveland, OH, United States)
Minnetyan, L.
(Clarkson Univ. Potsdam, NY, United States)
Date Acquired
August 26, 2013
Publication Date
September 1, 2012
Subject Category
Structural Mechanics
Report/Patent Number
NASA/TM-2012-217680
E-18355
Report Number: NASA/TM-2012-217680
Report Number: E-18355
Funding Number(s)
WBS: WBS 561581.02.08.03.13.05
Distribution Limits
Public
Copyright
Public Use Permitted.
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