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Mixed-Mode Decohesion Elements for Analyses of Progressive DelaminationA new 8-node decohesion element with mixed mode capability is proposed and demonstrated. The element is used at the interface between solid finite elements to model the initiation and propagation of delamination. A single displacement-based damage parameter is used in a strain softening law to track the damage state of the interface. The method can be used in conjunction with conventional material degradation procedures to account for inplane and intra-laminar damage modes. The accuracy of the predictions is evaluated in single mode delamination tests, in the mixed-mode bending test, and in a structural configuration consisting of the debonding of a stiffener flange from its skin.
Document ID
20010044119
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Davila, Carlos G.
(NASA Langley Research Center Hampton, VA United States)
Camanho, Pedro P.
(Porto Univ. Portugal)
deMoura, Marcelo F.
(Porto Univ. Portugal)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Publication Information
Publisher: American Institute of Aeronautics and Astronautics, Inc.
Subject Category
Structural Mechanics
Report/Patent Number
AIAA Paper 2001-1486
Report Number: AIAA Paper 2001-1486
Meeting Information
Meeting: 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Seattle, WA
Country: United States
Start Date: April 16, 2001
End Date: April 19, 2001
Sponsors: American Society of Civil Engineers, American Society of Mechanical Engineers, American Society for Composites, American Inst. of Aeronautics and Astronautics, American Helicopter Society, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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