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Cohesive Laws and Progressive Damage Analysis of Composite Bonded Joints, a Combined Numerical/Experimental ApproachThe results of an experimental/numerical campaign aimed to develop progressive damage analysis (PDA) tools for predicting the strength of a composite bonded joint under tensile loads are presented. The PDA is based on continuum damage mechanics (CDM) to account for intralaminar damage, and cohesive laws to account for interlaminar and adhesive damage. The adhesive response is characterized using standard fracture specimens and digital image correlation (DIC). The displacement fields measured by DIC are used to calculate the J-integrals, from which the associated cohesive laws of the structural adhesive can be derived. A finite element model of a sandwich conventional splice joint (CSJ) under tensile loads was developed. The simulations, in agreement with experimental tests, indicate that the model is capable of predicting the interactions of damage modes that lead to the failure of the joint.
Document ID
20150006866
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Girolamo, Donato
(National Inst. of Aerospace Hampton, VA, United States)
Davila, Carlos G.
(NASA Langley Research Center Hampton, VA, United States)
Leone, Frank A.
(NASA Langley Research Center Hampton, VA, United States)
Lin, Shih-Yung
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
April 28, 2015
Publication Date
January 5, 2015
Subject Category
Structural Mechanics
Report/Patent Number
NF1676L-20341
Report Number: NF1676L-20341
Meeting Information
Meeting: AIAA SciTech 2015 Meeting
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 544163.04.01.07.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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