This work investigates the mode I and II interlaminar fracturing behavior of laminated composites and the related size effects. Fracture tests on geometrically scaled double cantilever beam (DCB) and end notch flexure (ENF) specimens were conducted. The results show a significant difference between the mode I and mode II fracturing behaviors. The strength of the DCB specimens scales according to the linear elastic fracture mechanics (LEFM), whereas ENF specimens show a different behavior. For ENF tests, small specimens exhibit a pronounced pseudoductility. In contrast, larger specimens behave in a more brittle way, with the size effect on nominal strength closer to that predicted by LEFM. This transition from quasi-ductile to brittle behavior is associated with the size of the fracture process zone (FPZ), which is not negligible compared with the specimen size. For the size range investigated in this study, the nonlinear effects of the FPZ can lead to an underestimation of the fracture energy by as much as 55%. Both the mode I and II test data can be captured very accurately by the Bažant’s type II size effect law (SEL).
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September 2019
Research-Article
Mode I and II Interlaminar Fracture in Laminated Composites: A Size Effect Study
Marco Salviato,
Marco Salviato
William E. Boeing Department of Aeronautics and Astronautics,
Seattle, WA 98195
e-mail: salviato@aa.washington.edu
University of Washington
,Seattle, WA 98195
e-mail: salviato@aa.washington.edu
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Kedar Kirane,
Kedar Kirane
Department of Mechanical Engineering,
Stony Brook, NY 11794
e-mail: kedar.kirane@stonybrook.edu
Stony Brook University
,Stony Brook, NY 11794
e-mail: kedar.kirane@stonybrook.edu
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Zdeněk P. Bažant,
Zdeněk P. Bažant
Department of Civil and Environmental Engineering,
Evanston, IL 60208
e-mail: z-bazant@northwestern.edu
Northwestern University
,Evanston, IL 60208
e-mail: z-bazant@northwestern.edu
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Gianluca Cusatis
Gianluca Cusatis
1
Department of Civil and Environmental Engineering,
Evanston, IL 60208
e-mail: g-cusatis@northwestern.edu
Northwestern University
,Evanston, IL 60208
e-mail: g-cusatis@northwestern.edu
1Corresponding author.
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Marco Salviato
William E. Boeing Department of Aeronautics and Astronautics,
Seattle, WA 98195
e-mail: salviato@aa.washington.edu
University of Washington
,Seattle, WA 98195
e-mail: salviato@aa.washington.edu
Kedar Kirane
Department of Mechanical Engineering,
Stony Brook, NY 11794
e-mail: kedar.kirane@stonybrook.edu
Stony Brook University
,Stony Brook, NY 11794
e-mail: kedar.kirane@stonybrook.edu
Zdeněk P. Bažant
Department of Civil and Environmental Engineering,
Evanston, IL 60208
e-mail: z-bazant@northwestern.edu
Northwestern University
,Evanston, IL 60208
e-mail: z-bazant@northwestern.edu
Gianluca Cusatis
Department of Civil and Environmental Engineering,
Evanston, IL 60208
e-mail: g-cusatis@northwestern.edu
Northwestern University
,Evanston, IL 60208
e-mail: g-cusatis@northwestern.edu
1Corresponding author.
Contributed by the Applied Mechanics Division of ASME for publication in the Journal of Applied Mechanics. Manuscript received April 28, 2019; final manuscript received May 24, 2019; published online June 27, 2019. Assoc. Editor: Yonggang Huang.
J. Appl. Mech. Sep 2019, 86(9): 091008 (8 pages)
Published Online: June 27, 2019
Article history
Received:
April 28, 2019
Revision Received:
May 24, 2019
Accepted:
May 25, 2019
Citation
Salviato, M., Kirane, K., Bažant, Z. P., and Cusatis, G. (June 27, 2019). "Mode I and II Interlaminar Fracture in Laminated Composites: A Size Effect Study." ASME. J. Appl. Mech. September 2019; 86(9): 091008. https://doi.org/10.1115/1.4043889
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