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Dynamic mode-I delamination in composite DCB under impact loads with attunable dynamic effect
A dynamic mode-I energy release rate (ERR) of a double cantilever beam (DCB) under impact from a striker is derived for the first time for isotropic and orthotropic composite materials, accounting for DCB properties, a striker mass and an initial impact velocity. This is achieved in the context of structural vibration analysis by employing beam dynamics. It is found that the initial impact velocity determines the magnitude of the ERR, which is proportional to the velocity squared, while the delamination length ratio and the mass ratio between the striker and the DCB defines the response time. To understand the transient effect, a dynamic factor is defined as a function of the mass ratio. This factor decreases with an increasing striker mass, indicating a transition in the dynamic response from flexural-wave dominant to quasi-static-motion dominant, allowing an attunable dynamic effect. The developed theory is verified against the finite-element simulations for isotropic and orthotropic materials as well as experimental verification using published data. This work allows the measurements of fracture toughness under the impact load with the derived analytical solution. In addition, the developed theory can guide a design of impact tests and a fundamental understanding of impact-induced fracture for carbon-fiber-reinforced plastics.
Funding
Plastic constitutive theory and flow instability mechanism of disordered alloys
National Natural Science Foundation of China
Find out more...National Natural Science Foundation of China (Grant No. 12272392)
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
- Mechanical, Electrical and Manufacturing Engineering
Department
- Aeronautical and Automotive Engineering
Published in
Composites Science and TechnologyVolume
241Issue
2023Publisher
ElsevierVersion
- AM (Accepted Manuscript)
Rights holder
© ElsevierPublisher statement
This paper was accepted for publication in Composites Science and Technology published by Elsevier. The final publication is available at https://doi.org/10.1016/j.compscitech.2023.110120. This manuscript version is made available under the CC-BY-NC-ND 4.0 license https://creativecommons.org/licenses/by-nc-nd/4.0/Acceptance date
2023-06-15Publication date
2023-06-20Copyright date
2023ISSN
0266-3538eISSN
1879-1050Publisher version
Language
- en