Assessment of dynamic mode-I delamination driving force in double cantilever beam tests for fiber-reinforced polymer composite and adhesive materials
The double cantilever beam (DCB) tests are widely used to assess the interfacial delamination properties of laminated composites. For quasi-static loads, the DCB tests are standardized based on the beam mechanics; for dynamic loads, however, such as high-loading-rate impact and cyclic loads, there is no established analytical theory. This presents a significant obstacle preventing the research community from assessing the delamination behavior of composites or adhesives for their application under complex in-service loads. In this paper, the theory of evaluating dynamic mode-I delamination driving force for DCBs under general displacement loads is developed for the first time, accounting for structural vibration effects. The developed theory is demonstrated by two examples: high-loading-rate split Hopkinson bar impact and cyclic fatigue loads. The analytical solutions are validated by published experiment results and in-house tests. This work provides a fundamental analytical tool to study and assess the fracture behavior of fiber reinforced polymer composite and adhesive materials under various loading conditions.
Funding
National Natural Science Foundation of China (Grant No. 51401028, No. 51271193, No. 11790292)
Strategic Priority Research Program of the Chinese Academy of Sciences (Grant No. XDB22040303)
Innovation Program (237099000000170004)
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
- Mechanical, Electrical and Manufacturing Engineering
Department
- Aeronautical and Automotive Engineering
Published in
Composites Science and TechnologyVolume
228Issue
2022Publisher
ElsevierVersion
- AM (Accepted Manuscript)
Rights holder
© ElsevierPublisher statement
This paper was accepted for publication in the journal Composites Science and Technology and the definitive published version is available at https://doi.org/10.1016/j.compscitech.2022.109632Acceptance date
2022-07-06Publication date
2022-07-09Copyright date
2022ISSN
0266-3538eISSN
1879-1050Publisher version
Language
- en