Abstract
Composite laminates are widely used in various fields, but their structures are prone to cracks and damage. Due to the difference in angles of the instantaneous direction of the wave front propagation and the direction of the energy flow in an anisotropic material, the use of Lamb waves for damage localization in composite laminates is a challenging task. Establishing the wave front shape equation can overcome the difficulty of damage localization caused by anisotropy, but this usually requires a priori knowledge of the acoustic velocity distribution of the laminates, which is not convenient for efficient damage localization. In this paper, a damage localization method based on wave front shapes for composite laminates without any knowledge of the velocity profile is presented. Numerical simulation and experimental results show that the proposed method works. This method shows good damage localization accuracy and has broad application prospects in non-destructive testing for plate structures with strong anisotropy.
Original language | English (US) |
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Article number | 107357 |
Journal | Ultrasonics |
Volume | 142 |
DOIs | |
State | Published - Aug 2024 |
Externally published | Yes |
Keywords
- Composite laminates
- Damage localization
- Lamb waves
- Non-destructive testing
- Wave front shape
ASJC Scopus subject areas
- Acoustics and Ultrasonics