Baseline-free damage detection in composite plates using edge-reflected Lamb waves

Author:

Huang Liping,Zeng Liang,Lin Jing,Zhang Nan

Funder

National Natural Science Foundation of China

Natural Science Foundation of Shaanxi Province

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference32 articles.

1. Structural health monitoring of fiber-reinforced composite plates for low-velocity impact damage using ultrasonic lamb wave tomography;Sekhar;Struct Health Monit,2006

2. Federal Aviation Administration (FAA). Composite aircraft structure: advisory circular (AC) (20-107B, Change 1) Washington, DC: FAA, 2010.

3. US Department of Defense. Department of Defense Handbook, Composite materials handbook volume 3: polymer matrix composites—materials usage, design and analysis (Currently available as composite materials handbook CMH 17) Report no. MIL-HDBK-17-3F (US Fort Washington), 2002.

4. Guided Lamb waves for identification of damage in composite structures: a review;Su;J Sound Vib,2006

5. Guided wave based structural health monitoring: a review;Mitra;Smart Mater Struct,2016

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