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Aeronautical Manufacturing Technology  2021, Issue (21): 51-56    DOI: 10.16080/j.issn1671-833x.2021.21.051
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Evaluation of Composite Matrix Crack Using Nonlinear Ultrasonic Lamb Wave Detected by Fiber Bragg Grating
WANG Rong 1, 2 , WU Qi 2 , XIONG Ke 2 , ZHANG Hanqi 2
1. Nanjing Vocational University of Industry Technology, Nanjing 210023, China;
2. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
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