使线.

Suofeng Zhang1, Yuan Liu1, Shenfang Yuan1

  • 1Research Center of Structural Health Monitoring and Prognosis, State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China.

PubMed
概括

这项研究引入了一种先进的方法,用于使用非线性Lamb波来检测飞机机翼结构中的疲劳裂. 该技术有效地提高了裂检测,即使在具有大切口的复杂设计中也是如此.