Lamb wave interaction at debondings due to impact damage in complex stiffened CFRP structures
Author:
Affiliation:
1. Airbus Group Innovations (Germany)
2. German Aerospace Ctr. (Germany)
3. Univ. of Siegen (Germany)
Publisher
SPIE
Reference9 articles.
1. Active health monitoring of an aircraft wing with embedded piezoelectric sensor/actuator network: I. Defect detection, localization and growth monitoring
2. Reliability Aspects of Lamb Wave Interaction at Impact Damages in Complex Stiffened CFRP Structures;Eckstein,2016
3. Considerations on the Reliability of Guided Ultrasonic Wave-Based SHM Systems for CFRP Aerospace Structures;Eckstein,2012
4. Smart Intelligent Aircraft Structures (SARISTU)
5. Damage Introduction, Detection, and Assessment at CFRP Door Surrounding Panel;Bach,2016
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Structural health monitoring of an adhesively bonded CFRP aircraft fuselage by ultrasonic Lamb Waves;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-08-25
2. Second Harmonic Generation of Guided Wave at Crack-Induced Debonding in FRP-Strengthened Metallic Plates;International Journal of Structural Stability and Dynamics;2018-12-20
3. Lamb Wave Interaction at Delamination and Debondings Due to Impact Damage in Complex Stiffened CFRP Structures;Journal of Nondestructive Evaluation, Diagnostics and Prognostics of Engineering Systems;2018-05-03
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