Buckling behavior monitoring of composite wing box model using fiber Bragg grating sensor system
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SPIE
Cited by 9 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. Strain and damage monitoring in CFRP fuselage panels using fiber Bragg grating sensors. Part II: Mechanical testing and validation;Composite Structures;2014-01
2. Strain and damage monitoring in CFRP fuselage panels using fiber Bragg grating sensors. Part I: Design, manufacturing and impact testing;Composite Structures;2014-01
3. Damage monitoring of CFRP stiffened panels under compressive load using FBG sensors;Composite Structures;2012-02
4. Disbond monitoring at wing stringer tip based on built-in ultrasonic transducers and a pulsed laser;Smart Materials and Structures;2007-06-05
5. Finite-element modelling of non-destructive material evaluation, an addendum: a bibliography (1997–2003);Modelling and Simulation in Materials Science and Engineering;2004-07-06
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