Buckling behavior monitoring of composite wing box model using Fiber Bragg grating sensor system

Proceedings of SPIE - The International Society for Optical Engineering

Volumn 4327, Issue 1, 2001, Pages 660-668

  Hong, Chang Sun ^a   Ryu, Chi Young ^a   Lee, Jung Ryul ^a   Kim, Chun Gon ^a  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

Author keywords

Buckling behavior monitoring; Composite wing box; Fiber Bragg grating sensor system; Real time signal processing; Strain monitoring; Wavelength swept fiber laser

Indexed keywords

BUCKLING; FIBER BRAGG GRATINGS; FIBER LASERS; FINITE ELEMENT METHOD; SENSORS; SIGNAL PROCESSING; STRAIN; WAVELENGTH DIVISION MULTIPLEXING; WINGS;

STRAIN MONITORING;

COMPOSITE STRUCTURES;

EID: 0034769035     PISSN: 0277786X     EISSN: None     Source Type: Journal    
DOI: 10.1117/12.436572     Document Type: Article

References (10)

1. Fiber optic smart structures
2. Simultaneous sensing of the strain and failure instants of composite beams using fiber optic michelson sensor
3. Signal characteristics in the delaminated composite specimen with fiber optic sensor
4. Detection of buckling and crack growth in the delaminated composites using fiber optic sensor
5. Multiplexed fiber bragg grating strain-sensor system with a fiber fabry-perot wavelength filter
6. Strain sensing of modern composite materials with a spatial/wavelength-division multiplexed fiber grating network
7. Interrogation of Fiber grating sensor arrays with a wavelength-swept fiber laser
8. Development of fiber bragg grating sensor system using wavelength-swept fiber laser
9. Progress towards the development of practical fiber bragg grating instrumentation systems
10. Stain measurement of the laminated composites using attached fiber Bragg grating sensor