Structural Health Monitoring of Cracked Aircraft Panels Repaired with Bonded Patches Using Fiber Bragg Grating Sensors

Author: Sekine Hideki   Fujimoto Shin-Etsu   Okabe Tomonaga   Takeda Nobuo   Yokobori Toshimitsu  

Publisher: Springer Publishing Company

ISSN: 0929-189X

Source: Applied Composite Materials, Vol.13, Iss.2, 2006-03, pp. : 87-98

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Abstract