Structural Health Monitoring of Cracked Aircraft Panels Repaired with Bonded Patches Using Fiber Bragg Grating Sensors
Author:
Publisher
Springer Science and Business Media LLC
Subject
Ceramics and Composites
Link
http://link.springer.com/content/pdf/10.1007/s10443-006-9011-1.pdf
Reference15 articles.
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3. Baker, A.A., Rose, L.R.F., Walker, K.F., Wilson, E.S.: Repair substantiation for a bonded composite repair to F111 lower wing skin. Appl. Compos. Mater. 6, 251–267 (1999)
4. Baker, A.A.: Bonded composite repair of fatigue-cracked primary aircraft structure. Compos. Struct. 47, 431–443 (1999)
5. Chiu, W.K., Koh, Y.L., Galea, S.C., Rajic, N.: Smart structure application in bonded repairs. Compos. Struct. 50, 433–444 (2000)
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