Patching Efficiency in Cracked Structural Panels Repaired with a Bonded FRP Composite Patch Containing a Piezoelectric Fiber Composite Actuator Layer
Author:
Publisher
Japan Society for Aeronautical and Space Sciences
Link
https://www.jstage.jst.go.jp/article/jjsass/54/624/54_624_1/_pdf
Reference16 articles.
1. Crack Patching: Analysis and Design
2. Fibre composite repair of cracked metallic aircraft components — practical and basic aspects
3. Bonded composite repair of fatigue-cracked primary aircraft structure
4. Optical fibre sensors for health monitoring of bonded repair systems
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1. Patching Efficiency in Cracked Aircraft Structural Panels Repaired with Bonded Piezoelectric Patches;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2006
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