Localizations and force reconstruction of low-velocity impact in a composite panel using optical fiber sensors
Author:
Affiliation:
1. a Agency for Defense Development , Daejeon , Korea
2. b Department of Aerospace Engineering , Korea Advanced Institute of Science and Technology , Daejeon , Korea
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,Ceramics and Composites
Link
https://www.tandfonline.com/doi/pdf/10.1080/09243046.2012.736346
Reference15 articles.
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3. Neubauer M, Gunteher G, Fullhas K. Structural design aspects and criteria for military UAV. In: Proceedings of the UAV Design Processes and Criteria – RTO-MP-AVT 145; 2007; Florence, Italy.
4. Kosmatka JB, Oliver J. Development of an in-flight structural health monitoring system for composite unmanned aircraft. In: Proceedings of the 47th AISS/ASME/ASCE/AHS/ASV Structures, Structural Dynamics and Materials Conference – AIAA 2006-1881; 2006; Newport, Rhode Island.
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