Impact localization on composite wing using 1D array FBG sensor and RMS/correlation based reference database algorithm-Reference-Cited by-同舟云学术

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Impact localization on composite wing using 1D array FBG sensor and RMS/correlation based reference database algorithm

Published:2015-07 Issue: Volume:125 Page:159-169
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Shrestha Pratik,Kim Jin-Hyuk,Park Yurim,Kim Chun-Gon

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference18 articles.

1. Bhat NV. Delamination growth in graphite/epoxy composite laminates under tensile loading [Ph.D.]. Massachusetts Institute of Technology; 1993.

2. Composite materials for aircraft structures;Baker,2004

3. An introduction to structural health monitoring;Farrar;Philos Trans R Soc A Math Phys Eng Sci,2007

4. Overview of piezoelectric impedance-based health monitoring and path forward;Park;Shock Vib Digest,2003

5. Structural monitoring with fiber optic technology;Measures,2001

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