Table of Contents
Smart Materials Research
Volume 2013, Article ID 173605, 9 pages
http://dx.doi.org/10.1155/2013/173605
Research Article

Procedure to Use PZT Sensors in Vibration and Load Measurements

1Structural Technologies Division, Dynamics and Adaptive Structures Group, CSIR-National Aerospace Laboratories, Bangalore, Karnataka 560 017, India
2VTU, Belgaum, Karnataka 590 018, India

Received 21 March 2013; Revised 16 September 2013; Accepted 19 September 2013

Academic Editor: Chris Bowen

Copyright © 2013 C. N. Sathyanarayana et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Citations to this Article [3 citations]

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  • William C. Wilson, Jason P. Moore, and Peter D. Juarez, “Surface acoustic wave vibration sensors for measuring aircraft flutter,” 2016 IEEE International Conference on Prognostics and Health Management (ICPHM), pp. 1–7, . View at Publisher · View at Google Scholar
  • Xubin Lu, Chee Kiong Soh, Panduranga Vittal Avvari, Xubin Lu, Chee Kiong Soh, and Panduranga Vittal Avvari, “Lamb wave propagation in vibrating structures for effective health monitoring,” Health Monitoring Of Structural And Biological Systems 2015, vol. 9438, 2015. View at Publisher · View at Google Scholar
  • Mario Rosario Chiarelli, Vincenzo Binante, Stefano Botturi, Andrea Massai, Jan Kunzmann, Angelo Colbertaldo, and Diego Giuseppe Romano, “On the active deformations of hybrid specimens,” Aircraft Engineering and Aerospace Technology, vol. 88, no. 5, pp. 676–687, 2016. View at Publisher · View at Google Scholar