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Vibration control of the composite wing model using piezoelectric actuators

  • Lae Hyong Kang
  • , Hong Ll Kim
  • , Lee Juho
  • , Jae Won Parkl
  • , Jae Hung Han*
  • *Corresponding author for this work
  • Korea Advanced Institute of Science and Technology

Research output: Contribution to conferenceConference paperpeer-review

Abstract

This paper demonstrates the feasibility of using piezoelectric actuators in controlling flow-induced vibration of a lightweight composite wing structure. Vibration characteristics of the composite wing model were predicted analytically against the air flow speed and the results were compared with experimental results from wind tunnel tests. Vibration control tests were successfully accomplished using positive position feedback (PPF) controller and the real-time operating deflection shapes of the composite wing were measured using 3D optical motion capture system.

Original languageEnglish
Title of host publicationMulti-Functional Materials and Structures III
Pages1027-1030
Number of pages4
DOIs
StatePublished - 2010
Event3rd International Conference on Multi-Functional Materials and Structures, MFMS 2010 - Jeonju, Korea, Republic of
Duration: 2010.09.142010.09.18

Publication series

NameAdvanced Materials Research
Volume123-125
ISSN (Print)1022-6680

Conference

Conference3rd International Conference on Multi-Functional Materials and Structures, MFMS 2010
Country/TerritoryKorea, Republic of
CityJeonju
Period10.09.1410.09.18

Keywords

  • Flow-induced vibration
  • Flutter
  • Operating deflection shape
  • Piezoelectric actuator
  • Vibration control

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