Measurements of a symmetric airfoil morphed by macro fiber composite actuators

Yann Bouremel, Woei Leong Chan, Gareth Jones, Marco Debiasi

Research output: Chapter in Book/Report/Conference proceedingConference contribution

5 Citations (Scopus)

Abstract

This study presents the geometric and aerodynamic properties of a symmetric airfoil model that uses macro fiber composite actuators to change the shape of its upper and lower surfaces. In the design discussed, these thin and light piezoelectric actuators are bonded to the inside and become an integral part of the skin of the upper and lower surfaces of the airfoil. Still-air and wind-tunnel measurements in different flow regimes are performed to assess the characteristics associated with the changes of the shape of the airfoil. The results obtained will be used to design and fabricate a wing with morphing surfaces for testing in a remote-controlled aircraft.

Original languageEnglish
Title of host publication32nd AIAA Applied Aerodynamics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624102882
DOIs
Publication statusPublished - 2014
Event32nd AIAA Applied Aerodynamics Conference 2014 - Atlanta, GA, United States
Duration: 2014 Jun 162014 Jun 20

Publication series

Name32nd AIAA Applied Aerodynamics Conference

Conference

Conference32nd AIAA Applied Aerodynamics Conference 2014
Country/TerritoryUnited States
CityAtlanta, GA
Period14-06-1614-06-20

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Mechanical Engineering

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