Please use this identifier to cite or link to this item:
|Title:||Deformation of the upper surface of an airfoil by macro fiber composite actuators||Authors:||Debiasi, M.
|Issue Date:||2012||Citation:||Debiasi, M.,Bouremel, Y.,Khoo, H.H.,Luo, S.C. (2012). Deformation of the upper surface of an airfoil by macro fiber composite actuators. 30th AIAA Applied Aerodynamics Conference 2012 : 1911-1922. ScholarBank@NUS Repository.||Abstract:||In this follow-on study, macro fiber composite actuators are used to change the shape of the upper surface of an airfoil model with geometry close to that of the NACA 4415 type. 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 surface of the airfoil. The model used in this study incorporates some structural changes that allow a smoother shaping of the surface closer to the leading edge of the airfoil. Still-air and wind-tunnel measurements in different flow regimes are performed to assess the characteristics of the deformation of the upper surface. The results obtained can be used to design a wing with morphing upper surface for improved aerodynamics, for maneuvering without ailerons, and/or for active control of the flow over the wing. © 2012 by Temasek Laboratories - National University of Singapore.||Source Title:||30th AIAA Applied Aerodynamics Conference 2012||URI:||http://scholarbank.nus.edu.sg/handle/10635/73312||ISBN:||9781624101854|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Sep 8, 2019
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.