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https://scholarbank.nus.edu.sg/handle/10635/51646
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dc.title | Shape change of the upper surface of an airfoil by macro fiber composite actuators | |
dc.contributor.author | Debiasi, M. | |
dc.contributor.author | Bouremel, Y. | |
dc.contributor.author | Hock Hee, K. | |
dc.contributor.author | Siao Chung, L. | |
dc.contributor.author | Tan Zhiwei, E. | |
dc.date.accessioned | 2014-04-24T10:17:43Z | |
dc.date.available | 2014-04-24T10:17:43Z | |
dc.date.issued | 2011 | |
dc.identifier.citation | Debiasi, M.,Bouremel, Y.,Hock Hee, K.,Siao Chung, L.,Tan Zhiwei, E. (2011). Shape change of the upper surface of an airfoil by macro fiber composite actuators. 29th AIAA Applied Aerodynamics Conference 2011. ScholarBank@NUS Repository. | |
dc.identifier.isbn | 9781624101458 | |
dc.identifier.uri | http://scholarbank.nus.edu.sg/handle/10635/51646 | |
dc.description.abstract | Macro fiber composite actuators are used to displace inward or outward the upper surface of a NACA 4415 airfoil model. 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. Still-air and wind-tunnel measurements in different flow regimes were performed to assess the characteristics of static changes of the shape of the upper surface. The results obtained can be used to design a wing with morphing upper surfaces for improved aerodynamics, for maneuvering without ailerons, or for active control of the flow over the wing. © 2011 by Temasek Laboratories - National University of Singapore. Published by the American Institute of Aeronautics and Astronautics, Inc. | |
dc.source | Scopus | |
dc.type | Conference Paper | |
dc.contributor.department | TEMASEK LABORATORIES | |
dc.contributor.department | MECHANICAL ENGINEERING | |
dc.description.sourcetitle | 29th AIAA Applied Aerodynamics Conference 2011 | |
dc.identifier.isiut | NOT_IN_WOS | |
Appears in Collections: | Staff Publications |
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