Effects of leading-edge tubercles on wing flutter speeds

The dynamic aeroelastic effects on wings modified with bio-inspired leading-edge (LE) tubercles are examined in this study. We adopt a state-space aeroelastic model via the coupling of unsteady vortex-lattice method and a composite beam to evaluate stability margins as a result of LE tubercles on a...

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Main Authors: New, Tze How, Palacios, R., Ng, Bing Feng
其他作者: School of Mechanical and Aerospace Engineering
格式: Article
語言:English
出版: 2016
主題:
在線閱讀:https://hdl.handle.net/10356/80338
http://hdl.handle.net/10220/40684
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機構: Nanyang Technological University
語言: English