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 |
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其他作者: | School of Mechanical and Aerospace Engineering |
格式: | Article |
語言: | English |
出版: |
2016
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主題: | |
在線閱讀: | https://hdl.handle.net/10356/80338 http://hdl.handle.net/10220/40684 |
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