Aerodynamic Performance and Surface Flow Structures of Leading-Edge Tubercled Tapered Swept-Back Wings

Effects of leading-edge tubercles on the aerodynamic performance and surface flow structures for tapered swept-back wings have been determined experimentally across a range of Reynolds numbers (Re). The orientation of SD7032 profile and tubercles were also particularly evaluated at Re=2.2×105. Lift...

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Main Authors: Wei, Zhaoyu, New, Tze How, Cui, Y. D.
其他作者: School of Mechanical and Aerospace Engineering
格式: Article
語言:English
出版: 2018
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在線閱讀:https://hdl.handle.net/10356/89380
http://hdl.handle.net/10220/44881
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機構: Nanyang Technological University
語言: English