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: | , , |
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格式: | Article |
語言: | English |
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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 |