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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Bibliographic Details
Main Authors: Wei, Zhaoyu, New, Tze How, Cui, Y. D.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2018
Subjects:
Online Access:https://hdl.handle.net/10356/89380
http://hdl.handle.net/10220/44881
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Institution: Nanyang Technological University
Language: English
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