Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number

Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number

Flow separation characteristics for two tapered swept-back wings, one with straight leading-edge (LE) and the other with tubercled LE, were investigated in a water tunnel using time-resolved particle image velocimetry (TR-PIV) technique. The two wings were based on the SD7032 aerofoil profile, with...

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Bibliographic Details
Main Authors: Wei, Zhaoyu, New, Tze How, Lian, Lian, Zhang, Yanni
Other Authors: School of Mechanical and Aerospace Engineering
Format: Article
Language:English
Published: 2020
Subjects:
Engineering::Mechanical engineering
SD7032
Leading-edge Tubercles
Online Access:https://hdl.handle.net/10356/143072
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Institution: Nanyang Technological University
Language: English

Internet

https://hdl.handle.net/10356/143072

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