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

• المؤلفون الرئيسيون: Wei, Zhaoyu, New, Tze How, Lian, Lian, Zhang, Yanni
• مؤلفون آخرون: School of Mechanical and Aerospace Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2020
• الموضوعات: Engineering::Mechanical engineering; SD7032; Leading-edge Tubercles
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/143072

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...