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

• المؤلفون الرئيسيون: Wei, Zhaoyu, New, Tze How, Cui, Y. D.
• مؤلفون آخرون: School of Mechanical and Aerospace Engineering
• التنسيق: مقال
• اللغة: English
• منشور في: 2018
• الموضوعات: Surface Flow Structures; Aerodynamic Performance
• الوصول للمادة أونلاين: https://hdl.handle.net/10356/89380; http://hdl.handle.net/10220/44881
• المؤسسة: Nanyang Technological University

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...