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Performance enhancement of downwind sails due to leading edge flapping: A wind tunnel investigation

机译：由于领先的边缘拍打，下行风帆的性能提高：风洞调查

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N. Aubin; B. Augier; J. Deparday; M. Sacher; P. Bot;
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1. Performance enhancement of downwind sails due to leading edge flapping: A wind tunnel investigation [J] . Aubin N., Augier B., Deparday J., Ocean Engineering . 2018,第DECa1期

机译：由于前缘襟翼而提高了顺风帆的性能：风洞调查
2. Performance Evaluation of Vertical Axis Wind Turbine with a Leading Edge Flap [J] . K.K. Matrawy, Ayman A. Aly, A-F. Mahrous International Journal of Control, Automation and Systems . 2014,第1a4期

机译：带有前缘襟翼的垂直轴风力发电机的性能评估
3. Performance of wing sail with multi element by two-dimensional wind tunnel investigations [J] . Hiroyuki FURUKAWA, Alexander W. BLAKELEY, Richard G. J. FLAY, Journal of Fluid Science and Technology . 2015,第2期

机译：二维风洞研究多翼机翼风帆性能
4. Real-Time Adaptive Drag Minimization Wind Tunnel Investigation of a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System [C] . Nhan Nguyen, Nicholas Cramer, Kelley Hashemi, AIAA aviation forum . 2019

机译：可变弯度连续后缘襟翼系统的柔性机翼实时自适应风阻最小化风洞研究
5. Investigation of a Novel Turbulence Model and Using Leading-Edge Slots for Improving the Aerodynamic Performance of Airfoils and Wind Turbines. [D] . Beyhaghi, Saman. 2017

机译：研究新型湍流模型并使用前沿槽改善机翼和风力涡轮机的空气动力学性能。
6. Design Manufacturing and Testing of a New Concept for a Morphing Leading Edge using a Subsonic Blow Down Wind Tunnel [O] . David Communier, Franck Le Besnerais, Ruxandra Mihaela Botez, 2019

机译：设计制造和测试使用亚音速放空风洞的变形前沿的新概念
7. Numerical Investigation on the Effects of Airfoil Leading Edge Radius on the Aerodynamic Performance of H-Rotor Darrieus Vertical Axis Wind Turbine [O] . Chenguang Song, Guoqing Wu, Weinan Zhu, 2019

机译：翼型前缘半径对H-Royor Darrieus垂直轴风力涡轮机气动性能影响的数值研究
8. Wind-tunnel investigation at Mach numbers from 0.50 to 1.29 of an unswept, tapered wing of aspect ratio 2.67 with leading- and trailing-edge flaps - leading-edge flaps deflected [R] . Stivers, Louis S , Jr, Malick, Alexander W 1951

机译：风洞探测马赫数从0.50到1.29的未扫描，纵横比为2.67的锥形翼，带有前缘和后缘襟翼 - 前缘襟翼偏转

Performance enhancement of downwind sails due to leading edge flapping: A wind tunnel investigation

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