Influence of different flap settings on the wake-vortex structure of a rectangular wing with flaps and means of alleviation with wing fins

Ingmar Schell; Erol Ozger; Dieter Jacob

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Influence of different flap settings on the wake-vortex structure of a rectangular wing with flaps and means of alleviation with wing fins

机译：不同襟翼设置对带有襟翼的矩形机翼尾流涡流结构的影响以及减轻翼鳍的手段

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This paper presents the results of an experimental investigation of the wake-vortex structure behind a flapped rectangular wing. The wind-tunnel test is part of a project funded by the German Research Association (DFG) to investigate the flow structure in the wake of wings with different flap extensions. The purpose of this investigation is to study the main features of lift generated vortices in order to find ways to alleviate hazardous wake vortex encounters for following airplanes during start and approach such that an increase in airport capacity can be achieved.

机译：本文介绍了拍打矩形机翼后面尾流涡流结构的实验研究结果。风洞试验是由德国研究协会（DFG）资助的项目的一部分，该项目旨在研究具有不同襟翼伸展度的机翼尾流后的流动结构。这项研究的目的是研究升力产生的涡流的主要特征，以找到减轻起步和进近过程中跟随飞机的危险尾流涡流的方法，从而实现机场容量的增加。

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来源
《Aerospace science and technology》 |2000年第2期|p.79-90|共12页
作者
Ingmar Schell; Erol Ozger; Dieter Jacob;
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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
原文格式 PDF
正文语种 eng
中图分类航空、航天;
关键词
flapped wing; wake structure; wake vortex alleviation;

机译：扑翼尾流结构;唤醒涡流缓解;

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机译：X-Wing单杆双翼形翼片翼翅片悬停控制性能分析
2. Analysis on Hover Control Performance of T- and Cross-Shaped Tail Fin of X-Wing Single-Bar Biplane Flapping Wing [J] . Pingxia Zhang, Junru Zhu, Yongqiang Zhu Journal of robotics . 2020,第2期

机译：X翼单条双翼形翼片翼翅片悬停控制性能分析
3. Studies on the influence of outboard flaps on the vortex wake of a rectangular wing [J] . S. Haverkamp, G. Neuwerth, D. Jacob Aerospace science and technology . 2003,第5期

机译：舷外襟翼对矩形机翼涡流影响的研究
4. Compliant Multifunctional Wing Structures for Flapping Wing MAVs [C] . Ariel Perez-Rosado, Alyssa Philipps, Eli Barnett, SEM Annual Conference Exposition on Experimental and Applied Mechanics . 2014

机译：符合扑翼Mavs的多功能翼结构
5. Experimental study on influence of wing rotation and damage on flapping wing aerodynamic performance. [D] . Huang, Qingfeng. 2012

机译：机翼旋转和损伤对襟翼气动性能影响的实验研究。
6. Three-dimensional wing structure attenuates aerodynamic efficiency in flapping fly wings [O] . Thomas Engels, Henja-Niniane Wehmann, Fritz-Olaf Lehmann 2020

机译：三维机翼结构在拍打飞翼时衰减空气动力学效率
7. STUDY OF THE INFLUENCE OF A GAP BETWEEN THE WING AND SLOTTED FLAP ON THE AERODYNAMIC CHARACTERISTICS OF ULTRA-LIGHT AIRCRAFT WING AIRFOIL [O] . Cvetelina VELKOVA, Michael TODOROV 2015

机译：研究机翼与开槽襟翼之间间隙对超轻型飞机翼翼型空气动力学特性的影响
8. ESTIMATION OF MINIMUM FIELD REQUIREMENTS OF TWO OVERLOADED, PROPELLER-DRIVEN, TILT-WING VTOL AIRCRAFT (INCLUDING THE EFFECTS OF FLAP SETTING, RUNWAY SURFACE,WIND, WING TILT RATE AND FLAP BOUNDARY LAYER CONTROL, [R] . neal, b. lyster, h. n. c. 1965

机译：两架超载，螺旋桨驱动，倾斜式垂直起飞飞机的最小现场要求的估算（包括翼片设置，跑道表面，风，翼倾斜率和襟翼边界层控制的影响，

Influence of different flap settings on the wake-vortex structure of a rectangular wing with flaps and means of alleviation with wing fins

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