The effect of aspect ratio on the leading-edge vortex over an insect-like flapping wing

被引:68
|
作者
Phillips, Nathan [1 ]
Knowles, Kevin
Bomphrey, Richard J. [1 ]
机构
[1] Univ London, Royal Vet Coll, Struct & Mot Lab, Hatfield AL9 7TA, Herts, England
基金
英国工程与自然科学研究理事会;
关键词
leading-edge vortex; flapping wing; micro air vehicle; aspect ratio; PARTICLE IMAGE VELOCIMETRY; LIFT-GENERATING MECHANISMS; MICRO AIR VEHICLES; REVOLVING WINGS; MODEL HAWKMOTH; MANDUCA-SEXTA; FLIGHT; AERODYNAMICS; VORTICES; FLOW;
D O I
10.1088/1748-3190/10/5/056020
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Insect wing shapes are diverse and a renowned source of inspiration for the new generation of autonomous flapping vehicles, yet the aerodynamic consequences of varying geometry is not well understood. One of the most defining and aerodynamically significant measures of wing shape is the aspect ratio, defined as the ratio of wing length (R) to mean wing chord ((c) over bar). We investigated the impact of aspect ratio, AR, on the induced flow field around a flapping wing using a robotic device. Rigid rectangular wings ranging from AR = 1.5 to 7.5 were flapped with insect-like kinematics in air with a constant Reynolds number (Re) of 1400, and a dimensionless stroke amplitude of 6.5 (c) over bar (number of chords traversed by the wingtip). Pseudo-volumetric, ensemble-averaged, flow fields around the wings were captured using particle image velocimetry at 11 instances throughout simulated downstrokes. Results confirmed the presence of a high-lift, separated flow field with a leading-edge vortex (LEV), and revealed that the conical, primary LEV grows in size and strength with increasing AR. In each case, the LEV had an arch-shaped axis with its outboard end originating from a focus-sink singularity on the wing surface near the tip. LEV detachment was observed for AR > 1.5 around mid-stroke at similar to 70% span, and initiated sooner over higher aspect ratio wings. At AR > 3 the larger, stronger vortex persisted under the wing surface well into the next half-stroke leading to a reduction in lift. Circulatory lift attributable to the LEV increased with AR up to AR= 6. Higher aspect ratios generated proportionally less lift distally because of LEV breakdown, and also less lift closer to the wing root due to the previous LEV's continuing presence under the wing. In nature, insect wings go no higher than AR similar to 5, likely in part due to architectural and physiological constraints but also because of the reducing aerodynamic benefits of high AR wings.
引用
收藏
页数:18
相关论文
共 50 条
  • [41] Volumetric measurement and vorticity dynamics of leading-edge vortex formation on a revolving wing
    Chen, Long
    Wu, Jianghao
    Cheng, Bo
    EXPERIMENTS IN FLUIDS, 2019, 60 (01)
  • [42] Numerical and experimental investigations of a nonslender delta wing with leading-edge vortex flap
    Cai, Jinsheng
    Pan, Shucheng
    Li, Wenfeng
    Zhang, Zhengke
    COMPUTERS & FLUIDS, 2014, 99 : 1 - 17
  • [43] Leading-edge curvature effect on aerodynamic performance of flapping wings in hover and forward flight
    Addo-Akoto, Reynolds
    Han, Jong-Seob
    Han, Jae-Hung
    BIOINSPIRATION & BIOMIMETICS, 2024, 19 (05)
  • [44] Study on altitude control of Insect-Like Flapping-Wing Micro Aerial Vehicle
    Zhang, Zheng
    Zhang, Wei-ping
    Ke, Xi-jun
    Zou, Yang
    Hu, Nan
    Wu, Fan
    PROCEEDINGS OF THE 2015 5TH INTERNATIONAL CONFERENCE ON COMPUTER SCIENCES AND AUTOMATION ENGINEERING, 2016, 42 : 785 - 790
  • [45] Indirect Control and Design of Insect-Like Flapping-Wing Micro Aerial Vehicle
    Dong Weizhong
    Wang Zhi Dong
    2017 IEEE 3RD INFORMATION TECHNOLOGY AND MECHATRONICS ENGINEERING CONFERENCE (ITOEC), 2017, : 1257 - 1263
  • [46] Numerical Simulation of the Streamwise Transport of a Delta Wing Leading-Edge Vortex
    Francois, Daniela G.
    Probst, Silvia
    Knopp, Tobias
    Grabe, Cornelia
    Landa, Tim
    Radespiel, Rolf
    JOURNAL OF AIRCRAFT, 2021, 58 (06): : 1281 - 1293
  • [47] Modeling and Improvement for String-Based Drive Mechanism in Insect-like Flapping Wing Micro Air Vehicle
    Ye, Ruiqi
    Liu, Ziming
    Cui, Jin
    Wang, Chenyang
    Wu, Yirong
    APPLIED SCIENCES-BASEL, 2023, 13 (24):
  • [48] Scaling trends of bird's alular feathers in connection to leading-edge vortex flow over hand-wing
    Linehan, Thomas
    Mohseni, Kamran
    SCIENTIFIC REPORTS, 2020, 10 (01)
  • [49] Three-dimensional flow structures and evolution of the leading-edge vortices on a flapping wing
    Lu, Yuan
    Shen, Gong Xin
    JOURNAL OF EXPERIMENTAL BIOLOGY, 2008, 211 (08) : 1221 - 1230
  • [50] Development of an Insect-like Flapping-Wing Micro Air Vehicle with Parallel Control Mechanism
    Chen, Zihao
    Zhang, Weiping
    Mou, Jiawang
    Zhao, Jiaxin
    APPLIED SCIENCES-BASEL, 2022, 12 (07):