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

被引:67
|
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
  • [31] The inertia force of insect-like flapping wing Micro Air Vehicle
    Zhu, Dan
    Wang, Qiang
    Hu, Minglang
    ADVANCES IN MATERIALS SCIENCE-BOOK, 2011, 327 : 186 - 192
  • [32] New pair of leading-edge vortex structure for flow over delta wing
    Wang, JJ
    Zhan, JX
    JOURNAL OF AIRCRAFT, 2005, 42 (03): : 718 - 721
  • [33] Petiolate wings: effects on the leading-edge vortex in flapping flight
    Phillips, Nathan
    Knowles, Kevin
    Bomphrey, Richard J.
    INTERFACE FOCUS, 2017, 7 (01)
  • [34] Leading-edge vortex dynamics on a slender oscillating wing
    Jun, Young-Whoon
    Nelson, Robert C.
    1600, (25):
  • [35] LEADING-EDGE VORTEX DYNAMICS ON A SLENDER OSCILLATING WING
    JUN, YW
    NELSON, RC
    JOURNAL OF AIRCRAFT, 1988, 25 (09): : 815 - 819
  • [36] Formation of vortices and spanwise flow on an insect-like flapping wing throughout a flapping half cycle
    Phillips, N.
    Knowles, K.
    AERONAUTICAL JOURNAL, 2013, 117 (1191): : 471 - 490
  • [37] Flow over a Wing with Leading-Edge Undulations
    Skillen, A.
    Revell, A.
    Pinelli, A.
    Piomelli, U.
    Favier, J.
    AIAA JOURNAL, 2015, 53 (02) : 464 - 472
  • [38] Leading-edge vortex burst on a low-aspect-ratio rotating flat plate
    Medina, Albert
    Jones, Anya R.
    PHYSICAL REVIEW FLUIDS, 2016, 1 (04):
  • [39] Efficient flexures for insect-like flapping-wing micro aerial vehicle
    Zou, Cai-Jun
    Zhang, Wei-Ping
    Ke, Xi-Jun
    Shao, Yun-Li
    Zhang, Wei
    Chai, Shuang-Shuang
    Hu, Nan
    Ye, Yi-Nan
    Chen, Wen-Yuan
    Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2014, 48 (03): : 439 - 444
  • [40] Adaptive attitude and position control of an insect-like flapping wing air vehicle
    Banazadeh, Afshin
    Taymourtash, Neda
    NONLINEAR DYNAMICS, 2016, 85 (01) : 47 - 66