Wing-kinematics measurement and aerodynamics in a small insect in hovering flight

被引:61
|
作者
Cheng, Xin [1 ]
Sun, Mao [1 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Inst Fluid Mech, Beijing 100191, Peoples R China
来源
SCIENTIFIC REPORTS | 2016年 / 6卷
基金
中国国家自然科学基金;
关键词
LEADING-EDGE VORTEX; WEIS-FOGH MECHANISM; POWER REQUIREMENTS; FORCE GENERATION; FLOW STRUCTURE; MANDUCA-SEXTA; LIFT; DROSOPHILA; PERFORMANCE; CLAP;
D O I
10.1038/srep25706
中图分类号
O [数理科学和化学]; P [天文学、地球科学]; Q [生物科学]; N [自然科学总论];
学科分类号
07 ; 0710 ; 09 ;
摘要
Wing-motion of hovering small fly Liriomyza sativae was measured using high-speed video and flows of the wings calculated numerically. The fly used high wingbeat frequency (approximate to 265 Hz) and large stroke amplitude (approximate to 182 degrees); therefore, even if its wing-length (R) was small (R approximate to 1.4 mm), the mean velocity of wing reached approximate to 1.5m/s, the same as that of an average-size insect (R approximate to 3 mm). But the Reynolds number (Re) of wing was still low (approximate to 40), owing to the small wing-size. In increasing the stroke amplitude, the outer parts of the wings had a "clap and fling" motion. The mean-lift coefficient was high, approximate to 1.85, several times larger than that of a cruising airplane. The partial "clap and fling" motion increased the lift by approximate to 7%, compared with the case of no aerodynamic interaction between the wings. The fly mainly used the delayed stall mechanism to generate the high-lift. The lift-to-drag ratio is only 0.7 (for larger insects, Re being about 100 or higher, the ratio is 1-1.2); that is, although the small fly can produce enough lift to support its weight, it needs to overcome a larger drag to do so.
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页数:12
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