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Aerodynamic interaction between forewing and hindwing of a hovering dragonfly 被引量:4
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作者 Zheng Hu Xin-Yan Deng 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2014年第6期787-799,共13页
The phase change between the forewing and hindwing is a distinct feature that sets dragonfly apart from other insects.In this paper,we investigated the aerodynamic effects of varying forewing-hindwing phase di ff eren... The phase change between the forewing and hindwing is a distinct feature that sets dragonfly apart from other insects.In this paper,we investigated the aerodynamic effects of varying forewing-hindwing phase di ff erence with a60 inclined stroke plane during hovering flight.Force measurements on a pair of mechanical wing models showed that in-phase flight enhanced the forewing lift by 17%and the hindwing lift was reduced at most phase differences.The total lift of both wings was also reduced at most phase di ff erences and only increased at a phase range around in-phase.The results may explain the commonly observed behavior of the dragonfly where 0 is employed in acceleration.We further investigated the wing-wing interaction mechanism using the digital particle image velocimetry(PIV)system,and found that the forewing generated a downwash flow which is responsible for the lift reduction on the hindwing.On the other hand,an upwash flow resulted from the leading edge vortex of the hindwing helps to enhance lift on the forewing.The results suggest that the dragonflies alter the phase di ff erences to control timing of the occurrence of flow interactions to achieve certain aerodynamic effects. 展开更多
关键词 Dragonfly aerodynamics forewing-hindwing interaction Phase di ff erence Interactive flow
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模型蜻蜓翼在是停状态的气动力特性实验研究
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作者 申功炘 朱百六 陆远 《军民两用技术与产品》 2008年第2期43-44,48,共3页
在静水中模拟了靖蜓(Aeschna juncea)在悬停状态的拍动运动,采用三分量的应变式天平分别测出前后翼之间的相位差值在0°、90°和180°三个值中变化时,两翼上的升力和阻力。得出三点结论:(1)在前后两翼以0°、90°和... 在静水中模拟了靖蜓(Aeschna juncea)在悬停状态的拍动运动,采用三分量的应变式天平分别测出前后翼之间的相位差值在0°、90°和180°三个值中变化时,两翼上的升力和阻力。得出三点结论:(1)在前后两翼以0°、90°和180°三种相位差拍动时,两翼之间的相互干扰对升力的产生是有害的;(2)后翼所受的干扰比前翼大;(3)后翼领先前翼1/4个周期拍动时所产生的升力最大,而反相拍动时所产生的升力最小。 展开更多
关键词 干扰 悬停状态 测力实验 应变式天平 模型蜻蜓翼 气动力特性
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