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首页> 外文期刊>Experiments in Fluids >High-speed stereo DPIV measurement of wakes of two bat species flying freely in a wind tunnel
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High-speed stereo DPIV measurement of wakes of two bat species flying freely in a wind tunnel

机译:高速立体DPIV测量在风洞中自由飞行的两种蝙蝠的尾迹

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Previous studies on wake flow visualization of live animals using DPIV have typically used low repetition rate lasers and 2D imaging. Repetition rates of around 10 Hz allow ~1 image per wingbeat in small birds and bats, and even fewer in insects. To accumulate data representing an entire wingbeat therefore requires the stitching-together of images captured from different wingbeats, and at different locations along the wing span for 3D-construction of wake topologies. A 200 Hz stereo DPIV system has recently been installed in the Lund University wind tunnel facility and the high-frame rate can be used to calculate all three velocity components in a cube, whose third dimension is constructed using the Taylor hypothesis. We studied two bat species differing in body size, Glossophaga soricina and Leptonycteris curasoa. Both species shed a tip vortex during the downstroke that was present well into the upstroke, and a vortex of opposite sign to the tip vortex was shed from the wing root. At the transition between upstroke/downstroke, a vortex loop was shed from each wing, inducing an upwash. Vorticity iso-surfaces confirmed the overall wake topology derived in a previous study. The measured dimensionless circulation, Γ/Uc, which is proportional to a wing section lift coefficient, suggests that unsteady phenomena play a role in the aerodynamics of both species.
机译:先前关于使用DPIV对活体动物进行尾流可视化的研究通常使用低重复频率激光和2D成像。大约10 Hz的重复频率在小鸟和蝙蝠的每个拍子中可得到约1张图像,在昆虫中则更少。因此,要累积表示整个机翼拍动的数据,需要将从不同机翼拍动捕获的图像拼接在一起,并沿着机翼跨度的不同位置进行拼接,以实现尾迹拓扑的3D构造。最近在隆德大学的风洞设施中安装了200 Hz立体声DPIV系统,高帧频可用于计算立方体中的所有三个速度分量,该立方体的第三维是使用泰勒假设构造的。我们研究了两种蝙蝠物种,它们的体型不同,分别是Glossophaga soricina和Leptonycteris curasoa。两种物种在向下的冲程中都掉落了一个顶涡,该涡一直存在于向上的冲程中,并且与翼尖涡旋相反的符号的涡旋从机翼根部脱落了。在上冲/下冲之间的过渡处,每个机翼都形成了涡流环,引起上冲。涡度等值面证实了先前研究得出的整体尾流拓扑。测得的无量纲循环Γ/ Uc与机翼截面升力系数成正比,表明不稳定现象在两个物种的空气动力学中都起作用。

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