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Unsteady aerodynamic forces and power requirements of a bumblebee in forward flight

机译:大黄蜂在向前飞行中的不稳定空气动力和动力需求

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Aerodynamic forces and power requirements in forward flight in a bumblebee (Bombus terrestris) were studied using the method of computational fluid dynamics. Actual wing kinematic data of free flight were used in the study (the speed ranges from 0 m/s to 4.5 m/s; advance ratio ranges from 0-0.66). The bumblebee employs the delayed stall mechanism and the fast pitching-up rotation mechanism to produce vertical force and thrust. The leading-edge vortex does not shed in the translatory phase of the half-strokes and is much more concentrated than that of the fruit fly in a previous study. At hovering and low-speed flight, the vertical force is produced by both the half-strokes and is contributed by wing lift; at medium and high speeds, the vertical force is mainly produced during the downstroke and is contributed by both wing lift and wing drag. At all speeds the thrust is mainly produced in the upstroke and is contributed by wing drag.The power requirement at low to medium speeds is not very different from that of hovering and is relatively large at the highest speed (advance ratio 0.66), i.e. the power curve is Jshaped. Except at the highest flight speed, storing energy elastically can save power up to 20%-30%. At the highest speed,because of the large increase of aerodynamic torque and the slight decrease of inertial torque (due to the smaller stroke amplitude and stroke frequency used), the power requirement is dominated by aerodynamic power and the effect of elastic storage of energy on power requirement is limited.
机译:利用计算流体动力学方法研究了大黄蜂(Bombus terrestris)向前飞行中的空气动力和动力需求。在研究中使用了实际的自由飞行机翼运动学数据(速度范围从0 m / s到4.5 m / s;超前比范围是0-0.66)。大黄蜂采用延迟失速机制和快速向上旋转机制来产生垂直力和推力。在先前的研究中,前沿涡流在半冲程的平移阶段不会掉落,并且比果蝇的涡流集中得多。在悬停和低速飞行时,垂直力由两个半冲程产生,并且由机翼升力贡献;在中高速时,垂直力主要在下冲程期间产生,并且由机翼升力和机翼阻力共同作用。在所有速度下,推力主要在上冲程中产生,并且是由机翼阻力贡献的。低速至中速时的动力需求与悬停动力需求没有太大不同,在最高速度时动力需求相对较大(前进比为0.66),即功率曲线为J型。除了最高的飞行速度外,弹性存储能量最多可以节省20%-30%的功率。在最高速度下,由于空气动力扭矩大幅度增加,并且惯性扭矩略有下降(由于使用了较小的行程幅度和行程频率),因此动力需求主要由空气动力和弹性储能所决定。电力需求是有限的。

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