Park K J, Rosén M, Hedenström A
Department of Biological Sciences, University of Stirling, Stirling FK9 4LA, UK.
J Exp Biol. 2001 Aug;204(Pt 15):2741-50. doi: 10.1242/jeb.204.15.2741.
Two barn swallows (Hirundo rustica) flying in the Lund wind tunnel were filmed using synchronised high-speed cameras to obtain posterior, ventral and lateral views of the birds in horizontal flapping flight. We investigated wingbeat kinematics, body tilt angle, tail spread and angle of attack at speeds of 4-14 ms(-1). Wingbeat frequency showed a clear U-shaped relationship with air speed with minima at 8.9 ms(-1)(bird 1) and 8.7 ms(-1) (bird 2). A method previously used by other authors of estimating the body drag coefficient (C(D,par)) by obtaining agreement between the calculated minimum power (V(min)) and the observed minimum wingbeat frequency does not appear to be valid in this species, possibly due to upstroke pauses that occur at intermediate and high speeds, causing the apparent wingbeat frequency to be lower. These upstroke pauses represent flap-gliding, which is possibly a way of adjusting the force generated to the requirements at medium and high speeds, similar to the flap-bound mode of flight in other species. Body tilt angle, tail spread and angle of attack all increase with decreasing speed, thereby providing an additional lift surface and suggesting an important aerodynamic function for the tail at low speeds in forward flight. Results from this study indicate the high plasticity in the wingbeat kinematics and use of the tail that birds have available to them in order to adjust the lift and power output required for flight.
使用同步高速摄像机拍摄了在隆德风洞中飞行的两只家燕(Hirundo rustica),以获取鸟类水平扑翼飞行时的后部、腹部和侧面视图。我们研究了4-14米/秒速度下的翼拍运动学、身体倾斜角度、尾展和攻角。翼拍频率与空速呈现明显的U形关系,在8.9米/秒(鸟1)和8.7米/秒(鸟2)时达到最小值。其他作者先前使用的通过使计算出的最小功率(V(min))与观察到的最小翼拍频率达成一致来估计身体阻力系数(C(D,par))的方法,在该物种中似乎无效,这可能是由于在中高速时出现的上冲程停顿,导致明显的翼拍频率较低。这些上冲程停顿代表着扑翼滑翔,这可能是一种根据中高速时的需求来调整产生的力的方式,类似于其他物种的扑翼结合飞行模式。身体倾斜角度、尾展和攻角均随着速度降低而增加,从而提供了额外的升力表面,并表明在向前飞行的低速状态下,尾巴具有重要的空气动力学功能。本研究结果表明,鸟类在翼拍运动学和尾巴的使用方面具有高度可塑性,以便调整飞行所需的升力和功率输出。