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Wind tunnel test of Japanese arrows with the JAXA 60-cm magnetic suspension and balance system

机译:使用JAXA 60厘米磁悬浮和平衡系统对日本箭进行风洞测试

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In order to understand the aerodynamic properties of Japanese arrows, several types of shafts without fletching and various types of Japanese arrows were examined in a low-speed wind tunnel equipped with the JAXA 60-cm magnetic suspension and balance system. The main component of drag acting on the shaft is viscous drag from the boundary layer. This viscous drag can be evaluated analytically. A simple new method to estimate the effects of fletching on the lift of the arrow was proposed in which we found that lift is proportional to the angle of attack of the arrow but not to the rotation speed or angle. Time history results for the lift on rotating arrows in the magnetic suspension and balance system indicate that this method effectively estimates the lift on an actual rotating arrow in flight. The lift and pitching moment were mainly generated by fletching, and the drag from the fletching was similar in magnitude to that of the arrow shaft. For Japanese bamboo arrows tested with a field point, the drag, lift, and pitching moment coefficients were evaluated to be in the ranges of 3.5–3.7, 0.4–0.8, and −0.15 to −0.25, respectively, at Reynolds numbers of an arrow in flight.
机译:为了了解日式箭的空气动力学特性,在配备有JAXA 60厘米磁悬浮和平衡系统的低速风洞中,研究了几种无飞边的杆身和各种日式箭。作用在轴上的阻力的主要成分是来自边界层的粘性阻力。该粘性阻力可以通过分析来评估。提出了一种简单的新方法来估计跳动对箭头的升力的影响,其中我们发现升力与箭头的迎角成正比,而不与旋转速度或角度成正比。磁悬浮和平衡系统中旋转箭头上的升力的时间历史结果表明,该方法有效地估计了飞行中实际旋转箭头上的升力。升力和俯仰力矩主要是由飞掠产生的,并且从飞掠产生的阻力在大小上与箭杆相似。对于用视场点测试的日本竹箭,在箭的雷诺数下,阻力系数,升力系数和俯仰力矩系数分别估计在3.5–3.7、0.4–0.8和-0.15至-0.25的范围内在飞行中。

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