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Method of controlling aerodynamic characteristics of spiked flying object, and spiked flying object

机译:控制尖刺飞行物的空气动力学特性的方法以及尖刺飞行物

摘要

To provide a method of controlling the aerodynamic characteristics of a spiked flying object with an easy method without using a complicated variable mechanism or fluid energy supply system. A plurality of injection holes that are communicated with an internal channel are disposed on the front portion of a hollow shaft, and a valve for opening/closing an outlet section is disposed on the outlet section of the hollow shaft, to change either or both the opening/closing speed Vf of the valve and the duty ratio DR of the valve by means of a valve driver, whereby the aerodynamic characteristics of the hollow shaft are suitably controlled.
机译:提供一种不使用复杂的可变机构或流体能量供给系统而通过简单的方法来控制尖刺的飞行物体的空气动力特性的方法。在中空轴的前部设置有与内部通道连通的多个喷孔,在中空轴的出口部上设置有用于开闭出口部的阀,以改变一个或两个。借助于阀驱动器,阀的打开/关闭速度Vf和阀的占空比DR,由此适当地控制了空心轴的空气动力学特性。

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