多排盘可伸缩气刺气动特性研究

Hiroaki Kobayashi, Y. Maru, Tetsuya Sato
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引用次数: 0

摘要

本文报道了多盘伸缩气刺的实验研究。可伸缩的气动杆是一种有效的气动控制装置;然而,许多研究人员报告说,改变它的长度会引起嗡嗡声现象。嗡嗡声的发生可能对飞行器至关重要,因为它会在表面造成严重的压力振荡。轴上的圆盘通过将单个分离流划分为多个锥形腔流来产生稳定的再循环区。带稳定盘的可伸缩气刺在没有任何长度限制的情况下是有用的。通过一系列风洞试验,研究了可伸缩气刺的气动特性。普通尖峰的再循环/再附着流动模式的转变会导致阻力系数的较大变化。由于这种滞回现象和嗡嗡声,普通的脉冲不适合用于精细气动控制装置。增加稳定盘对改善气刺的控制是有效的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Aerodynamic Characteristics of Telescopic Aerospikes with Multiple-Row-Disk
This paper reports experimental studies on telescopic aerospikes with multiple disks. The telescopic aerospike is useful as an aerodynamic control device; however, changing its length causes a buzz phenomenon, which many researchers have reported. The occurrence of buzzing might be critical to the vehicle because it brings about severe pressure oscillations on the surface. Disks on the shaft produce stable recirculation regions by dividing the single separation flow into several conical cavity flows. The telescopic aerospikes with stabilizer disks are useful without any length constraints. Aerodynamic characteristics of the telescopic aerospikes were investigated through a series of wind tunnel tests. Transition of recirculation/reattachment flow modes of a plain spike causes a large change in the drag coefficient. Because of this hysteresis phenomenon and the buzzing, the plain spike is unsuitable for fine aerodynamic control devices. Adding stabilizer disks is effective for the improved control of aerospikes.
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