Temperature rise and pressure dynamics in the early stages of Hartmann–Sprenger tube operation

IF 1.7 4区 工程技术 Q3 MECHANICS
Y. Kudo, S. Sawada, N. Itouyama, K. Matsuoka, J. Kasahara
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Abstract

In this study, we focus on the early stages of the Hartmann–Sprenger tube operation in the jet regurgitant mode to investigate three key relationships: (1) between the nozzle dynamic pressure and the start time of temperature rise at the resonance tube end, (2) between the nozzle dynamic pressure and the resonance tube end pressure, and (3) between the distance l from the resonance tube end to the contact surface and the rise in the end gas temperature of the resonance tube. The results showed that the condition for the rise in the resonance tube end gas temperature after the gas jet from the nozzle reached sonic flow was the stabilization of the average fluctuation pressure value at the resonance tube end in conjunction with the nozzle dynamic pressure. At the time of operation stabilization of the Hartmann–Sprenger tube, the average fluctuation pressure at the resonance tube end converged to a constant value almost equal to the nozzle dynamic pressure. This result means that the nozzle dynamic pressure is almost equivalent to the fluctuation pressure at the resonance tube end. Moreover, the distance l did not significantly increase with the resonance tube length L and remained nearly constant. The gas temperature at the resonance tube end obtained from the experimental results generally agreed with the temperature calculated from compression through an adiabatic and isentropic process from L to l.

Hartmann-Sprenger管操作初期的温升和压力动态
在这项研究中,我们关注的初期阶段Hartmann-Sprenger管操作飞机回流的方式调查三个关键关系:(1)之间的动态压力和喷嘴温度上升的开始时间共鸣管一端,(2)动态压力和喷嘴之间的共鸣管一端的压力,和(3)之间的距离l共鸣管接触表面和共振的废气温度上升管。结果表明,喷管气体射流达到声速流动后,共振管端气体温度升高的条件是共振管端平均波动压力值与喷管动压力的稳定相结合。在Hartmann-Sprenger管稳定运行时,谐振管端平均波动压力收敛到一个几乎等于喷嘴动压力的恒定值。这意味着喷嘴动压力几乎等于谐振管端波动压力。距离l不随共振管长度l的增加而显著增加,基本保持不变。由实验结果得到的谐振管端气体温度与从L到L的绝热等熵压缩过程计算得到的温度基本一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Shock Waves
Shock Waves 物理-力学
CiteScore
4.10
自引率
9.10%
发文量
41
审稿时长
17.4 months
期刊介绍: Shock Waves provides a forum for presenting and discussing new results in all fields where shock and detonation phenomena play a role. The journal addresses physicists, engineers and applied mathematicians working on theoretical, experimental or numerical issues, including diagnostics and flow visualization. The research fields considered include, but are not limited to, aero- and gas dynamics, acoustics, physical chemistry, condensed matter and plasmas, with applications encompassing materials sciences, space sciences, geosciences, life sciences and medicine. Of particular interest are contributions which provide insights into fundamental aspects of the techniques that are relevant to more than one specific research community. The journal publishes scholarly research papers, invited review articles and short notes, as well as comments on papers already published in this journal. Occasionally concise meeting reports of interest to the Shock Waves community are published.
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