基于双喉道Ludwieg管风洞稳定段的匀流加热融合设计

  • 荣国梁 ,
  • 杨逸帆 ,
  • 李创创 ,
  • 李志远 ,
  • 李学良 ,
  • 赵家权 ,
  • 吴杰
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  • 1. 华中科技大学航空航天学院
    2. 布里斯托大学
    3. 华中科技大学

收稿日期: 2024-07-04

  修回日期: 2024-08-23

  网络出版日期: 2024-08-26

Integrated design of flow homogenious mixing and heating based on dual-throat Ludwieg tube tunnel

  • RONG Guo-Liang ,
  • YANG Yi-Fan ,
  • LI Chuang-Chuang ,
  • LI Zhi-Yuan ,
  • LI Xue-Liang ,
  • ZHAO Jia-Quan ,
  • WU Jie
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Received date: 2024-07-04

  Revised date: 2024-08-23

  Online published: 2024-08-26

摘要

双喉道Ludwieg管风洞能够有效消除由快开阀开启带来的扰动,但会导致风洞的有效运行时间大幅降低。此外,受限于快开阀的材料,Ludwieg管风洞储气段加热温度提升困难。为了解决以上问题,本文提出一种在稳定段内放置环状加热器的改进方案,以实现风洞匀流与加热的融合设计。本文首先采用非定常数值模拟的方法验证了该气动布局的可行性;然后,分析了风洞的非定常启动过程,并定量研究了风洞运行过程中不同位置处马赫数与压强的变化特征,最后探究了加热器对风洞启动过程与稳定运行流场的影响。结果表明,带有稳定段加热的双喉道Ludwieg管风洞有效运行时间可达80ms,与传统双喉道布局相比风洞的有效运行时间提高了23%。同时,当加热器温度从434K提高到1234K时,喷管出口流场核心区域马赫数的最大偏差降低了0.21%,均方根偏差降低了0.005,温度提高了约40K,有效提高了Ludwieg管风洞的实验能力。

本文引用格式

荣国梁 , 杨逸帆 , 李创创 , 李志远 , 李学良 , 赵家权 , 吴杰 . 基于双喉道Ludwieg管风洞稳定段的匀流加热融合设计[J]. 航空学报, 0 : 0 -0 . DOI: 10.7527/S1000-6893.2024.30906

Abstract

The dual-throat Ludwieg tube tunnel can effectively eliminate disturbances caused by the opening process of the fast-acting valve, but it will significantly reduce the effective running time of wind tunnel. Additionally, due to the limi-tations of the material of the fast-acting valve, it is difficult to further increase the heating temperature of the storage section of the Ludwieg tube tunnel. To solve this problem, this paper proposes a novel design for the dual-throat Ludwieg tube wind tunnel by placing the annular heater in the settling chamber to achieve an integrated design of flow uniformity and heating. Firstly, the unsteady numerical simulation is used to verify the feasibility of the dual-throat Ludwieg wind tunnel with new layout. Then, the start-up characteristics was analyzed, and the variation of Mach number and pressure at different stations during the running is quantitatively studied. Finally, the effect of the heater on the running process of the tunnel is explored. The results show that the effective running time of dual-throat Ludwieg tube tunnel with a heater in the settling chamber up to 80 ms, which can be increased by 23% com-pared to the traditional dual-throat layout. Additionally, when the heater temperature is increased from 434K to 1234K, the maximum deviation of Mach number in the core region at the exit of the second nozzle can be de-creased by 0.21%, the root mean square deviation can be decreased by 0.005, and the temperature can be in-creased by nearly 40K, the testing capability of the wind tunnel effectively enhanced.

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