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The effects that changes in the diaphragm aperture have on the resulting shock tube flow

机译:膜片孔径的变化对所产生的冲击管流量的影响

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摘要

In a conventional shock tube, the driver and the driven sections have similar (if not identical) cross-sectional area and the diaphragm opened area, upon rupturing, is practically equal to the tube cross-sectional area. Such geometry results in generating a well-formed shock wave in the tube’s driven section. The present experimental work checks the effects that changes in the diaphragm ruptured area have on the generated shock and rarefaction waves. Experiments were conducted in an 80 mm by 80 mm cross section shock tube generating incident shock waves having Mach numbers within the range from 1.06 to 1.25. In each run, pressure histories were recorded along the driven and the driver sections of the shock tube. The recorded pressures reveal that progressive reduction in the diaphragm open space resulted in a weaker shock and both longer time and distance until the compression waves generated close to the diaphragm coalesces into a shock wave. In addition, reducing the open space of the diaphragm resulted in a significant slow down in the high pressure reduction prevailing in the driver section.
机译:在传统的减震管中,驱动器和从动部具有相似(如果不相同)的横截面积,并且膜片的开口面积在破裂时实际上等于管的横截面积。这种几何形状会在管子的驱动部分中产生形式良好的冲击波。本实验工作检查了隔膜破裂区域的变化对所产生的冲击波和稀疏波的影响。实验在横截面为80 mm x 80 mm的激波管中进行,产生的马赫数在1.06至1.25范围内的入射激波。在每次运行中,沿冲击管的驱动部分和驱动部分记录压力历史记录。记录的压力表明,隔膜开口空间的逐渐减小会导致较弱的冲击,以及更长的时间和距离,直到靠近隔膜产生的压缩波合并为冲击波为止。另外,减小隔膜的开放空间导致驱动器部分中普遍存在的高压下降显着减慢。

著录项

  • 来源
    《Shock Waves》 |2012年第4期|p.287-293|共7页
  • 作者单位

    IUSTI-CNRS, Aix-Marseille Université, 5 rue Enrico Fermi, 13013, Marseille, France;

    IUSTI-CNRS, Aix-Marseille Université, 5 rue Enrico Fermi, 13013, Marseille, France;

    IUSTI-CNRS, Aix-Marseille Université, 5 rue Enrico Fermi, 13013, Marseille, France;

    Department of Mechanical Engineering, Ben Gurion University of the Negev, Beer Sheva, Israel;

    IUSTI-CNRS, Aix-Marseille Université, 5 rue Enrico Fermi, 13013, Marseille, France;

    AIRBUS Operations SAS, CoC Powerplant, M01125, 316 route de Bayonne, 31060, Toulouse, France;

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  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Shock wave; Shock tube; Shock wave formation;

    机译:激波;激波管;激波形成;

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