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首页> 外文期刊>Acta astronautica >Characteristics of methane-air continuous rotating detonation wave in hollow chambers with different diameters
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Characteristics of methane-air continuous rotating detonation wave in hollow chambers with different diameters

机译:具有不同直径的空腔中甲烷 - 空气连续旋转爆轰波的特性

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摘要

Due to the low chemical activity and large detonation cell size, methane-air continuous rotating detonation (CRD) is hard to be realized in a traditional small annular chamber without extra additives. In order to investigate the characteristics of methane-air CRD wave in a small chamber, three hollow chambers with Laval nozzles are adopted in this research. The methane-air CRD can be realized in a quite small chamber (diameter of 80 mm) under very particular condition. The operating range enlarges with the increase of chamber diameter. The CRD wave propagation frequencies vary apparently with chamber diameter while the propagation velocities stay in a quite narrow range of 1744-1812 m/s, and the relative deviation is within 4%. The CRD wave propagation process is very stable, and the propagation velocity accounts for 99% of the theoretical C-J velocity in the chosen test. Optical observation results illustrate that the reduction in chamber diameter or increase in nozzle contraction ratio will lead to CRD deterioration. By comparing the frequencies of high-frequency pressure and optical observations, the coupling of inducing shock wave and combustion flame is proved quantitatively.
机译:由于化学活性和大的爆轰电池尺寸,甲烷 - 空气连续旋转爆炸(CRD)在传统的小环形室中难以实现而无需额外的添加剂。为了研究小室中的甲烷 - 空气CRD波的特性,本研究采用了具有拉瓦尔喷嘴的三个空心室。甲烷 - 空气CRD可以在非常小的腔室(直径为80mm)的情况下实现。随着腔室直径的增加,运行范围将增大。 CRD波传播频率随着腔室直径而变化,而传播速度保持在1744-1812 m / s的相当窄范围内,并且相对偏差在4%范围内。 CRD波传播过程非常稳定,传播速度占所选择的测试中理论C-J速度的99%。光学观察结果说明腔室直径或喷嘴收缩比的增加将导致CRD劣化。通过比较高频压力和光学观察的频率,定量证明了诱导冲击波和燃烧火焰的耦合。

著录项

  • 来源
    《Acta astronautica》 |2021年第6期|1-10|共10页
  • 作者单位

    Natl Univ Def Technol Coll Aerosp Sci & Engn Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;

    Natl Univ Def Technol Coll Aerosp Sci & Engn Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;

    Natl Univ Def Technol Coll Aerosp Sci & Engn Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;

    Natl Univ Def Technol Coll Aerosp Sci & Engn Sci & Technol Scramjet Lab Changsha 410073 Hunan Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Methane-air; Continuous rotating detonation; Hollow chamber; Chamber diameter;

    机译:甲烷 - 空气;连续旋转爆轰;中空腔室;腔室直径;

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