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Numerical study of acoustic coupling in spinning detonation propagating in a circular tube

机译:圆管内旋转爆轰传播中声耦合的数值研究

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摘要

Spinning detonations propagating in a circular tube were numerically investigated with a two-step reaction model by Korobeinikov et al. The time evolutions of the simulation results were utilized to reveal the propagation behavior of single-headed spinning detonation. Three distinct propagation modes, steady, unstable, and pulsating modes, are observed in a circular tube. The track angles on a wall were numerically reproduced with various initial pressures and diameters, and the simulated track angles of steady and unstable modes showed good agreement with those of the previous reports. In the case of steady mode, transverse detonation always couples with an acoustic wave at the contact surface of burned and unburned gas and maintains stable rotation without changing the detonation front structure. The detonation velocity maintains almost a CJ value. We analyze the effect of acoustic coupling in the radial direction using the acoustic theory and the extent of Mach leg. Acoustic theory states that in the radial direction transverse wave and Mach leg can rotate in the circumferential direction when Mach number of unburned gas behind the incident shock wave in the transverse detonation attached coordinate is larger than 1.841. Unstable mode shows periodical change in the shock front structure and repeats decoupling and coupling with transverse detonation and acoustic wave. Spinning detonation maintains its propagation with periodic generation of sub-transverse detonation (new reaction front at transverse wave). Corresponding to its cycle, whisker is periodically generated, and complex Mach interaction periodically appears at shock front. Its velocity history shows the fluctuation whose behavior agrees well with that of rapid fluctuation mode by Lee et al. In the case of pulsating mode, as acoustic coupling between transverse detonation and acoustic wave is not satisfied, shock structure of spinning detonation is disturbed, which causes failure of spinning detonation.
机译:Korobeinikov等人使用两步反应模型对在圆管中传播的自旋爆炸进行了数值研究。利用仿真结果的时间演变来揭示单头旋转爆轰的传播行为。在圆形管中观察到三种不同的传播模式,稳定模式,不稳定模式和脉动模式。在各种初始压力和直径下,数值模拟了墙壁上的轨道角,并且稳态和不稳定模式的模拟轨道角与先前的报道显示出良好的一致性。在稳定模式下,横向爆炸总是在燃烧的和未燃烧的气体接触面与声波耦合,并在不改变爆炸前部结构的情况下保持稳定的旋转。爆震速度几乎保持CJ值。我们使用声学理论和马赫腿的延伸范围来分析径向声耦合的影响。声学理论认为,当横向爆震附加坐标中入射激波后面的未燃烧气体的马赫数大于1.841时,横波和马赫腿沿径向旋转。不稳定模式显示了冲击波前部结构的周期性变化,并与横向爆震和声波重复进行去耦和耦合。自旋爆轰会随着周期性产生的次横向爆轰(在横波处出现新的反应前沿)而保持其传播。与其周期相对应,晶须会定期产生,而复杂的马赫相互作用会周期性地出现在激波前沿。它的速度历史显示出波动,其行为与Lee等人的快速波动模式的行为非常吻合。在脉动模式的情况下,由于不满足横向爆震与声波之间的声耦合,因此破坏了旋转爆震的冲击结构,从而导致旋转爆震的失败。

著录项

  • 来源
    《Combustion and Flame》 |2013年第11期|2457-2470|共14页
  • 作者

    Yuta Sugiyama; Akiko Matsuo;

  • 作者单位

    Department of Mechanical Engineering, Keio University, Yokohama, 3-14-1 Hiyoshi, Kohoku-ku, Yokohama, Kanagawa, Japan;

    Department of Mechanical Engineering, Keio University, Yokohama, 3-14-1 Hiyoshi, Kohoku-ku, Yokohama, Kanagawa, Japan;

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

    Spinning detonation; Propagation mechanism; Detonation limit; CFD;

    机译:旋转爆炸传播机制;爆炸极限;差价合约;

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