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Initiation and propagation of shock and detonation waves in gases due to power deposition.

机译:由于功率沉积,气体中的冲击波和爆震波的引发和传播。

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摘要

This thesis is in two parts. In part 'A' the problem of unsteady planar shock wave generation and propagation in an inert gas, confined between two infinite parallel plane walls, due to time-dependent power deposition at the boundary is investigated. A numerical solution is obtained for the system of Euler equations that describe the flow driven by the moving edge of an expanding conduction layer described by Clarke et al. (1984 b). The MacCormack finite-difference, explicit second-order accurate scheme is used with the Flux-Corrected Transport technique to reduce the oscillations that appear near the large gradients.; The results show that the numerical code is capable of capturing the shock wave with excellent accuracy. The results also show that the pressure and speed of the edge of the conduction layer increase as the power deposition at the boundary increases with time and accordingly, the shock speed and strength increase with time. The increase in the pressure level with time provides a source of compression heating to the gas contained in the conduction layer. This study indicates also that the fluid properties between the edge of the conduction layer and the generated shock wave are time and space-dependent.; In part 'B' the deflagration to detonation transition (DDT) and the unsteady behavior of the planar detonation wave is studied in a reactive mixture contained between two parallel plane walls. It is assumed that the gas undergoes a one-step exothermic chemical reaction with an Arrhenius law. The reactants and products behave as an ideal gas. The mixture is ignited by bulk power deposition of limited duration in a thin layer adjacent to the wall.; The resulting gas dynamic and chemical phenomena lead to the formation of several localized shock and combustion waves. An exothermic reaction center forms behind the lead shock. The forward moving front of the expanding reaction center drives a new shock wave which overtakes the lead shock. The coalesced shock is strong enough to induce a strongly coupled reaction zone in the gas just behind it. As a result, an over-driven detonation wave appears and exhibits oscillatory phenomena. This is associated with a time-dependent variation in the net chemical heat release and in the lead shock strength. The mean properties of the detonation asymptotes to the C.J. values for the gas considered.
机译:本论文分为两个部分。在“ A”部分中,研究了由于边界上随时间变化的功率沉积而限制在两个无限的平行平面壁之间的惰性气体中不稳定平面冲击波的产生和传播的问题。欧拉方程系统获得了一个数值解,该方程描述了由Clarke等人描述的扩展传导层的运动边缘驱动的流动。 (1984 b)。 MacCormack有限差分显式二阶精确方案与通量校正输运技术一起使用,可减少大梯度附近出现的振荡。结果表明,该数字编码器能够很好地捕获冲击波。结果还表明,导电层边缘的压力和速度随着边界处的功率沉积随时间增加而增加,因此,冲击速度和强度随时间增加。压力水平随时间的增加为传导层中所含的气体提供了压缩加热的来源。这项研究还表明,导电层边缘和所产生的冲击波之间的流体性质是时间和空间相关的。在“ B”部分中,研究了在两个平行平面壁之间包含的反应混合物中的爆燃到爆轰过渡(DDT)和平面爆震波的非稳态行为。假定气体按照阿伦尼乌斯定律进行了一步式放热化学反应。反应物和产物表现为理想的气体。通过在壁附近的薄层中以有限的持续时间进行大功率沉积来点燃混合物。产生的气体动力学和化学现象导致形成若干局部冲击波和燃烧波。铅冲击后会形成放热反应中心。不断扩大的反应中心向前移动的前部会驱动新的冲击波,该冲击波将超过前导冲击。凝聚的冲击足够强大,足以在其后面的气体中引起强烈耦合的反应区。结果,出现了过度驱动的爆炸波,并显示出振荡现象。这与净化学放热和引线冲击强度随时间的变化有关。爆炸的平均性能渐近至所考虑气体的C.J.值。

著录项

  • 作者

    Sileem, Ahmed Abdel-Mageed.;

  • 作者单位

    University of Colorado at Boulder.;

  • 授予单位 University of Colorado at Boulder.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 1989
  • 页码 166 p.
  • 总页数 166
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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