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A reduced-order deterministic model describing an intermittency route to combustion instability

机译:简化的确定性模型,描述了燃烧不稳定性的间歇性路线

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Recently, there has been a growing interest in understanding and characterising intermittent burst oscillations that presage the onset of combustion instability. We construct a deterministic model to capture this intermittency route to instability in a bluff-body stabilised combustor by coupling the equations governing vortex shedding and the acoustic wave propagation in a confinement. A feedback mechanism is developed wherein the sound generated due to unsteady combustion affects the vortex shedding. This feedback leads to a variation in the time of impingement of the vortices with the bluff body causing the system to exhibit chaos, intermittency, and limit cycle oscillations. Experimental validation of the model is provided using various precursor measures that quantify the observed intermittent states.
机译:近来,人们对理解和表征间歇性突发振荡的兴趣日益增长,这些突发性突发振荡预示着燃烧不稳定性的开始。我们建立一个确定性模型,通过耦合控制涡旋脱落和声波在有限范围内传播的方程,来捕获在钝体稳定燃烧器中这种通往不稳定性的间歇性路径。开发了一种反馈机制,其中由于不稳定燃烧而产生的声音会影响涡旋脱落。该反馈导致涡流与钝体碰撞的时间发生变化,从而导致系统出现混乱,间歇性和极限循环振荡。使用各种量化观察到的间歇状态的前体测量值提供了模型的实验验证。

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