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arXiv 2312.04887physics.flu-dynphysics.app-ph
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预混射流火焰对爆炸波的响应

Response of premixed Jet Flames to Blast Waves

Akhil Aravind, Gautham Vadlamudi, Saptarshi Basu

AI总结:

本研究通过金属丝爆炸产生爆炸波,实验研究预混射流火焰沿轴响应,发现火焰抬升后依条件熄灭或再附着,并建立模型解释火焰基部抬升与尖端变形,揭示夹断机制。

摘要:

本研究探讨了预混射流火焰在沿射流轴线入射爆炸波时的响应动力学。在本工作中,采用金属丝爆炸技术产生爆炸波。产生的爆炸波与稳定在薄燃料-空气射流喷嘴上的预混射流火焰相互作用。研究在广泛的参数空间内进行,改变了预混射流的雷诺数($Re$)和归一化当量比($Φ$)以及产生的爆炸波前的强度($M_{s,r}$)。爆炸波施加了一个衰减的流场剖面,其特征是在爆炸波前处存在尖锐的不连续性。随后,随着爆炸引起的流场衰减到低于环境水平,由于周围环境的卷吸作用,产生了一个诱导流。虽然观察到射流火焰对爆炸波前产生抖动运动,但发现火焰在与诱导流相互作用后发生抬升。根据操作条件($Re$、$Φ$和$M_{s,r}$),火焰抬升后会发生熄灭或重新附着事件。根据相互作用后火焰基部和火焰尖端的响应动力学,火焰响应进一步分为两个重新附着子区域和三个熄灭子区域。火焰响应涉及火焰基部抬升和火焰尖端变形,可能根据操作条件导致火焰夹断事件。开发了一个数学模型来解释火焰基部响应动力学,得出了火焰基部抬升高度的标度律。通过扩展涡量输运方程来估计火焰周围剪切边界中的涡卷起速率,阐明了火焰尖端响应趋势。当剪切层涡达到临界环量极限并在低于火焰高度的长度尺度上脱落时,观察到火焰夹断。

英文摘要:

The study investigates the response dynamics of premixed jet flames when incident with blast waves along the jet axis. In the present work, blast waves are generated using the wire-explosion technique. The generated blast wave interacts with premixed jet flames that are stabilised over a thin fuel-air jet nozzle. The study is performed over a wide range of parametric space, varying the Reynolds number ($Re$) and normalised equivalence ratio ($Φ$) of the premixed jet and the strength of the generated blast fronts ($M_{s,r}$). The blast wave imposes a decaying flow field profile characterised by a sharp discontinuity at the blast front. This is accompanied by a subsequent induced flow arising due to entertainment from the surroundings as the blast-imposed flow fields decay to sub-ambient levels. While the jet flame is observed to respond to the blast front with a jittery motion, it is found to lift off following the interaction with the induced flow. Depending on the operating conditions ($Re$, $Φ$, and $M_{s,r}$), the flame lift-off is followed by an extinction or a re-attachment event. The flame response is further classified into two re-attachment and three extinction sub-regimes based on the response dynamics of the flame base and flame tip following the interaction process. The flame response entails flame base lift-off and flame tip distortion, potentially leading to a flame pinch-off event contingent on the operating conditions. A mathematical model was developed to explain the flame base response dynamics, yielding a scaling law for flame base lift-off height. Flame tip response trends were elucidated by extending the vorticity transport equation to estimate the vortex roll-up rate in the shear boundary surrounding the flame. Flame pinch-off was observed when shear layer vortices reached critical circulation limits and shed at length scales lower than the flame height.

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