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Computational investigations of the coupling between transient flame dynamics and thermo-acoustic instability in a self-excited resonance combustor

机译:在自激共振燃烧器中瞬态火焰动态和热声不稳定性耦合的计算研究

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Combustion instability due to thermo-acoustic interactions is a critical combustion problem that requires a thorough understanding because of its adverse impact on stable and reliable operation of combustors in high-speed propulsion devices like gas turbines and rockets. This work conducts computational investigations of the coupling between the transient flame dynamics such as the ignition delay and local extinction and the thermo-acoustic instability developed in a self-excited resonance combustor to gain deep insights into the mechanisms of thermo-acoustic instability. A 2D modelling framework that employs different flamelet models (the steady flamelet model and the flamelet/progress variable approach) is developed to enable the examination of the effect of the transient flame dynamics caused by the strong coupling of the turbulent mixing and finite-rate chemical kinetics on the occurrence of thermo-acoustic instability. The models are validated by using the available experimental data for the pressure signal. Parametric studies are performed to examine the effect of the occurrence of the transient flame dynamics, the effect of artificial amplification of the Damkohler number, and the effect of neglecting mixture fraction fluctuations on the predictions of the thermo-acoustic instability. The parametric studies reveal that the occurrence of transient flame dynamics has a strong influence on the onset of the thermo-acoustic instability. Further analysis is then conducted to localise the effect of a particular flame dynamic event, the ignition delay, on the thermo-acoustic instability. The reverse effect of the occurrence of the thermo-acoustic instability on the transient flame dynamics in the combustor is also investigated by examining the temporal evolution of the local flame events in conjunction with the pressure wave propagation. The above observed two-way coupling between the transient flame dynamics (the ignition delay) and the thermo-acoustic instability p
机译:由于热声相互作用导致的燃烧不稳定性是一种关键的燃烧问题,这需要彻底了解,因为它对燃气轮机和火箭等高速推进装置的燃烧器稳定和可靠运行的不利影响。该工作对瞬态火焰动力学(例如点火延迟和局部灭火)之间的耦合以及在自激式共振燃烧器中产生的热声不稳定性进行了计算研究,以获得深入了解热声不稳定的机制。采用不同的爆震模型(稳定的轰动架模型和火焰/进展变量方法)采用不同的爆震模型(稳定的爆震模型和爆震/进展变量方法),以便检查湍流混合和有限速率化学的强耦合引起的瞬态火焰动力学的效果动力学发生在热声不稳定的情况下。通过使用用于压力信号的可用实验数据来验证模型。进行参数研究以检查发生瞬态火焰动力学的发生的效果,达到达摩尔数的人工扩增的影响,以及忽略混合分数波动对热声不稳定性的预测的影响。参数研究表明,瞬态火焰动态的发生对热声不稳定性的开始具有很大的影响。然后进行进一步分析以定位特定火焰动态事件,点火延迟对热声不稳定性的效果。还通过检查局部火焰事件的时间演变与压力波传播相结合,研究了在燃烧器中发生燃烧器中的瞬态火焰动力学的逆向效果。以上观察到瞬态火焰动力学(点火延迟)和热声不稳定P之间的双向耦合

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