Evolution dynamics and instability mechanisms of four-wave collisions in rotating detonation engines

IF 6.2 2区 工程技术 Q2 ENERGY & FUELS
Yuechen Hou, Peilin Liu, Yixiang Li, Yiting Dang, John Z. Ma, Jianping Wang
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引用次数: 0

Abstract

This study presents the first systematic investigation of instability mechanisms in four-wave collision regimes of rotating detonation engines (RDEs), within a methane/oxygen-enriched air (30%O2, 50%O2) annular combustor. Compared to two-wave collisions, four-wave collisions exhibit inherently unstable wave symmetry and heightened sensitivity to inflow variations: elevated oxygen enrichment, equivalence ratio, and mass flow rate induce detonation strength imbalance, driving progressive transitions from symmetric four-wave collisions with stationary collision points to inducing collision-point migration (CPM), asynchronous behaviors (Async 4CR), and eventual single-wave dominance. The Async 4CR regime is uniquely characterized by subharmonic components at half the dominant frequency, originating from temporal offsets between successive wave collisions. Its unstable transitions to single-wave modes involve amplified upstream pressure feedback and elevated wall temperature growth rates. To quantify these instabilities, an analytical framework combining pressure peak-interval calculation and auto-correlation was developed to correlate periodic peak bifurcation and CPM dynamics. A linear model linking pressure peak-interval to angular CPM deviations was established based on near-constant CPM velocities, enabling single-sensor tracking of time-resolved CPM trajectories. The nonlinear and stochastic nature of CPM was revealed, featuring arbitrary migration directions, diverse maximal deviation angles (20–45°), and irregular periods (5–39 ms). The model remains valid under temporally oscillating fuel inflow, capturing transiently amplified CPM angles and reduced detonation stability during fuel flow rise. These findings reveal the complex instabilities and mode evolution patterns of four-wave collision regimes in RDEs, critical for advancing mode control and evaluating RDE performance.
Novelty and significance
(1) This study resolved typical CPM patterns during mode evolutions associated with four-wave collision instabilities. Unstable asynchronous collision regimes unique to four-wave collision systems were identified for the first time. (2) The developed linear model enables quantitative reconstruction of time-resolved CPM trajectories through peak bifurcation analysis of easily-accessible single-sensor pressure, offering direct extensibility to two-wave collisions and other high-frequency signals. (3) The stochastic nature of CPM driven by nonlinear detonation dynamics was underscored, while providing the experimental evidence on the destabilizing effects of time-varying oscillating inflow.
旋转爆震发动机四波碰撞演化动力学及不稳定机制
本研究首次对旋转爆震发动机(RDEs)在甲烷/富氧空气(30%O2, 50%O2)环形燃烧室中的四波碰撞不稳定性机制进行了系统研究。与两波碰撞相比,四波碰撞表现出固有的不稳定波对称性和对流入变化的高度敏感性:氧浓度、等效比和质量流量的升高导致爆轰强度失衡,推动从具有固定碰撞点的对称四波碰撞逐步过渡到诱导碰撞点迁移(CPM)、异步行为(Async 4CR),最终形成单波优势。异步4CR体制的独特特征是,在连续波碰撞之间的时间偏移中,亚谐波分量占主导频率的一半。它向单波模式的不稳定转变涉及上游压力反馈放大和壁面温度增长率升高。为了量化这些不稳定性,开发了一个结合压力峰间隔计算和自相关的分析框架,将周期性峰分岔与CPM动力学联系起来。基于接近恒定的CPM速度,建立了将压力峰值间隔与角CPM偏差联系起来的线性模型,实现了单传感器对时间分辨CPM轨迹的跟踪。CPM的非线性和随机性表现为任意偏移方向、不同的最大偏移角(20 ~ 45°)和不规则周期(5 ~ 39 ms)。该模型在燃油流入时间振荡的情况下仍然有效,捕获了燃油流量上升过程中瞬时放大的CPM角和降低的爆轰稳定性。这些发现揭示了RDE中四波碰撞机制的复杂不稳定性和模式演化模式,这对于推进模式控制和评估RDE性能至关重要。(1)该研究解决了与四波碰撞不稳定性相关的模式演化过程中的典型CPM模式。首次确定了四波碰撞系统特有的不稳定异步碰撞状态。(2)开发的线性模型可以通过易于获取的单传感器压力的峰值分岔分析来定量重建时间分辨的CPM轨迹,并可直接扩展到两波碰撞和其他高频信号。(3)强调了非线性爆轰动力学驱动下CPM的随机性质,同时为时变振荡入流的失稳效应提供了实验证据。
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来源期刊
Combustion and Flame
Combustion and Flame 工程技术-工程:化工
CiteScore
9.50
自引率
20.50%
发文量
631
审稿时长
3.8 months
期刊介绍: The mission of the journal is to publish high quality work from experimental, theoretical, and computational investigations on the fundamentals of combustion phenomena and closely allied matters. While submissions in all pertinent areas are welcomed, past and recent focus of the journal has been on: Development and validation of reaction kinetics, reduction of reaction mechanisms and modeling of combustion systems, including: Conventional, alternative and surrogate fuels; Pollutants; Particulate and aerosol formation and abatement; Heterogeneous processes. Experimental, theoretical, and computational studies of laminar and turbulent combustion phenomena, including: Premixed and non-premixed flames; Ignition and extinction phenomena; Flame propagation; Flame structure; Instabilities and swirl; Flame spread; Multi-phase reactants. Advances in diagnostic and computational methods in combustion, including: Measurement and simulation of scalar and vector properties; Novel techniques; State-of-the art applications. Fundamental investigations of combustion technologies and systems, including: Internal combustion engines; Gas turbines; Small- and large-scale stationary combustion and power generation; Catalytic combustion; Combustion synthesis; Combustion under extreme conditions; New concepts.
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