Numerical and experimental investigation of flame dynamics in opposed-flow solid fuel burner

IF 6.2 2区 工程技术 Q2 ENERGY & FUELS Combustion and Flame Pub Date : 2025-03-01 Epub Date: 2025-01-08 DOI:10.1016/j.combustflame.2024.113960
Ryan DeBoskey , Clayton Geipel , David Kessler , Brian Bojko , Brian Fisher , Ryan F. Johnson , Venkat Narayanaswamy
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Abstract

Understanding the complex coupled physics of phase change and turbulent gas-phase combustion in solid fuel combustors is critical to the design of advanced propulsion systems. This study considers the combustion of hydroxyl-terminated polybutadiene (HTPB) in an opposed-flow burner (OFB) configuration. High-speed shadowgraph imaging on the OFB is conducted to capture the unsteady flame dynamics surrounding the burner. Unsteady two-dimensional axisymmetric simulations, performed using a high-fidelity 20-species, 109-reaction pressure comprehensive skeletal kinetics mechanism, show improved agreement in the prediction of flame thickness in comparison to previous quasi-one-dimensional modeling, attributed to the significant deviation from self-similarity in the OFB configuration. Experimental and numerical data are compared showing strong trend-wise agreement and providing novel insight into the hitherto unexplored complex dynamics of the OFB configuration. Power spectral density (PSD) profiles of the flame oscillations demonstrate strong agreement in the broad peak frequency between simulations and experiments. PSD of flame thickness, regression rate, and azimuthal vorticity from the computed flame dynamics show strong coupling between the instantaneous regression rate and flame thickness, which is largely driven by the low-frequency vortex shedding from the OFB nozzle lip. Snapshots of the flowfield show a secondary diffusion flame with the majority of CO to CO2 oxidation downstream of the fuel grain edge. Variations in the species composition along the fuel surface highlight the complex balance between convective and diffusive forces arising from the proximity of the stagnation plane adjacent to the fuel surface.
Novelty and Significance Statement
This work utilizes large-eddy simulation (LES) to improve the prediction of flame thickness by 1000+% in an opposed flow solid fuel burner (OFB). Demonstration of significant deviation from self-similarity profiles highlight the limitations of current state-of-the art quasi one-dimensional modeling techniques and provides a viable strategy for predictive modeling of solid fuel combustion systems. Accurate prediction of heterogeneous combustion is a critical challenge limiting propellant and fuel discovery. Alongside validating experimental data, high-fidelity numerical simulations of heterogeneous combustion systems are of topical importance to advancing community understanding. High-fidelity modeling and experimental imaging gives unprecedented insight into the coupling between solid fuel combustion, unsteady flame dynamics, and unsteady fluid dynamics.
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固体燃料对流燃烧器火焰动力学的数值与实验研究
了解固体燃料燃烧室中相变和湍流气相燃烧的复杂耦合物理对先进推进系统的设计至关重要。本研究考虑了端羟基聚丁二烯(HTPB)在对流燃烧器(OFB)配置中的燃烧。采用高速阴影成像技术对燃烧器周围的非定常火焰动态进行了捕捉。利用高保真的20种物质、109种反应压力综合骨架动力学机制进行的非定常二维轴对称模拟显示,与之前的准一维模型相比,火焰厚度预测的一致性有所提高,这归因于OFB结构的自相似性存在显著偏差。实验和数值数据进行了比较,显示出强烈的趋势一致性,并为迄今为止尚未探索的OFB结构的复杂动力学提供了新的见解。火焰振荡的功率谱密度(PSD)曲线在宽峰值频率上与实验结果吻合较好。火焰动力学计算的火焰厚度、回归速率和方位角涡量的PSD表明,瞬时回归速率和火焰厚度之间存在较强的耦合,这主要是由OFB喷嘴唇部的低频涡脱落驱动的。流场的快照显示了二次扩散火焰,大部分CO在燃料颗粒边缘下游氧化成CO2。沿着燃料表面的物质组成的变化突出了对流和扩散力之间的复杂平衡,这是由燃料表面附近的停滞面引起的。本工作利用大涡模拟(LES)将对对流固体燃料燃烧器(OFB)火焰厚度的预测提高了1000+%。对自相似曲线的显著偏离的论证突出了当前最先进的准一维建模技术的局限性,并为固体燃料燃烧系统的预测建模提供了一种可行的策略。非均相燃烧的准确预测是限制推进剂和燃料发现的关键挑战。除了验证实验数据外,高保真的非均质燃烧系统数值模拟对于促进社区理解具有重要意义。高保真建模和实验成像为固体燃料燃烧,非定常火焰动力学和非定常流体动力学之间的耦合提供了前所未有的见解。
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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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