Large eddy simulations of turbulent premixed bluff body flames operated with ethanol, n-heptane, and jet fuels

IF 6.2 2区 工程技术 Q2 ENERGY & FUELS Combustion and Flame Pub Date : 2025-02-01 Epub Date: 2024-12-11 DOI:10.1016/j.combustflame.2024.113895
Arvid Åkerblom, Christer Fureby
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Abstract

Large Eddy Simulations (LES) are carried out targeting an unconfined premixed bluff body burner operated with ethanol, n-heptane, Jet A, and a Sustainable Aviation Fuel (SAF) labeled C1. The purpose is to validate the chosen simulation methodology for these fuels, which have not been simulated in the targeted case before, and to provide new information about how they burn and stabilize. The combustion of each fuel is modeled using Finite Rate Chemistry (FRC) and a pathway-centric chemical reaction mechanism. Subgrid-scale turbulence-chemistry interactions are modeled using a Partially Stirred Reactor (PaSR) approach. In accordance with previous experiments, snapshots of the OH and CH2O distributions, as well as velocity, are extracted from the simulations and subjected to statistical analysis to obtain mean flame progress variable distributions, flame surface density, and CH2O layer thickness. A mesh sensitivity analysis is carried out for all fuels, revealing that a crucial filter width threshold between 0.375 and 0.25 mm must be reached to achieve a stable flame and low mesh sensitivity. Statistically, the simulations show good agreement with previous experimental measurements. The flame sheet diameter is found to be approximately linearly correlated with extinction strain rate and Damköhler number, suggesting that resistance to turbulence is the determining factor for the flame size. The C1 flame is found to experience the weakest fluctuations, and a mechanism based on the relative time scales of flame propagation and the ignition of fuel decomposition products is proposed to explain this effect.
Novelty and significance statement
Sustainable aviation fuels are of major importance in reducing the climate impact of aviation, but their combustion is not nearly as well-understood as that of fossil jet fuels. Both experimental and numerical research is needed to map out the relationship between fuel composition and combustion performance, so that blending limits can be increased while guaranteeing safety, operability, and performance in aircraft engines. This work explores the turbulent flame dynamics of one commercial sustainable aviation fuel, C1. It is also the first numerical study to consider ethanol, n-heptane, Jet A, or C1 in the Cambridge bluff body burner, a case which has primarily been studied with methane. The results reveal several trends among the fuels which may be investigated further in future studies. C1 is found to be particularly resistant to outward fluctuations into the reactants, which connects fuel decomposition to flame stability.
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用乙醇、正庚烷和喷气燃料操作的紊流预混钝体火焰的大涡模拟
本文以乙醇、正庚烷、Jet A和标记为C1的可持续航空燃料(SAF)为燃料,对无限预混钝体燃烧器进行了大涡模拟(LES)。目的是验证这些燃料所选择的模拟方法,这些方法之前没有在目标情况下进行模拟,并提供关于它们如何燃烧和稳定的新信息。每种燃料的燃烧使用有限速率化学(FRC)和路径中心化学反应机理建模。采用部分搅拌反应器(PaSR)方法对亚网格尺度湍流-化学相互作用进行了建模。根据之前的实验,从模拟中提取OH和CH2O分布以及速度的快照,并进行统计分析,得到平均火焰进程变量分布、火焰表面密度和CH2O层厚度。对所有燃料进行了网格灵敏度分析,揭示了必须达到0.375和0.25 mm之间的关键过滤器宽度阈值才能实现稳定的火焰和低网格灵敏度。从统计上看,模拟结果与以往的实验结果吻合较好。发现火焰片直径与消光应变率和Damköhler数近似线性相关,表明湍流阻力是火焰尺寸的决定因素。发现C1火焰的波动最弱,并提出了基于火焰传播和燃料分解产物点火的相对时间尺度的机制来解释这种影响。新颖性和重要性声明可持续航空燃料在减少航空对气候的影响方面具有重要意义,但人们对其燃烧的了解远不如化石航空燃料。为了在保证飞机发动机的安全性、可操作性和性能的同时提高混合限值,需要通过实验和数值研究来确定燃料成分与燃烧性能的关系。这项工作探讨了一种商业可持续航空燃料C1的湍流火焰动力学。这也是第一个考虑乙醇、正庚烷、喷气机A或C1在剑桥钝体燃烧器中的数值研究,这种情况主要是用甲烷研究的。结果揭示了燃料之间的几个趋势,这些趋势可以在未来的研究中进一步研究。人们发现C1对反应物的向外波动具有特别的抵抗力,这将燃料分解与火焰稳定性联系起来。
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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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