Large eddy simulation of fuel/air co-flow jet mixing enhancement in supersonic crossflow

IF 3 3区 工程技术 Q3 COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS
Xin Li, Yu Pan, Chaoyang Liu, Junbo Zou
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引用次数: 0

Abstract

Efficient mixing is critical for combustion organization in a high Mach number flows, and fuel/air co-flow jets continue to gain attention as a potential injection scheme. To further investigate the flow and mixing characteristics of co-flow transverse jets in a supersonic crossflow, high-fidelity Large Eddy Simulations are conducted by implementing a low numerical dissipation scheme. The reliability of the numerical method is confirmed by comparison with the experimental data. Then the effects of central air jet pressure, annular fuel jet pressure, and central jet activation/deactivation on the mixing process are systematically analyzed. Current research indicates that increasing central air jet pressure suppresses velocity fluctuations in the windward shear layer, while raising annular fuel jet pressure enhances mixing in this region. Deactivating the central jet introduces an additional recirculation zone, weakens jet penetration, reduces the leeward recirculation zone, and concentrates turbulent kinetic energy in the jet shear layer and wake. Mixing efficiency analysis shows that increasing central jet pressure or deactivating the central jet elevates downstream mixing efficiency to approximately 45 %, which is significantly better than the annular fuel jet pressurization scheme. Vortex dynamics investigation demonstrates that higher annular fuel jet pressure increases the average vorticity peak. The baroclinic term and the compressible dilatational stretching term show a bidirectional adjustment effect on the shear layer/wake region. Increased central jet pressure introduces supplementary air, raising the viscous term contribution to 48 % and significantly inhibiting vorticity growth. Furthermore, the vorticity stretching term and compressible dilatational stretching term dominate the vorticity generation and transport processes. This study provides theoretical foundations for enhancing the mixing performance of co-flow jet configurations.
超音速横流中燃油/空气共流射流混合增强的大涡模拟
在高马赫数流动中,高效混合对燃烧组织至关重要,燃油/空气共流射流作为一种潜在的喷射方案不断受到关注。为了进一步研究超声速横流中共流横向射流的流动和混合特性,采用低数值耗散格式进行了高保真大涡模拟。通过与实验数据的比较,验证了数值方法的可靠性。然后系统分析了中心空气喷射压力、环形燃料喷射压力和中心喷射激活/停用对混合过程的影响。目前的研究表明,中心气流压力的增加抑制了迎风切变层的速度波动,而环形燃油射流压力的提高则增强了该区域的混合。中央急流的失活引入了一个额外的再循环区,削弱了急流的穿透,减少了下风再循环区,并将湍流动能集中在急流切变层和尾流中。混合效率分析表明,增加中心射流压力或停用中心射流可使下游混合效率提高到45%左右,明显优于环形燃料射流增压方案。涡动力学研究表明,环空燃油射流压力越高,平均涡度峰值越大。斜压项和可压缩膨胀拉伸项对剪切层/尾流区有双向调节作用。增加的中心射流压力引入了补充空气,将粘性项贡献提高到48%,并显著抑制了涡度的增长。涡度拉伸项和可压缩膨胀拉伸项主导了涡度的产生和输送过程。该研究为提高共流射流构型的混合性能提供了理论依据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Computers & Fluids
Computers & Fluids 物理-计算机:跨学科应用
CiteScore
5.30
自引率
7.10%
发文量
242
审稿时长
10.8 months
期刊介绍: Computers & Fluids is multidisciplinary. The term ''fluid'' is interpreted in the broadest sense. Hydro- and aerodynamics, high-speed and physical gas dynamics, turbulence and flow stability, multiphase flow, rheology, tribology and fluid-structure interaction are all of interest, provided that computer technique plays a significant role in the associated studies or design methodology.
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