1. 中国科学院 力学研究所 高温气体动力学国家重点实验室,北京,100190
2. 中国科学院大学 工程科学学院,北京,100049
吴坤(1990-), 男, 博士, 主要研究方向:湍流燃烧数值模拟, 化学反应机理简化, 射流与喷雾动力学.E-mail:wukun@imech.ac.cn
范学军(1967-), 男, 博士, 研究员, 博士生导师, 主要研究方向:吸热碳氢燃料热物性及燃烧特性, 燃烧室性能优化, 燃烧室热环境分析与再生冷却系统研究.E-mail:xfan@imech.ac.cn
纸质出版:2020
移动端阅览
吴坤, 范学军. 超声速燃烧数值模拟中复杂化学反应的建模方法[J]. 空气动力学学报, 2020, 38(3): 552-576.
WU Kun, FAN Xuejun. Modeling methodology for complex chemical mechanism involved in supersonic combustion simulation[J]. 2020, 38(3): 552-576.
吴坤, 范学军. 超声速燃烧数值模拟中复杂化学反应的建模方法[J]. 空气动力学学报, 2020, 38(3): 552-576. DOI: 10.7638/kqdlxxb-2020.0027.
WU Kun, FAN Xuejun. Modeling methodology for complex chemical mechanism involved in supersonic combustion simulation[J]. 2020, 38(3): 552-576. DOI: 10.7638/kqdlxxb-2020.0027.
高保真度的数值模拟有助于研究超声速条件下点火、熄火、火焰传播以及稳焰等关键物理-化学过程,推动对冲压发动机中复杂燃烧现象的准确理解与可靠预测。然而,实际发动机中碳氢燃料燃烧导致的广泛时空尺度对湍流燃烧的建模带来了极大的挑战。为此,必须首先解决超声速燃烧数值模拟中复杂化学反应的高保真建模问题。本文对超声速燃烧模拟中湍流-化学反应相互作用模型、机理简化以及求解加速方法的研究现状进行了总结。以典型燃料燃烧建模为主线,介绍了复杂化学反应的高保真建模方法以及不同化学反应机理在超燃模拟中的适用性及其影响。以反应机理三层次保真度评估体系为基础,进一步明确了简化机理在超燃数值模拟中的优势与不足,阐明了动态自适应化学方法在研究超声速条件下细致燃烧过程的必要性和可行性。
High-fidelity numerical simulation is considered as an indispensable approach to reveal key physical-chemical process such as ignition
extinction
flame propagation
and stabilization in supersonic flows
and promotes accurate understanding and reliable prediction of complex combustion phenomenon in ramjet engines. However
the extensive spatiotemporal scales caused by the combustion of hydrocarbon fuels in actual engines pose great challenges to turbulent combustion modeling. To overcome these challenges
high-fidelity modeling of complex chemistries in numerical simulation of supersonic combustion should be carefully handled. This paper gives a summary of the main research progresses in turbulence-combustion interaction model
mechanism reduction
and solution acceleration methods in supersonic combustion simulation. Taking typical fuels as prototypes
the high-fidelity modeling of complex chemistries
as well as applicability and influences of different chemical mechanisms in supersonic combustion are introduced. Based on the three-level fidelity evaluation methodology of chemical mechanism
the advantages and disadvantages of reduced mechanism are further clarified
and the necessity and feasibility of using dynamic adaptive chemistry method in the investigation of detailed combustion processes in supersonic flows are also elaborated.
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