A forced ignition probability analysis method using kernel formation analysis with turbulent transport and Lagrangian flame particle tracking
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作者:
Qing XIE
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机构:
School of Aerospace Engineering, Tsinghua UniversitySchool of Aerospace Engineering, Tsinghua University
Qing XIE
[1
]
Zhuyin REN
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机构:
School of Aerospace Engineering, Tsinghua University
Institute for Aero Engine, Tsinghua UniversitySchool of Aerospace Engineering, Tsinghua University
Zhuyin REN
[1
,2
]
Ke WANG
论文数: 0引用数: 0
h-index: 0
机构:
Aero Engine Academy of ChinaSchool of Aerospace Engineering, Tsinghua University
Ke WANG
[3
]
Hongjun LIN
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机构:
AECC Shenyang Engine Research InstituteSchool of Aerospace Engineering, Tsinghua University
Hongjun LIN
[4
]
Shoutang SHANG
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机构:
AECC Shenyang Engine Research InstituteSchool of Aerospace Engineering, Tsinghua University
Shoutang SHANG
[4
]
Wei XIAO
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机构:
AECC Hunan Aviation Powerplant ResearchSchool of Aerospace Engineering, Tsinghua University
Wei XIAO
[5
]
机构:
[1] School of Aerospace Engineering, Tsinghua University
[2] Institute for Aero Engine, Tsinghua University
A forced ignition probability analysis method is developed for turbulent combustion, in which kernel formation is analyzed with local kernel formation criteria, and flame propagation and stabilization are simulated with Lagrangian flame particle tracking. For kernel formation, the effect of turbulent scalar transport on flammability is modelled through the incorporation of turbulenceinduced diffusion in a spherically outwardly propagating flame kernel model. The dependence of flammability limits on turbulent intensities is tabulated and serves as the flammability criterion for kernel formation. For Lagrangian flame particle tracking, flame particles are tracked in a structured grid with flow fields being interpolated from a Computational Fluid Dynamics(CFD) solution. The particle velocity follows a Langevin model consisting of a linear drift and an isotropic diffusion term. The Karlovitz number is employed for the extinction criterion, which compares chemical and turbulent timescales. The integration of the above two-step analysis approach with non-reacting CFD is achieved through a general interpolation interface suitable for general unstructured CFD grids. The method is demonstrated for a methane/air bluff-body flame, in which flow and fuel/air mixing characteristics are extracted from a non-reacting simulation. Results show that the computed ignition probability map agrees qualitatively with experimental results. A reduction of the ignition probability in the recirculation zone and a high ignition probability on the shear layer of the recirculation zone near the mean stoichiometric surface are well captured. The tools can facilitate optimization of spark placement and offer insights into ignition processes.
机构:
School of Aerospace Engineering, Tsinghua UniversitySchool of Aerospace Engineering, Tsinghua University
Qing XIE
Zhuyin REN
论文数: 0引用数: 0
h-index: 0
机构:
School of Aerospace Engineering, Tsinghua University
Institute for Aero Engine, Tsinghua UniversitySchool of Aerospace Engineering, Tsinghua University
Zhuyin REN
Ke WANG
论文数: 0引用数: 0
h-index: 0
机构:
Aero Engine Academy of ChinaSchool of Aerospace Engineering, Tsinghua University
Ke WANG
Hongjun LIN
论文数: 0引用数: 0
h-index: 0
机构:
AECC Shenyang Engine Research InstituteSchool of Aerospace Engineering, Tsinghua University
Hongjun LIN
Shoutang SHANG
论文数: 0引用数: 0
h-index: 0
机构:
AECC Shenyang Engine Research InstituteSchool of Aerospace Engineering, Tsinghua University
Shoutang SHANG
Wei XIAO
论文数: 0引用数: 0
h-index: 0
机构:
AECC Hunan Aviation Powerplant Research InstituteSchool of Aerospace Engineering, Tsinghua University
机构:
Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R China
Xiang, Yuanyun
Wu, Yuyang
论文数: 0引用数: 0
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机构:
Aero Engine Corp China, Sichuan Gas Turbine Estab, Chengdu, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R China
Wu, Yuyang
Zhou, Sunyu
论文数: 0引用数: 0
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机构:
Aero Engine Corp China, Sichuan Gas Turbine Estab, Chengdu, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R China
Zhou, Sunyu
Li, Wei
论文数: 0引用数: 0
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机构:
Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R China
Li, Wei
Yan, Yingwen
论文数: 0引用数: 0
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机构:
Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R ChinaNanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Nanjing, Peoples R China