Numerical investigations of two-phase spray combustion flow fields in slinger annular combustor
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Numerical investigations of two-phase spray combustion flow fields in slinger annular combustor
Vol. 26, Issue 5, (2011)
作者机构:
1. 南京航空航天大学 能源与动力学院,南京,210016
2. 中国航空工业集团公司 中国航空动力机械研究所,湖南,株洲,412002
作者简介:
基金信息:
DOI:
CLC:
Published:2011
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YAN Ying-wen, SONG Shuang-wen, HU Hao-sheng, et al. Numerical investigations of two-phase spray combustion flow fields in slinger annular combustor[J]. 2011, 26(5).
DOI:
YAN Ying-wen, SONG Shuang-wen, HU Hao-sheng, et al. Numerical investigations of two-phase spray combustion flow fields in slinger annular combustor[J]. 2011, 26(5).DOI:
Numerical investigations of two-phase spray combustion flow fields in slinger annular combustor
numerical investigations of three-dimensional two-phase spray combustion flow fields for a slinger annular combustor were carried out.Three-dimensional body-fitted grids were generated by TTM (Thompson-Thames-Martin) method
k-ε model was used to simulate the turbulent viscosity;EBU (eddy break-up ) -Arrhenius combustion model
EDC (eddy dissipation concept) combustion model and SOM (second-order-moment) combustion model were applied to predict turbulent combustion rate.The gas and liquid phases were treated with Eulerian-Lagrangian method and the gas-liquid coupling was calculated with PSIC (particle-source-in-cell) arithmetic.The effects of different combustion models on two-phase spray combustion flow fields were studied.The numerical results are in good agreement with the experimental data.It shows that all of the combustion models are used to simulate the combustion process in slinger annular combustor
but the SOM combustion model and EBU combustion model are better than EDC combustion model for simulation of two-phase spray combustion flow fields in the slinger annular combustor.
Numerical investigation of two-phase spray combustion performance for LPP low-emission combustor
Numerical study and verification on combustion characteristics of afterburner with chevron mixer
Application of the Elliptic-Type Conditional Moment Closure Method to Turbulent Diffusion Bluff-Body Flames
考虑多源不确定性的复合材料风扇叶片高周疲劳失效概率评估
组合式弹性金属密封泄漏特性实验研究与结构优化
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Related Institution
Jiangsu Province Key Laboratory of Aerospace Power Systems, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
the Fifth Electronics Research Institute, Ministry of Industry and Information Technology of the Peoples Republic of China
Shenyang Aeroengine Research Institute, Aviation Industry Corporation of China
Beijing University of Aeronautics and Astronautics