Linear stability analysis of modal premixed combustor

被引:0
作者
20152801022769
机构
[1] National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing
来源
| 2015年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 30期
关键词
Bluff body flame holder; Combustion instability; Linear stability; Longitudinal mode; Premixed combustion; Vortex shedding;
D O I
10.13224/j.cnki.jasp.2015.05.010
中图分类号
学科分类号
摘要
Linear stability analysis was conducted in modal premixed combustor with bluff body flame holder. The software COMSOL Multiphysics was used to solve the three-dimensional Helmoholtz equation. The time lag model was the source term of equation. The periodic change of chemical reaction rate was studied by unsteady calculation for modal premixed combustor, and the unsteady heat release occurred at the top of the flame. The delay times of 0.6, 0.3, 0.9, 0.6 ms were obtained for equivalence ratios of 0.72, 0.8, 0.88 and 0.97 respectively in four cases based on the phase difference of pressure and temperature signals. The linear stability analysis obtained the real part and imaginary part of frequency of longitudinal mode for modal premixed combustor, and the negative imaginary part represented linear instability. The results show that the second, third, and fourth longitudinal modes are linear instability in the first five longitudinal modes. The imaginary part of the third longitudinal mode has the largest absolute value, indicating the largest growth rate in small disturbance. So there is the biggest possibility to occur linear unstable and combustion instability for the third longitudinal mode in disturbance. ©, 2015, BUAA Press. All right reserved.
引用
收藏
页码:1099 / 1105
页数:6
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