Comparative Validation Study on Identification of Premixed Flame Transfer Function

被引:105
作者
Tay-Wo-Chong, Luis [1 ]
Bomberg, Sebastian [1 ]
Ulhaq, Ahtsham [1 ]
Komarek, Thomas [1 ]
Polifke, Wolfgang [1 ]
机构
[1] Tech Univ Munich, Lehrstuhl Thermodynam, D-85748 Garching, Germany
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2012年 / 134卷 / 02期
关键词
BOUNDARY-CONDITIONS; COMBUSTION; MODEL; SIMULATIONS; BURNER;
D O I
10.1115/1.4004183
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The flame transfer function (FTF) of a premixed swirl burner was identified from a time series generated with computational fluid dynamics simulations of compressible, turbulent, reacting flow at nonadiabatic conditions. Results were validated against experimental data. For large eddy simulation (LES), the dynamically thickened flame combustion model with one step kinetics was used. For unsteady simulation in a Reynolds-averaged Navier-Stokes framework (URANS), the Turbulent Flame Closure model was employed. The FTF identified from LES shows quantitative agreement with experiment for amplitude and phase, especially for frequencies below 200 Hz. At higher frequencies, the gain of the FTF is underpredicted. URANS results show good qualitative agreement, capturing the main features of the flame response. However, the maximum amplitude and the phase lag of the FTF are underpredicted. Using a low-order network model of the test rig, the impact of the discrepancies in predicted FTFs on frequencies and growth rates of the lowest order eigenmodes were assessed. Small differences in predicted FTFs were found to have a significant impact on stability limits. Stability behavior in agreement with experimental data was achieved only with the LES-based flame transfer function. [DOI: 10.1115/1.4004183]
引用
收藏
页数:8
相关论文
共 29 条
[11]   Impact of Swirl Fluctuations on the Flame Response of a Perfectly Premixed Swirl Burner [J].
Komarek, Thomas ;
Polifke, Wolfgang .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2010, 132 (06) :1-7
[12]   A model for the thermoacoustic response of a premixed swirl burner, - Part II: The flame response [J].
Lawn, CJ ;
Polifke, W .
COMBUSTION SCIENCE AND TECHNOLOGY, 2004, 176 (08) :1359-1390
[13]  
Leandro R., 2010, LOW ORDER MODELING T
[14]  
Legier J. P., 2000, P SUMM PROGR 2000 ST, P157
[15]  
Lieuwen T., 2005, Combustion Instabilities in Gas Turbine Engines-Operational Experience, Fundamental Mechanisms, and Modeling-Progress in Astronautics and Aeronautics
[16]  
Menter F., 2003, Turbulence, Heat and Mass Transfer, V4, P625
[17]   Subgrid-scale stress modelling based on the square of the velocity gradient tensor [J].
Nicoud, F ;
Ducros, F .
FLOW TURBULENCE AND COMBUSTION, 1999, 62 (03) :183-200
[18]   The combined dynamics of swirler and turbulent premixed swirling flames [J].
Palies, P. ;
Durox, D. ;
Schuller, T. ;
Candel, S. .
COMBUSTION AND FLAME, 2010, 157 (09) :1698-1717
[19]  
Poinsot T., 2012, Theoretical and Numerical Combustion, Vthird
[20]   BOUNDARY-CONDITIONS FOR DIRECT SIMULATIONS OF COMPRESSIBLE VISCOUS FLOWS [J].
POINSOT, TJ ;
LELE, SK .
JOURNAL OF COMPUTATIONAL PHYSICS, 1992, 101 (01) :104-129