Advanced Identification of Coherent Structures in Swirl-Stabilized Combustors

被引:36
作者
Sieber, Moritz [1 ]
Paschereit, Christian Oliver [1 ]
Oberleithner, Kilian [1 ]
机构
[1] Tech Univ Berlin, Chair Fluid Dynam, Hermann Fottinger Inst, Muller Breslau St 8, D-10623 Berlin, Germany
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2017年 / 139卷 / 02期
关键词
VORTEX CORE; DECOMPOSITION; JET;
D O I
10.1115/1.4034261
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
We present an application of a newly introduced method to analyze the time-resolved experimental data from the flow field of a swirl-stabilized combustor. This method is based on the classic proper orthogonal decomposition (POD) extended by a temporal constraint. The filter operation embedded in this method allows for continuous fading from the classic POD to the Fourier mode decomposition. This new method-called spectral proper orthogonal decomposition (SPOD)-allows for a clearer separation of the dominant mechanisms due to a clean spectral separation of phenomena. In this paper, the fundamentals of SPOD are shortly introduced. The actual focus is put on the application to a combustor flow. We analyze high-speed particle image velocimetry (PIV) measurements from flow fields in a combustor at different operation conditions. In these measurements, we consider externally actuated, as well as natural dynamics and reveal how the natural and actuated modes interact with each other. As shown in the paper, SPOD provides detailed insight into coherent structures in the swirl flames. Two distinct PVC structures are found that are very differently affected by acoustic actuation. The coherent structures are related to the heat release fluctuations, which are derived from simultaneously acquired OH* chemiluminescence measurements. Besides the actuated modes, a low frequency mode was found that significantly contribute to the global heat release fluctuations.
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页数:8
相关论文
共 18 条
[1]   Extended proper orthogonal decomposition:: a tool to analyse correlated events in turbulent flows [J].
Borée, J .
EXPERIMENTS IN FLUIDS, 2003, 35 (02) :188-192
[2]  
Holmes P., 1998, Cambridge Monographs on Mechanics
[3]  
HUANG HT, 1993, EXP FLUIDS, V15, P263
[4]   Nonlinear interaction between a precessing vortex core and acoustic oscillations in a turbulent swirling flame [J].
Moeck, Jonas P. ;
Bourgouin, Jean-Francois ;
Durox, Daniel ;
Schuller, Thierry ;
Candel, Sebastien .
COMBUSTION AND FLAME, 2012, 159 (08) :2650-2668
[5]   A hierarchy of low-dimensional models for the transient and post-transient cylinder wake [J].
Noack, BR ;
Afanasiev, K ;
Morzynski, M ;
Tadmor, G ;
Thiele, F .
JOURNAL OF FLUID MECHANICS, 2003, 497 :335-363
[6]   Three-dimensional coherent structures in a swirling jet undergoing vortex breakdown: stability analysis and empirical mode construction [J].
Oberleithner, K. ;
Sieber, M. ;
Nayeri, C. N. ;
Paschereit, C. O. ;
Petz, C. ;
Hege, H-C. ;
Noack, B. R. ;
Wygnanski, I. .
JOURNAL OF FLUID MECHANICS, 2011, 679 :383-414
[7]   Shear flow instabilities in swirl-stabilized combustors and their impact on the amplitude dependent flame response: A linear stability analysis [J].
Oberleithner, Kilian ;
Schimek, Sebastian ;
Paschereit, Christian Oliver .
COMBUSTION AND FLAME, 2015, 162 (01) :86-99
[8]   Measurement of transfer matrices and source terms of premixed flames [J].
Paschereit, CO ;
Schuermans, B ;
Polifke, W ;
Mattson, O .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2002, 124 (02) :239-247
[9]   VORTEX-DRIVEN ACOUSTICALLY COUPLED COMBUSTION INSTABILITIES [J].
POINSOT, TJ ;
TROUVE, AC ;
VEYNANTE, DP ;
CANDEL, SM ;
ESPOSITO, EJ .
JOURNAL OF FLUID MECHANICS, 1987, 177 :265-292
[10]   Increasing Flashback Resistance in Lean Premixed Swirl-Stabilized Hydrogen Combustion by Axial Air Injection [J].
Reichel, Thoralf G. ;
Terhaar, Steffen ;
Paschereit, Oliver .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2015, 137 (07)