Dynamic Mode Analysis on Internally-Staged-Swirling Stratified Premixed Flame
1.National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Energy and Power Engineering,Beihang University,Beijing100191,China;2.Collaborative Innovation Center for Advanced Aero-Engine,Beijing100191,China
[1] Dolan B,Villalva R,Munday D,et al.OH* Chemiluminescence in a Multipoint Combustion System: Steady State and Limit Cycle Behavior[R].ASMEGTP-18-1745.
[2] Han X,Hui X,Zhang C,et al.Combustion Instabilities in a Lean Premixed Pre-Vaporized Combustor at High-Pressure High-Temperature[R].ASME GT-2017-65190.
[3] 张 弛,王 波,邹鹏飞,等.同心旋流分层火焰的外激脉动特性统计学分析[J].航空动力学报,2017,32(8):1801-1808.
[4] Hochgreb S,Dennis D,Ayranci I,et al.Forced and Self-Excited Instabilities from Lean Premixed,Liquid-Fuelled Aeroengine Injectors at High Pressures and Temperatures[R].ASME GT-2013-95311.
[5] Fu X,Yang F,Guo Z.Combustion Instability of Pilot Flame in a Pilot Bluff Body Stabilized Combustor[J].Chinese Journal of Aeronautics,2015,28(6):1606-1615.
[6] Dolan B,Villalva R,Munday D,et al.Flame Dynamics in a Multi-Nozzle Staged Combustor During High Power Operation[R].ASME GT-2014-26164.
[7] Sundaram S S,Babu V.Numerical Investigation of Combustion Instability in a V-Gutter Stabilized Combustor[J].Journal of Engineering for Gas Turbines and Power,2013,135(12).
[8] Iudiciani P,Duwig C,Hosseini S,et al.Proper Orthogonal Decomposition for Experimental Investigation of Swirling Flame Instabilities[R].AIAA2010-584.
[9] Ryan P B,Ng W,Vandsburger U.Temperature Ratio Effects on Bluff-Body Wake Dynamics Using Large Eddy Simulation and Proper Orthogonal Decomposition[J].Journal of Engineering for Gas Turbines and Power,2015,137(12).
[10] Meadows J,Agrawal A K.Time-Resolved PIV of Lean Premixed Combustion Without and with Porous Inert Media for Acoustic Control[J].Combustion and Flame,2015,162(4):1063-1077.
[11] Sieber M,Oliver Paschereit C,Oberleithner K.Advanced Identification of Coherent Structures in Swirl-Stabilized Combustors[J].Journal of Engineering for Gas Turbines and Power,2016,139(2).
[12] St?hr M,Oberleithner K,Sieber M,et al.Experimental Study of Transient Mechanisms of Bistable Flame Shape Transitions in a Swirl Combustor[J].Journal of Engineering for Gas Turbines and Power,2017,139(1).
[13] Sieber M,Paschereit C,Oberleithner K.Identification of Unstable Coherent Modes in Reacting Swirling Flows and Their Control[R].AIAA2016-1840.
[14] Ghani A,M G L Y,Poinsot T.Acoustic Analysis of a Liquid Fuel Swirl Combustor Using Dynamic Mode Decomposition[R].ASME GT-2015-42769.
[15] Rajasegar R,Choi J,McGann B,et al.Comprehensive Combustion Stability Analysis Using Dynamic Mode Decomposition[J].Energy & Fuels,2018,32(9):9990-9996.
[16] Buschhagen T,Gejji R,Philo J,et al.Experimental Investigation of Self-Excited Combustion Instabilities in a Lean, Premixed, Gas Turbine Combustor at High Pressure[J].Journal of Engineering for Gas Turbines and Power,2018,140(11).
[17] Carlsson H,Carlsson C,Fuchs L,et al.Large Eddy Simulation and Extended Dynamic Mode Decomposition of Flow-Flame Interaction in a Lean Premixed Low Swirl Stabilized Flame[J].Flow,Turbulence and Combustion,2014,93(3):505-519.
[18] Ghani A,Poinsot T,Gicquel L,et al.LES of Longitudinal and Transverse Self-Excited Combustion Instabilities in a Bluff-Body Stabilized Turbulent Premixed Flame[J].Combustion and Flame,2015,162(11):4075-4083.
[19] Buschhagen T,Gejji R,Philo J,et al.Self-Excited Transverse Combustion Instabilities in a High Pressure Lean Premixed Jet Flame[J].Proceedings of the Combustion Institute,2019,37(4):5181-5188.
[20] Chen J,Hsu T Y ,Chen C C,et al.Monitoring Combustion Systems Using HMM Probabilistic Reasoning in Dynamic Flame Images[J].Applied Energy,2010,87(7):2169-2179.
[21] Sung H G.Combustion Dynamics in a Model Lean-Premixed Gas Turbine with a Swirl Stabilized Injector[J].Journal of Mechanical Science and Technology,2007,21(3):495-504.
[22] Ma X,Geisler R,Schr?der A.Experimental Investigation of Three-Dimensional Vortex Structures Downstream of Vortex Generators Over a Backward-Facing Step[J].Flow,Turbulence and Combustion,2017,98(2):3 89-415.
[23] Li M,Tong Y,Klingmann J,et al.Experimental Study of Hydrogen Addition Effects on a Swirl-Stabilized Methane-Air Flame[J].Energies,2017,10(1):1769-1785.
[24] Kim J,Lee C.Transition of Combustion Instability in Hybrid Rocket by Swirl Injection[J].Acta Astronautica,2018,158(1):323-333.
[25] Li Q,Wang Z.Dynamic Mode Decomposition of Turbulent Combustion Process in DLR Scramjet Combustor[J].Journal of Aerospace Engineering,2017,30(5).
[26] Tautschnig G,Hampel B,Hirsch C,et al.Experimental Investigation of OH* and CH* Chemiluminescence Under Varying Operating Conditions[R].ASME GT-2013-95850.
[27] 刘泽宇,张 弛,韩 啸,等.分层比对分开分层旋流预混火焰结构的影响 [J].航空学报,2018,39(3):78-88.
[28] Schmid P J,Li L,Juniper M P,et al.Applications of the Dynamic Mode Decomposition[J].Theoretical and Computational Fluid Dynamics,2011,25(1-4):249-259.
[29] Peter S.Dynamic Mode Decomposition of Numerical and Experimental Data[J].Journal of Fluid Mechanics,2010,656(10):5-28.
[30] Chen K K,Tu J H,Rowley,et al.Variants of Dynamic Mode Decomposition: Boundary Condition, Koopman, and Fourier Analyses[J].Journal of Nonlinear Science,2012,22(6):887-915.
[31] 童福林,李新亮,段焰辉.超声速压缩拐角激波边界层干扰动力学模态分解[J].航空学报,2017,38(12):86-97.
[32] 唐豪杰,高 原,朱 民.预混火焰传递函数的测量与分析[J].工程热物理学报,2011,32(1):173-176.
[33] Su J,Rupp J,Garmory A,et al.Measurements and Computational Fluid Dynamics Predictions of the Acoustic Impedance of Orifices[J].Joural of Sound and Vibration,2015,352(4):174-191.