Large eddy simulation/thickened flame model simulations of a lean partially premixed gas turbine model combustor

被引:11
作者
Zhang, Peiyu [1 ]
Park, Ji-Woong [1 ]
Wu, Bifen [1 ]
Zhao, Xinyu [1 ]
机构
[1] Univ Connecticut, Dept Mech Engn, Storrs, CT 06269 USA
关键词
Large-eddy simulation; gas turbine model combustor; thickened flame model; finite-rate chemistry; chemical explosive mode analysis; THICKENED FLAME; TURBULENT COMBUSTION; HEAT-TRANSFER; SWIRL FLAMES; JET FLAME; LES; CHEMISTRY; FLOW; INSTABILITIES; AUTOIGNITION;
D O I
10.1080/13647830.2021.1976421
中图分类号
O414.1 [热力学];
学科分类号
摘要
Large-eddy simulation with the thickened flame model (LES/TFM) is conducted to simulate a three-dimensional dual swirl partially premixed methane/air gas turbine model combustor. Finite-rate chemistry is described by a skeletal chemical mechanism consisting of 16 species and 41 reactions. Flame sensors based on formyl radical (HCO) and chemical explosive mode analysis (CEMA) are proposed and implemented within the TFM framework. The two sensors are designed for multi-step chemical kinetic models to avoid thickening the low-intensity heat release rate (HRR) region. One-dimensional freely-propagating laminar premixed flames are first employed to assess the two new sensors. The HCO-based sensor can successfully avoid the low-intensity HRR region for lean flames, but can fail under fuel-rich conditions. The CEMA-based sensor can robustly avoid low-intensity HRR regions under both fuel-lean and fuel-rich conditions. A second test case using a hydrogen/air reheat burner further demonstrates the robustness of the CEMA-based sensor. The two new sensors are subsequently applied to the gas turbine model combustor, and effects of different flame sensors are studied. Baseline results from the HCO-based sensor are first compared with experimental measurements to validate the LES/TFM solver. The mean and r.m.s. velocity, temperature, and mass fractions of O $ _{2} $ 2 and CO agree reasonably well with the experiment, although the mixture fraction within the inner recirculation zone (IRZ) is under-predicted. The predicted mean and r.m.s. temperature and species profiles are comparable at most locations, except near the IRZ where the CEMA-based sensor predicts the largest fluctuations by only thickening the chemically explosive regions. After optimisation, only 15% of overhead in computational cost is imposed when the CEMA sensor is employed on-the-fly. Future work includes further reduction of the computational cost of the CEMA-based sensor.
引用
收藏
页码:1296 / 1323
页数:28
相关论文
共 50 条
[1]   Direct numerical simulation of flame stabilization assisted by autoignition in a reheat gas turbine combustor [J].
Aditya, Konduri ;
Gruber, Andrea ;
Xu, Chao ;
Lu, Tianfeng ;
Krisman, Alex ;
Bothien, Mirko R. ;
Chen, Jacqueline H. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 37 (02) :2635-2642
[2]  
[Anonymous], 2016, CHEMK PRO 15151 REAC
[3]   Large-Eddy Simulation of the lean-premixed PRECCINSTA burner with wall heat loss [J].
Benard, P. ;
Lartigue, G. ;
Moureau, V ;
Mercier, R. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 37 (04) :5233-5243
[4]   Numerical investigation of turbulent swirling flames with validation in a gas turbine model combustor [J].
Benim, Ali Cemal ;
Iqbal, Sohail ;
Meier, Wolfgang ;
Joos, Franz ;
Wiedermann, Alexander .
APPLIED THERMAL ENGINEERING, 2017, 110 :202-212
[5]   Effects of mesh resolution on large eddy simulation of reacting flows in complex geometry combustors [J].
Boudier, G. ;
Gicquel, L. Y. M. ;
Poinsot, T. J. .
COMBUSTION AND FLAME, 2008, 155 (1-2) :196-214
[6]   Comparison of LES, RANS and experiments in an aeronautical gas turbine combustion chamber [J].
Boudier, G. ;
Gicquel, L. Y. M. ;
Poinsot, T. ;
Bissieres, D. ;
Berat, C. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2007, 31 :3075-3082
[7]   A power-law flame wrinkling model for LES of premixed turbulent combustion. Part I: Non-dynamic formulation and initial tests [J].
Charlette, F ;
Meneveau, C ;
Veynante, D .
COMBUSTION AND FLAME, 2002, 131 (1-2) :159-180
[8]   Large Eddy Simulation of a dual swirl gas turbine combustor: Flame/flow structures and stabilisation under thermoacoustically stable and unstable conditions [J].
Chen, Zhi X. ;
Langella, Ivan ;
Swaminathan, Nedunchezhian ;
Stoehr, Michael ;
Meier, Wolfgang ;
Kolla, Hemanth .
COMBUSTION AND FLAME, 2019, 203 :279-300
[9]   Interaction between self-excited oscillations and fuel-air mixing in a dual swirl combustor [J].
Chen, Zhi X. ;
Swaminathan, Nedunchezhian ;
Stoehr, Michael ;
Meier, Wolfgang .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 37 (02) :2325-2333
[10]   A thickened flame model for large eddy simulations of turbulent premixed combustion [J].
Colin, O ;
Ducros, F ;
Veynante, D ;
Poinsot, T .
PHYSICS OF FLUIDS, 2000, 12 (07) :1843-1863