Large eddy simulations for radiation-spray coupling for a lean direct injector combustor

被引:21
作者
El-Asrag, Hossam A. [1 ]
Iannetti, Anthony C. [2 ]
Apte, Sourabh V. [3 ]
机构
[1] Stanford Univ, Ctr Turbulence Res, Stanford, CA 94305 USA
[2] NASA, Glenn Res Ctr, Cleveland, OH USA
[3] Oregon State Univ, Dept Mech Engn, Corvallis, OR 97331 USA
关键词
Large eddy simulation; Radiation; Lean direct injection; Turbulent flames; Spray modeling; Stochastic secondary breakup; TURBULENCE; FLAMES; LES; EXTINCTION; REIGNITION; PREDICTION;
D O I
10.1016/j.combustflame.2013.09.020
中图分类号
O414.1 [热力学];
学科分类号
摘要
Large Eddy Simulations (LESs) for a lean-direct injection (LDI) combustor are performed and compared with experimental data. The LDI emissions characteristics, and radiation-spray coupling effect on the predictions are analyzed. The flamelet progress variable approach is employed for chemistry tabulation coupled with a stochastic secondary breakup model. Good comparisons are shown with the experimental data mean and root mean square for both the gas phase and spray droplets profiles. The effect of combustion is found to change the shape and structure of the central recirculation zone to be more compact in length but larger in diameter in the transverse direction. In-addition the results show that the gas phase radiation alters the spray dynamics by changing the local gas-phase temperature distribution. This impacts the spray evaporation rate, the local mixture fraction, and consequently the combustion heat released rate and the predicted emissions. The simulation with no radiation modeling shows over prediction in the temperature distribution, pollutants emissions, higher fuel evaporation rate, and narrower range of droplet size distribution with lower number density for the smaller size particles. The current study suggests that, even for low pressure systems, radiation modeling can be important for accurate emissions prediction. (C) 2013 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:510 / 524
页数:15
相关论文
共 63 条
[1]  
[Anonymous], 46 AIAA AER SCI M EX
[2]  
[Anonymous], 2006, COMBUSTION PHYS
[3]   Unsteady flow evolution and combustion dynamics of homogeneous solid propellant in a rocket motor [J].
Apte, S ;
Yang, V .
COMBUSTION AND FLAME, 2002, 131 (1-2) :110-131
[4]   Stochastic modeling of atomizing spray in a complex swirl injector using large eddy simulation [J].
Apte, Sourabh V. ;
Mahesh, Krishnan ;
Gorokhovski, Michael ;
Moin, Parviz .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2009, 32 :2257-2266
[5]   Large-eddy simulation of evaporating spray in a coaxial combustor [J].
Apte, Sourabh V. ;
Mahesh, Krishnan ;
Moin, Parviz .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2009, 32 :2247-2256
[6]   LES of atomizing spray with stochastic modeling of secondary breakup [J].
Apte, SV ;
Gorokhovski, M ;
Moin, P .
INTERNATIONAL JOURNAL OF MULTIPHASE FLOW, 2003, 29 (09) :1503-1522
[7]   Scalar profiles and NO formation in laminar opposed-flow partially premixed methane/air flames [J].
Barlow, RS ;
Karpetis, AN ;
Frank, JH ;
Chen, JY .
COMBUSTION AND FLAME, 2001, 127 (03) :2102-2118
[8]   ON REDUCED MECHANISMS FOR METHANE AIR COMBUSTION IN NONPREMIXED FLAMES [J].
BILGER, RW ;
STARNER, SH ;
KEE, RJ .
COMBUSTION AND FLAME, 1990, 80 (02) :135-149
[9]   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
[10]  
Cai J., 2005, P 43 AIAA AER SCI M, P1424