A General Study of Counterflow Diffusion Flames for Supercritical CO2 Combustion

被引:14
作者
Manikantachari, K. R., V [1 ]
Martin, Scott [2 ]
Rahman, Ramees K. [1 ]
Velez, Carlos [3 ]
Vasu, Subith [1 ]
机构
[1] Univ Cent Florida, Ctr Adv Turbomachinery & Energy Res, Orlando, FL 32816 USA
[2] Embry Riddle Aeronaut Univ, Eagle Flight Res Ctr, Daytona Beach, FL 32114 USA
[3] GE Global Res Ctr, Niskayuna, NY 12309 USA
来源
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME | 2019年 / 141卷 / 12期
关键词
MOLECULAR-DYNAMICS; CARBON-DIOXIDE;
D O I
10.1115/1.4045195
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
A counterflow diffusion flame for supercritical CO2 combustion is investigated at various CO2 dilution levels and pressures by accounting for real gas effects into both thermal and transport properties. The UCF 1.1 24-species mechanism is used to account the chemistry. The nature of important nonpremixed combustion characteristics such as Prandtl number, thermal diffusivity, Lewis number, stoichiometric scalar dissipation rate, flame thickness, and Damkohler number are investigated with respect to CO2 dilution and pressure. The results show that the aforementioned parameters are influenced by both dilution and pressure; the dilution effect is more dominant. Further, the result shows that Prandtl number increases with CO2 dilution and at 90% CO2 dilution, the difference between the Prandtl number of the inlet jets and the flame is minimal. Also, the common assumption of unity Lewis number in the theory and modeling of nonpremixed combustion does not hold reasonable for sCO(2) applications due to large difference of Lewis number across the flame and the Lewis number on the flame drop significantly with an increase in the CO2 dilution. An interesting relation between Lewis number and CO2 dilution is observed. The Lewis number of species drops by 15% when increasing the CO2 dilution by 30%. Increasing the CO2 dilution increases both the flow and chemical timescales; however, chemical timescale increases faster than the flow timescales. The magnitudes of the Damkohler number signify the need to consider finite rate chemistry for sCO(2) applications. Further, the Damkohler numbers at 90% sCO(2) dilution are very small; hence, laminar flamelet assumptions in turbulent combustion simulations are not physically correct for this application. Also, it is observed that the Damkohler number drops nonlinearly with increasing CO2 dilution in the oxidizer stream. This is a very important observation for the operation of sCO(2) combustors. Further, the flame thickness is found to increase with CO2 dilution and reduce with pressure.
引用
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页数:11
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