Fuel flexibility, stability and emissions in premixed hydrogen-rich gas turbine combustion: Technology, fundamentals, and numerical simulations (vol 154, pg 1020, 2015)

被引:1
|
作者
Taamallah, S. [1 ]
Vogiatzaki, K. [1 ]
Alzahrani, F. M. [2 ]
Mokheimer, E. M. A. [2 ]
Habib, M. A. [2 ]
Ghoniem, A. F. [1 ]
机构
[1] MIT, Dept Mech Engn, Cambridge, MA 02139 USA
[2] KFUPM, Dept Mech Engn, Dhahran, Saudi Arabia
关键词
D O I
10.1016/j.apenergy.2017.12.080
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
引用
收藏
页码:426 / 426
页数:1
相关论文
共 2 条
  • [1] Fuel flexibility, stability and emissions in premixed hydrogen-rich gas turbine combustion: Technology, fundamentals, and numerical simulations
    Taamallah, S.
    Vogiatzaki, K.
    Alzahrani, F. M.
    Mokheimer, E. M. A.
    Habib, M. A.
    Ghoniem, A. F.
    [J]. APPLIED ENERGY, 2015, 154 : 1020 - 1047
  • [2] Extension of the Combustion Stability Range in Dry Low NOx Lean Premixed Gas Turbine Combustor Using a Fuel Rich Annular Pilot Burner (vol 136, 051509, 2014)
    Rosentsvit, L.
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2014, 136 (08):