Combustion of H2/air supersonic mixing layers with splitter plate: Growth rates and transport characteristic

被引:12
作者
Yao, Xiao [1 ]
Tan, Jianguo [1 ]
Zhang, Dongdong [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China
关键词
Supersonic mixing layer; Combustion; Splitter plate; Transport characteristic; Heat release effect; HEAT RELEASE; TURBULENT; COMPRESSIBILITY; PERFORMANCE; SIMULATION; MODEL; RATIO; FIELD; AIR;
D O I
10.1016/j.actaastro.2019.09.036
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
H2/air supersonic mixing layers were calculated with different splitter plates thickness in both inert and reactive cases. The decay of mixing layer growth rates with the presence of heat release indicates the inhibition of fluctuations of velocity and scalar. Analyses of mean pressure and mean scalar show that the combustion efficiency increases with thickening of splitter plate. Heat release effect strengthens local compressibility, and then the relation among local compressibility, mean shear and velocity fluctuations is built. Considering heat release effect, the peak value of turbulent kinetic energy of moderate thickness splitter plates (the thickness equals 4 mm) is smallest. Similar phenomena are observed in scalar variance and vorticity variance, indicating the turbulent development of moderate thickness splitter plates is slowest.
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页码:401 / 413
页数:13
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