TY  - EJOU
AU  - Zheng, Yongkang 
AU  - Jiang, Qinxue 
AU  - Tian, Hao 
AU  - Ye, Youda 
AU  - Wang, Jingying 

TI  - Numerical Application of the Flamelet Model to Supersonic Turbulent Combustion
T2  - Fluid Dynamics \& Materials Processing

PY  - 2022
VL  - 18
IS  - 4
SN  - 1555-2578

AB  - In this study, the flow field structure inside a scramjet combustor is numerically simulated using the flamelet/progress variable model. Slope injection is considered, with fuel mixing enhanced by means of a streamwise vortex. The flow field structure and combustion characteristics are analyzed under different conditions. Attention is also paid to the identification of the mechanisms that keep combustion stable and support enhanced mixing. The overall performances of the combustion chamber are discussed.
KW  - Steady flamelet model; flamelet/progress variable model; supersonic combustion

DO  - 10.32604/fdmp.2022.019048