| Citation: | WANG Fang, CAI Jiangtao, ZHANG Jian, et al. Different reaction mechanism on simulations of jet flames using flamelet model[J]. Journal of Aerospace Power, 2022, 37(11):2465-2478 doi: 10.13224/j.cnki.jasp.20220204 |
The effects of different chemical reaction mechanisms on the flame surface database and simulation results based on the steady laminar flamelet model (SLFM) were analyzed by using one-dimensional flame analysis and constructing a flamelet database. Based on the large eddy simulation (LES) program AECSC (aero engine combustor simulation code) software, the SLFM model was combined with DRG (direct relation graph) method simplified mechanism, Smooke mechanism, and GRI 3.0 detailed mechanism to simulate Flame D, E, and F jet flames, among which the average temperature and pulsation values of GRI 3.0 mechanism were the closest to the experimental data. The LES-SLFM model was faster and had comparable overall accuracy compared with the LES and probability density functional transport equation turbulent combustion (TPDF) models. The chemical mechanism affected the flamelet database and thus the time and accuracy of the simulation. The LES-SLFM model combined with the detailed mechanism was fast and had suitable accuracy, which should be further tested in the combusor simulation, presenting potential and value for future applications.
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