TY - GEN
T1 - Simulation of a methane-air jet flame by les and rans model
AU - Wang, F.
AU - Zhou, L. X.
AU - Xu, C. X.
AU - Huang, Y.
N1 - Publisher Copyright:
Copyright © 2007 by ASME.
PY - 2007
Y1 - 2007
N2 - A piloted methane/air jet flame, measured in the Sandia National Laboratory, is simulated by both 3-D large eddy simulation (LES) and Reynolds-Averaged Navier-Stokes (RANS) modeling. In LES, an algebra second order moment sub-grid scale (ASOM-SGS) combustion model is applied, while the second order moment (SOM) transport equation combustion model is employed in RANS method. The LES predicted time-averaged and root mean square (RMS) fluctuation temperature and methane concentration are in good agreement with the experimental data, showing the feasibility of the ASOM-SGS combustion model. For time-averaged temperature and species concentration, the performance of the RANS SOM model is rather good. Considering the difference of nearly two orders of magnitude in the computation time between LES and RANS modeling, the latter is considered to be more appropriate for engineering application. The LES instantaneous results show the coherent structures in the flame. It is found that reaction enhances the coherent structures, and conversely the coherent structures intensify combustion, forming a wrinkled-flame surface.
AB - A piloted methane/air jet flame, measured in the Sandia National Laboratory, is simulated by both 3-D large eddy simulation (LES) and Reynolds-Averaged Navier-Stokes (RANS) modeling. In LES, an algebra second order moment sub-grid scale (ASOM-SGS) combustion model is applied, while the second order moment (SOM) transport equation combustion model is employed in RANS method. The LES predicted time-averaged and root mean square (RMS) fluctuation temperature and methane concentration are in good agreement with the experimental data, showing the feasibility of the ASOM-SGS combustion model. For time-averaged temperature and species concentration, the performance of the RANS SOM model is rather good. Considering the difference of nearly two orders of magnitude in the computation time between LES and RANS modeling, the latter is considered to be more appropriate for engineering application. The LES instantaneous results show the coherent structures in the flame. It is found that reaction enhances the coherent structures, and conversely the coherent structures intensify combustion, forming a wrinkled-flame surface.
UR - https://www.scopus.com/pages/publications/84928598398
U2 - 10.1115/IMECE200742845
DO - 10.1115/IMECE200742845
M3 - 会议稿件
AN - SCOPUS:84928598398
T3 - ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)
SP - 769
EP - 774
BT - Energy Systems
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 2007 International Mechanical Engineering Congress and Exposition, IMECE 2007
Y2 - 11 November 2007 through 15 November 2007
ER -