| Citation: | HOU Jin-li, JIN Ping, CAI Guo-biao. Reduced mechanism for oxygen/methane combustion based on sensitivity analysis[J]. Journal of Aerospace Power, 2012, 27(7): 1549-1554. |
| [1] |
禹天福,李亚裕.液氧/甲烷发动机的应用前景[J].航天制造技术,2007(2):1-4. YU Tianfu,LI Yayu.The application prospect of LOX/CH4 engine[J].Aerospace Manufacturing Technology,2007(2):1-4.(in Chinese)
|
| [2] |
孙宏明.液氧/甲烷发动机评述[J].火箭推进,2006,32(2):23-31. SUN Hongming.Review of liquid oxygen/methane rocket engine [J].Journal of Rocket Propulsion,2006,32(2):23-31.(in Chinese)
|
| [3] |
Miller J A,Kee R J.Chemical kinetics and combustion modeling[J].Annu. Rev. in Phys. Chem.,1990,41(1):345-387.
|
| [4] |
Wdrnatz J,Maas U,Dibble R W.Combustion[M].Germany:Springer-Verlag,1999.
|
| [5] |
Turanyi T,Berees T,Vajda S.Reaction rate analysis of complex kinetic system[J].International Journal of Chemical Kinetics,1989,21(2):83-99.
|
| [6] |
Turanyi T.Applications of sensitivity analysis to combustion chemistry[J].Reliability Engineering and System Safety,1997,57(1):41-48.
|
| [7] |
Turanyi T.Sensitivity analysis of complex kinetic systems:tools and applications[J].J. Math. Chem.,1990,5(3):203-248.
|
| [8] |
董刚.简化CH4/O2/N2基元反应模型在爆轰模拟中的应用[J].计算力学学报,2005,22(4):431-436. DONG Gang.An application of reduced CH4/O2/N2 reaction mechanism on numerical simulation of detonation[J].Chinese Journal of Computational Mechanics,2005,22(4):431-436(in Chinese)
|
| [9] |
Hoffmann A,Wetzel F,Zarzalis N.Extension of kinetic scheme to highly diluted combustion .GRDl-2001-40198,2001.
|
| [10] |
Tong T W.Mathematical modeling of catalytic-surface combustion of reacting flows .AIAA-2006-3185,2006.
|
| [11] |
Katta V R.Simulation of dynamic methane jet diffusion flames using finite rate chemistry models [J].AIAA Journal,1998,36(11):2044-2054.
|
| [12] |
Smith G P,Golden D M.Gri-mech version 3.0 . .http://www.me.berkeley.edu/gri_mech/version3.0/taxt30.html.
|