Formation and stability of near Chapman-Jouguet standing oblique detonation waves

被引:44
作者
Fusina, G [1 ]
Sislian, JP
Parent, B
机构
[1] Def Res & Dev Canada, Ottawa, ON K1A 0Z4, Canada
[2] Univ Toronto, Downsview, ON M3H 5T6, Canada
[3] Seoul Natl Univ, Seoul 151744, South Korea
关键词
D O I
10.2514/1.9128
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A numerical investigation of the behavior of standing oblique detonation waves (ODWs) near the Chapman-Jouguet (minimum entropy) point is the main purpose of this investigation. The laminar, two-dimensional Navier-Stokes equations coupled with a nonequilibrium hydrogen-air combustion model based on chemical kinetics are used to represent the physical system. The equations are solved with the window allocatable resolver for propulsion computational fluid dynamics code (Parent, B., and Sislian, J. P., "The Use of Domain Decomposition in Accelerating the Convergence of Quasihyperbolic Systems," journal of Computational Physics, Vol. 179, No. 1, 2002, pp. 140-169). A time-accurate simulation of the formation of a standing ODW near the Chapman-Jouguet condition yields a nonoscillatory, stable structure. The stability of the ODW to inhomogeneities in the oncoming fuel-air mixture is assessed through other time-accurate simulations by artificially introducing small disturbances consisting of pure air just upstream of the ODW structure. The ODW is shown to be resilient to these disturbances. The induction process and radical formation within the ODW structure are also analyzed.
引用
收藏
页码:1591 / 1604
页数:14
相关论文
共 38 条
[1]  
Anderson J. D., 1989, Hypersonic and High Temperature Gas Dynamics
[2]  
CHASE MW, 1985, J PHYS CHEM REFERENC, V14
[3]  
CHOI J, 1998, 27 INT S COMB COMB I
[4]   Computational fluid dynamics algorithms for unsteady shock-induced combustion, part 1: Validation [J].
Choi, JY ;
Jeung, IS ;
Yoon, YB .
AIAA JOURNAL, 2000, 38 (07) :1179-1187
[5]  
Dixon-Lewis G., 1984, COMBUSTION CHEM, P21
[6]   Numerical simulation of hypersonic shock-induced combustion ramjets [J].
Dudebout, R ;
Sislian, JP ;
Oppitz, R .
JOURNAL OF PROPULSION AND POWER, 1998, 14 (06) :869-879
[7]  
DUDEBOUT R, 1995, THESIS U TORONTO TOR
[8]  
FUSINA G, 2003, THESIS U TORONTO TOR
[9]  
Grismer MJ, 1996, SHOCK WAVES, V6, P147, DOI 10.1007/BF02510995
[10]  
HOLDEN MS, 1970, 700002 ARL