Impact of Axial Vortices on Mixing at a High Convective Mach Number
暂无分享,去创建一个
[1] Frank E. Marble,et al. Investigation of a contoured wall injector for hypervelocity mixing augmentation , 1993 .
[2] Jean P. Sislian,et al. The Use of Domain Decomposition in Accelerating the Convergence of Quasihyperbolic Systems , 2002 .
[3] D. Wilcox. Turbulence modeling for CFD , 1993 .
[4] Jonathan W. Naughton,et al. An experimental study of the effect of streamwise vorticity on supersonic mixing enhancement , 1989 .
[5] Jean P. Sislian,et al. Numerical Investigation of the Turbulent Mixing Performance of a Cantilevered Ramp Injector , 2002 .
[6] D. Wilcox. Reassessment of the scale-determining equation for advanced turbulence models , 1988 .
[7] J. Schumacher,et al. A comparative study of hypersonic fuel/air mixing enhancement by ramp and cantilevered ramp injectors , 1999 .
[8] James C. McDaniel,et al. Experimental and Numerical Study of Swept Ramp Injection into a Supersonic Flowfield , 1994 .
[9] David C. Wilcox,et al. Dilatation-dissipation corrections for advanced turbulence models , 1992 .
[10] Jean P. Sislian,et al. Hypervelocity Fuel/Air Mixing in a Shcramjet Inlet , 2004 .
[11] David W. Riggins,et al. Vortex generation and mixing in three-dimensional supersonic combustors , 1993 .
[12] J. Sislian,et al. Numerical Simulation of Hypersonic Shock-Induced Combustion Ramjets , 1998 .
[13] A. Roshko,et al. The compressible turbulent shear layer: an experimental study , 1988, Journal of Fluid Mechanics.