Validation procedure for the analysis of shock-wave/boundary-layer interaction problems
暂无分享,去创建一个
[1] V. Dicristina,et al. Three-dimensional laminar boundary-layer transition on a sharp 8 degcone at Mach 10 , 1969 .
[2] Eli Turkel,et al. On Central-Difference and Upwind Schemes , 1992 .
[3] H. Lomax,et al. Thin-layer approximation and algebraic model for separated turbulent flows , 1978 .
[4] M. Holden,et al. A study of flow separation in regions of shock wave-boundary layer interaction in hypersonic flow , 1978 .
[5] Francesco Grasso,et al. High-Speed Turbulence Modeling of Shock-Wave/ Boundary-Layer Interaction , 1993 .
[6] Joseph G. Marvin. Dryden lectureship in research, a perspective on CFD validation , 1993 .
[7] F. Grasso,et al. Solutions of hypersonic viscous flows with total variation diminishing multigrid techniques , 1995 .
[8] A. Jameson,et al. Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes , 1981 .
[9] D. O. Barnett,et al. Shockwave-boundary layer interference heating analysis. , 1973 .
[10] F. Grasso,et al. Multigrid techniques for hypersonic viscous flows , 1993 .
[11] Dean R. Chapman,et al. Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition , 1958 .
[12] Joseph G. Marvin,et al. Accuracy requirements and benchmark experiments for CFD validation , 1988 .