Large-eddy simulation of supersonic compression-ramp flows
暂无分享,去创建一个
[1] Nikolaus A. Adams,et al. Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reθ = 1685 , 2000, Journal of Fluid Mechanics.
[2] Robert D. Moser,et al. Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5 , 2000, Journal of Fluid Mechanics.
[3] F. Nicoud,et al. Large-Eddy Simulation of the Shock/Turbulence Interaction , 1999 .
[4] S. Ghosal. Mathematical and Physical Constraints on Large-Eddy Simulation of Turbulence , 1999 .
[5] Miguel R. Visbal,et al. High-Order-Accurate Methods for Complex Unsteady Subsonic Flows , 1999 .
[6] Miguel R. Visbal,et al. Numerical investigation of synthetic-jet flowfields , 1999 .
[7] Nikolaus A. Adams,et al. Direct Numerical Simulation of Turbulent Compression Ramp Flow , 1998 .
[8] Miguel R. Visbal,et al. Direct numerical simulation of a forced transitional plane wall jet , 1998 .
[9] Gregory A. Blaisdell,et al. Large-Eddy Simulation of a Spatially Evolving Supersonic Turbulent Boundary-Layer Flow , 1998 .
[10] D. Gaitonde,et al. Practical aspects of high-order accurate finite-volume schemes for electromagnetics , 1997 .
[11] Miguel R. Visbal,et al. Onset of vortex breakdown above a pitching delta wing , 1994 .
[12] Raymond E. Gordnier,et al. Computation of Delta-Wing Roll Maneuvers , 1993 .
[13] Parviz Moin,et al. Direct numerical simulation of isotropic turbulence interacting with a weak shock wave , 1993, Journal of Fluid Mechanics.
[14] Miguel R. Visbal,et al. Numerical simulation of delta-wing roll , 1993 .
[15] S. Lele. Compact finite difference schemes with spectral-like resolution , 1992 .
[16] R. C. Swanson,et al. On Central-Difference and Upwind Schemes , 1992 .
[17] D. Lilly,et al. A proposed modification of the Germano subgrid‐scale closure method , 1992 .
[18] P. Moin,et al. A dynamic subgrid‐scale model for compressible turbulence and scalar transport , 1991 .
[19] Mehmet Erengil,et al. Correlation of separation shock motion with pressure fluctuations inthe incoming boundary layer , 1991 .
[20] Mehmet Erengil,et al. Unsteady wave structure near separation in a Mach 5 compression rampinteraction , 1991 .
[21] P. Moin,et al. A dynamic subgrid‐scale eddy viscosity model , 1990 .
[22] Alexander J. Smits,et al. Experimental study of three shock wave/turbulent boundary layer interactions , 1987, Journal of Fluid Mechanics.
[23] J. Andreopoulos,et al. Some new aspects of the shock-wave/boundary-layer interaction in compression-ramp flows , 1987, Journal of Fluid Mechanics.
[24] A. Yoshizawa. Statistical theory for compressible turbulent shear flows, with the application to subgrid modeling , 1986 .
[25] C. T. Or,et al. Unsteadiness of the shock wave structure in attached and separated compression ramp flows , 1985 .
[26] D. Dolling,et al. Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp Flowfield , 1983 .
[27] B. V. Leer,et al. Towards the ultimate conservative difference scheme V. A second-order sequel to Godunov's method , 1979 .
[28] Gary S. Settles,et al. Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow , 1979 .
[29] R. F. Warming,et al. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations , 1977 .
[30] J. Smagorinsky,et al. GENERAL CIRCULATION EXPERIMENTS WITH THE PRIMITIVE EQUATIONS , 1963 .
[31] E. R. V. Driest. On Turbulent Flow Near a Wall , 1956 .