DNS of compressible turbulent boundary layer around a sharp cone

[1]  X. Zhong.  Numerical Simulation of Surface Roughness Effects on Receptivity of Hypersonic Flow over Blunt Cones , 2007 .

[2]  F. Dexun,et al.  Direct Numerical Simulation of a Spatially Evolving Supersonic Turbulent Boundary Layer at Ma=6 , 2006 .

[3]  Xiaolin Zhong,et al.  Boundary-layer receptivity of Mach 7.99 flow over a blunt cone to free-stream acoustic waves , 2006, Journal of Fluid Mechanics.

[4]  D. Fu,et al.  Optimized group velocity control scheme and DNS of decaying compressible turbulence of relative high turbulent Mach number , 2005 .

[5]  F. Dexun,et al.  Direct Numerical Simulation of Supersonic Turbulent Boundary Layer Flow , 2005 .

[6]  Heng Zhou,et al.  Inherent mechanism of breakdown in laminar-turbulent transition of plane channel flows , 2005 .

[7]  李新亮,et al.  DNS of compressible turbulent boundary layer over a blunt wedge , 2005 .

[8]  Sergio Pirozzoli,et al.  Direct numerical simulation and analysis of a spatially evolving supersonic turbulent boundary layer at M=2.25 , 2004 .

[9]  Xiaolin Zhong,et al.  Receptivity of a supersonic boundary layer over a flat plate. Part 1. Wave structures and interactions , 2003, Journal of Fluid Mechanics.

[10]  Scott A. Berry,et al.  Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6 Wind Tunnels , 2002 .

[11]  N. Adams,et al.  Direct simulation of turbulent supersonic boundary layers by an extended temporal approach , 2001, Journal of Fluid Mechanics.

[12]  Robert D. Moser,et al.  Direct numerical simulation of a supersonic turbulent boundary layer at Mach 2.5 , 2000, Journal of Fluid Mechanics.

[13]  S. Schneider.  Flight Data for Boundary-Layer Transition at Hypersonic and Supersonic Speeds , 1999 .

[14]  Yanwen Ma,et al.  A High Order Accurate Difference Scheme for Complex Flow Fields , 1997 .

[15]  Gordon Erlebacher,et al.  Direct simulation of spatially evolving compressible turbulent boundary layers , 1995 .

[16]  T. G. Johansson,et al.  LDV measurements of higher order moments of velocity fluctuations in a turbulent boundary layer , 1986 .

[17]  L. Chauvin,et al.  Boundary-Layer-Transition and Heat-Transfer Measurements from Flight Tests of Blunt and Sharp 50 Degree Cones at Mach Numbers from 1.7 to 4.7 , 1957 .

[18]  L. Rabb,et al.  Boundary-Layer Transition at High Reynolds Numbers as Obtained in Flight of a 20 Degree Cone-Cylinder With Wall to Local Stream Temperature Ratios Near 1.0 , 1955 .

[19]  S. Simpkinson,et al.  Free-flight Heat-transfer Measurements on Two 20 Degree-cone-cylinders at Mach Numbers from 1.3 to 4.9 , 1955 .