Aspects of Hypersonic Boundary Layer Transition Control
暂无分享,去创建一个
[1] G. Rushton,et al. Shock tunnel investigation of boundary-layer transition at M equals 5.5. , 1966 .
[2] W. Saric,et al. Effects of curvature variations on the nonlinear evolution of Goertler vortices , 1994 .
[3] Egon Stanewsky,et al. Boundary-layer transition on swept cylinders at hypersonic speeds , 1996 .
[4] James Serrin,et al. Mathematical Principles of Classical Fluid Mechanics , 1959 .
[5] D. Poll,et al. Boundary layer transition on the windward face of Space Shuttle during re-entry , 1985 .
[7] E. Reshotko. Transient growth: A factor in bypass transition , 2001 .
[8] R. Kimmel,et al. Drag Prediction and Transition in Hypersonic Flow , 1997 .
[9] Robert E. Spall,et al. Effect of Transverse Curvature on the Stability of Compressible Boundary Layers , 1991 .
[10] Hans G. Hornung,et al. Stabilization of Hypersonic Boundary Layers by Porous Coatings , 2001 .
[11] Charles Cockrell,et al. Aerodynamics for Optimal Engine-Integrated Airbreathing Launcher Configurations , 2004 .
[12] A. Demetriades. Stabilization of a nozzle boundary layer by surface heating , 1994 .
[13] Anthony Demetriades. Stabilization of a nozzle boundary layer by local surface heating , 1996 .
[14] Roughness-Induced Attachment-Line Transition on a Swept Cylinder in Supersonic Flow , 2001 .
[15] Colin P. Coleman,et al. Boundary layer transition in the leading edge region of a swept cylinder in high speed flow , 1997 .
[16] Kenjiro Inagaki,et al. Experimental and numerical analysis of laminar flow control at Mach 1.4 , 1999 .
[17] Venkit Iyer,et al. Computational study of transition front on a swept wing leading-edge model , 1992 .
[18] Helen L. Reed,et al. Transition correlations in three-dimensional boundary layers , 1994 .
[19] Steven P. Schneider,et al. Effects of High-Speed Tunnel Noise on Laminar-Turbulent Transition , 2000 .
[20] Ivan E. Beckwith,et al. Gortler instability and supersonic quiet nozzle design , 1992 .
[21] D. Reda. Review and synthesis of roughness-dominated transition correlations for reentry applications , 2002 .
[22] A. Fedorov,et al. Experiments on passive hypervelocity boundary layer control using a porous surface , 2001 .
[23] G. Gerbeth,et al. Experiments on cylinder wake stabilization in an electrolyte solution by means of electromagnetic forces localized on the cylinder surface , 1998 .
[24] W. Saric,et al. Stability and control of high-speed flows , 2001 .
[25] Kenneth F Stetson. Comments on Hypersonic Boundary-Layer Transition , 1990 .
[26] Vernon J Rossow. Boundary-layer stability diagrams for electrically conducting fluids in the presence of a magnetic field , 1958 .
[27] M. Malik,et al. Effect of nose bluntness on boundary layer stability and transition , 1990 .
[28] William S. Saric,et al. Application of Variable Leading-Edge Roughness for Transition Control. on Swept Wings , 2000 .
[29] N. A. Jaffe. Effects of a transverse magnetic field and spanwise electric field on the boundary layer of a conducting fluid. , 1966 .
[30] M. R. Malik,et al. Goertler vortices in supersonic and hypersonic boundary layers , 1989 .
[31] D Poll. The effect of wing sweep back upon transition in hypersonic flow , 1995 .
[32] Roger L. Kimmel,et al. The Effect of Pressure Gradients on Transition Zone Length in Hypersonic Boundary Layers. , 1997 .
[33] S. Schneider. Design of a Mach-6 Quiet-Flow Wind-Tunnel Nozzle using the e**N Method for Transition Estimation , 1998 .
[34] E. Benard,et al. Influence of roughness on attachment line boundary layer transition in hypersonic flow , 1997 .
[35] Scott A. Berry,et al. Boundary Layer Transition on Slender Cones in Conventional and Low Disturbance Mach 6 Wind Tunnels , 2002 .
[36] George Em Karniadakis,et al. Control of external flows via electro-magnetic fields , 1995 .
[37] G. Selby,et al. An Experimental Investigation of Wall-Cooling Effects on Hypersonic Boundary-Layer Stability in a Quiet Wind Tunnel , 1996 .
[38] William B. Bush. Compressible Flat-Plate Boundary-Layer Flow with an Applied Magnetic Field , 1960 .
[39] M. Malik,et al. On the stability of compressible flow past axisymmetric bodies , 1991, Journal of Fluid Mechanics.
[40] E. Bénard,et al. Smooth leading edge transition in hypersonic flow , 1999 .
[41] V. Rossow. On flow of electrically conducting fluids over a flat plate in the presence of a transverse magnetic field , 1957 .
[42] M. Malik,et al. Instability and transition in three-dimensional supersonic boundary layers , 1992 .
[43] Edward J. Hopkins,et al. Effects of Mach Number, Leading-Edge Bluntness, and Sweep on Boundary-Layer Transition on a Flat Plate , 1961 .
[44] Roger L. Kimmel,et al. A comparison of planar and conical boundary layer stability and transition at a Mach number of 8 , 1991 .
[45] A. Demetriades. Cooling and Roughness Effects on Transition on Nozzle Throats and Blunt Bodies , 1992 .
[46] J. Murphy,et al. Flat plate boundary layer transition at hypersonic speeds , 1965 .
[47] K. Stetson,et al. Laminar boundary layer stability experiments on a cone at Mach 8. V - Tests with a cooled model , 1989 .
[48] J. Stace,et al. Experimental investigation of a salt water turbulent boundary layer modified by an applied streamwise magnetohydrodynamic body force , 1995 .
[49] P. Stephen,et al. A Review of Hypersonic Boundary Layer Stability Experiments in a Quiet Mach 6 Wind Tunnel , 1997 .
[50] M. Malik. Prediction and control of transition in supersonic and hypersonic boundary layers , 1989 .
[51] I. E. Beckwith,et al. Transition on swept leading edges at Mach 3.5 , 1987 .
[52] Ndaona Chokani,et al. Nonlinear Aspects of Hypersonic Boundary-Layer Stability on a Porous Surface , 2005 .
[53] Roger L. Kimmel,et al. Effect of applied magnetic field on the instability of Mach 4.5 boundary layer over a flat plate , 2002 .
[54] J. Schmisseur,et al. Effect of pressure gradients on axisymmetric hypersonic boundary layer stability , 2000 .
[55] Subrahmanyan Chandrasekhar,et al. The stability of viscous flow between rotating cylinders in the presence of a magnetic field , 1953, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.
[56] J. T. Stuart,et al. the presence of , 1953 .
[57] J. Potter,et al. Review of the influence of cooled walls on boundary-layer transition , 1980 .
[58] Roger L. Kimmel,et al. Laminar-Turbulent Transition in a Mach 8 Elliptic Cone Flow , 1999 .
[59] Roger L. Kimmel,et al. Effect of Total Temperature on Boundary-Layer Stability at Mach 6 , 2000 .
[60] Paul Wercinski,et al. Sharp-L1 technology demonstrator development - An aerothermodynamic perspective , 2000 .
[61] Thomas Elias,et al. Stability studies of planar transition in supersonic flows , 1990 .
[62] R. C. Lock,et al. The stability of the flow of an electrically conducting fluid between parallel planes under a transverse magnetic field , 1955, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.
[63] A. Nayfeh,et al. Laminar flow control of subsonic boundary layers by suction and heat‐transfer strips , 1992 .
[64] T. Bussing,et al. Chemistry associated with hypersonic vehicles , 1987 .
[65] W. R. Sears,et al. Magnetohydrodynamic Effects in Aerodynamic Flows , 1959 .
[66] Roger L. Kimmel,et al. Surface temperature effects on boundary-layer transition , 1992 .
[67] Roger L. Kimmel,et al. Example of Second-Mode Instability Dominance at a Mach Number of 5.2 , 1992 .
[68] Samuel R Pate. Dominance of Radiated Aerodynamic Noise on Boundary-Layer Transition in Supersonic-Hypersonic Wind Tunnels. Theory and Application , 1978 .
[69] J. Kendall. Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer Transition , 1974 .
[70] H. Reed,et al. Stability of three‐dimensional supersonic boundary layers , 1991 .
[71] Ndaona Chokani,et al. Boundary-layer stability measurements in a hypersonic quiet tunnel , 1996 .
[72] D. Poll,et al. The development of intermittent turbulence on a swept attachment line including the effects of compressibility , 1983 .
[73] K. Stetson. Nosetip bluntness effects on cone frustum boundary layer transition in hypersonic flow , 1983 .
[74] Ndaona Chokani,et al. Effect of angle of attack on hypersonic boundary-layer stability , 1997 .
[75] Ndaona Chokani,et al. Effect of Angle of Attack on Hypersonic , 1997 .
[76] Kenneth F. Stetson,et al. Laminar boundary layer stability experiments on a cone at Mach 8. I - Sharp cone , 1983 .
[77] M. Holden,et al. Attachment line transition studies on swept cylindrical leading edges at Mach numbers from 10 to 12 , 1995 .
[78] V. Garg,et al. The effect of heating on the stability of flow over concave walls , 1984 .
[79] L. Mack,et al. Stability of axisymmetric boundary layers on sharp cones at hypersonic Mach numbers , 1987 .