Effect of Heating on Quiet Flow in a Mach 4 Ludwieg Tube
暂无分享,去创建一个
[1] S. Novopashin,et al. Axial symmetry loss of a supersonic preturbulent jet , 1989 .
[2] J. Potter,et al. Review of the influence of cooled walls on boundary-layer transition , 1980 .
[3] Gerald C. Lauchle,et al. Laminar flow performance of a heated body in particle-laden water , 1995 .
[4] J. B. Anders,et al. Nozzle Wall Boundary-Layer Transition and Freestream Disturbances at Mach 5 , 1975 .
[5] Gregory S Elliott,et al. On streamwise vortices in high Reynolds number supersonic axisymmetric jets , 1993 .
[6] C. J. Schueler,et al. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels. , 1969 .
[7] E. Reshotko. Boundary layer instability, transition and control , 1994 .
[8] S. Schneider. Design of a Mach-6 Quiet-Flow Wind-Tunnel Nozzle using the e**N Method for Transition Estimation , 1998 .
[9] E. F. Spina,et al. Constant-temperature anemometry in hypersonic flow: critical issues and Sample results , 1994 .
[10] Ndaona Chokani,et al. Effect of Angle of Attack on Hypersonic , 1997 .
[11] Scott E. Munro. Effects of Elevated Driver-Tube Temperature on the Extent of Quiet Flow in the Purdue Ludwieg Tube. , 1996 .
[12] M. Mungal,et al. Small-perturbation mixing enhancement in compressible shear layers , 1997 .
[13] S. Schneider,et al. Quiet-flow Ludwieg tube for high-speed transition research , 1995 .
[14] Anthony Demetriades. Stabilization of a nozzle boundary layer by local surface heating , 1996 .
[15] J. Masad. Transition in flow over heat‐transfer strips , 1995 .
[16] Paul J Strykowski,et al. The effect of counterflow on the development of compressible shear layers , 1996, Journal of Fluid Mechanics.
[17] Ardeshir Hanifi,et al. An experimental and theoretical investigation of instabilities in hypersonic flat plate boundary layer flow , 1995 .
[18] Anjaneyulu Krothapalli,et al. Streamwise vortices in an underexpanded axisymmetric jet , 1991 .