Effect of angle of attack on hypersonic boundary-layer stability
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[1] G. R. Sarma,et al. A new approach to high-speed flow measurements using constant voltage anemometry , 1992 .
[2] N. Sheetz. Free-flight boundary layer transition investigations at hypersonic speeds. , 1965 .
[3] S. Pate,et al. Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High Speeds , 1971 .
[4] L. Mack,et al. Stability of axisymmetric boundary layers on sharp cones at hypersonic Mach numbers , 1987 .
[5] Ndaona Chokani,et al. Hypersonic Boundary Layer Stability Experiments in a Quiet Wind Tunnel with Bluntness Effects , 1996 .
[6] G. Rushton,et al. Shock tunnel investigation of boundary-layer transition at M equals 5.5. , 1966 .
[7] Kenneth F. Stetson. Hypersonic Laminar Boundary Layer Transition. Part 1. Nosetip Bluntness Effects on Cone Frustum Transition. Part 2. Mach 6 Experiments of Transition on a Cone at Angle of Attack , 1982 .
[8] J. Laufer,et al. Aerodynamic noise in supersonic wind tunnels , 1961 .
[9] Kenneth F. Stetson,et al. Laminar boundary layer stability experiments on a cone at Mach 8. I - Sharp cone , 1983 .
[10] Ndaona Chokani,et al. Hypersonic Boundary-Layer Stability Experiments on a Flared-Cone Model at Angle of Attack in a Quiet Wind Tunnel , 1997 .
[11] G. R. Sarma. Analysis of a constant voltage anemometer circuit , 1993, 1993 IEEE Instrumentation and Measurement Technology Conference.
[12] G. Selby,et al. An Experimental Investigation of Wall-Cooling Effects on Hypersonic Boundary-Layer Stability in a Quiet Wind Tunnel , 1996 .
[13] R. Kimmel,et al. On hypersonic boundary-layer stability , 1992 .
[14] S. Wilkinson,et al. Status of NASA Langley quiet flow facility developments , 1994 .
[15] Steven P. Schneider,et al. Effect of Heating on Quiet Flow in a Mach 4 Ludwieg Tube , 1998 .