1. 1Baumgartner, M.L. 1997. Turbulence Structure in a Hypersonic Boundary Layer. Ph.D. Thesis,Princeton University.
2. 4Fernholz,H.H.andFinley,P.J.1976. Acriticalcompilationofcompressibleturbulentboundarylayerdata. AGARDograph 223. Figure 14. Mach 7.2 turbulent boundary layer flow. The field of view is about 12 × 9 mm, and the boundary layer thickness is about 8 mm. Left: streamwise velocity contour map derived from 200 particle image pairs, with time delay of 0.2 µs. Right: Mean velocity profile for the same flow. Figure 15. Mach 7.2 turbulent boundary layer flow. The field of view is about 15 × 10 mm, and the boundary layer thickness is about 8 mm. Left: streamwise velocity contour map derived from 200 particle image pairs, with time delay of 0.3 µs. Right: Mean velocity profile for the same flow.
3. 5Fernholz,H.H.andFinley,P.J.1980. Acriticalcommentaryonmeanflowdatafortwo-dimensionalcompressibleturbulent boundary layers. AGARDograph 253.