A study of shock-wave turbulent boundary layer interaction using laser velocimeter and hot-wire anemometer techniques
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[1] Insensitivity of single particle time domain measurements to laser velocimeter 'Doppler ambiguity.' , 1973 .
[2] L. Kovasznay. Turbulence in Supersonic Flow , 1953 .
[3] W. Rose. Turbulence measurements in a compressible boundary layer subjected to a shock-wave-induced adverse pressure gradient. , 1973 .
[4] A. Kistler,et al. Fluctuation Measurements in a Supersonic Turbulent Boundary Layer , 1959 .
[5] L. Kovasznay,et al. The Hot-Wire Anemometer in Supersonic Flow , 1950 .
[6] P. L. Eggins,et al. Laser Doppler velocity measurements in a supersonic flow without artificial seeding , 1972 .