Abstract
The flow characteristics of a three-dimensional, compressible, turbulent boundary layer have been investigated experimentally. The three dimensionality was generated by inclining a cylindrical afterbody at 10-deg angle of attack to a Mach 2.45 freestream. The objective was to determine the mechanisms that govern the growth and behavior of pressure-driven, three-dimensional, compressible, turbulent boundary layers. Laser Doppler velocimetry was used to determine mean velocity components and turbulence statistics
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