REYNOLDS-NUMBER EFFECTS ON THE TURBULENCE FIELD IN COMPRESSIBLE BOUNDARY-LAYERS

Detailed experiments were conducted in a zero pressure gradient, supersonic turbulent boundary layer, including measurements of the three components of velocity fluctuations and the turbulent shear stress, for Reynolds numbers ranging from 11.7 to 105×l06 at a freestream Mach number of 2.3. The mean flow measurements established the fully developed and equilibrium nature of the boundary layer. Measurements of the turbulence field show that the vertical and transverse fluctuations ⟨ t' ⟩ and ⟨ w' ⟩ are essentially equal throughout the boundary layer at all Reynolds numbers, a feature that is different from observations in incompressible flows. The data show that the boundary layer exhibits similarity in the turbulence profiles for the entire Reynolds number range and agrees with previous compressible and incompressible data using Morkovin's scaling to account for compressibility effects. © 1979 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.