A synergistic laser Doppler velocimetry and multiple overheat cross-fi
lm anemometry analysis was developed to allow for direct measurements
of the mean and turbulent flow properties in a supersonic turbulent fl
ow. The present technique facilitated, for thin-layer, nonreacting flo
ws, the measurement of the Reynolds (time) and Favre (mass-weighted ti
me) averaged turbulent shear stress, heat flux, and apparent mass flux
, without the usual ad hoc assumption of negligible static pressure fl
uctuations. The mean velocity, mass flux, and density were also acquir
ed. The directly measured mean flow and turbulence results, in a Mach
2.8 wall boundary layer (Re-theta = 1.12 x 10(4)), were found to compa
re very well with numerical predictions based on the k-w two-equation
(for the Favre approach) and the compressible apparent mass mixing len
gth extension algebraic (for the Reynolds approach) turbulence model.