Laser-Doppler measurements were conducted in a plane turbulent wall je
t at a Reynolds number based on inlet velocity, Re-0, of 9600. The ini
tial development as well as the fully developed flow was studied. Spec
ial attention was given to the near-wall region, including the use of
small measuring volumes and the application of specific near-wall data
corrections, so that wall sheer stresses were determined directly fro
m the mean velocity gradient at the wail using only data below y(+) =
4. It was possible to resolve the inner peak in the streamwise turbule
nce intensity as well as the inner (negative) peak in the shear stress
. Limiting values of (u')(+) and uv(+) were determined. Turbulence dat
a from the outer region of the flow were compared to earlier hot wire
measurements and large differences in the normal turbulence intensity
and the shear stress were found. These differences can be attributed t
o high turbulence intensity effects on the hot-wires.