Experiments were conducted in a wind tunnel to assess the effect of a movin
g wall on a fully developed, equilibrium turbulent boundary layer. Pitot-st
atic and total head probes were used in conjunction with both single- and t
wo-component hot-wire anemometer probes to quantify the effect of wall moti
on on the boundary layer velocity statistics. A variable speed, seamless be
lt formed the wind tunnel test section wall. When stationary, the belt was
found to possess a fully developed, equilibrium turbulent boundary layer in
excellent agreement with archival data. With the tunnel wall moving at the
free-stream speed, and at a sufficient distance above the wall, the veloci
ty statistics in the moving-wall boundary layer were found to collapse well
when scaled as a self-preserving turbulent wake. The near-wall mean veloci
ty profile of the moving wall was found to exhibit an extended region of li
nearity compared to canonical turbulent boundary layer and internal flows.
This can be attributed to the reduced shear resulting from wall motion and
the subsequent reduction in Reynolds stress.