The effect of spatial resolution on the coherent structures in the outer region of a turbulent
boundary layer which subjected to a strong adverse pressure gradient has been studied using
particle image velocimetry (PIV). The experimental set-up is designed to achieve flow conditions
corresponding to trailing-edge stall of an airfoil. Large sets of instantaneous velocity fields are acquired by PIV in streamwise-wall-normal planes at three different streamwise locations. The vortices are detected using λci criteria. The essential features of the vortices and vortex packets are similar to those found in zero-pressure-gradient turbulent boundary layers. The vortices are however slightly more intense in the zero-pressure-gradient turbulent boundary layers. Some of the characteristics of the spanwise vortices are also documented.
