Uniform blowing in wall bounded shear flows is well known for its drag reducing effects and has long been investigated ever since. However, many contemporary and former research on the present topic has confirmed the drag reducing effect but very less is known regarding how blowing mechanism is effecting the coherent structures, more importantly, their influence on the Reynolds stresses at high Reynolds number. Therefore, effect of uniform blowing has been experimentally investigated in a zero pressure gradient turbulent boundary layer (TBL). The wind tunnel used for the measurement was particularly suitable to obtain high resolution data (Boundary layer thickness 1 , δ > 0.24m) at high Reynolds number with Stereo Particle Image Velocimetry (SPIV) measurements. The data presented in this literature covers a large range of high Reynolds number flow e.g. Re θ = 7500 ∼ 19763 where Reynolds number is based on the momentum thickness. Upstream effect of blowing was varied from 1% ∼ 6% of free stream velocity by tuning the flow rate of the compressed air and measurements were taken downstream after a short interval. In order to access statistics and turbulence properties of the TBL with focus on the logarithmic and outer region, the streamwise SPIV plane (Vertical plane parallel to flow direction) configuration was used to obtain velocity fields.