The current numerical study recommends using a vortex generator (VG) to lessen the impacts of a counter-rotating vortex pair (CRVP). For this study, the delta winglet pair (DWP) arrangement with common-flow-down (CFD) is recommended. The blowing ratios for the jet to cross flows are preserved at unity, while the Reynolds number is kept at 17000 based on free stream velocity and film cooling hole dimension. The numerical analysis is carried out using the FLUENT commercial code and the k-omega SST turbulence model. The effect of the length and height of the vortex generator on the features of film cooling effectiveness are investigated. The consequences of using multiple VG and impact of their different downstream locations on cooling effectiveness, has been discovered. The influence of changing turbulence intensity (TI=5, 10, 15) and Reynolds number (Re=15000, 17000, 20000) on cooling efficacy was studied. The Vortex generator, which is placed downstream of the circular film cooling hole, appears to be more successful. With the increment of TI and Reynolds number, film cooling efficiency decreases.