Abstract

Counter-rotating vortex pairs in an otherwise e at-plate turbulent boundary layer were studied in a wind-tunnel model experiment. The vortices were produced with pairs of inclined round jets with nozzle exit e ush with the plate surface. The skew angle and pitch angle of the nozzle were 45 deg. The Reynolds number based on the momentum thickness of the oncoming boundary layer was 3 :8 ££ 10 3 . A velocity e eld survey was performed with a three-component laser Doppler anemometry system. The effects of jet speed on the streamwise development of the vortices were investigated. The e ow had an upwash region in between the vortices that were embedded in the turbulent boundary layer. The upwash was produced by the vortices and the interaction between diametrically opposed secondary, near-wall e ows. Velocity measurements indicated e ow separation and entrainment behind the jet exit, and this was corroborated by surface e ow observation. The vortex development was divided into two stages: a near-e eld stage where the wake of the jet plays an important role and a far-e eld stage where turbulent dissipation and diffusion are important.

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