Abstract
Flow visualization results are presented for a highly curved flow resulting from the collision of plane turbulent wall jet with a boundary layer. This configuration can be found in the case of impinging jets of a V/STOL aircraft operating in ground vicinity. The experiments were carried out for wall jet to boundary layer velocity ratio of 1.57. The present results revealed the existence of two small vortexes located in the collision zone, that exhibit an unsteady behaviour.
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