3. Particle image velocimetry

A.S. Guzeev, S.U. Soloviev, A.S. Vorobyev, A.V. Mityakov, V.U. Mityakov, S.A. Mogaiskiy, S.Z. Sapognikov
Krylov Shipbuilding research Institute, Russia, Saint-Petersburg State Polytechnical University, Russia

A tip vortces spreading downstream the wing attached to the flat surface

This paper introduces experimental and computational fluid dynamics researches of the tip vortex structure spreading downstream the wing. The wing was attached to the flat surface. Flow structure visualization in several cuts downstream the wing were realize by the PIV method. As a result the vortex trajectories and velocity fields were obtained in the far fields of the wing.
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