Streak control within a turbulent boundary layer using streamwise arrays of plasma actuators
M. Hennevelt (TU Delft - Aerospace Engineering)
F. Scarano – Mentor (TU Delft - Flow Physics and Technology)
G.E. Elsinga – Mentor (TU Delft - Fluid Mechanics)
Marios Marios – Mentor (TU Delft - Aerodynamics)
S Ghaemi – Mentor (TU Delft - Aerodynamics)
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Abstract
The coherent structures within the turbulent boundary layers have been investigated extensively over the past five decades. In particular, the long alternating low- and high speed streaks in the near-wall region. Along these streaks ejection and sweep events occur which play a major role in the production of Reynolds shear stress. Hence, studies on turbulent boundary layer control were focused on manipulating the low-speed streaks, to either reduce wall skin-friction by attenuating the streaks or by intensifying the streaks for separation control.