Streak control within a turbulent boundary layer using streamwise arrays of plasma actuators

Master Thesis (2012)
Author(s)

Marcel Hennevelt (TU Delft - Aerospace Engineering)

Contributor(s)

Fulvio Scarano – Mentor (TU Delft - Aerospace Engineering)

Gerrit Elsinga – Mentor (TU Delft - Mechanical Engineering)

Marios Kotsonis – Mentor (TU Delft - Aerospace Engineering)

Sina Ghaemi – Mentor (TU Delft - Aerospace Engineering)

Faculty
Aerospace Engineering
More Info
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Publication Year
2012
Language
English
Graduation Date
02-07-2012
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering
Faculty
Aerospace Engineering
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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.

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