Titlebook: Active Flow Control II; Papers Contributed t Rudibert King Conference proceedings 20101st edition Springer-Verlag Berlin Heidelberg 2010 Pi

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Starting at the Bottom: The Authorsairfoil incidence variations are accounted for by using the velocity at the boundary layer edge at the actuation location, rather than the fixed free-stream velocity as a velocity scale. The main finding of this study is that the Reynolds number scaled momentum coefficient provides good amplitude sc

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https://doi.org/10.1007/978-3-031-43352-8 were determined by a six-component balance. In addition, pressure measurements in the middle section of the model as well as TR-PIV measurements were carried out. All experiments were conducted in the Collaborative Research Centre 557 . set up at the Berlin University of Technology.

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Kyriaki Hadjiafxendi,Polina Mackayown, that this approach is very effective in controlling higher order mode sound fields at blade passage frequency and its harmonics. The main goal of the present work is to introduce fast feedback control to this application.

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1612-2909 hnology, sensing, robust and optimal open- and closed-loop cThe interest in the field of active flow control (AFC) is steadily increasing. In - cent years the number of conferences and special sessions devoted to AFC org- ized by various institutions around the world continuously rises. New advanced

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