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An Atmospheric Pressure Plasma Setup to Investigate the Reactive Species Formation
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Sensing and control of flow separation using plasma actuators.

Thomas C Corke1, Patrick O Bowles, Chuan He

  • 1University of Notre Dame, Institute for Flow Physics and Control, Hessert Laboratory for Aerospace Research, Notre Dame, IN 46556, USA. tcorke@nd.edu

Philosophical Transactions. Series A, Mathematical, Physical, and Engineering Sciences
|March 9, 2011
PubMed
Summary

Plasma actuators can control airflow separation. A new method uses surface pressure sensors to detect imminent separation for effective flow control on airfoils.

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Area of Science:

  • Fluid dynamics
  • Aerospace engineering
  • Plasma physics

Background:

  • Single dielectric barrier discharge plasma actuators are utilized for flow separation control.
  • Optimized pulsing frequencies of plasma actuators can induce coherent spanwise vortices, enhancing control effectiveness.

Purpose of the Study:

  • To demonstrate a novel flow separation indicator using surface pressure sensors.
  • To propose and validate a feedback control strategy for flow separation on airfoils.

Main Methods:

  • Utilizing spanwise-oriented asymmetric electrodes in plasma actuators.
  • Applying short-time spectral analysis of surface pressure sensor data.
  • Testing on an airfoil with increasing angle of attack and a sinusoidally pitching airfoil.

Main Results:

  • Surface pressure sensors can detect the onset of flow separation.
  • The proposed feedback control successfully managed flow separation on an airfoil.

Conclusions:

  • Plasma actuator pulsing can be sensed to indicate flow separation.
  • This sensing capability enables effective feedback control for aerodynamic applications.