Closed-Loop Control of Unsteady Transient Growth Disturbances in a Blasius Boundary Layer using DBD Plasma Actuators

ORAL

Abstract

Plasma actuators have recently been shown to negate the effect of the transient growth instability occurring in a Blasius boundary layer for the purpose of delaying bypass transition. Specifically, during steady operation, the energy of a disturbance introduced via an array of static cylindrical roughness elements was reduced by up to 68\%, as shown by Hanson et al (Exp.\ Fluids, 2010). In the present work, the actuators used in the aforementioned study were integrated into a complete closed-loop control system capable of negating unsteady transient growth disturbances induced in a Blasius boundary layer established in a wind tunnel. Shear stress measurements from an array of hot-wires mounted just above the surface of the boundary-layer plate downstream of the actuators are used to provide feedback information about the state of the boundary layer. The effectiveness and robustness of the closed-loop controller are rigorously established based on both control-model simulations and experiments.

*NSERC and NSF grant number: CMMI 0932546

Authors

  • Philippe Lavoie

    • University of Toronto, Institute for Aerospace Studies
    • University of Toronto Institute for Aerospace Studies
    • University of Toronto
  • Ronald Hanson

    • University of Toronto, Institute for Aerospace Studies
  • Kyle Bade

    • Michigan State University
    • Michigan State University, Dept. of Mechanical Engineering
  • Ahmed Naguib

    • Michigan State University
    • Michigan State University, Dept. of Mechanical Engineering
  • Brandt Belson

    • Princeton University, Dept. of Mechanical and Aerospace Engineering
    • Princeton University
  • Clarence Rowley

    • Princeton University
    • Princeton University, Dept. of Mechanical and Aerospace Engineering