Experimental Model-Based Estimation and Control of Natural Tollmien-Schlichting Waves

被引:10
作者
Tol, H. J. [1 ]
de Visser, C. C. [1 ]
Kotsonis, M. [1 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, NL-2629 HS Delft, Netherlands
关键词
TRANSITION; FLOW;
D O I
10.2514/1.J057209
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A compensator strategy based on the linearized Navier-Stokes equations, aimed to suppress Tollmien-Schlichting waves naturally occurring in low freestream turbulence conditions, is experimentally demonstrated. Experiments have been conducted on a flat-plate geometry under the influence of an externally imposed adverse pressure gradient. A Kalman filter is used to estimate the effect of upstream disturbances based on pressure information from a single wall-embedded microphone. This information is used by the controller to cancel the incoming perturbations using a surface dielectric barrier discharge plasma actuator. The estimates obtained from the Kalman filter are compared with experimental data obtained using particle image velocimetry. It is shown that the Kalman filter is able to estimate the spatiotemporal behavior of the perturbation field even though it relies on a priori assumptions on the upstream disturbance environment. The performance of the controller and its robustness to varying freestream velocities are analyzed in comparison with open-loop continuous forcing. It is shown that the controller is able to additionally reduce the fluctuating pressure power at the most amplified frequencies with more than one order of magnitude and is capable of reducing the standard deviation of the downstream sensor signal between 30 and 60% for a range of offdesign freestream velocities.
引用
收藏
页码:2344 / 2355
页数:12
相关论文
共 33 条
  • [1] Input-Output Analysis and Control Design Applied to a Linear Model of Spatially Developing Flows
    Bagheri, S.
    Henningson, D. S.
    Hoepffner, J.
    Schmid, P. J.
    [J]. APPLIED MECHANICS REVIEWS, 2009, 62 (02) : 1 - 27
  • [2] Input-output analysis, model reduction and control of the flat-plate boundary layer
    Bagheri, Shervin
    Brandt, Luca
    Henningson, Dan S.
    [J]. JOURNAL OF FLUID MECHANICS, 2009, 620 : 263 - 298
  • [3] FEEDBACK-CONTROL OF FLEXIBLE SYSTEMS
    BALAS, MJ
    [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1978, 23 (04) : 673 - 679
  • [4] Feedback control of instabilities in the two-dimensional Blasius boundary layer: The role of sensors and actuators
    Belson, Brandt A.
    Semeraro, Onofrio
    Rowley, Clarence W.
    Henningson, Dan S.
    [J]. PHYSICS OF FLUIDS, 2013, 25 (05)
  • [5] BEWLEY T, 1949, J FLUID MECH, V365, P305
  • [6] Output Feedback Control of Blasius Flow with Leading Edge Using Plasma Actuator
    Dadfar, Reza
    Semeraro, Onofrio
    Hanifi, Ardeshir
    Henningson, Dan S.
    [J]. AIAA JOURNAL, 2013, 51 (09) : 2192 - 2207
  • [7] On active control of laminar-turbulent transition on two-dimensional wings
    Erdmann, Ralf
    Paetzold, Andreas
    Engert, Marcus
    Peltzer, Inken
    Nitsche, Wolfgang
    [J]. PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2011, 369 (1940): : 1382 - 1395
  • [8] On the role of adaptivity for robust laminar flow control
    Fabbiane, Nicolo
    Simon, Bernhard
    Fischer, Felix
    Grundmann, Sven
    Bagheri, Shervin
    Henningson, Dan S.
    [J]. JOURNAL OF FLUID MECHANICS, 2015, 767 : R1 - R12
  • [9] Feed-forward control of a perturbed backward-facing step flow
    Gautier, N.
    Aider, J. -L.
    [J]. JOURNAL OF FLUID MECHANICS, 2014, 759 : 181 - 196
  • [10] Laminar flow control with distributed surface actuation: damping Tollmien-Schlichting waves with active surface displacement
    Goldin, Nikolas
    King, Rudibert
    Paetzold, Andreas
    Nitsche, Wolfgang
    Haller, Daniel
    Woias, Peter
    [J]. EXPERIMENTS IN FLUIDS, 2013, 54 (03)