Skin-friction drag reduction via robust reduced-order linear feedback control

被引:30
作者
Cortelezzi, L [1 ]
Lee, KH
Kim, J
Speyer, JL
机构
[1] Univ Calif Los Angeles, Dept Aerosp & Mech Engn, Los Angeles, CA 90095 USA
[2] Univ Calif Los Angeles, Dept Math, Los Angeles, CA 90095 USA
基金
美国国家航空航天局;
关键词
robust feedback flow control; model reduction; shear flows; skin-friction; drag reduction;
D O I
10.1080/10618569808940866
中图分类号
O3 [力学];
学科分类号
08 [工学]; 0801 [力学];
摘要
A successful application of a linear controller to a two-dimensional channel flow is presented. An optimal and robust reduced-order linear feedback controller is derived by using multi-variable linear-quadratic-Gaussian synthesis, or, in modern term, H-2 synthesis, combined with model reduction techniques. This controller based on a reduced-model of the linearized Navier - Stokes equations is applied to suppress finite-amplitude near-wall disturbances in a channel flow at Re = 1500. The controller efficiently reduced near-wall disturbances obtaining a substantial drag reduction and eventually the flow is relaminarized.
引用
收藏
页码:79 / +
页数:17
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