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Real-time feedback control of 3D Tollmien-Schlichting waves using a dual-slot actuator geometry

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Title: Real-time feedback control of 3D Tollmien-Schlichting waves using a dual-slot actuator geometry
Authors: Vemuri, H
Bosworth, R
Morrison, JF
Kerrigan, EC
Item Type: Journal Article
Abstract: The growth of Tollmien-Schlichting (TS) waves is experimentally attenuated using a single-input and single-output (SISO) feedback system, where the TS wave packet is generated by a surface point source in a flat-plate boundary layer. The SISO system consists of a single wall-mounted hot wire as the sensor and a miniature speaker as the actuator. The actuation is achieved through a dual-slot geometry to minimise the cavity near-field effects on the sensor. The experimental set-up to generate TS waves or wave packets is very similar to that used by Li and Gaster [1]. The aim is to investigate the performance of the SISO control system in attenuating single-frequency, two-dimensional disturbances generated by these configurations. The necessary plant models are obtained using system identification, the controllers are then designed based on the models and implemented in real-time to test their performance. Cancellation of the rms streamwise velocity fluctuation of TS waves is evident over a significant domain.
Issue Date: 21-May-2018
Date of Acceptance: 19-Apr-2018
URI: http://hdl.handle.net/10044/1/59231
DOI: https://dx.doi.org/10.1103/PhysRevFluids.3.053903
ISSN: 2469-990X
Publisher: American Physical Society
Journal / Book Title: Physical Review Fluids
Volume: 3
Issue: 3
Copyright Statement: ©2018 American Physical Society
Sponsor/Funder: Engineering & Physical Science Research Council (E
EADS UK Limited
Funder's Grant Number: EP/I037946/1
PO 8000031666/U01
Keywords: Science & Technology
Physical Sciences
Physics, Fluids & Plasmas
Physics
LAMINAR-INSTABILITY WAVES
BOUNDARY-LAYER
ACTIVE CONTROL
TRANSITION
DISTURBANCES
CANCELLATION
Publication Status: Published
Article Number: 053903
Appears in Collections:Electrical and Electronic Engineering
Aeronautics
Faculty of Engineering