Global mode-based control of laminar and turbulent high-speed jets

Mahesh Natarajan; Jonathan B. Freund; Daniel J. Bodony

doi:10.1016/j.crme.2018.07.005

Global mode-based control of laminar and turbulent high-speed jets

Mahesh Natarajan ¹ ; Jonathan B. Freund ² ; Daniel J. Bodony ¹

¹ Department of Aerospace Engineering, University of Illinois at Urbana–Champaign, Urbana, IL 61801, USA
² Department of Mechanical Science & Engineering and Department of Aerospace Engineering, University of Illinois at Urbana–Champaign, Urbana, IL 61801, USA

Comptes Rendus. Mécanique, Volume 346 (2018) no. 10, pp. 978-996.

Résumé

The emitted noise from round jets is reduced using linear feedback controllers designed using structural sensitivity analysis. Linear global modes inform the selection and placement of the controller, and Navier–Stokes simulations are used to demonstrate effectiveness in a Mach-1.5 cold axisymmetric jet and in a Mach-0.9 cold turbulent jet. In both jets, each fitted with a cylindrical nozzle, the control reduces the radiated noise and modifies the baseflow in a way that enhances the relative amplitudes of low-frequency $St \approx 0.05$ global modes that do not have significant support in the acoustic field.

Reçu le : 2017-06-09
Accepté le : 2018-05-16
Publié le : 2018-08-14

DOI : 10.1016/j.crme.2018.07.005

Mots clés : Active flow control, Global modes, Jet noise

Affiliations des auteurs :

Mahesh Natarajan ¹ ; Jonathan B. Freund ² ; Daniel J. Bodony ¹

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Mahesh Natarajan; Jonathan B. Freund; Daniel J. Bodony. Global mode-based control of laminar and turbulent high-speed jets. Comptes Rendus. Mécanique, Volume 346 (2018) no. 10, pp. 978-996. doi : 10.1016/j.crme.2018.07.005. https://comptes-rendus.academie-sciences.fr/mecanique/articles/10.1016/j.crme.2018.07.005/

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Cité par Sources :

^☆ Financial support from the United States Office of Naval Research (Drs. Brenda Henderson, Joseph Doychak and Knox Millsaps, technical monitors) is gratefully acknowledged (grant no. N00014-13-1-0545). This material is also based in part upon work supported by the Department of Energy, National Nuclear Security Administration, under Award Number DE-NA0002374.

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