Fluidic wallpaper: An active control concept for low frequency broadband noise

M Czech, A Andersson - 9th AIAA/CEAS Aeroacoustics Conference and …, 2003 - arc.aiaa.org
The fluidic wallpaper is a novel concept to reduce lowfrequency broadband noise, operating
entirely in the fluid domain without any moving parts or electrical wiring. Pressure …

Contrôle actif multi-actionneur des nuisances en écoulements internes

J Tartarin, S Renault - Comptes Rendus de l'Académie des Sciences-Series …, 2000 - Elsevier
Experimentally, we demonstrate the feasability of a device build from the association of two
kinds of actuators, with specific controllers, to actively control the perturbations generated by …

A numerical study of an acoustic–hydrodynamic system exhibiting an intermittent prelude to instability

M Kamin, J Mathew, RI Sujith - International Journal of …, 2019 - journals.sagepub.com
A model problem comprising two subsytems (acoustic and hydrodynamic), both admitting
unsteady flows, has been studied using numerical simulations. Simulations capture all key …

Active control of coherent structures on an axisymmetric jet

M Marques Goncalves, S Salehian… - AIAA SCITECH 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-0123. vid The primary objective of
this work is to develop a high-fidelity simulation model for active jet noise control predictions …

Actuator selection and placement for linear feedback control of compressible flows

M Natarajan - 2017 - ideals.illinois.edu
Actuator and sensor placement for active control of high-Reynolds number flows is largely
based on experience and trial-and-error because of the system's large dimensionality and …

Global response to forcing in a subsonic jet: instability wavepackets and acoustic radiation

X Garnaud, RD Sandberg, L Lesshafft - 19th AIAA/CEAS Aeroacoustics …, 2013 - arc.aiaa.org
19th AIAA/CEAS Aeroacoustics Conference : Global response to forcing in a subsonic jet:
instability wavepackets and acoustic rad Page 1 Global response to forcing in a subsonic jet …

An investigation of airfoil dual acoustic feedback mechanisms at low-to-moderate Reynolds number

E Arcondoulis, CJ Doolan, AC Zander… - Journal of Sound and …, 2019 - Elsevier
An experimental investigation was performed in an anechoic wind tunnel involving acoustic
measurements, hot-wire anemometry and surface flow visualisation techniques to …

The use of micro-jets for airfoil self-noise control

M Szoke, D Fiscaletti, M Azarpeyvand - 2018 AIAA/CEAS Aeroacoustics …, 2018 - arc.aiaa.org
The current work is an experimental investigation on the use of open-loop flow control
techniques to reduce trailing edge noise of a flat plate. An array of inclined transverse jet …

Active control of cavity aeroacoustics in high speed flows

A Vakili, R Wolfe, T Nagle, E Lambert - 33rd Aerospace sciences …, 1995 - arc.aiaa.org
The research presented in this paper has been directed to study the effects of mass injection
into the flow upstream of a cavity to actively control the development of upstream boundary …

Large-Scale Simulations of Acoustic Synthetic Jets

M Mankbadi - 48th AIAA Aerospace Sciences Meeting Including the …, 2010 - arc.aiaa.org
A Large-Scale Simulations (LSS) code is developed herein to model and optimize the
performance of a synthetic jet device when the forcing amplitude is an acoustic wave …