High Bandwidth Powered Resonance Tube Actuators with Feedback Control

Author:

Khanafseh Samer1,Raman Ganesh1,Cain Alan2

Affiliation:

1. Illinois Institute of Technology

2. Innovative Technology Applications Company

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. Brocher,E., Maresca,C.andBournay,M.H. 1970Fluiddynamicsoftheresonancetube.J. FluidMech.Vol.43,part2,pp. 369-384.

2. Cain,A.B. 1997PrivateComunicationon theuseofhighfiequencyexcititiontosuppress flowinducedresonance.

3. On a New Method for the Generation of Sound-Waves

4. Hartmann,J. 1931Ontheproductionof acousticwavesbymeansofanair-jetofavelocity exceedingthatofsound.PhilMag.AndJ.Sci.XI, 926.

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1. Powered resonance tubes: resonance characteristics and actuation signal directivity;Experiments in Fluids;2005-09-30

2. Active Control of a Sonic Transverse Jet in Supersonic Cross-Flow Using a Powered Resonance Tube;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

3. Simulation of Powered Resonance Tubes: Helmholtz Resonator Geometries;2nd AIAA Flow Control Conference;2004-06-20

4. Actuation Signal Directivity and Supply Pressure Effects in Powered Resonance Tubes;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

5. Simulation of Powered Resonance Tubes: Understanding Parameter Space;9th AIAA/CEAS Aeroacoustics Conference and Exhibit;2003-05-12

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