On présente le contrôle actif des instabilités aéroacoustiques générées en cavité sous écoulement affleurant effectué à l'aide de la mise en vibration du bord aval de la cavité. Mesures de pression et vélocimétrie par images de particules synchronisée montrent qu'il est possible de moduler l'amplitude des oscillations de la couche de mélange afin d'atténuer ou d'amplifier le bruit rayonné par l'écoulement. Les résultats fournis par un modèle analytique développé au préalable permettent de caractériser les effets du contrôle.
Active control of the aeroacoustics of flow-induced oscillations in a rectangular cavity using a vibrating plate inserted at the downstream edge is demonstrated. Pressure and phase-locked Particle Image Velocimetry measurements show that the oscillations of the mixing layer can be controlled in order to attenuate or amplify the radiated sound. Results obtained from a previously developed analytical model are used to characterize the effects of the control.
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Mots clés : Mécanique des fluides, Acoustique, Expérimental, Instabilité, Contrôle, PIV
Ludovic Chatellier 1 ; Janick Laumonier 1 ; Yves Gervais 2
@article{CRMECA_2006__334_4_259_0, author = {Ludovic Chatellier and Janick Laumonier and Yves Gervais}, title = {Active control of the aeroacoustics of cavity flows from the downstream edge}, journal = {Comptes Rendus. M\'ecanique}, pages = {259--265}, publisher = {Elsevier}, volume = {334}, number = {4}, year = {2006}, doi = {10.1016/j.crme.2006.03.003}, language = {en}, }
TY - JOUR AU - Ludovic Chatellier AU - Janick Laumonier AU - Yves Gervais TI - Active control of the aeroacoustics of cavity flows from the downstream edge JO - Comptes Rendus. Mécanique PY - 2006 SP - 259 EP - 265 VL - 334 IS - 4 PB - Elsevier DO - 10.1016/j.crme.2006.03.003 LA - en ID - CRMECA_2006__334_4_259_0 ER -
Ludovic Chatellier; Janick Laumonier; Yves Gervais. Active control of the aeroacoustics of cavity flows from the downstream edge. Comptes Rendus. Mécanique, Volume 334 (2006) no. 4, pp. 259-265. doi : 10.1016/j.crme.2006.03.003. https://comptes-rendus.academie-sciences.fr/mecanique/articles/10.1016/j.crme.2006.03.003/
[1] Wind tunnel experiments of the flow over rectangular cavities at subsonic and transonic speeds, Aero. Res. Counc. R. & M., Volume 3438 (1964)
[2] H.H. Heller, D.B. Bliss, Flow-induced pressure fluctuations in cavities and concepts for their suppression, AIAA paper 75-491, 1975, pp. 281–296
[3] Suppression of aerodynamically induced cavity pressure oscillations, J. Acoust. Soc. Am., Volume 66 (1979) no. 3, pp. 880-884
[4] M.J. Staneck, G. Raman, V. Kibens, J.A. Ross, J. Odedra, J.W. Peto, Suppression of cavity resonance using high frequency forcing—the characteristic signature of effective devices, in: 7th AIAA/CEAS Aeroacoustics Conference and Exhibit, Maastricht, The Netherlands, May 2001, pp. 2001–2128
[5] Contrôle actif des oscillations dans les cavités excitées par un écoulement, C. R. Acad. Sci., Volume 303 (1986) no. 12, pp. 1085-1088
[6] On the active control of shear layer oscillations across a cavity in the presence of pipeline acoustic resonance, J. Fluids Structures, Volume 5 (1991), pp. 207-219
[7] Influence of adaptive control on vortex-driven instabilities in a scaled model of solid propellant motors, J. Sound Vib., Volume 262 ( May 2003 ) no. 5, pp. 1009-1046
[8] Experimental investigation of oscillations in flows over shallow cavities, AIAA Journal, Volume 15 ( July 1977 ) no. 7, pp. 984-991
[9] R.H. Cabell, M.A. Kegerise, D.E. Cox, G.P. Gibbs, Experimental feedback control of flow induced cavity tones, in: 8th AIAA/CEAS Aeroacoustics Conference and Exhibit, Breckenridge, Colorado, June 2002, pp. 2002–2497
[10] Suppression of flow-induced pressure oscillations in cavities, J. Aircraft, Volume 31 ( January 1994 ) no. 1, pp. 90-96
[11] L.N. Cattafesta, III, S. Garg, M. Choudari, F. Li, Active control of flow-induced cavity resonance, AIAA paper 97-1804, 1997
[12] C.W. Rowley, V. Juttijudata, D.R. Williams, Cavity flow control simulations and experiments, in: 43rd AIAA Aerospace Sciences Meeting, January 2005
[13] T. Kestens, F. Nicoud, Active control of unsteady flow over a rectangular cavity, in: 4th AIAA/CEAS Aeroacoustics Conference and Exhibit, Toulouse, France, 98-2348, May 1998
[14] T. Kestens, Etude numérique du controle adaptatif multivoies des instabilités aéroacoustiques des cavités, PhD thesis, Institut National Polytechnique de Toulouse, 1999
[15] Review: Self-sustaining oscillations of flow past cavities, J. Fluids Eng., Volume 100 (1978), pp. 152-165
[16] Theoretical and experimental investigations in low Mach number turbulent cavity flows, Experiments in Fluids, Volume 36 ( May 2004 ) no. 5, pp. 728-740
[17] L. Chatellier, Modélisation et contrôle actif des instabilités aéroacoustiques en cavité sous écoulement affleurant, PhD thesis, Université de Poitiers, 2002
[18] Edge, cavity and aperture tones at very low Mach numbers, J. Fluid Mech., Volume 330 (1996), pp. 61-84
[19] Low Strouhal number instabilities of flow over apertures and wall cavities, J. Acoust. Soc. Am., Volume 102 (1997) no. 2, pp. 772-780
[20] Acoustics of Fluid-Structure Interactions, Cambridge Univ. Press, Cambridge, UK, 1998
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