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articles
1.David RAUS, Benjamin COTTÉ, Romain MONCHAUX, Emmanuel JONDEAU, Pascal SOUCHOTTE, Michel ROGERorcid_16x16.png (2022).
Experimental study of the dynamic stall noise on an oscillating airfoil
J. Sound Vib. 537, 117144 (18 pages). doi:10.1016/j.jsv.2022.117144 doi.ico clarivate_16x16.png
2.Michel ROGERorcid_16x16.png, Daniel ACEVEDO GIRALDOorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2022).
Acoustic versus aerodynamic installation effects on a generic propeller-driven flying architecture
Int. J. Aeroacoustics 21, 585–609. doi:10.1177/1475472X221107372 doi.ico hal.ico clarivate_16x16.png
3.Gabriele GRASSOorcid_16x16.png, Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2022).
Advances in the prediction of the statistical properties of wall-pressure fluctuations under turbulent boundary layers
Fluids 7, 161 (19 pages). doi:10.3390/fluids7050161 doi.ico clarivate_16x16.png
4.Georgios BAMPANIS, Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2022).
On a three-dimensional investigation of airfoil turbulence-impingement noise and its reduction by leading-edge tubercles
J. Sound Vib. 520, 116635 (18 pages). doi:10.1016/j.jsv.2021.116635 doi.ico clarivate_16x16.png
5.Gabriele GRASSOorcid_16x16.png, Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2021).
Analytical model of the source and radiation of sound from the trailing edge of a swept airfoil
J. Sound Vib. 493, 115838 (21 pages). doi:10.1016/j.jsv.2020.115838 doi.ico hal.ico clarivate_16x16.png
6.Lap NGUYEN, Vladimir V. GOLUBEV, Reda R. MANKBADI, Gyuzel R. YAKHINA, Michel ROGERorcid_16x16.png (2021).
Numerical investigation of tonal trailing-edge noise radiated by low Reynolds number airfoils
Applied Sciences 11, 2257 (29 pages). doi:10.3390/app11052257 doi.ico hal.ico clarivate_16x16.png
7.Gabriele GRASSOorcid_16x16.png, Haiquan WU, Susanna ORESTANO, Marlène SANJOSÉorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2021).
CFD-based prediction of wall-pressure spectra under a turbulent boundary layer with adverse pressure gradient
Aeronaut. J. 12, 125–133. doi:10.1007/s13272-020-00484-5 doi.ico hal.ico clarivate_16x16.png
8.David LAMIDELorcid_16x16.png, Guillaume DAVILLERorcid_16x16.png, Michel ROGERorcid_16x16.png, Hélène POSSONorcid_16x16.png (2021).
Numerical prediction of the aerodynamics and acoustics of a tip leakage flow using large-eddy simulation
Int. J. Turbomach. Propuls. Power 6, 27 (16 pages). doi:10.3390/ijtpp6030027 doi.ico hal.ico clarivate_16x16.png
9.Gabriele GRASSOorcid_16x16.png, P. JAISWAL, Hao WUorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2019).
Analytical models of the wall-pressure spectrum under a turbulent boundary layer with adverse pressure gradient
J. Fluid Mech. 877, 1007–1062. doi:10.1017/jfm.2019.616 doi.ico hal.ico clarivate_16x16.png
10.Michel ROGERorcid_16x16.png, Korcan KUCUKCOSKUN (2019).
Near-and-far field modeling of advanced tail-rotor noise using source-mode expansions
J. Sound Vib. 453, 328–354. doi:10.1016/j.jsv.2019.02.007 doi.ico hal.ico clarivate_16x16.png
11.Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2018).
Advanced noise modeling for future propulsion systems
Int. J. Aeroacoustics 17, 576–599. doi:10.1177/1475472X18789005 doi.ico hal.ico clarivate_16x16.png
12.Michel ROGERorcid_16x16.png, Benjamin FRANCOIS (2017).
Combined analytical models for sound generation and transmission in cambered axial-flow outlet guide vanes
Eur. J. Mech. B-Fluids 61, 218–225. doi:10.1016/j.euromechflu.2016.10.006 doi.ico hal.ico clarivate_16x16.png
13.Michael E. QUAGLIA, Thomas LÉONARD, Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2017).
A 3D analytical model for orthogonal blade-vortex interaction noise
J. Sound Vib. 399, 104–123. doi:10.1016/j.jsv.2017.03.023 doi.ico hal.ico clarivate_16x16.png
14.Marlène SANJOSÉorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Miguel PESTANA, Michel ROGERorcid_16x16.png (2017).
Effect of weak outlet-guide-vane heterogeneity on rotor-stator tonal noise
AIAA J. 55, 3440–3457. doi:10.2514/1.J055525 doi.ico hal.ico clarivate_16x16.png
15.Simon BOULEY, Benjamin FRANCOIS, Michel ROGERorcid_16x16.png, Hélène POSSONorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2017).
On a two-dimensional mode-matching technique for sound generation and transmission in axial-flow outlet guide vanes
J. Sound Vib. 403, 190–213. doi:10.1016/j.jsv.2017.04.031 doi.ico hal.ico clarivate_16x16.png
16.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Korcan KUCUKCOSKUN (2016).
On sound scattering by rigid edges and wedges in a flow, with applications to high-lift device aeroacoustics
J. Sound Vib. 362, 252–275. doi:10.1016/j.jsv.2015.10.004 doi.ico hal.ico clarivate_16x16.png
17.Michel ROGERorcid_16x16.png, Benjamin FRANCOIS, Stéphane MOREAUorcid_16x16.png (2016).
Cascade trailing-edge noise modeling using a mode-matching technique and the edge-dipole theory
J. Sound Vib. 382, 310–327. doi:10.1016/j.jsv.2016.06.035 doi.ico hal.ico clarivate_16x16.png
18.Michel ROGERorcid_16x16.png, Christophe SCHRAM, Stéphane MOREAUorcid_16x16.png (2014).
On vortex-airfoil interaction noise including span-end effects, with application to open-rotor aeroacoustics
J. Sound Vib. 333, 283–306. doi:10.1016/j.jsv.2013.09.012 doi.ico hal.ico clarivate_16x16.png
19.Vladimir V. GOLUBEV, Lap NGUYEN, Reda R. MANKBADI, Michel ROGERorcid_16x16.png, Miguel R. VISBAL (2014).
On flow-acoustic resonant interactions in transitional airfoils
Int. J. Aeroacoustics 13, 1–38. doi: 10.1260/1475-472X.13.1-2.1 doi.ico hal.ico clarivate_16x16.png
20.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2012).
Addendum to the back-scattering correction of Amiet's trailing-edge noise model
J. Sound Vib. 331, 5383–5385. doi:10.1016/j.jsv.2012.06.019 doi.ico clarivate_16x16.png
21.Benoît G. MARINUS, W. BOSSCHAERTS, Michel ROGERorcid_16x16.png (2012).
Aerodynamic study of a 'humpy' propeller
International Journal of Engineering Systems Modelling and Simulation 4, 27–35. doi:10.1504/IJESMS.2012.044841 doi.ico clarivate_16x16.png
22.Hélène POSSONorcid_16x16.png, Michel ROGERorcid_16x16.png (2011).
Experimental validation of a cascade response function for fan broadband noise predictions
AIAA J. 49, 1907–1918. doi:10.2514/1.J050728 doi.ico clarivate_16x16.png
23.Hélène POSSONorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2011).
Broadband noise prediction of fan outlet guide vane using a cascade response function
J. Sound Vib. 330, 6153–6183. doi:10.1016/j.jsv.2011.07.040 doi.ico clarivate_16x16.png
24.Y.J. MOON, J.H. SEO, Y.M. BAE, Michel ROGERorcid_16x16.png, S. BECKER (2010).
A hybrid prediction method for low-subsonic turbulent flow noise
Comput. Fluids 39, 1125–1135. doi:10.1016/j.compfluid.2010.02.005 doi.ico clarivate_16x16.png
25.Hélène POSSONorcid_16x16.png, Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2010).
On a uniformly valid analytical rectilinear cascade response function
J. Fluid Mech. 663, 22–52. doi:10.1017/S0022112010003368 doi.ico clarivate_16x16.png
26.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2010).
Extensions and limitations of analytical airfoil broadband noise models
Int. J. Aeroacoustics 9, 273–305.
27.Michel ROGERorcid_16x16.png (2010).
On broadband jet-ring interaction noise and aerofoil turbulence-interaction noise predictions
J. Fluid Mech. 653, 337–364. doi:10.1017/S0022112010000285 doi.ico clarivate_16x16.png
28.Hélène POSSONorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2010).
On the use of a uniformly valid analytical cascade response function for fan broadband noise predictions
J. Sound Vib. 329, 3721–3743. doi:10.1016/j.jsv.2010.03.009 doi.ico clarivate_16x16.png
29.Yannick ROZENBERG, Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2010).
Rotating blade trailing-edge noise : experimental validation of analytical model
AIAA J. 48, 951–962. doi:10.2514/1.43840 doi.ico clarivate_16x16.png
30.A. GUEDEL, Yannick ROZENBERG, Michel ROGERorcid_16x16.png, G. PERRIN (2009).
Experimental validation of a model of fan trailing-edge noise
Noise Control Eng. J. 27, 318–326. doi:10.3397/1.3151955 doi.ico clarivate_16x16.png
31.M. WANG, Stéphane MOREAUorcid_16x16.png, G. IACCARINO, Michel ROGERorcid_16x16.png (2009).
LES prediction of wall-pressure fluctuations and noise of a low-speed airfoil
Int. J. Aeroacoustics 21, 177–197. doi:10.1260/147547208786940017 doi.ico clarivate_16x16.png
32.Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2009).
Back-scattering correction and further extensions of Amiet's trailing-edge noise model. Part II: Application
J. Sound Vib. 323, 397–425. doi:10.1016/j.jsv.2008.11.051 doi.ico clarivate_16x16.png
33.Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2007).
Competing broadband noise mechanisms in low-speed axial fans
AIAA J. 45, 48–57. doi:10.2514/1.14583 doi.ico clarivate_16x16.png
34.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, A. GUEDEL (2006).
Broadband fan noise prediction using single-airfoil theory
Noise Control Eng. J. 54, 5–14.
35.Michel ROGERorcid_16x16.png, Stéphane AUBERTorcid_16x16.png (2006).
Aeroacoustics of the bullroarer
Acta Acust. United Acust. 92, 826–841.
36.Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2005).
Effect of airfoil aerodynamic loading on trailing-edge noise sources.
AIAA J. 43, 41–52.
37.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2005).
Back-scattering correction and further extensions of Amiet's trailing-edge noise model. Part 1 : theory.
J. Sound Vib. 286, 477–506.
38.Damiano CASALINO, Michel ROGERorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2004).
Prediction of sound propagation in ducted potential flows using Green's function discretization.
AIAA J. 42, 736–744. doi:10.2514/1.1315 doi.ico hal.ico clarivate_16x16.png
39.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2004).
Broadband self-noise from loaded fan blades.
AIAA J. 42, 536–544.
40.Stéphane MOREAUorcid_16x16.png, Manuel HENNER, G. IACCARINO, M. WANG, Michel ROGERorcid_16x16.png (2003).
Analysis of flow conditions in freejet experiments for studying airfoil self-noise.
AIAA J. 41, 1895–1905.
41.Damiano CASALINO, Marc C. JACOBorcid_16x16.png, Michel ROGERorcid_16x16.png (2003).
Prediction of rod-airfoil interaction noise using the Ffowcs-Williams-Hawkings analogy.
AIAA J. 41, 182–191. doi:10.2514/2.1959 doi.ico hal.ico clarivate_16x16.png
42.Michel ROGERorcid_16x16.png (1997).
Introduction au numéro Spécial Salon du Bourget 1997.
Acoust. Tech. 10.
43.Michel ROGERorcid_16x16.png (1996).
Modélisation du bruit de raies d'un fenestron d'hélicoptère en vol d'avancement.
Acta Acustica 82, 238–250.
44.C. RAFFAITIN, Michel ROGERorcid_16x16.png, Libor RUFER, M. FABICKI (1994).
Caractérisation des sources de bruit aérodynamique sur un ventilateur centrifuge à flux axial.
Journal de Physique 4, Suppl. JPIII C5, 985–988.
45.Michel ROGERorcid_16x16.png (1994).
Sur l'utilisation d'un modèle de sillages pour le calcul du bruit d'interaction rotor-stator.
Acustica 80, 238–246.
46.Michel ROGERorcid_16x16.png (1994).
Contrôle du bruit aérodynamique des machines tournantes axiales par modulation de pales.
Exp. Fluids 80, 247–259.
47.Marc C. JACOBorcid_16x16.png, Michel ROGERorcid_16x16.png (1994).
Synthèse du bruit rayonné par une machine tournante carénée.
Journal de Physique 4, Suppl. JPIII C5, 981–984. doi:10.1051/jp4:19945215 doi.ico hal.ico clarivate_16x16.png
48.Marc C. JACOBorcid_16x16.png, Michel ROGERorcid_16x16.png (1990).
Diffraction de modes tournants par un écran axisymétrique - Etude théorique et expérimentale.
Journal de Physique (supplément) II, C2, 1177–1180. doi:10.1051/jphyscol:19902276 doi.ico hal.ico clarivate_16x16.png
49.Marc C. JACOBorcid_16x16.png, Michel ROGERorcid_16x16.png (1990).
Rayonnement acoustique d'une source ponctuelle située sur l'axe d'un écran mince de révolution. Etude théorique et expérimentale.
Journal d'Acoustique 3, 113–124. hal.ico
50.Francette FOURNIER, Michel ROGERorcid_16x16.png (1989).
Prédiction du bruit d'interaction rayonné par les fenestrons d'hélicoptères.
Journal d'Acoustique 2, 393–400.
51.Francette FOURNIER, Michel ROGERorcid_16x16.png (1989).
Prédiction du bruit d'interaction potentielles dans les machines tournantes. Application au fenestron d'hélicoptère.
C. r. Acad. sci., Sér. IIb Méc. 308, 831–834.
52.Francette FOURNIER, Michel ROGERorcid_16x16.png (1989).
Prédiction du bruit d'interaction de sillages dans les machines tournantes. Application au fenestron d'hélicoptère.
C. r. Acad. sci., Sér. IIb Méc. 308, 703–706.
 
thèses/hdr
1.Ignacio ZURBANO FERNANDEZ (dir.: Michel ROGER) (2021).
Reduction of the broadband noise of centrifugal fans used for HVAC in buildings
Thèse Université de Lyon hal.ico
2.Miguel PESTANA (dir.: Michel ROGER, Stéphane MOREAU) (2020).
Effets de stators hétérogènes sur le bruit d’interaction rotor-stator : étude analytique, expérimentale et numérique
Thèse Université de Lyon hal.ico
3.Vianney MASSONorcid_16x16.png (dir.: Michel ROGER, Stéphane MOREAU) (2018).
Propagation sonore dans un conduit annulaire traité en présence d’un écoulement moyen tournant et cisaillé : application à la prédiction du bruit à large-bande des soufflantes de turboréacteurs.
Thèse École centrale de Lyon
4.Justine GIEZ (dir.: Michel ROGER) (2018).
Effets de charge et de géométrie sur le bruit d’interaction rotor-rotor des doublets d’hélices contra-rotatives
Thèse École centrale de Lyon
5.Simon BOULEY (dir.: Michel ROGER, Jérôme ANTONI) (2017).
Modélisations analytiques du bruit tonal d’interaction rotor / stator par la technique de raccordement modal
Thèse École centrale de Lyon hal.ico
6.Nassim JAOUANI (dir.: Michel ROGER) (2017).
Modélisation des effets d’installation sur le bruit de raies rayonné par les hélices contrarotatives
Thèse École centrale de Lyon
7.Gyuzel R. YAKHINA (dir.: Michel ROGER, Vladimir V. GOLUBEV) (2017).
Experimental study of the tonal trailing-edge noise generated by low-Reynolds number airfoils and comparison with numerical simulations
Thèse École centrale de Lyon hal.ico
8.Benoit LEMOINE (dir.: Michel ROGER) (2013).
Etude aéroacoustique de configurations génériques de dispositifs hypersustentateurs par approches analytique et expérimentale
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2348_blemoine.pdf
9.Arnulfo CARAZO (dir.: Michel ROGER) (2012).
Analytical modelling of wake-interaction tonal noise in counter-rotating opten rotors
Thèse École centrale de Lyon
10.Arthur FINEZ (dir.: Marc C. JACOB, Michel ROGER) (2012).
Etude expérimentale du bruit de bord de fuite à large bande d?une grille d?aubes linéaire et de sa réduction par dispositifs passifs
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2267_afinez.pdf
11.Korcan KUCUKCOSKUN (dir.: Michel ROGER) (2012).
Prediction of free and scattered acoustic fields of low-speed fans
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2270_kkucukcoskun.pdf
12.Benoît G. MARINUS (dir.: Michel ROGER) (2011).
Multidisciplinary optimization of aircraft propeller blades
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2234_bmarinus.pdf
13.M. LEMOULT (dir.: Michel ROGER) (2010).
Bruit à large bande à l'éjection des turbomoteurs d'hélicoptères
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2217_mlemoult.pdf
14.Gabriel REBOUL (dir.: Michel ROGER) (2010).
Modélisation du bruit à large bande de soufflantes de turboréacteurs
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2192_greboul.pdf
15.Johanna INGENITO (dir.: Michel ROGER) (2010).
Vers une modélisation d'aide à la conception acoustique d'étages de compresseurs subsoniques de turbomachines
Thèse École centrale de Lyon
16.Frédéric SICOT (dir.: Francis LEBOEUF, Michel ROGER) (2009).
Simulation efficace des écoulements instationnaires périodiques en turbomachines
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/fsicot.pdf
17.Julien GRILLIAT (dir.: Marc C. JACOB, Michel ROGER) (2009).
Contribution à l'étude aéroacoustique des écoulements de jeu
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/jgrilliat.pdf
18.Hélène POSSONorcid_16x16.png (dir.: Michel ROGER) (2008).
Fonctions de réponse de grilles d'aubes et effet d'écran pour le bruit à large bande des soufflantes
Thèse École centrale de Lyon hal.ico
19.Johanna CHAPPUIS (dir.: Michel ROGER) (2007).
Modélisation analytique et numérique des effets d'installation sur le bruit des moteurs d'avions
Thèse École centrale de Lyon
20.Yannick ROZENBERG (dir.: Michel ROGER) (2007).
Contribution à la modélisation analytique du bruit à large bande des machines tournantes à l'aide de simulations RANS
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/yrozenberg.pdf
21.Y. DRUON (dir.: Michel ROGER) (2006).
Etude de la propagation et du rayonnement acoustique par les conduits d'éjection de turboréacteurs : modélisations analytiques et numériques.
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/ydruon.pdf
22.S. CARO (dir.: Michel ROGER) (2003).
Méthode de calcul du bruit de raies d'un ventilateur de refroidissement automobile.
Thèse École centrale de Lyon
23.Damiano CASALINO (dir.: Michel ROGER, Gianfranco CHIOCCHIA, Marc C. JACOB) (2002).
Analytical and numerical methods in vortex-body aeroacoustics.
Thèse Politecnico di Torino
24.Michel ROGERorcid_16x16.png (1989).
Habilitation Université Claude-Bernard Lyon 1
 
communications avec actes
1.Daniel ACEVEDO GIRALDOorcid_16x16.png, Michel ROGERorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Hadrien BÉRIOT (2022).
Experimental and analytical study of the aerodynamic noise emitted by distributed electric propulsion systems
28th AIAA/CEAS Aeroacoustics 2022 Conference, Southampton, United Kingdom. doi:10.2514/6.2022-2830 doi.ico hal.ico
In: proceeding of the 28th AIAA/CAES Aeroacoustics 2022 Conference , AIAA, Reston, Virginia, USA, Paper n°2022-2830 (17 pages). doi:10.2514/6.2022-2830 doi.ico hal.ico
2.Léo GIRIER, Michel ROGERorcid_16x16.png, Hadrien BÉRIOT, Anthony LAFITTE, Hélène POSSONorcid_16x16.png (2019).
A two-dimensional model of sound transmission through curved and staggered OGV: Effect of inter-vane channel mode transitions
25th AIAA/CEAS Aeroacoustics Conference, Delft, Netherlands. doi:10.2514/6.2019-2690 doi.ico hal.ico
In: Proceedings of the 25th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2019-2690. doi:10.2514/6.2019-2690 doi.ico hal.ico
3.Miguel PESTANA, Antonio PEREIRA, Édouard SALZE, Johan THISSE, Marlène SANJOSÉorcid_16x16.png, Emmanuel JONDEAU, Pascal SOUCHOTTE, Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Josselin REGNARD, Mathieu GRUBER (2017).
Aeroacoustics of an axial ducted low Mach-number stage: numerical and experimental investigation
23rd AIAA/CEAS Aeroacoustics Conference, Denver, United States. doi:10.2514/6.2017-3215 doi.ico hal.ico
In: Proceedings of the 23rd AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2017-3215 (22 pages). doi:10.2514/6.2017-3215 doi.ico hal.ico
4.Vladimir V. GOLUBEV, Lap NGUYEN, Warren HINER, Marco SANSONE, Saman SALEHIAN, Reda R. MANKBADI, Gyuzel R. YAKHINA, Michel ROGERorcid_16x16.png (2015).
Parametric investigations of tonal trailing-edge noise generation by moderate Reynolds number airfoils. Part II-numerical studies
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2528 doi.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2528 doi.ico
AIAA-2015-2528
5.Simon BOULEY, Benjamin FRANCOIS, Michel ROGERorcid_16x16.png, Hélène POSSONorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2015).
On a mode-matching technique for sound generation and transmission in a linear cascade of outlet guide vanes
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2825 doi.ico hal.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2825 doi.ico hal.ico
AIAA-2015-2825
6.Benjamin FRANCOIS, Simon BOULEY, Michel ROGERorcid_16x16.png, Hélène POSSONorcid_16x16.png (2015).
On the Kutta condition for the sound transmission through outlet guide vanes
CFM 2015 : Congrès Français de Mécanique, Lyon, France. hal.ico
In: Alain COMBESCURE (Ed.), Michel LANCE (Ed.), Actes du 22ème Congrès Français de Mécanique, Association Française de Mécanique, Courbevoie. hal.ico
7.Fabrice FALISSARD, P. ZEHNER, Michel ROGERorcid_16x16.png, Xavier GLOERFELT (2015).
Numerical and analytical investigation of orthogonal blade/vortex interaction noise
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2843 doi.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2843 doi.ico
8.Nassim JAOUANI, Michel ROGERorcid_16x16.png, Thomas NODÉ-LANGLOIS, Gilles SERRE (2015).
Analytical prediction of the pylon-wake effect on the tonal noise radiated by the front rotor of CROR propulsion systems
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2985 doi.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2985 doi.ico
AIAA-2015-2985
9.Gyuzel R. YAKHINA, Michel ROGERorcid_16x16.png, Emmanuel JONDEAU, Lap NGUYEN, Vladimir V. GOLUBEV (2015).
Parametric investigation of tonal trailing-edge noise generation by moderate-Reynolds number airfoils. Ppart I - Experimental studies
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2527 doi.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2527 doi.ico
AIAA-2015-2527
10.Michel ROGERorcid_16x16.png, Benjamin FRANCOIS, Stéphane MOREAUorcid_16x16.png (2015).
Towards cascade trailing-edge noise modeling using a mode-matching technique
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2541 doi.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2541 doi.ico
AIAA-2015-2541
11.Michel TOURNOUR, Mark BOYLE, Michel ROGERorcid_16x16.png, Pierre ROLAND, Jean-Michel PERRIN (2014).
Applying the hierarchical matrix bem solver to locomotive noise emissions
21st International Congress on Sound and Vibration, Beijing, China.
In: Proceedings of ICSV21, International Institute of Acoustics and Vibration, Auburn, USA .
12.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Aurélien MARSAN (2014).
Generation and transmission of spiral acoustic waves in multi-stage subsonic radial compressors
20th AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, United States.
In: Proceedings of the 20th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2014-3232.
13.Vladimir V. GOLUBEV, Lap NGUYEN, Warren HINER, Reda R. MANKBADI, Michel ROGERorcid_16x16.png, Jonathan G. DUDLEY, Miguel R. VISBAL (2014).
Effect of upstream turbulence on flow-Acoustic resonance interactions in transitional airfoils
20th AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, United States.
In: Proceedings of the 20th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2014-3303.
14.Michel ROGERorcid_16x16.png, Christophe SCHRAM, L. DE SANTANA (2013).
Reduction of airfoil turbulence-impingement noise by means of leading-edge serrations and/or porous materials
19th AIAA/CEAS Aeroacoustics Conference, Berlin, Germany.
In: Proceeding of the 19th AIAA/CEAS Aeroacoutics Conference, AIAA, Reston, Virginia, USA, AIAA-2013-2108 (20 pages).
15.Vladimir V. GOLUBEV, Lap NGUYEN, Reda R. MANKBADI, Michel ROGERorcid_16x16.png, Miguel R. VISBAL (2013).
Acoustic feedback-loop interactions in transitional airfoils
19th AIAA/CEAS Aeroacoustics Conference, Berlin, Germany.
In: Proceeding of the 19th AIAA/CEAS Aeroacoutics Conference, AIAA, Reston, Virginia, USA, AIAA-2013-2111.
16.Marlène SANJOSÉorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Julien CHRISTOPHE, Michel ROGERorcid_16x16.png (2012).
Effect of span and compressibility on the noise prediction of a Katana blade
18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, United States.
In: Proceedings of the 18th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2012-2112 (13 pages).
17.Benoit LEMOINE, Michel ROGERorcid_16x16.png (2012).
Aeroacoustic study of a simplified wing/flap system in generic configurations
Acoustics 2012 : 11ème Congrès Français d'Acoustique & 2012 Annual IOA Meeting, Nantes, France. hal.ico
In: Proceedings of the Acoustics 2012 Nantes Conference, SFA, Paris, 2365–2370. hal.ico
18.Michel ROGERorcid_16x16.png, Christophe SCHRAM, Stéphane MOREAUorcid_16x16.png (2012).
On open-rotor blade-vortex interaction noise
18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, United States.
In: Proceedings of the 18th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2012-2216 (21 pages).
19.Vladimir V. GOLUBEV, Lap NGUYEN, Jonathan G. DUDLEY, Michel ROGERorcid_16x16.png, Miguel R. VISBAL (2012).
High-accuracy simulations of flow-acoustic resonant interactions in airfoil transitional boundary layers
18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, United States.
In: Proceedings of the 18th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2012-2136.
20.Korcan KUCUKCOSKUN, Michel ROGERorcid_16x16.png (2012).
On the scattering of aerodynamic noise by a rigid corner
18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, United States.
In: Proceedings of the 18th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2012-2113 (17 pages).
21.Frédéric CONTE, Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Marlène SANJOSÉorcid_16x16.png, Patrice CAULE (2011).
Modeling of installation effects on the noise from subsonic axial fans
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2011-2948 (19 pages).
22.Benoît G. MARINUS, Michel ROGERorcid_16x16.png, R.A. VAN DEN BRAEMBUSSHE, W. BOSSCHAERTS (2011).
Multidisciplinary optimization of propeller blades: focus on the aeroacoustic results
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2011-2801 (20 pages).
23.Arthur FINEZ, Emmanuel JONDEAU, Michel ROGERorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2011).
Experimental investigation of trailing edge noise from a linear cascade of cambered airfoils
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States. doi:10.2514/6.2011-2876 doi.ico hal.ico
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2876. doi:10.2514/6.2011-2876 doi.ico hal.ico
24.Vladimir V. GOLUBEV, Lap NGUYEN, Michel ROGERorcid_16x16.png, Miguel R. VISBAL (2011).
On interaction of airfoil leading and trailing edge noise sources in turbulent
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2011-2859.
25.Arthur FINEZ, Emmanuel JONDEAU, Michel ROGERorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2011).
Broadband noise reduction of linear cascades with trailing edge serrations
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States. doi:10.2514/6.2011-2874 doi.ico hal.ico
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2874. doi:10.2514/6.2011-2874 doi.ico hal.ico
26.Louis CORRIVEAU, Marlène SANJOSÉorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Julien CHRISTOPHE, Michel ROGERorcid_16x16.png (2011).
Predictions of acoustic sources and self-noise of a Katana blade at Zero and high incidence
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2011-2933 (14 pages).
27.Arnulfo CARAZO, Michel ROGERorcid_16x16.png, M. OMAIS (2011).
Analytical prediction of wake-Interaction noise in counter-rotating propellers
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2758 (19 pages).
28.Benoit LEMOINE, Michel ROGERorcid_16x16.png, Ingrid LE GRIFFON (2011).
Aeroacoustics of a model non-lifting wing-flap system in a parallel flow,
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2735 (18 pages).
29.Benoît G. MARINUS, Michel ROGERorcid_16x16.png, R.A. VAN DEN BRAEMBUSSHE (2010).
Aeroacoustic and aerodynamic optimization of aircraft propeller blades
16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), Stockholm, Sweden.
In: Proceeding of the 16th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2010-3850 (17 pages).
30.Michel ROGERorcid_16x16.png, Arnulfo CARAZO (2010).
Blade-geometry considerations in analytical gust-airfoil interaction noise models
16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), Stockholm, Sweden.
In: Proceeding of the 16th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2010-3799 (17 pages).
31.Louis CORRIVEAU, Stéphane MOREAUorcid_16x16.png, Julien CHRISTOPHE, Michel ROGERorcid_16x16.png (2010).
Experimental and numerical unsteady acoustic sources and self-noise of a Katana blade
16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), Stockholm, Sweden.
In: Proceeding of the 16th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2010-3804 (17 pages).
32.Arthur FINEZ, Emmanuel JONDEAU, Michel ROGERorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2010).
Broadband noise reduction with trailing edge brushes
16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), Stockholm, Sweden. doi:10.2514/6.2010-3980 doi.ico hal.ico
In: Proceeding of the 16th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2010-3980 (13 pages). doi:10.2514/6.2010-3980 doi.ico hal.ico
33.Johanna INGENITO, Michel ROGERorcid_16x16.png (2009).
Measurement and prediction of the tonal noise of a centrifugal compressor at inlet
15th AIAA/CEAS Aeroacoustics Conference, Miami, United States.
In: Proceedings of the 15th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2009-3360 (18 pages).
34.Julien GRILLIAT, Emmanuel JONDEAU, Marc C. JACOBorcid_16x16.png, Michel ROGERorcid_16x16.png, Roberto CAMUSSIorcid_16x16.png (2008).
Broadband noise prediction models and measurements of tip leakage flows
14th AIAA/CEAS Aeroacoustics Conference, Vancouver, Canada. doi:10.2514/6.2008-2845 doi.ico hal.ico
In: Proceedings of the 14th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2008-2845. doi:10.2514/6.2008-2845 doi.ico hal.ico
35.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2008).
Edge scattering of distributed sources - application to high-lift device noise
14th AIAA/CEAS Aeroacoustics Conference, Vancouver, Canada.
In: Proceedings of the 14th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2008-2866 (18 pages).
36.Hélène POSSONorcid_16x16.png, Michel ROGERorcid_16x16.png (2008).
Experimental validation of a cascade response function for fan broadband noise predictions
14th AIAA/CEAS Aeroacoustics Conference, Vancouver, Canada.
In: Proceedings of the 14th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2008-2844 (20 pages).
37.Stéphane MOREAUorcid_16x16.png, Christophe SCHRAM, Michel ROGERorcid_16x16.png (2007).
Numerical modelling of realistic installation effects for airfoil broadband noise prediction and validation
Third International Symposium Fan Noise 2007, Lyon, France.
In: Proceedings of Fan Noise 2007, CETIAT, VILLEURBANNE.
38.Marc C. JACOBorcid_16x16.png, Julien GRILLIAT, Michel ROGERorcid_16x16.png, Roberto CAMUSSIorcid_16x16.png (2007).
Aeroacoustic investigation of a tip clearance flow
14th International Congress on Sound and Vibration, Caims, Australia. hal.ico
In: Proceedings of the 14th International Congress on Sound and Vibration, IIAV, Mechanical Engineering Department 270 Ross Hall Auburn University Auburn, AL 36849, USA. hal.ico
39.Stéphane MOREAUorcid_16x16.png, Christophe SCHRAM, Michel ROGERorcid_16x16.png (2007).
Diffraction effects on the trailing-edge noise measured in an open-jet anechoic wind-tunnel
13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy.
In: Proceedings of the 13th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2007-3409.
40.Yannick ROZENBERG, Michel ROGERorcid_16x16.png, A. GUEDEL, Stéphane MOREAUorcid_16x16.png (2007).
Rotating blade self noise : experimental validation of analytical models
13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy.
In: Proceedings of the 13th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2007-3709.
41.Hélène POSSONorcid_16x16.png, Michel ROGERorcid_16x16.png (2007).
Parametric study of gust scattering and sound transmission through a blade row
13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy.
In: Proceedings of the 13th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2007-3690.
42.Johanna INGENITO, Michel ROGERorcid_16x16.png (2007).
Analytical modelling of sound transmission through the passage of centrifugal compressors
13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy.
In: Proceedings of the 13th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2007-3704.
43.M. LEMOULT, A. VALLON, Michel ROGERorcid_16x16.png (2007).
Exhaust noise from helicopter turboshaft engines
8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Lyon, France.
In: Proceedings of the 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, , , ISAIF8-0019.
44.A. GUEDEL, Yannick ROZENBERG, Michel ROGERorcid_16x16.png (2007).
Prediction of fan broadband noise
Third International Symposium Fan Noise 2007, Lyon, France.
In: Proceedings of Fan Noise 2007, CETIAT, VILLEURBANNE.
45.Michel ROGERorcid_16x16.png (2007).
Near-field fan noise modelling and installation effects due to scattering surfaces
Third International Symposium Fan Noise 2007, Lyon, France.
In: Proceedings of Fan Noise 2007, CETIAT, VILLEURBANNE.
46.Michel ROGERorcid_16x16.png, Antoine MOREAU, Y.J. MOON (2006).
Fan broadband noise prediction using hybrid methods and analytical modeling
Inter-Noise 2006, Honolulu, United States.
In: Proceedings of Inter-Noise 2006, International Institute of Noise Control Engineering, Purdue University West Lafayette, USA, 4006–4015.
47.Johanna CHAPPUIS, J. RICOUARD, Michel ROGERorcid_16x16.png (2006).
Aft fan noise shielding by lifting surfaces : analytical, numerical and experimental results
12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2006-2617.
48.K. CHANG, J.H. SEO, Y.J. MOON, Michel ROGERorcid_16x16.png (2006).
Prediction of flat plate self-noise
12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2006-2513.
49.Yannick ROZENBERG, Michel ROGERorcid_16x16.png, Antoine MOREAU (2006).
Effect of blade design at equal loading on broadband noise
12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2006-2563 (20 pages).
50.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, A. GUEDEL (2006).
Vortex-shedding noise and potential-interaction noise modeling by a reversed Sears'problem
12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2006-2607 (18 pages).
51.J.H. SEO, Y.J. MOON, Marc C. JACOBorcid_16x16.png, Michel ROGERorcid_16x16.png (2006).
Computational prediction methods for the aerodynamic broadband noise generated from long-span bodies
Inter-Noise 2006, Honolulu, United States. hal.ico
In: Proceedings of Inter-Noise 2006, International Institute of Noise Control Engineering, Purdue University West Lafayette, USA, 4335–4344. hal.ico
 
communications sans actes
1.Benjamin FRANCOIS, Simon BOULEY, Michel ROGERorcid_16x16.png (2016).
On the Kutta condition for sound transmission in an annular cascade of vanes
16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, United States. hal.ico
2.A. GUEDEL, Arthur FINEZ, G. PERRIN, Michel ROGERorcid_16x16.png (2008).
Prediction of blade trailing-edge noise of an axial-flow fan
Acoustics'08, Paris, France.
3.M. WANG, Stéphane MOREAUorcid_16x16.png, G. IACCARINO, Michel ROGERorcid_16x16.png (2008).
LES prediction of wall-pressure fluctuations and noise of a low-speed airfoil
Acoustics'08, Paris, France.
4.Yannick ROZENBERG, Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2008).
Fan blade trailing-edge noise prediction using RANS simulations
Acoustics'08, Paris, France.
5.Michel ROGERorcid_16x16.png (2008).
Coupled oscillations in the aeroacoustics of a Katana blade
Acoustics'08, Paris, France.
6.Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2008).
Aero-acoustic installation effects in cooling fan systems - Part 2: near-field and ground effects
12th ISROMAC, Honolulu, United States.
paper 20223
7.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2008).
Aero-acoustic installation effects in cooling fan systems - Part 1: scattering by surrounding surfaces
12th ISROMAC, Honolulu, United States.
paper 20222
8.Johanna INGENITO, Michel ROGERorcid_16x16.png (2006).
Modélisation du rayonnement sonore par un front de grille d'aubes à l'aide d'une technique de raccordement modal
Bruit aérodynamique des Ventilateurs, Lyon, France.
9.Julien GRILLIAT, Marc C. JACOBorcid_16x16.png, Michel ROGERorcid_16x16.png (2006).
Caractérisation expérimentale et prédiction du bruit d'un jeu en extrémité de pale
Bruit aérodynamique des Ventilateurs, Lyon, France.
 
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