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articles
1.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
2.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
3.Antonio ALGUACILorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2022).
Deep learning surrogate for the temporal propagation and scattering of acoustic waves
AIAA J. (17 pages). doi:10.2514/1.J061495 doi.ico hal.ico clarivate_16x16.png
4.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
5.Antonio ALGUACILorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2021).
Predicting the propagation of acoustic waves using deep convolutional neural networks
J. Sound Vib. 512, 116285 (23 pages). doi:10.1016/j.jsv.2021.116285 doi.ico hal.ico clarivate_16x16.png
6.Danny LEWISorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Marlène SANJOSÉorcid_16x16.png (2021).
ACAT1 fan stage broadband noise prediction using large-eddy simulation and analytical models
AIAA J. 60, 360–380. doi:10.2514/1.J060163 doi.ico hal.ico clarivate_16x16.png
7.Danny LEWISorcid_16x16.png, Jérôme DE LABORDERIE, Marlène SANJOSÉorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Vianney MASSONorcid_16x16.png (2021).
Parametric study on state-of-the-art analytical models for fan broadband interaction noise predictions
J. Sound Vib. 514, 116423 (28 pages). doi:10.1016/j.jsv.2021.116423 doi.ico hal.ico clarivate_16x16.png
8.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
9.Paul LAFFAY, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Josselin REGNARD (2020).
Experimental investigation of the noise radiated by a ducted air flow discharge though diaphragms and perforated plates
J. Sound Vib. 472, 115–177. doi:10.1016/j.jsv.2020.115177 doi.ico hal.ico clarivate_16x16.png
10.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
11.Vianney MASSONorcid_16x16.png, James R. MATHEWSorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Hélène POSSONorcid_16x16.png, Edward J. BRAMBLEYorcid_16x16.png (2018).
The impedance boundary condition for acoustics in swirling ducted flow
J. Fluid Mech. 849, 645–675. doi:10.1017/jfm.2018.429 doi.ico hal.ico clarivate_16x16.png
12.James R. MATHEWSorcid_16x16.png, Vianney MASSONorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Hélène POSSONorcid_16x16.png (2018).
The modified Myers boundary condition for swirling flow
J. Fluid Mech. 847, 868–906. doi:10.1017/jfm.2018.326 doi.ico hal.ico clarivate_16x16.png
13.Paul LAFFAY, Stéphane MOREAUorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Josselin REGNARD (2018).
Experimental study of the noise radiated by an air flow discharge through diaphragms and perforated plates
J. Sound Vib. 434, 145–165. doi:10.1016/j.jsv.2018.07.036 doi.ico hal.ico clarivate_16x16.png
14.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
15.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
16.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
17.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
18.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
19.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
20.Michaël BAUERHEIMorcid_16x16.png, Ignacio DURAN, Thomas LIVEBARDON, Gaofeng WANG, Stéphane MOREAUorcid_16x16.png, Thierry POINSOT (2016).
Transmission and reflection of acoustic and entropy waves through a stator-rotor stage
J. Sound Vib. 374, 260–278. doi:10.1016/j.jsv.2016.03.041 doi.ico hal.ico clarivate_16x16.png
21.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
22.Flore CREVEL, Nicolas GOURDAINorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2014).
Numerical simulation of aerodynamic instabilities in a multistage high-speed high-pressure compressor on its test-rig - Part I : rotating stall
J. Turbomach. 136, 101003 (14 pages). doi:10.1115/1.4027967 doi.ico hal.ico clarivate_16x16.png
23.Martin BUISSON, Pascal FERRAND, Laurent SOULAT, Stéphane AUBERTorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Claire RAMBEAU, Manuel HENNER (2013).
Optimal design of an automotive fan using the Turb'Opty meta-model
Comput. Fluids 80, 207–213. doi:10.1016/j.compfluid.2012.03.015 doi.ico hal.ico clarivate_16x16.png
24.Laurent SOULAT, Pascal FERRAND, Stéphane MOREAUorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Martin BUISSON (2013).
Efficient optimisation procedure for design problems in fluid mechanics
Comput. Fluids 82, 73–86. doi:10.1016/j.compfluid.2013.04.009 doi.ico hal.ico clarivate_16x16.png
25.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
26.Yannick ROZENBERG, Gilles ROBERT, Stéphane MOREAUorcid_16x16.png (2012).
Wall-pressure spectral model including the adverse pressure gradient effects
AIAA J. 50, 2168–2179. doi:10.2514/1.J051500 doi.ico clarivate_16x16.png
27.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
28.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
29.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2010).
Extensions and limitations of analytical airfoil broadband noise models
Int. J. Aeroacoustics 9, 273–305.
30.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
31.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
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.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
34.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
35.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.
36.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.
37.Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2005).
Effect of airfoil aerodynamic loading on trailing-edge noise sources.
AIAA J. 43, 41–52.
38.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2004).
Broadband self-noise from loaded fan blades.
AIAA J. 42, 536–544.
39.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.
 
thèses/hdr
1.Danny LEWISorcid_16x16.png (dir.: Marc C. JACOB, Stéphane MOREAU) (2020).
From analytical to fully numerical predictions of the broadband noise radiated by a full fan-OGV stage
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.Paul LAFFAY (dir.: Marc C. JACOB, Stéphane MOREAU) (2019).
Étude aéroacoustique de la détente d'un écoulement haute pression à travers des plaques perforées
Thèse Université de Lyon hal.ico
4.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
 
communications avec actes
1.Andrea ARROYO RAMO, Stéphane MOREAUorcid_16x16.png, Richard D. SANDBERGorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2022).
Direct Numerical Simulation of Controlled Diffusion airfoil self-noise
28th AIAA/CEAS Aeroacoustics 2022 Conference, Southampton, United Kingdom. doi:10.2514/6.2022-2815 doi.ico hal.ico
In: proceeding of the 28th AIAA/CAES Aeroacoustics 2022 Conference , AIAA, Reston, Virginia, USA, Paper n°2022-2815 (18 pages). doi:10.2514/6.2022-2815 doi.ico hal.ico
2.Antonio ALGUACILorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Lorenzo BECHERUCCI, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2022).
Predicting the sound refraction on shear layers with deep neural networks
28th AIAA/CEAS Aeroacoustics 2022 Conference, Southampton, United Kingdom. doi:10.2514/6.2022-2841 doi.ico hal.ico
In: proceeding of the 28th AIAA/CAES Aeroacoustics 2022 Conference , AIAA, Reston, Virginia, USA, AIAA Paper n°2022-2841 (9 pages). doi:10.2514/6.2022-2841 doi.ico hal.ico
3.Antonio ALGUACILorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Wagner GONÇALVES PINTOorcid_16x16.png (2021).
Effects of boundary conditions in fully convolutional networks for learning spatio-temporal dynamics
European Conference on Machine Learning and Principles and Practice of Knowledge Discovery in Databases / ECML PKDD 2021, Bilbao / virtual, Spain. doi:10.1007/978-3-030-86517-7_7 doi.ico hal.ico
In: Proceedings of European Conference on Machine Learning and Principles and Practice of Knowledge in Databases (ECML PKDD 2021), , . doi:10.1007/978-3-030-86517-7_7 doi.ico hal.ico
4.Antonio ALGUACILorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2021).
A generic deep learning framework for propagation and scattering of acoustic waves in quiescent flows
27th AIAA/CEAS Aeroacoustics Conference / Aviation 2021, virtual, United States. doi:0.2514/6.2021-2239 doi.ico hal.ico
In: Proceedings of the 27th AIAA/CEAS Aeroacoustics Conference , AIAA, Reston, Virginia, USA, Paper n°2021-2239 (22 pages). doi:0.2514/6.2021-2239 doi.ico hal.ico
5.Antonio ALGUACILorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2020).
Predicting the Propagation of Acoustic Waves using Deep Convolutional Neural Networks
26th AIAA/CEAS Aeroacoustics Conference / Aviation 2020, Reno / virtual, United States. doi:10.2514/6.2020-2513 doi.ico hal.ico
In: Proceedings of the 26th AIAA/CEAS Aeroacoustics Conference , AIAA, Reston, Virginia, USA, Paper n° 2020-2513 (18 pages). doi:10.2514/6.2020-2513 doi.ico hal.ico
6.Danny LEWISorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2020).
Broadband noise predictions on the ACAT1 fan stage using Large-Eddy Simulations and analytical models
26th AIAA/CEAS Aeroacoustics Conference / Aviation 2020, Reno / virtual, United States. doi:10.2514/6.2020-2519 doi.ico hal.ico
In: Proceedings of the 26th AIAA/CEAS Aeroacoustics Conference , AIAA, Reston, Virginia, USA. doi:10.2514/6.2020-2519 doi.ico hal.ico
7.Danny LEWISorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2019).
On the use of large-eddy simulations and analytical models to perform broadband rotor-stator interaction noise predictions
25th AIAA/CEAS Aeroacoustics Conference, Delft, Netherlands. doi:10.2514/6.2019-2667 doi.ico hal.ico
In: Proceedings of the 25th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, Paper n° 2019-2667 (17 pages). doi:10.2514/6.2019-2667 doi.ico hal.ico
8.Paul LAFFAY, Stéphane MOREAUorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Josselin REGNARD (2018).
Experimental investigation of the output duct role in the transient bleed valve noise
24th AIAA/CEAS Aeroacoustics Conference, Atlanta, United States. doi:10.2514/6.2018-3606 doi.ico hal.ico
In: Proceedings of the 2018 AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, Paper n°2018-3606 (16 pages). doi:10.2514/6.2018-3606 doi.ico hal.ico
9.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
10.Paul LAFFAY, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Josselin REGNARD (2017).
Experimental investigation of the transient bleed valve noise
23rd AIAA/CEAS Aeroacoustics Conference, Denver, United States. doi:10.2514/6.2017-3528 doi.ico hal.ico
In: Proceedings of the 23rd AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, Paper n°2017-3528 (17 pages). doi:10.2514/6.2017-3528 doi.ico hal.ico
11.Aurélien MARSAN, Gilles LEROY, Isabelle TRÉBINJAC, Stéphane MOREAUorcid_16x16.png (2015).
A multi-slots suction strategy for controlling the unsteady hub–corner separation in a radial vaned diffuser
12th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Lerici, Italy. hal.ico
In: Proceedings of the 12th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, , . hal.ico
12.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
13.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
14.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.
15.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).
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.Martin BUISSON, Pascal FERRAND, Laurent SOULAT, Stéphane AUBERTorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Claire RAMBEAU, Manuel HENNER (2012).
Turb'opty based optimization of a shrouded fan with casing treatment
28th Congress of the International Council of the Aeronautical Sciences, Brisbane, Australia.
In: Proceedings of ICAS 2012, Optimage Ltd, Edinburgh, Scotland, Paper ICAS 2012-4.4.4 .
full text
18.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).
19.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).
20.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).
21.Laurent SOULAT, Pascal FERRAND, Stéphane AUBERTorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2009).
Numerical evaluation of a new casing treatment based on Holweck type vacuum pumps
8th European Turbomachinery Conference, Graz, Austria.
In: Proceedings of the 8th European Conference on Turbomachinery, , , ETC paper 089.
22.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).
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13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy.
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13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy.
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12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
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communications sans actes
1.Aurélien MARSAN, Stéphane MOREAUorcid_16x16.png (2016).
Aeroacoustic analysis of the tonal noise of a large-scale radial blower
16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, United States. hal.ico
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12th ISROMAC, Honolulu, United States.
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LES prediction of wall-pressure fluctuations and noise of a low-speed airfoil
Acoustics'08, Paris, France.
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Fan blade trailing-edge noise prediction using RANS simulations
Acoustics'08, Paris, France.
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Aero-acoustic installation effects in cooling fan systems - Part 2: near-field and ground effects
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