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articles
1.Danny LEWISorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Marlène SANJOSÉorcid_16x16.png (2023).
Large Eddy Simulation of the ACAT1 fan stage for broadband noise prediction
J. Sound Vib. 565, 117888 (42 pages). doi:10.1016/j.jsv.2023.117888 doi.ico hal.ico openalex-16x16.png
2.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 openalex-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 openalex-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 openalex-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 openalex-16x16.png
6.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 openalex-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 openalex-16x16.png
8.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 openalex-16x16.png
9.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 openalex-16x16.png
10.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 openalex-16x16.png
11.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 openalex-16x16.png
12.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 openalex-16x16.png
13.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 openalex-16x16.png
14.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 openalex-16x16.png
15.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 openalex-16x16.png
16.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 openalex-16x16.png
17.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 openalex-16x16.png
18.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 openalex-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 openalex-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 openalex-16x16.png
21.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 openalex-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 openalex-16x16.png
23.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 openalex-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 openalex-16x16.png
25.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 openalex-16x16.png
26.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 openalex-16x16.png
27.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 openalex-16x16.png
28.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 openalex-16x16.png
29.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 openalex-16x16.png
30.Michel ROGERorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2010).
Extensions and limitations of analytical airfoil broadband noise models
Int. J. Aeroacoustics 9, 273–305.
31.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 openalex-16x16.png
32.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 openalex-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 openalex-16x16.png
34.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 openalex-16x16.png
35.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 openalex-16x16.png
36.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.
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.Stéphane MOREAUorcid_16x16.png, Michel ROGERorcid_16x16.png (2005).
Effect of airfoil aerodynamic loading on trailing-edge noise sources.
AIAA J. 43, 41–52.
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.
 
thèses/hdr
1.Antonio ALGUACILorcid_16x16.png (dir.: Michaël BAUERHEIM, Marc C. JACOB, Stéphane MOREAU) (2022).
Predicting the Propagation of Acoustic Waves in Complex Media with Deep Neural Networks
Thèse Institut Supérieur de l'Aéronautique et de l'Espace
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.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
4.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
5.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.Antonio ALGUACILorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Marc C. JACOBorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2023).
Correcting the prediction of noise scattering at sharp edges for a spatio-temporal deep learned acoustic surrogate
2023 AIAA Aviation and Aeronautics Forum and Exposition, San Diego, United States. doi:10.2514/6.2023-3341 doi.ico
In: Patrick YEE (Ed.), Alexandre DELACHE (Ed.), Daniel DELAURENTIS (Ed.), Geoffrey JERAM (Ed.), Vincent SCHULTZ (Ed.), Darrell CROWE (Ed.), Proceedings of the 2023 AIAA Aviation and Aeronautics Forum and Exposition, AIAA, Reston, Virginia, USA, 2023-3341 (19 pages). doi:10.2514/6.2023-3341 doi.ico
2.Andrea ARROYO RAMO, Stéphane MOREAUorcid_16x16.png, Richard D. SANDBERGorcid_16x16.png, Michaël BAUERHEIMorcid_16x16.png, Marc C. JACOBorcid_16x16.png (2023).
Controlled diffusion airfoil self-noise, an acoustic far-field prediction
2023 AIAA Aviation and Aeronautics Forum and Exposition, San Diego, United States. doi:10.2514/6.2023-3505 doi.ico
In: Patrick YEE (Ed.), Alexandre DELACHE (Ed.), Daniel DELAURENTIS (Ed.), Geoffrey JERAM (Ed.), Vincent SCHULTZ (Ed.), Darrell CROWE (Ed.), Proceedings of the 2023 AIAA Aviation and Aeronautics Forum and Exposition, AIAA, Reston, Virginia, USA, 2023-3505 (16 pages). doi:10.2514/6.2023-3505 doi.ico
3.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
4.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
5.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
6.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
7.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
8.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
9.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
10.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
11.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
12.Miguel PESTANA, Antonio PEREIRAorcid_16x16.png, 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
13.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
14.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
15.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
16.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.
17.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).
18.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).
19.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
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