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1.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2015).
Large-eddy simulation of underexpanded round jets impinging on a flat plate 4 to 9 radii downstream from the nozzle
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2210 doi.ico hal.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2210 doi.ico hal.ico
AIAA-2015-2210
2.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
3.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
4.Édouard SALZE, Christophe BAILLYorcid_16x16.png, Aurélien MARSAN, Emmanuel JONDEAU, Daniel JUVÉ (2015).
An experimental investigation of wall pressure fluctuations beneath pressure gradients
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-3148 doi.ico hal.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2015-3148 (12 pages). doi:10.2514/6.2015-3148 doi.ico hal.ico
5.Jun ZHENG, Maxime HUET, Franck CLÉRO, Alexis GIAUQUEorcid_16x16.png, Sébastien DUCRUIX (2015).
A 2D-axisymmetric analytical model for the estimation of indirect combustion noise in nozzle flows
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2974 doi.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2974 doi.ico
AIAA-2015-2974
6.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
7.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
8.Gwendoline BRICHET, Maxime KOENIG, Christophe BAILLYorcid_16x16.png (2015).
Installation noise of a turbofan jet engine under an airfoil
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2208 doi.ico hal.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2015-2208 (14 pages). doi:10.2514/6.2015-2208 doi.ico hal.ico
9.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
10.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2015).
Large-eddy simulation of supersonic planar jets impinging on a flat plate at an angle of 60 to 90 degrees
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-2209 doi.ico hal.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-2209 doi.ico hal.ico
AIAA-2015-2209
11.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
12.Sophie LE BRASorcid_16x16.png, Hugues DENIAU, Christophe BOGEYorcid_16x16.png, Guillaume DAVILLERorcid_16x16.png (2015).
Development of compressible large-eddy simulations combining high-order schemes and wall modeling
21st AIAA/CEAS Aeroacoustics Conference, Dallas, United States. doi:10.2514/6.2015-3135 doi.ico
In: Proceedings of the 21st AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA. doi:10.2514/6.2015-3135 doi.ico
 
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