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articles
1.Nicolas DE CACQUERAY, Christophe BOGEYorcid_16x16.png (2014).
Noise of an overexpanded Mach 3.3 jet: Non-linear propagation effects and correlations with flow
Int. J. Aeroacoustics 13, 607–632. doi:10.1260/1475-472X.13.7-8.607 doi.ico hal.ico openalex-16x16.png
2.Nicolas DE CACQUERAY, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2011).
Investigation of a high-mach-number overexpanded jet using Large-Eddy Simulation
AIAA J. 49, 2171–2182. doi:10.2514/1.J050952 doi.ico openalex-16x16.png
3.Christophe BOGEYorcid_16x16.png, Nicolas DE CACQUERAY, Christophe BAILLYorcid_16x16.png (2011).
Finite differences for coarse azimuthal discretization and for reduction of effective resolution near origin of cylindrical flow equations
J. Comput. Phys. 230, 1134–1146. doi:10.1016/j.jcp.2010.10.031 doi.ico openalex-16x16.png
4.J. SCHULZE, J. SESTERHENN, Peter J. SCHMIDorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Nicolas DE CACQUERAY, Julien BERLAND, Christophe BAILLYorcid_16x16.png (2009).
Numerical simulation of supersonic jet noise
Notes Num. Fluid Mech. 104, 29–46. doi:10.1007/978-3-540-89956-3_2 doi.ico openalex-16x16.png
5.Christophe BOGEYorcid_16x16.png, Nicolas DE CACQUERAY, Christophe BAILLYorcid_16x16.png (2009).
A shock-capturing methodology based on adaptative spatial filtering for high-order non-linear computations
J. Comput. Phys. 228, 1447–1465. doi:10.1016/j.jcp.2008.10.042 doi.ico openalex-16x16.png
 
thèses/hdr
1.Nicolas DE CACQUERAY (dir.: Christophe BAILLY, Christophe BOGEY) (2010).
Méthodes numériques pour les écoulements supersoniques avec application au calcul du bruit rayonné par un jet sur-détendu
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2197_ndecacqueray.pdf
 
communications avec actes
1.Thomas BONTEMPS, Stéphane AUBERTorcid_16x16.png, Nicolas DE CACQUERAY (2019).
Prediction of the acoustic influence of an intake on fan flutter: a comparison of numerical methods
European Turbomachinery Conference (ETC 13), Lausanne, Switzerland.
In: Proceedings of 15th European Turbomachinery Conference (ETC 13), , , 2-s2.0-85065962800.
2.Nicolas DE CACQUERAY, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2011).
Investigation of highly supersonic jet noise: non-linear propagation effects and flow-acoustics correlations
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2747 (18 pages).
3.Nicolas DE CACQUERAY, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2010).
Direct noise computation of a shocked and heated jet at a Mach number of 3.30
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 2010-3732 (23 pages).
4.Christophe BOGEYorcid_16x16.png, Nicolas DE CACQUERAY, Christophe BAILLYorcid_16x16.png (2008).
Recent developments in Direct Noise Computation of turbulent flows: numerical methods and applications
37th International Congress and Exposition on Noise Control Engineering (Inter-Noise), Shangai, China.
In: Proceedings of Inter- Noise 08, International Institute of Noise Control Engineering, Purdue University West Lafayette, USA.
5.Christophe BOGEYorcid_16x16.png, Nicolas DE CACQUERAY, Christophe BAILLYorcid_16x16.png (2008).
Self-adjusting shock-capturing spatial filtering for high-order non-linear computations
14th AIAA/CEAS Aeroacoustics Conference, Vancouver, Canada.
In: Proceedings of the 14th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2008-2968 (25 pages).
 
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