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articles
1.Laura MARTIN-MARTINorcid_16x16.png, Vincent CLAIRorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Gwénaël GABARDorcid_16x16.png (2024).
Numerical study of the scattering of acoustic waves by an elliptic vortex
J. Acoust. Soc. Am. 155, 1707–1718. doi:10.1121/10.0025138 doi.ico openalex-16x16.png
2.Mathieu VARÉorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2024).
Acoustic tones generated by impinging jets: Differences between laminar and highly-disturbed nozzle-exit boundary layers
Int. J. Aeroacoustics 23, 342–362. doi:10.1177/1475472X241230647 doi.ico openalex-16x16.png
3.Hugo VINCENTorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2024).
Influence of the boundary-layer thickness on the generation of tonal noise components by subsonic impinging jets
J. Fluid Mech. 985, A26 (31 pages). doi:10.1017/jfm.2024.281 doi.ico openalex-16x16.png
4.Stefan SCHODERorcid_16x16.png, Étienne SPIESERorcid_16x16.png, Hugo VINCENTorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2024).
Correction: Acoustic modeling using the aeroacoustic wave equation based on Pierce’s operator
AIAA J. (1 pages). doi:10.2514/1.J062558.c1 doi.ico openalex-16x16.png
5.Hugo VINCENTorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2023).
Application of the complex differentiation method to the sensitivity analysis of aerodynamic noise
Comput. Fluids 264, 105965 (16 pages). doi:10.1016/j.compfluid.2023.105965 doi.ico openalex-16x16.png
6.Stefan SCHODERorcid_16x16.png, Étienne SPIESERorcid_16x16.png, Hugo VINCENTorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2023).
Acoustic modeling using the aeroacoustic wave equation based on Pierce’s operator
AIAA J. 61, 4008–4017. doi:10.2514/1.J062558 doi.ico openalex-16x16.png
7.Mathieu VARÉorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2023).
Mach number dependence of tone generation by impinging round jets
AIAA J. . doi:10.2514/1.J062746 doi.ico hal.ico openalex-16x16.png
8.Giorgio PALMAorcid_16x16.png, Stefano MELONIorcid_16x16.png, Roberto CAMUSSIorcid_16x16.png, Umberto IEMMAorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2023).
Data-driven multiobjective optimization of wave-packets for near-field subsonic jet noise
AIAA J. . doi:10.2514/1.J062261 doi.ico openalex-16x16.png
9.Étienne SPIESERorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2023).
Noise predictions of a Mach 0.9 round jet using tailored adjoint Green's functions
J. Sound Vib. 548, 117532 (24 pages). doi:10.1016/j.jsv.2022.117532 doi.ico openalex-16x16.png
10.Valentin MORIN, Julien TROYES, François VUILLOT, Christophe BOGEYorcid_16x16.png (2023).
Large-eddy simulation of a water jet exhausting into quiescent air
AIAA J. 61, 665–680. doi:10.2514/1.J062067 doi.ico hal.ico openalex-16x16.png
11.Christophe BOGEYorcid_16x16.png (2022).
Interactions between upstream-propagating guided jet waves and shear-layer instability waves near the nozzle of subsonic and nearly ideally expanded supersonic free jets with laminar boundary layers
J. Fluid Mech. 949, A41 (34 pages). doi:10.1017/jfm.2022.776 doi.ico hal.ico openalex-16x16.png
12.Gaetano Luca MICCI, Roberto CAMUSSIorcid_16x16.png, Stefano MELONIorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2022).
Intermittency and stochastic modeling of low- and high-Reynolds-number compressible jets
AIAA J. 60, 1983–1990. doi:10.2514/1.j061128 doi.ico hal.ico openalex-16x16.png
13.Mathieu VARÉorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2022).
Flow and acoustic fields of rocket jets impinging on a perforated plate
AIAA J. (14 pages). doi:10.2514/1.J061253 doi.ico hal.ico openalex-16x16.png
14.Mathieu VARÉorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2022).
Generation of acoustic tones in round jets at a Mach number of 0.9 impinging on a plate with and without a hole
J. Fluid Mech. 936, A16 (32 pages). doi:10.1017/jfm.2022.47 doi.ico hal.ico openalex-16x16.png
15.Andres ADAMorcid_16x16.png, Dimitri PAPAMOSCHOUorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2022).
Imprint of vortical structures on the near-field pressure of a turbulent jet
AIAA J. 60, 1578–1591. doi:10.2514/1.J061010 doi.ico hal.ico openalex-16x16.png
16.Roberto CAMUSSIorcid_16x16.png, Stefano MELONIorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2022).
On the influence of the nozzle exhaust initial conditions on the near field acoustic pressure
Acta Acustica 6, 57 (9 pages). doi:10.1051/aacus/2022051 doi.ico openalex-16x16.png
17.Pierre PINEAUorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2021).
Links between steepened Mach waves and coherent structures for a supersonic jet
AIAA J. 59, 1673–1681. doi:10.2514/1.j059859 doi.ico hal.ico openalex-16x16.png
18.Christophe BOGEYorcid_16x16.png (2021).
Generation of excess noise by jets with highly disturbed laminar boundary-layer profiles
AIAA J. 59, 569–579. doi:10.2514/1.J059610 doi.ico hal.ico openalex-16x16.png
19.Roberto CAMUSSIorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2021).
Intermittent statistics of the 0-mode pressure fluctuations in the near field of Mach 0.9 circular jets at low and high Reynolds numbers
Theor. Comput. Fluid Dyn. (19 pages). doi:10.1007/s00162-020-00553-9 doi.ico hal.ico openalex-16x16.png
20.Pierre PINEAUorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2021).
Numerical investigation of wave steepening and shock coalescence near a cold Mach 3 jet
J. Acoust. Soc. Am. 149, 357–370. doi:10.1121/10.0003343 doi.ico hal.ico openalex-16x16.png
21.Christophe BOGEYorcid_16x16.png (2021).
Tones in the acoustic far field of jets in the upstream direction
AIAA J. . doi:10.2514/1.J061013 doi.ico hal.ico openalex-16x16.png
22.Pierre PINEAUorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2021).
Acoustic shielding and interaction effects for strongly heated supersonic twin jets
AIP Advances 11, 075114 (14 pages). doi:10.1063/5.0059789 doi.ico hal.ico openalex-16x16.png
23.Christophe BOGEYorcid_16x16.png (2021).
Acoustic tones in the near-nozzle region of jets: characteristics and variations between Mach numbers 0.5 and 2
J. Fluid Mech. 921, A3 (41 pages). doi:10.1017/jfm.2021.426 doi.ico hal.ico openalex-16x16.png
24.Pierre PINEAUorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2020).
Temperature effects on convection speed and steepened waves of temporally developing supersonic jets
AIAA J. 58, 1227–1239. doi:10.2514/1.J058589 doi.ico hal.ico openalex-16x16.png
25.Pierre PINEAUorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2019).
Steepened Mach waves near supersonic jets: study of azimuthal structure and generation process using conditional averages
J. Fluid Mech. 880, 594–619. doi:10.1017/jfm.2019.729 doi.ico hal.ico openalex-16x16.png
26.Christophe BOGEYorcid_16x16.png, Roberto SABATINI (2019).
Effects of nozzle-exit boundary-layer profile on the initial shear-layer instability, flow field and noise of subsonic jets
J. Fluid Mech. 876, 288–325. doi:10.1017/jfm.2019.546 doi.ico hal.ico openalex-16x16.png
27.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2019).
Effects of the angle of impact on the aeroacoustic feedback mechanism in supersonic impinging planar jets
Int. J. Aeroacoustics 18, 258–278. doi:10.1177/1475472X18812808 doi.ico hal.ico openalex-16x16.png
28.Christophe BOGEYorcid_16x16.png (2019).
On noise generation in low Reynolds number temporal round jets at a Mach number of 0.9
J. Fluid Mech. 859, 1022–1056. doi:10.1017/jfm.2018.864 doi.ico hal.ico openalex-16x16.png
29.Christophe BOGEYorcid_16x16.png, Pierre PINEAUorcid_16x16.png (2019).
Potential-core closing of temporally developing jets at Mach numbers between 0.3 and 2: Scaling and conditional averaging of flow and sound fields
Phys. Rev. Fluids 4, 124601 (25 pages). doi:10.1103/PhysRevFluids.4.124601 doi.ico hal.ico openalex-16x16.png
30.Sophie LE BRASorcid_16x16.png, Hugues DENIAU, Christophe BOGEYorcid_16x16.png (2019).
A technique of flux reconstruction at the interfaces of nonconforming grids for aeroacoustic simulations
Int. J. Numer. Methods Fluids 91, 587–614. doi:10.1002/fld.4767 doi.ico hal.ico openalex-16x16.png
31.Christophe BOGEYorcid_16x16.png (2018).
Grid sensitivity of flow field and noise of high-Reynolds-number jets computed by large-eddy simulation
Int. J. Aeroacoustics 17, 399–424. doi:10.1177/1475472X18778287 doi.ico hal.ico openalex-16x16.png
32.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Mihai MIHAESCU (2018).
Oscillation modes in screeching jets
AIAA J. 56, 2918–2924. doi:10.2514/1.J056936 doi.ico hal.ico openalex-16x16.png
33.Marion CAPUANO, Christophe BOGEYorcid_16x16.png, Peter D.M. SPELTorcid_16x16.png (2018).
Simulations of viscous and compressible gas-gas flows using high-order finite difference schemes
J. Comput. Phys. 361, 56–81. doi:10.1016/j.jcp.2018.01.047 doi.ico hal.ico openalex-16x16.png
34.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2018).
Flow features near plate impinged by ideally expanded and underexpanded round jets
AIAA J. 56, 445–457. doi:10.2514/1.J056421 doi.ico hal.ico openalex-16x16.png
35.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2017).
Numerical study of the flow and the near acoustic fields of an underexpanded round free jet generating two screech tones
Int. J. Aeroacoustics 16, 603–625. doi:10.1177/1475472X17727606 doi.ico hal.ico openalex-16x16.png
36.Christophe BOGEYorcid_16x16.png, Romain GOJONorcid_16x16.png (2017).
Feedback loop and upwind-propagating waves in ideally expanded supersonic impinging round jets
J. Fluid Mech. 823, 562–591. doi:10.1017/jfm.2017.334 doi.ico hal.ico openalex-16x16.png
37.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2017).
Flow structure oscillations and tone production in underexpanded impinging round jets
AIAA J. 55, 1792–1805. doi:10.2514/1.J055618 doi.ico hal.ico openalex-16x16.png
38.Sophie LE BRASorcid_16x16.png, Hugues DENIAU, Christophe BOGEYorcid_16x16.png (2017).
Development of compressible Large-Eddy Simulations combining high-order schemes and wall modeling
AIAA J. 55, 1152–1163. doi:10.2514/1.J055107 doi.ico hal.ico openalex-16x16.png
39.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2016).
Investigation of tone generation in ideally expanded supersonic planar impinging jets using large-eddy simulation
J. Fluid Mech. 808, 90–115. doi:10.1017/jfm.2016.628 doi.ico hal.ico openalex-16x16.png
40.Roberto SABATINI, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2016).
A numerical study of nonlinear infrasound propagation in a windy atmosphere
J. Acoust. Soc. Am. 140, 641. doi:10.1121/1.4958998 doi.ico hal.ico openalex-16x16.png
41.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2016).
Simulations of initially highly disturbed jets with experiment-like exit boundary layers
AIAA J. 54, 1299–1312. doi:10.2514/1.J054426 doi.ico hal.ico openalex-16x16.png
42.François KREMER, Christophe BOGEYorcid_16x16.png (2015).
Large-eddy simulation of turbulent channel flow using relaxation filtering: Resolution requirement and Reynolds number effects
Comput. Fluids 116, 17–28. doi:10.1016/j.compfluid.2015.03.026 doi.ico hal.ico openalex-16x16.png
43.François KREMER, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2014).
Semi-Implicit Runge-Kutta schemes: Development and application to compressible channel flow
AIAA J. 52, 516–527. doi:10.2514/1.J052236 doi.ico hal.ico openalex-16x16.png
44.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
45.Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2014).
A study of infrasound propagation based on high-order finite difference solutions of the Navier-Stokes equations
J. Acoust. Soc. Am. 135, 1083–1095. doi:10.1121/1.4864793 doi.ico hal.ico openalex-16x16.png
46.Stefan BÜHLER, Leonhard KLEISER, Christophe BOGEYorcid_16x16.png (2014).
Simulation of subsonic turbulent nozzle jet flow and its near-field sound
AIAA J. 52, 1653–1669. doi:10.2514/1.J052673 doi.ico hal.ico openalex-16x16.png
47.Didier DRAGNAorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Maarten C. J. HORNIKX, Philippe BLANC-BENONorcid_16x16.png (2013).
Analysis of the dissipation and dispersion properties of the multi-domain Chebyshev pseudospectral method
J. Comput. Phys. 255, 31–47. doi:10.1016/j.jcp.2013.07.036 doi.ico hal.ico openalex-16x16.png
48.D. FAUCONNIER, Christophe BOGEYorcid_16x16.png, E. DICK (2013).
On the performance of relaxation filtering for large-eddy simulation
J. Turbul. 14, 22–49. doi:10.1080/14685248.2012.740567 doi.ico hal.ico openalex-16x16.png
49.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2013).
Identification of the effects of the nozzle-exit boundary-layer thickness and its corresponding Reynolds number in initially highly disturbed subsonic jets
Phys. Fluids 25, 055106 (27 pages). doi:10.1063/1.4807071 doi.ico hal.ico openalex-16x16.png
50.Sergey KARABASOV, Christophe BOGEYorcid_16x16.png, Tom HYNES (2013).
An investigation of the mechanisms of sound generation in initially laminar subsonic jets using the Goldstein acoustic analogy
J. Fluid Mech. 714, 24–57. doi:10.1017/jfm.2012.448 doi.ico hal.ico openalex-16x16.png
51.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2012).
Influence of initial turbulence level on the flow and sound fields of a subsonic jet at a diameter-based Reynolds number of 10(5)
J. Fluid Mech. 701, 352–385. doi:10.1017/jfm.2012.162 doi.ico openalex-16x16.png
52.Olivier MARSDEN, Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Emmanuel JONDEAU (2012).
Investigation of flow features and acoustic radiation of a round cavity
J. Sound Vib. 331, 3521–3543. doi:10.1016/j.jsv.2012.03.017 doi.ico openalex-16x16.png
53.Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2012).
Investigation of flow features around shallow round cavities subject to subsonic grazing flow
Phys. Fluids 24, 125107 (24 pages). doi:10.1063/1.4772194 doi.ico openalex-16x16.png
54.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2012).
Effects of moderate Reynolds numbers on subsonic round jets with highly disturbed nozzle-exit boundary layers
Phys. Fluids 24, 105107 (24 pages). doi:10.1063/1.4757667 doi.ico openalex-16x16.png
55.F. KERHERVÉ, P. JORDAN, A.V.G CAVALIERI, J. DELVILLE, Christophe BOGEYorcid_16x16.png, Daniel JUVÉ (2012).
Educing the source mechanism associated with downstream radiation in subsonic jets
J. Fluid Mech. 710, 606–640. doi:10.1017/jfm.2012.378 doi.ico openalex-16x16.png
56.Julien BERLAND, Philippe LAFON, Frédéric DAUDE, Fabien CROUZET, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2011).
Filter shape dependence and effective scale separation in large-eddy simulations based on relaxation filtering
Comput. Fluids 47, 65–74. doi:10.1016/j.compfluid.2011.02.016 doi.ico openalex-16x16.png
57.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
58.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2011).
Large-eddy simulation of the flow and acoustic fields of a Reynolds number 105 subsonic jet with tripped exit boundary layers
Phys. Fluids 23, 035104 (20 p. pages). doi:10.1063/1.3555634 doi.ico openalex-16x16.png
59.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2011).
On the spectra of nozzle-exit velocity disturbances in initially nominally turbulent, transitional jets
Phys. Fluids 23, 091702 (4 pages). doi:10.1063/1.3642642 doi.ico openalex-16x16.png
60.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
61.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Sébastien M. CANDEL (2010).
Modelling of sound generation by turbulent reacting flows
Int. J. Aeroacoustics 9, 461–489.
62.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2010).
Progress in direct noise computation
Int. J. Aeroacoustics 9, 123–143.
63.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2010).
Influence of nozzle-exit boundary-layer conditions on the flow and acoustic fields of initially laminar jets
J. Fluid Mech. 663, 507–538. doi:10.1017/S0022112010003605 doi.ico openalex-16x16.png
64.Damien DESVIGNE, Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2010).
Development of noncentered wavenumber-based optimized interpolation schemes with amplification control for overlapping grids
SIAM J. Sci. Comput. 32, 2074–2098. doi:10.1137/090758702 doi.ico openalex-16x16.png
65.Christophe BOGEYorcid_16x16.png, Sébastien BARRÉ, Daniel JUVÉ, Christophe BAILLYorcid_16x16.png (2009).
Simulation of a hot coaxial jet: direct noise prediction and flow-acoustics correlations
Phys. Fluids 21, 035105 (14 pages). doi:10.1063/1.3081561 doi.ico openalex-16x16.png
66.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
67.Benjamin COTTÉorcid_16x16.png, Philippe BLANC-BENONorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Franck POISSON (2009).
Time-domain impedance boundary conditions for simulations of outdoor sound propagation
AIAA J. 47, 2391–2403. doi:10.2514/1.41252 doi.ico openalex-16x16.png
68.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2009).
Turbulence and energy budget in a self-preserving round jet: direct evaluation using large eddy simulation
J. Fluid Mech. 627, 129–160. doi:10.1017/S0022112009005801 doi.ico openalex-16x16.png
69.F. KEIDERLING, Leonhard KLEISER, Christophe BOGEYorcid_16x16.png (2009).
Numerical study of eigenmode forcing effects on jet flow development and noise generation mechanisms
Phys. Fluids 21, 045106 (20 pages). doi:10.1063/1.3112686 doi.ico openalex-16x16.png
70.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
71.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2008).
Investigation using statistical closure theory of the influence of the filter shape on scale separation in large-eddy simulation
J. Turbul. 9, 1–22. doi:10.1080/14685240802244116 doi.ico openalex-16x16.png
72.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2008).
A study of differentiation errors in large-eddy simulations based on EDQNM theory
J. Comput. Phys. 227, 8314–8340. doi:10.1016/j.jcp.2008.05.026 doi.ico openalex-16x16.png
73.Sébastien BARRÉ, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2008).
Direct simulation of isolated elliptic vortices and of their radiated noise
Theor. Comput. Fluid Dyn. 22, 65–82. doi:10.1007/s00162-007-0066-x doi.ico openalex-16x16.png
74.Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2008).
Direct noise computation of the turbulent flow around a zero-incidence airfoil
AIAA J. 46, 874–883. doi:10.2514/1.29825 doi.ico openalex-16x16.png
75.Christophe BOGEYorcid_16x16.png, Sébastien BARRÉ, Christophe BAILLYorcid_16x16.png (2008).
Direct computation of the noise generated by subsonic jets originating from a straight pipe nozzle
Int. J. Aeroacoustics 7, 1–22. doi:10.1260/147547208784079917 doi.ico openalex-16x16.png
76.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2007).
Numerical study of screech generation in a planar supersonic jet
Phys. Fluids 19, 075105 (14 pages). doi:10.1063/1.2747225 doi.ico openalex-16x16.png
77.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2007).
An analysis of the correlations between the turbulent flow and the sound pressure fields of subsonic jets
J. Fluid Mech. 583, 71–97. doi:10.1017/S002211200700612X doi.ico hal.ico openalex-16x16.png
78.Christophe BOGEYorcid_16x16.png, Sébastien BARRÉ, Vincent FLEURY, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (2007).
Experimental study of the spectral properties of near-field and far-field jet noise
Int. J. Aeroacoustics 6, 73–92. hal.ico
79.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2007).
On the application of explicit spatial filtering to the variables or fluxes of linear equations
J. Comput. Phys. 225, 1211–1217. doi:10.1016/j.jcp.2007.04.007 doi.ico openalex-16x16.png
80.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2007).
High-order, low dispersive and low dissipative explicit schemes for multiple-scale and boundary problems
J. Comput. Phys. 224, 637–662. doi:10.1016/j.jcp.2006.10.017 doi.ico openalex-16x16.png
81.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Investigation of downstream and sideline subsonic jet noise using Large Eddy Simulations
Theor. Comput. Fluid Dyn. 20, 23–40. doi:10.1007/s00162-005-0005-7 doi.ico hal.ico openalex-16x16.png
82.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Low-dissipation and low-dispersion fourth-order Runge?Kutta algorithm
Comput. Fluids 35, 1459–1463. doi:10.1016/j.compfluid.2005.04.003 doi.ico openalex-16x16.png
83.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Large Eddy Simulations of transitional round jets : influence of the Reynolds number on flow development and energy dissipation
Phys. Fluids 18, 065101 (14 pages). doi:10.1063/1.2204060 doi.ico hal.ico openalex-16x16.png
84.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Computation of a high Reynolds number jet and its radiated noise using large eddy simulation based on explicit filtering
Comput. Fluids 35, 1344–1358. doi:10.1016/j.compfluid.2005.04.008 doi.ico openalex-16x16.png
85.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Large eddy simulations of round jets using explicit filtering with/without dynamic Smagorinsky model
Int. J. Heat Fluid Flow 27, 603–610. doi:10.1016/j.ijheatfluidflow.2006.02.008 doi.ico hal.ico openalex-16x16.png
86.Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2005).
High-order curvilinear simulations of flows around non-cartesian bodies.
J. Comput. Acoust. 13, 731–748.
87.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Xavier GLOERFELT (2005).
Some useful hybrid approaches for predicting aerodynamic noise.
C. R. Méc. 333, 666–675.
88.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2005).
Effects of inflow conditions and forcing on subsonic jet flows and noise.
AIAA J. 43, 1000–1007.
89.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2005).
Decrease of the effective Reynolds number with eddy-viscosity subgrid-scale modeling.
AIAA J. 43, 437–439.
90.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2004).
Contributions of computational aeroacoustics to jet noise research and prediction.
Combustion 18, 481–491.
91.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2004).
A family of low dispersive and low dissipative explicit schemes for flow and noise computations.
J. Comput. Phys. 194, 194–214.
92.Xavier GLOERFELT, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2003).
Numerical evidence of mode switching in the flow-induced oscillations by a cavity.
Proc. R. Soc. A-Math. Phys. Eng. Sci. 22, 193–217.
93.Christophe BOGEYorcid_16x16.png, Xavier GLOERFELT, Christophe BAILLYorcid_16x16.png (2003).
Illustration of the inclusion of sound-flow interactions in Lighthill's equation
AIAA J. 41, 1604–1606. hal.ico
94.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (2003).
Noise investigation of a high subsonic moderate Reynolds number jet using a compressible large eddy simulation.
Theor. Comput. Fluid Dyn. 16, 273–297. doi:10.1007/s00162-002-0079-4 doi.ico hal.ico openalex-16x16.png
95.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2002).
Rayonnement acoustique aval des jets subsoniques : lien avec l'intrusion de structures tourbillonnaires dans le cone potentiel.
J. Fluids Struct. 330, 527–533.
96.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2002).
Three-dimensional non-reflective boundary conditions for acoustic simulations : far field formulation and validation test cases.
Acta Acustica 88, 463–471.
97.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (2002).
Computation of flow noise using source terms in linearized Euler's equations.
AIAA J. 40, 235–243. hal.ico
98.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (2000).
Numerical simulation of sound generated by vortex pairing in a mixing layer.
AIAA J. 38, 2210–2218. hal.ico
99.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2000).
Génération de bruit par appariement de tourbillons dans les zones cisaillées.
Mécanique et Industries 1, 487–497.
100.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (2000).
Calcul du rayonnement acoustique d'une couche de mélange à l'aide des équations d'Euler linéarisées.
C. r. Acad. sci., Sér. IIb Méc. 238, 341–347.
101.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (1999).
Calcul direct du rayonnement acoustique d'une couche de mélange par macrosimulation.
C. r. Acad. sci., Sér. IIb Méc. 327, 1029–1034.
 
thèses/hdr
1.Pierre PINEAUorcid_16x16.png (dir.: Christophe BOGEY) (2018).
Étude numérique de la production et de la propagation d’ondes non linéaires dans les jets supersoniques
Thèse Université de Lyon hal.ico
2.Marion CAPUANO (dir.: Christophe BOGEY, Peter D.M. SPELT) (2018).
Simulations numériques d’écoulements diphasiques compressibles, visqueux et conductifs à l’aide de schémas aux différences finies centrées d’ordre élevé
Thèse École centrale de Lyon hal.ico
3.Sophie LE BRASorcid_16x16.png (dir.: Christophe BOGEY) (2016).
Modélisation de paroi et traitement aux interfaces des maillages non-conformes pour les simulations aéroacoustiques avec une approche numérique d'ordre élevé
Thèse École centrale de Lyon hal.ico
4.Romain GOJONorcid_16x16.png (dir.: Christophe BOGEY) (2015).
Etude de jets supersoniques impactant une paroi par simulation numérique. Analyse aérodynamique et acoustique des mécanismes de rétroaction
Thèse École centrale de Lyon
5.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
6.Christophe BOGEYorcid_16x16.png (2007).
Contribution de la simulation des grandes échelles compressible à l'étude de la turbulence et du rayonnement acoustique
Habilitation École centrale de Lyon
7.Julien BERLAND (dir.: Christophe BAILLY, Christophe BOGEY) (2006).
Modélisation des erreurs numériques dans une simulation des grandes échelles et étude du screech dans un jet rectangulaire supersonique.
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/jberland.pdf
8.Sébastien BARRÉ (dir.: Christophe BAILLY, Christophe BOGEY) (2006).
Etude numérique et expérimentale du bruit aérodynamique avec application aux jets ronds subsoniques.
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/sbarre.pdf
9.Christophe BOGEYorcid_16x16.png (2000).
Calcul direct du bruit aérodynamique et validation de modèles acoustiques hybrides.
Thèse École centrale de Lyon
 
conférences invitées
1.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2008).
Advances in computational aeroacoustics: challenges and issues
7th International ERCOFTAC Symposium on Engineering Turbulence Modelling and Measurements, Limassol, Cyprus.
In: Proceedings of the 7th International ERCOFTAC Symposium on Engineering Turbulence Modelling and Measurements, , , 612–621.
2.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2006).
Large Eddy Simulation for jet noise prediction
10th CEAS Aeroacoustics Workshop on Jet Noise Prediction, Dublin, Ireland.
3.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2006).
Current understanding of jet-noise mechanisms from compressible large-eddy simulations
6th ERCOFTAC Workshop on ?Direct and Large-Eddy Simulation? (DLES-6), Poitiers, France. doi:10.1007/978-1-4020-5152-2_4 doi.ico
In: Direct & large-eddy simulation VI, Springer, Dordrecht, The Netherlands, 39–48. doi:10.1007/978-1-4020-5152-2_4 doi.ico
 
communications avec actes
1.Pierre PINEAUorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2019).
Temperature effects on the generation of steepened waves by supersonic temporal round jets
25th AIAA/CEAS Aeroacoustics Conference, Delft, Netherlands. doi:10.2514/6.2019-2707 doi.ico hal.ico
In: Proceedings of the 25th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, 2019-2707 (12 pages). doi:10.2514/6.2019-2707 doi.ico hal.ico
2.Marion CAPUANO, Christophe BOGEYorcid_16x16.png, Peter D.M. SPELTorcid_16x16.png (2017).
Viscous simulations of shock-bubble interaction and Richtmyer-Meshkov instability
23 ème Congrès Français de Mécanique, Lille, France.
In: Actes du 23 ème Congrès Français de Mécanique, Association Française de Mécanique, Courbevoie, 133735 (7 pages).
3.Romain GOJONorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2015).
Simulation numérique du rayonnement acoustique de jets ronds supersoniques impactant une paroi
CFM 2015 : Congrès Français de Mécanique, Lyon, France.
In: Alain COMBESCURE (Ed.), Michel LANCE (Ed.), Actes du 22ème Congrès Français de Mécanique, Association Française de Mécanique, Courbevoie.
full text
4.Sophie LE BRASorcid_16x16.png, Hugues DENIAU, Christophe BOGEYorcid_16x16.png, Guillaume DAVILLERorcid_16x16.png (2015).
Modélisation de paroi pour la simulation des grandes échelles avec une approche numérique d'ordre élevé
CFM 2015 : Congrès Français de Mécanique, Lyon, France.
In: Alain COMBESCURE (Ed.), Michel LANCE (Ed.), Actes du 22ème Congrès Français de Mécanique, Association Française de Mécanique, Courbevoie.
5.Marion CAPUANO, Christophe BOGEYorcid_16x16.png, Peter D.M. SPELTorcid_16x16.png (2015).
Simulation numérique d'écoulements diphasiques compressibles à l'aide de différences finies d'ordre élevé
CFM 2015 : Congrès Français de Mécanique, Lyon, France.
In: Alain COMBESCURE (Ed.), Michel LANCE (Ed.), Actes du 22ème Congrès Français de Mécanique, Association Française de Mécanique, Courbevoie.
full text
6.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
7.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
8.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
9.Christophe BOGEYorcid_16x16.png (2014).
A study of the effects of temperature on velocity and density fluctuations in high-subsonic jets
52nd Aerospace Sciences Meeting, National Harbor, United States.
In: Proceedings of the 52nd Aerospace Sciences Meeting, AIAA, Reston, Virginia, USA, AIAA-2014-0524 (15 pages).
10.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2014).
Influence of nozzle-exit boundary-layer profile on high-subsonic jets
20th AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, United States.
In: Proceedings of the 20th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2014-2600 (18 pages).
11.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2013).
Flow and sound field of heated subsonic turbulent jets
TSFP 8 : International Symposium onTurbulence and Shear Flow Phenomena Conferences, Poitiers, France.
In: Proceedings of Turbulence and Shear Flow Phenomena Conferences, , .
12.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2013).
Numerical investigation of temperature effects on properties of subsonic turbulent jets
19th AIAA/CEAS Aeroacoustics Conference, Berlin, Germany.
In: Proceeding of the 19th AIAA/CEAS Aeroacoutics Conference, AIAA, Reston, Virginia, USA, AIAA-2013-2140 (19 pages).
13.François KREMER, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2013).
Influence of resolution and Reynolds number on large-eddy simulations of channel flow using relaxation filtering
51st Aerospace Sciences Meeting, Grapevine, Texas, United States.
In: Proceedings of the 51st Aerospace Sciences Meeting, AIAA, Reston, Virginia, USA, AIAA-2013-0517 (15 pages).
14.Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2012).
Depth effects on the flow features and noise signature of shallow cylindrical cavities at a Mach number of 0.25
18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, United States.
In: Proceedings of the 18th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2012-2232 (15 pages).
15.François KREMER, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2012).
Development of semi-implicit Runge-Kutta schemes and application to a turbulent channel flow
18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, United States.
In: Proceedings of the 18th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA2012-2066 (19 pages).
16.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2012).
Effects of initial shear-layer thickness on turbulent subsonic jets at moderate Reynolds numbers
18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, United States.
In: Proceedings of the 18th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2012-2249 (18 pages).
17.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2012).
Flow and sound fields of initially tripped jets at Reynolds numbers ranging from 25,000 to 200,000
50th AIAA Aerospace Sciences Meeting, Nashville, Tennessee, United States.
In: Proceedings of the 50th AIAA Aerospace Sciences Meeting, AIAA, Reston, Virginia, USA, AIAA-2012-1172 (17 pages).
18.François KREMER, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2012).
Investigation of a turbulent channel flow using large eddy simulation
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, 1273–1278. hal.ico
19.Sergey KARABASOV, Christophe BOGEYorcid_16x16.png (2011).
Computation of the noise of initially laminar jets using a statistical approach for the acoustic analogy: application and discussion
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2929.
20.Gaël HANIQUE-COCKENPOT, Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2011).
Etude numérique de la propagation des infrasons en haute atmosphère
20ème Congrès Français de Mécanique, Besançon, France.
In: Actes du CFM 2011, Association Française de Mécanique, Courbevoie.
full text
21.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2011).
Influence of Reynolds number and grid resolution on large-eddy simulations of self-similar jets based on relaxation filtering
QLES2009, Pise, Italy. doi:10.1007/978-94-007-0231-8_29 doi.ico
In: Quality and Reliability of Large-Eddy Simulation II, Springer, Dordrecht, The Netherlands, 319–328. doi:10.1007/978-94-007-0231-8_29 doi.ico
22.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).
23.François KREMER, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2011).
Etude de schémas de Runge-Kutta semi-implicites pour la simulation des écoulements de paroi
20ème Congrès Français de Mécanique, Besançon, France.
In: Actes du CFM 2011, Association Française de Mécanique, Courbevoie.
full text
24.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2011).
A further step towards grid-converged solutions for an initially nominally turbulent jet
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2836 (11 pages).
25.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2011).
A computational study of the effects of nozzle-exit turbulence level on the flow and acoustic fields of a subsonic jet
17th AIAA/CEAS Aeroacoustics Conference, Portland, Oregon, United States.
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2837 (18 pages).
26.F. KERHERVÉ, P. JORDAN, J. DELVILLE, Christophe BOGEYorcid_16x16.png, Daniel JUVÉ (2010).
Jet turbulence characteristics associated with downstream and sideline sound emission
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 2010-3965 (13 pages).
27.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).
28.Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2010).
Numerical investigation of flow features and acoustic radiation around a round cavity
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 2010-3988 (13 pages).
29.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2010).
Flow and acoustic fields of Reynolds number 105, subsonic jets with tripped exit boundary layers
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 2010-3727 (18 pages).
30.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2010).
On the importance of specifying appropriate nozzle-exit conditions in jet noise prediction
IUTAM Symposium on Computational Aero-Acoustics for Aircraft Noise Prediction, Southampton, United Kingdom. doi:10.1016/j.proeng.2010.09.005 doi.ico
In: Procedia Engineering, Elsevier, Amsterdam, The Netherlands, 38–43. doi:10.1016/j.proeng.2010.09.005 doi.ico
31.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2009).
Explicit low dispersive and low dissipative non-centered finite differences and filters
Fourth International Conference on Computational Fluid Dynamics, ICCFD4, Ghent, Belgium.
In: Proceedings of the Fourth International Conference on Computational Fluid Dynamics, Springer, Dordrecht, The Netherlands, 825–830.
32.Olivier MARSDEN, Emmanuel JONDEAU, Pascal SOUCHOTTE, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (2008).
Investigation of flow features and acoustic radiation of a round cavity
14th AIAA/CEAS Aeroacoustics Conference, Vancouver, Canada.
In: Proceedings of the 14th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2008-2851 (13 pages).
33.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.
34.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2008).
Analysis of numerical error reduction in explicitly filtered LES using two-point turbulence closure
Workshop on Quality and Reliability in Large-Eddy Simulations, Leuven, Belgium.
In: Quality and Reliability of Large-Eddy Simulations, Springer, Dordrecht, The Netherlands, 143–154.
35.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2008).
Assessment of dissipation in LES based on explicit filtering from the computation of kinetic energy budget
Workshop on Quality and Reliability in Large-Eddy Simulations, Leuven, Belgium.
In: Quality and Reliability of Large-Eddy Simulations, Springer, Dordrecht, The Netherlands, 81–92.
36.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).
37.J. SCHULZE, C. SCHAUPP, J. SESTERHENN, R. FRIEDRICH, Julien BERLAND, Christophe BOGEYorcid_16x16.png, Daniel JUVÉ (2007).
Shock-induced noise in 2D sub- and supersonic mixing layers
CEMRACS 2005 - Computational Aeroacoustics and Computational Fluid Dynamics in Turbulent Flows, Marseille, France. hal.ico
In: ESAIM : Proceedings of CEMRACS 2005, EDP Sciences, 91940 Les Ulis, France, 51–65. hal.ico
38.E. DEYKINA, Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Daniel JUVÉ (2007).
Simulation numérique de la propagation de signaux acoustiques basses fréquences dans l'atmosphère
18ème Congrès français de mécanique, Grenoble, France.
In: Jacqueline ETAY (Ed.), E.J. HOPFINGER (Ed.), Philippe MARTY (Ed.), Actes du 18ème Congrès Français de Mécanique, Association Française de Mécanique, Courbevoie.
39.Christophe BOGEYorcid_16x16.png, Sébastien BARRÉ, Christophe BAILLYorcid_16x16.png (2007).
Direct computation of the noise generated by a hot coaxial jet
13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy.
In: Proceedings of the 13th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2007-3587 (17 pages).
40.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2007).
Large Eddy Simulation of a self-preserving turbulent jet using high-order schemes
The Fifth International Conference on Fluid Mechanics, Shangai, China.
In: New Trends in Fluid Mechanics Research : Proceedings of the Fifth International Conference on Fluid Mechanics, Springer, Dordrecht, The Netherlands, 95–98.
41.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2007).
Turbulence and energy balance in an axisymmetric jet computed by large eddy simulation
Eleventh European Turbulence Conference, Porto, Portugal.
In: José M. L. M. PALMA (Ed.), A. SILVA LOPEZ (Ed.), Advances in Turbulence XI, Springer, Dordrecht, The Netherlands, 316–318.
42.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Large Eddy Simulation of screech tone generation in a planar underexpanded jet
12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2006-2496 (23 pages).
43.Sébastien BARRÉ, Vincent FLEURY, Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (2006).
Experimental study of the properties of near-field and far-field jet noise
12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA Paper 2006-2649 (14 pages).
44.Sébastien BARRÉ, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Computation of the noise radiated by jets with laminar turbulent nozzle-exit conditions
12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA Paper 2006-2443 (15 pages).
45.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2006).
An overview of numerical methods for acoustic wave propagation
European Conference of Computational Fluid Dynamics, ECCOMAS CFD 2006, Egmond aan Zee, Netherlands.
In: Proceedings ECCOMAS CFD 2006, , .
46.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Computation of a shock containing planar jet and its screech tones using Large-Eddy Simulation
Conference on Turbulence and Interactions, Porquerolles, France.
In: Proceedings of the Conference on Turbulence and Interactions, , .
47.Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Turbulent boundary layers around a NACA 0012 airfoil and their radiated sound
12th AIAA/CEAS Aeroacoustics Conference, Cambridge, Massachusetts, United States.
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2006-2503 (11 pages).
48.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2004).
Study of the effective Reynolds number of jets computed by LES
Tenth European Turbulence Conference, Trondheim, Norway.
In: H. I. ANDERSSON (Ed.), P.-Å. KROGSTAD (Ed.), Advances in Turbulence X, International Center for Numerical Methods in Engineering (CIMNE), Barcelona, Spain, 852.
 
communications sans actes
1.D. FAUCONNIER, E. DICK, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2011).
Assessment of large-eddy simulation based on relaxation filtering: application to the Taylor-Green vortex
7th International Symposium on Turbulence and Shear Flow Phenomena, Ottawa, Canada.
full text
2.Christophe BOGEYorcid_16x16.png, Olivier MARSDEN, Christophe BAILLYorcid_16x16.png (2011).
Investigation of the effects of initial turbulence level on the flow field properties of a subsonic jet
7th International Symposium on Turbulence and Shear Flow Phenomena, Ottawa, Canada.
full text
3.Christophe BOGEYorcid_16x16.png, C. COIFFET, Christophe BAILLYorcid_16x16.png, Daniel JUVÉ (2008).
Identification of sound generation from LES data using flow-noise correlations
Ercoftac Symposium on sound source mechanisms in turbulent shear-flow, Poitiers, France.
4.Olivier MARSDEN, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Turbulent boundary layer development around a NACA 0012 airfoil
Whither Turbulence Prediction and Control 2006, Seoul, Korea, Republic of.
WTPC-007
5.Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Influence of the Reynolds number on the development of transitional jets computed by Large Eddy Simulation
Whither Turbulence Prediction and Control 2006, Seoul, Korea, Republic of.
WTPC-003
6.Julien BERLAND, Christophe BOGEYorcid_16x16.png, Christophe BAILLYorcid_16x16.png (2006).
Investigation of shock-induced noise in a supersonic jet using large-eddy simulation
10th CEAS Aeroacoustics Workshop on Jet Noise Prediction, Dublin, Ireland.
 
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