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articles
1.Stefano MELONIorcid_16x16.png, Roberto CAMUSSIorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2025).
An analysis of the effect of the jet initial conditions on the wavelet separated near-field acoustic pressure
Theor. Comput. Fluid Dyn. 39, 5 (14 pages). doi:10.1007/s00162-024-00727-9 doi.ico hal.ico openalex-16x16.png
2.Shota MORITA, AIko YAKENO, Christophe BOGEYorcid_16x16.png, Obayashi SHIGERU (2024).
Study of an aeroacoustic internal feedback loop in a high-speed jet using mode decomposition methods
J. Flow Energy 2, 67–83. doi:10.60197/flowenergy.2.0_67 doi.ico hal.ico openalex-16x16.png
3.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 hal.ico openalex-16x16.png
4.Giorgio PALMAorcid_16x16.png, Stefano MELONIorcid_16x16.png, Roberto CAMUSSIorcid_16x16.png, Umberto IEMMAorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2024).
Subsonic jet noise prediction in near and far field with optimized wave-packet approach
AIAA J. 62, 4144–4152. doi:10.2514/1.J064232 doi.ico hal.ico openalex-16x16.png
5.Christophe BOGEYorcid_16x16.png (2024).
Gain in efficiency of jet receptivity to acoustic disturbances with increasing nozzle-lip thickness
J. Fluid Mech. 997, A71 (26 pages). doi:10.1017/jfm.2024.849 doi.ico hal.ico openalex-16x16.png
6.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 hal.ico openalex-16x16.png
7.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 hal.ico openalex-16x16.png
8.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
9.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 hal.ico openalex-16x16.png
10.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 hal.ico openalex-16x16.png
11.Mathieu VARÉorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2023).
Mach number dependence of tone generation by impinging round jets
AIAA J. 61, 3551–3565. doi:10.2514/1.J062746 doi.ico hal.ico openalex-16x16.png
12.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. 61, 2179–2188. doi:10.2514/1.J062261 doi.ico hal.ico openalex-16x16.png
13.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 hal.ico openalex-16x16.png
14.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
15.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
16.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
17.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
18.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
19.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
20.Mathieu VARÉorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2022).
Presence and properties of acoustic peaks near the nozzle of impinging rocket jets
Acta Acustica 6, 36 (11 pages). doi:10.1051/aacus/2022033 doi.ico hal.ico openalex-16x16.png
21.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 hal.ico openalex-16x16.png
22.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
23.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
24.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
25.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
26.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
27.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
28.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
29.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
30.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
31.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
32.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
33.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
34.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
35.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
36.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
37.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
38.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
39.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
40.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
41.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
42.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
43.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
44.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
45.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
46.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
47.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
48.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
49.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
50.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
51.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
52.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
53.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
54.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
55.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
56.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
57.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
58.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
59.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
60.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
61.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
62.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
63.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
64.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
65.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
66.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.
67.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png, Olivier MARSDEN (2010).
Progress in direct noise computation
Int. J. Aeroacoustics 9, 123–143.
68.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
69.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
70.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
71.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
72.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
73.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
74.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
75.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
76.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
77.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
78.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
79.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
80.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
81.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
82.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
83.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
84.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 hal.ico openalex-16x16.png
85.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
86.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
87.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
88.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
89.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
90.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
91.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.
92.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.
93.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.
94.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.
95.Christophe BAILLYorcid_16x16.png, Christophe BOGEYorcid_16x16.png (2004).
Contributions of computational aeroacoustics to jet noise research and prediction.
Combustion 18, 481–491.
96.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.
97.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.
98.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. doi:10.2514/2.2115 doi.ico hal.ico openalex-16x16.png
99.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
100.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.
101.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.
102.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
103.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
104.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.
105.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.
106.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.Hugo VINCENTorcid_16x16.png (dir.: Christophe BOGEY) (2024).
Simulations et analyses de sensibilité du bruit produit des écoulements cisaillés
Thèse École centrale de Lyon hal.ico
2.Valentin MORIN (dir.: Christophe BOGEY) (2023).
Étude numérique de l'injection d'eau pour la réduction du bruit de jet de lanceurs spatiaux
Thèse École centrale de Lyon hal.ico
3.Mathieu VARÉorcid_16x16.png (dir.: Christophe BOGEY) (2020).
Étude du rayonnement acoustique et des mécanismes de rétroaction des jets impactant une plaque trouée par simulation des grandes échelles
Thèse École centrale de Lyon hal.ico
4.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
5.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
6.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
7.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
8.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
9.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
10.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
11.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
12.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.
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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. hal.ico
In: Proceedings of the 17th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2011-2929. hal.ico
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
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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).
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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. hal.ico
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA 2006-2496 (23 pages). hal.ico
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. hal.ico
In: Proceedings of the 12th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA Paper 2006-2649 (14 pages). hal.ico
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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