Christophe Bogey
32%
Libre accès
100
Documents
Identifiants chercheurs
- cbogey
- 0000-0003-3243-747X
- IdRef : 133433803
Présentation
Domaines de recherche
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Publications
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Aeroacoustic wave equation based on Pierce's operator applied to the sound generated by a mixing layer28th AIAA/CEAS Aeroacoustics 2022 Conference, Jun 2022, Southampton, United Kingdom. ⟨10.2514/6.2022-2896⟩
Communication dans un congrès
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Influence of resolution and Reynolds number on large-eddy simulations of channel flow using relaxation filtering51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Jan 2013, Grapevine (Dallas/Ft. Worth Region), United States. ⟨10.2514/6.2013-517⟩
Communication dans un congrès
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Development of semi-implicit Runge-Kutta schemes and application to a turbulent channel flow18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), Jun 2012, Colorado Springs, United States. ⟨10.2514/6.2012-2066⟩
Communication dans un congrès
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Effects of initial shear-layer thickness on turbulent subsonic jets at moderate Reynolds numbers18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), Jun 2012, Colorado Springs, United States. ⟨10.2514/6.2012-2249⟩
Communication dans un congrès
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Investigation of a turbulent channel flow using large eddy simulationAcoustics 2012, Apr 2012, Nantes, France
Communication dans un congrès
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Flow and sound fields of initially tripped jets at Reynolds numbers ranging from 25,000 to 200,00050th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Jan 2012, Nashville, United States. ⟨10.2514/6.2012-1172⟩
Communication dans un congrès
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Depth effects on the flow features and noise signature of shallow cylindrical cavities at a Mach number of 0.2518th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), Jun 2012, Colorado Springs, United States. ⟨10.2514/6.2012-2232⟩
Communication dans un congrès
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A computational study of the effects of nozzle-exit turbulence level on the flow and acoustic fields of a subsonic jet17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), Jun 2011, Portland, United States. ⟨10.2514/6.2011-2837⟩
Communication dans un congrès
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A further step towards grid-converged solutions for an initially nominally turbulent jet17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), Jun 2011, Portland, United States. ⟨10.2514/6.2011-2836⟩
Communication dans un congrès
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Etude numérique de la propagation des infrasons en haute atmosphèreCFM 2011 - 20ème Congrès Français de Mécanique, Aug 2011, Besançon, France
Communication dans un congrès
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Investigation of high supersonic jet noise: non-linear propagation effects and flow-acoustics correlations17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), Jun 2011, Portland, United States. ⟨10.2514/6.2011-2747⟩
Communication dans un congrès
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Etude de schémas de Runge-Kutta semi-implicites pour la simulation des écoulements de paroiCFM 2011 - 20ème Congrès Français de Mécanique, Aug 2011, Besançon, France
Communication dans un congrès
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Direct computation of the noise radiated by a propulsive jet at a Mach number of 3.310ème Congrès Français d'Acoustique, Apr 2010, Lyon, France
Communication dans un congrès
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Flow and acoustic fields of Reynolds number 10 5, subsonic jets with tripped exit boundary layers16th AIAA/CEAS Aeroacoustics Conference, Jun 2010, Stockholm, Sweden. ⟨10.2514/6.2010-3727⟩
Communication dans un congrès
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Direct Noise Computation of a Shocked and Heated Jet at a Mach Number of 3.3016th AIAA/CEAS Aeroacoustics Conference, Jun 2010, Stockholm, Sweden. ⟨10.2514/6.2010-3732⟩
Communication dans un congrès
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Calcul direct du bruit rayonné par un écoulement laminaire à Mach 0.2 affleurant une cavité cylindrique10ème Congrès Français d'Acoustique, Apr 2010, Lyon, France
Communication dans un congrès
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Intégration de la relaxation dans les équations de Navier-Stokes pour la propagation sonore10ème Congrès Français d'Acoustique, Apr 2010, Lyon, France
Communication dans un congrès
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Numerical Investigation of Flow Features and Acoustic Radiation of a Round Cavity16th AIAA/CEAS Aeroacoustics Conference, Jun 2010, Stockholm, Sweden. ⟨10.2514/6.2010-3988⟩
Communication dans un congrès
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Influence of the Nozzle-Exit Boundary-Layer Thickness on the Flow and Acoustic Fields of Initially Laminar Jets15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference), May 2009, Miami, United States. ⟨10.2514/6.2009-3409⟩
Communication dans un congrès
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Développement de schémas d'interpolation décentrés stables pour le calcul multidomaine en aéroacoustique.CFM 2009 - 19ème Congrès Français de Mécanique, Aug 2009, Marseille, France
Communication dans un congrès
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Large-eddy simulations of round jets: effects of initial conditions on self-similarity regionCFM 2009 - 19ème Congrès Français de Mécanique, Aug 2009, Marseille, France
Communication dans un congrès
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Développement d une méthode de filtrage adaptatif et conservatif pour la capture de chocCFM 2009 - 19ème Congrès Français de Mécanique, Aug 2009, Marseille, France
Communication dans un congrès
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Self-Adjusting Shock-Capturing Spatial Filtering for High-Order Non-Linear Computations14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), May 2008, Vancouver, Canada. ⟨10.2514/6.2008-2968⟩
Communication dans un congrès
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Investigation of flow features and acoustic radiation of a round cavity.14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference), May 2008, Vancouver, Canada. ⟨10.2514/6.2008-2851⟩
Communication dans un congrès
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Simulation numérique de la propagation de signaux acoustiques basse fréquences dans l'atmosphèreCFM 2007 - 18ème Congrès Français de Mécanique, Aug 2007, Grenoble, France
Communication dans un congrès
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Direct Computation of the Noise Generated by a Hot Coaxial Jet13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), May 2007, Rome, Italy. ⟨10.2514/6.2007-3587⟩
Communication dans un congrès
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Contributions de la simulation numérique à la physique du bruit d’origine aérodynamiqueCFM 2007 - 18ème Congrès Français de Mécanique, Aug 2007, Grenoble, France
Communication dans un congrès
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Experimental Study of the Properties of Near-Field and Far-Field Jet Noise12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), May 2006, Cambridge, United States. ⟨10.2514/6.2006-2649⟩
Communication dans un congrès
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Computation of the Noise Radiated by Jets with Laminar/Turbulent Nozzle-Exit Conditions12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), May 2006, Cambridge, United States. ⟨10.2514/6.2006-2443⟩
Communication dans un congrès
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Large Eddy Simulation of Screech Tone Generation in a Planar Underexpanded Jet12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), May 2006, Cambridge, United States. ⟨10.2514/6.2006-2496⟩
Communication dans un congrès
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Direct Noise Computation around a 3-D NACA 0012 airfoil12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), May 2006, Cambridge, United States. ⟨10.2514/6.2006-2503⟩
Communication dans un congrès
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Investigation of sound sources in subsonic jets using causality methods on LES data11th AIAA/CEAS Aeroacoustics Conference, May 2005, Monterey, United States. ⟨10.2514/6.2005-2885⟩
Communication dans un congrès
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Calcul direct du bruit aérodynamique rayonné par des géométries complexes17e Congrès Français de Mécanique 2005, Aug 2005, Troyes, France
Communication dans un congrès
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DNS of a High-Aspect-Ratio Elliptic Vortex and Its Generated Noise11th AIAA/CEAS Aeroacoustics Conference, May 2005, Monterey, United States. ⟨10.2514/6.2005-2956⟩
Communication dans un congrès
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Noise Radiated by a High-Reynolds-number 3-D Airfoil11th AIAA/CEAS Aeroacoustics Conference, May 2005, Monterey, United States. ⟨10.2514/6.2005-2817⟩
Communication dans un congrès
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Optimized Explicit Schemes: Matching and Boundary Schemes, and 4th-order Runge-Kutta Algorithm10th AIAA/CEAS Aeroacoustics Conference, May 2004, Manchester, United Kingdom. ⟨10.2514/6.2004-2814⟩
Communication dans un congrès
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High-order Curvilinear Simulations of Flows Around Non-Cartesian Bodies10th AIAA/CEAS Aeroacoustics Conference, May 2004, Manchester, United Kingdom. ⟨10.2514/6.2004-2813⟩
Communication dans un congrès
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Investigation of Subsonic Jet Noise Using LES: Mach and Reynolds Number Effects10th AIAA/CEAS Aeroacoustics Conference, May 2004, Manchester, United Kingdom. ⟨10.2514/6.2004-3023⟩
Communication dans un congrès
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LES of a High Reynolds, High Subsonic Jet: Effects of the Inflow Conditions on Flow and Noise9th AIAA/CEAS Aeroacoustics Conference and Exhibit, May 2003, Hilton Head, United States. ⟨10.2514/6.2003-3170⟩
Communication dans un congrès
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Numerical Investigation of the Coexistence of Multiple Tones in Flow-induced Cavity Noise9th AIAA/CEAS Aeroacoustics Conference and Exhibit, May 2003, Hilton Head, United States. ⟨10.2514/6.2003-3234⟩
Communication dans un congrès
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LES of a High Reynolds, High Subsonic Jet: Effects of the Subgrid Modellings on Flow and Noise16th AIAA Computational Fluid Dynamics Conference, Jun 2003, Orlando, United States. ⟨10.2514/6.2003-3557⟩
Communication dans un congrès
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A Family of Low Dispersive and Low Dissipative Explicit Schemes for Computing Aerodynamic Noise8th AIAA/CEAS Aeroacoustics Conference & Exhibit, Jun 2002, Breckenridge, United States. ⟨10.2514/6.2002-2509⟩
Communication dans un congrès
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Aerodynamic Noise Induced by Laminar and Turbulent Boundary Layers over Rectangular Cavities8th AIAA/CEAS Aeroacoustics Conference & Exhibit, Jun 2002, Breckenridge, United States. ⟨10.2514/6.2002-2476⟩
Communication dans un congrès
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Noise computation using Lighthill's equation with inclusion of mean flow-acoustics interactions7th AIAA/CEAS Aeroacoustics Conference and Exhibit, May 2001, Maastricht, Netherlands. ⟨10.2514/6.2001-2255⟩
Communication dans un congrès
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Computation of the sound radiated by a 3-D jet using large eddy simulation6th Aeroacoustics Conference and Exhibit, Jun 2000, Lahaina, United States. ⟨10.2514/6.2000-2009⟩
Communication dans un congrès
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Computation of flow noise using source terms in linearized Euler's equations6th Aeroacoustics Conference and Exhibit, Jun 2000, Lahaina, United States. ⟨10.2514/6.2000-2047⟩
Communication dans un congrès
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Computation of mixing layer noise using large eddy simulation5th AIAA/CEAS Aeroacoustics Conference and Exhibit, May 1999, Bellevue, United States. ⟨10.2514/6.1999-1871⟩
Communication dans un congrès
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Numerical simulation of supersonic jet noiseChristophe Brun, Daniel Juvé, Michael Manhart, Claus-Dieter Munz. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 104 (-), Springer, pp.29-46, 2009, 978-3-540-89955-6. ⟨10.1007/978-3-540-89956-3_2⟩
Chapitre d'ouvrage
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