Guillaume Brès

Journal publications

Second-mode attenuation and cancellation by porous coatings in a high-speed boundary layer: G. A. Brès, M. Inkman, T. Colonius and A. V. Fedorov; Submitted for publication in Journal of Fluid Mechanics, 2012
Flow and Noise Predictions for the Tandem Cylinder Aeroacoustic Benchmark: G. A. Brès, D. Freed, M. Wessels, S. Noelting and F.Pérot; Physics of Fluids, 24(036101), 2012
Acoustic Analogy Formulation for Moving Sources in Uniformly Moving Media: A. Najafiyazdi, G. A. Brès and L. Mongeau; Proc. of the Royal Society, London A., Vol 467, pp. 144-165, 2011
Acoustic Properties of Porous Coatings for Hypersonic Boundary-Layer Control: G. A. Brès, T. Colonius and A. V. Fedorov; AIAA Journal, Vol 48 (2), pp. 267-274, 2010
Three-Dimensional Instabilities in Compressible Flow over Open Cavities: G. A. Brès and T. Colonius; Journal of Fluid Mechanics , Vol. 599, pp. 309-339, 2008
A First Step toward the Prediction of Rotorcraft Maneuver Noise: G. Perez, K. S. Brentner, G. A. Brès and H. E. Jones; Journal of the American Helicopter Society 50 (3): 230-237, 2005
Maneuvering Rotorcraft Noise Prediction: G. A. Brès, K. S. Brentner, G. Perez and H. E. Jones; Journal of Sound and Vibration 275 (3-5): 719-738, 2004

Towards Best Practices for Jet Noise Predictions with Unstructured Large Eddy Simulations: G. A. Brès, J. W. Nichols, S. K. Lele and F. E. Ham; AIAA-2012-2965 42nd AIAA Fluid Dynamics Conf., New Orleans, LA, June 2012
Towards Numerical Aircraft Noise Certification: Analysis of a Full-Scale Landing Gear in Fly-Over Configuration: D. Casalino, S. Nölting, E. Fares, T. Van de Ven, F. Pérot and G. A. Brès; AIAA-2012-2235, 18th AIAA/CEAS Aeroacoustics Conf., Colorado Springs, CO, June 2012
Unstructured Large Eddy Simulation of a Hot Supersonic Over-Expanded Jet with Chevrons: G. A. Brès, J. W. Nichols, S. K. Lele, F. E. Ham, R. H. Schlinker, R. A. Reba and J. Simonich; AIAA-2012-2213, 18th AIAA/CEAS Aeroacoustics Conf., Colorado Springs, CO, June 2012
Parabolized Stability Equation Models in Turbulent Supersonic Jets: D. Rodriguez, A. Sinha, G. A. Brès and T. Colonius; AIAA-2012-2117, 18th AIAA/CEAS Aeroacoustics Conf., Colorado Springs, CO, June 2012

Unstructured Large Eddy Simulation Technology for Aeroacoustics of Complex Jet Flows: G. A. Brès, Y. Khalighi, F. E. Ham and S. K. Lele; Proceedings of Inter-Noise 2011 Conf., Osaka, Japan, Sept. 2011
Numerical Simulations of the Transient Flow Response of a 3D, Low-Aspect-Ratio Wing to Pulsed Actuation: G. A. Brès, E. Fares, D. R. Williams and T. Colonius; AIAA-2011-3440, 41st AIAA Fluid Dynamic Conf., Honolulu, HI, June 2011
Flow and Noise Predictions for Tandem Cylinders in a Realistic Wind-Tunnel Configuration: G. A. Brès; AIAA-2011-2824, 17th AIAA/CEAS Aeroacoustics Conf., Portland, OR, June 2011
Instability of Hypersonic Boundary Layer on a Wall with Resonating Micro-Cavities: A. V. Fedorov, G. A. Brès, M. Inkman and T. Colonius; AIAA-2011-373, 49th AIAA Aerospace Sciences Meeting, Orlando, FL, Jan. 2011

Numerical Simulations of Natural and Actuated Flow over a 3D Low-Aspect-Ratio Airfoil: G. A. Brès, D. R. Williams and T. Colonius; AIAA-2010-4713, 40th AIAA Fluid Dynamic Conf., Chicago, IL, June 2010
An Hybrid Lattice Boltzmann/FW-H Method to Predict Sources and Propagation of Landing Gear Noise: S. Noelting, G. A. Brès, P. Dethioux, T. Van de Ven and R. Vieito; AIAA-2010-3976, 16th AIAA/CEAS Aeroacoustics Conf., Stockholm, Sweden, June 2010
Tandem Cylinder Noise Predictions using Lattice Boltzmann and Ffowcs Williams-Hawkings Methods: G. A. Brès, M. Wessels and S. Noelting; AIAA-2010-3791, 16th AIAA/CEAS Aeroacoustics Conf., Stockholm, Sweden, June 2010
A Ffowcs Williams-Hawkings Solver for Lattice-Boltzmann based Computational Aeroacoustics: G. A. Brès, F. Pérot and D. Freed; AIAA-2010-3711, 16th AIAA/CEAS Aeroacoustics Conf., Stockholm, Sweden, June 2010
An Acoustic Analogy Formulation for Arbitrary Source Motion in Uniformly Moving Media: A. Najafiyazdi, L. Mongeau and G. A. Brès; AIAA-2010-3706, 16th AIAA/CEAS Aeroacoustics Conf., Stockholm, Sweden, June 2010

Alternate Designs of Ultrasonic Absorptive Coatings for Hypersonic Boundary Layer Control: G. A. Brès, M. Inkman, T. Colonius and A. V. Fedorov; AIAA-2009-4217, 39th AIAA Fluid Dynamic Conf., San Antonio, TX, June 2009
Properties of the Lattice Boltzmann Method for Acoustics: G. A. Brès, F. Pérot and D. Freed; AIAA-2009-3395, 15th AIAA/CEAS Aeroacoustics Conf., Miami, FL, May 2009

Stability of Temporally Evolving Supersonic Boundary Layers over Micro-Cavities for Ultrasonic Absorptive Coatings: G. A. Brès, T. Colonius and A. V. Fedorov; AIAA-2008-4337, 5th Theoretical Fluid Mechanics Conf., Seattle, WA, June 2008
Interaction of Acoustic Disturbances with Micro-Cavities for Ultrasonic Absorptive Coatings: G. A. Brès, T. Colonius and A. V. Fedorov; AIAA-2008-3903, 5th Theoretical Fluid Mechanics Conf., Seattle, WA, June 2008

Direct Numerical Simulations of Three-Dimensional Cavity Flows: G. A. Brès and T. Colonius; AIAA-2007-3405, 13th AIAA/CEAS Aeroacoustics Conf., Rome, Italy, May 2007
Three-Dimensional Linear Stability Analysis of Cavity Flows: G. A. Brès and T. Colonius; AIAA-2007-1126, 45th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 2007
Toward a Better Understanding of Maneuvering Rotorcraft Noise: K. S. Brentner, G. Perez, G. A. Brès and H. E. Jones; Proc. Vol. 2, pp. 1552-1562, AHS 58th Forum, Montréal, Canada, June 2002
Maneuvering Rotorcraft Noise Prediction: A New Code for a New Problem: K. S. Brentner, G. A. Brès, G. Perez and H. E. Jones; AHS Aerodynamics and Acoustic Meeting, San Francisco, CA, Jan. 2002