Details
- SCHRAM, C. – von Karman Institute for Fluid Dynamics, Belgium
An introduction to linear acoustics and flow noise at low Mach numbers - EWERT, R.; BAUER, M.; LUMMER, M. – DLR, Germany
State-of-the-art CAA approaches - ROGER, M. – Ecole Centrale de Lyon, France
Overview of sound-generating mechanisms in high-lift devices and landing gears
Analytical modeling of high-lift device noise - SIJTSMA, P. – National Aerospace Laboratory NLR, The Netherlands
Acosutic beamforming for the ranking of aircraft noise - MANOHA, E. – ONERA, France
Designing validation experiments in aeroacoustics - TERRACOL, M. – ONERA, France
Advanced RANS/LES methods for aeroacoustics - SHUR, M.1; STRELETS, M.1; TRAVIN, A.1, SPALART, P.2 - 1New Technologies and Services (NTS) & Saint-Petersburg State Polytechnic University (SPbSPU), Russia - 2Boeing Commercial Airplanes, USA
Generation of turbulent inflow conditions for aeroacoustics - MARTÍNEZ-LERA, P. – LMS International, Belgium
Source modeling for boundary and finite element methods - GICQUEL, L.Y.M.1 & MOREAU, S.2 – 1CERFACS CFD Team (Combustion Group), France & 2Université de Sherbrooke, Canada
Large Eddy Simulations of aeronautical compressible flows - ABALAKIN, I.1; BAKHVALOV, P.2; KOZUBSKAYA, T.1 - 1Keldysh Institute of Applied Mathematics RAS & 2Moscow Institute of Physics and Technology, Russia
Edge-based methods in CAA - KNACKE, T. – Technische Universität Berlin, Germany
Potential effects of Rhie & Chow type interpolations in airframe noise simulations
Additional Information
| Manufacturer | von Karman Institute for Fluid Dynamics |
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