A parametric study of the noise radiated by the flow around multiple bodies: direct noise computation of the influence of the separating distance in rod-airfoil flow configurations
Author:
Affiliation:
1. National Center for Scientific Research (CNRS)
2. EDF
3. École Centrale de Lyon
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2819
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3. Numerical Insight into Sound Sources of a Rod-Airfoil Flow Configuration Using Direct Noise Calculation
4. A family of low dispersive and low dissipative explicit schemes for flow and noise computations
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1. Numerical Investigation of Wavy Leading Edges on Rod–Airfoil Interaction Noise;AIAA Journal;2018-07
2. Noise Source Analysis of a Rod–Airfoil Configuration Using Unstructured Large-Eddy Simulation;AIAA Journal;2015-04
3. Experimental study of vortex–structure interaction noise radiated from rod–airfoil configurations;Journal of Fluids and Structures;2014-11
4. Prediction of LAGOON landing-gear noise using an unstructured LES Solver;19th AIAA/CEAS Aeroacoustics Conference;2013-05-24
5. Prediction of the sound generated by a rod-airfoil configuration using a compressible unstructured LES solver and a FW-H analogy;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04
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