Prediction of the sound generated by a rod-airfoil configuration using a compressible unstructured LES solver and a FW-H analogy
Author:
Affiliation:
1. Airbus
2. University of Sherbrooke
3. CERFACS
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2058
Reference34 articles.
1. Compact finite difference schemes with spectral-like resolution
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3. 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
4. A Comparison between Galerkin and Compact Schemes for Jet Noise Simulations
5. A rod-airfoil experiment as a benchmark for broadband noise modeling
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