Acoustic radiation modelling of aeroengine intake comparison between analytical and numerical methods
Author:
Affiliation:
1. EADS Airbus SA, Toulouse, France
2. Lyon, Ecole Centrale, Ecully, France
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2140
Reference25 articles.
1. A finite element method for transmission in non-uniform ducts without flow: Comparison with the method of weighted residuals
2. On the acoustic boundary condition in the presence of flow
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