Towards the use of boundary element method in computational aeroacoustics
Author:
Affiliation:
1. ONERA, Chatillon, France
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1980
Reference8 articles.
1. Direct computation of the sound from a compressible co-rotating vortex pair
2. Sound generation in a mixing layer
3. Computation of jet mixing noise due to coherent structures: the plane jet case
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