Numerical Methods: Fast Multipole Method for Shielding Effects
Author:
Affiliation:
1. Airbus France
2. EADS
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2971
Reference4 articles.
1. Acoustic radiation modelling of aeroengine intake comparison between analytical and numerical methods
2. 2Druon,Y.,Lidoine,S.and Roger,M."Acousticradiation modellingofaeroengineExhaust.Comparison betweenanalytical andnumerical methods.",10thAIAA/CEASAeroacousticsConference,Manchester, 2004.
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