The prediction of ducted fan engine noise via a boundary integral equation method
Author:
Affiliation:
1. Old Dominion Univ., Norfolk, VA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1770
Reference16 articles.
1. A boundary integral formulation for thin‐walled shapes of revolution
2. Development of a sound radiation model for a finite-length duct of arbitrary shape
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