Computation of sound radiating from engine inlets
Author:
Affiliation:
1. Pennsylvania State University, University Park, Pennsylvania 16802-1401
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13165
Reference24 articles.
1. Wave envelope and finite element approximations for turbofan noise radiation in flight
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