Directivity of landing-gear noise based on flyover measurements
Author:
Affiliation:
1. German Aerospace Center, Inst. of Propulsion Technology, Berlin, Germany
2. Northwestern Polytechnical Univ., Xian, China
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1956
Reference5 articles.
1. Full-scale noise testing on Airbus landing gears in the German Dutch Wind tunnel
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