The Reduction of Main Landing Gear Noise
Author:
Affiliation:
1. Trinity College Dublin
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-2900
Reference28 articles.
1. Full-scale noise testing on Airbus landing gears in the German Dutch Wind tunnel
2. Experimental study on Noise Generation of a Two-Wheel Main Landing Gear
3. Characterization of Low Noise Technologies Applied to a Full Scale Fuselage Mounted Nose Landing Gear
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