Experimental Studies on a Rudimentary Four-Wheel Landing Gear
Author:
Affiliation:
1. National Aerospace Laboratories, Bangalore 560017, India
2. The Boeing Company, Seattle, WA 98108
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051639
Reference17 articles.
1. Sound Radiation from Aircraft Wheel-WelVLanding-Gear Configurations
2. Full-scale noise testing on Airbus landing gears in the German Dutch Wind tunnel
3. Experimental Study on Aircraft Landing Gear Noise
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