System Noise Assessment of Hybrid Wing–Body Aircraft with Open-Rotor Propulsion
Author:
Affiliation:
1. Boeing Research and Technology, Huntington Beach, California 92647
2. Aeroacoustics Branch, NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033048
Reference33 articles.
1. Sound generated from the interruption of a steady flow by a supersonically moving aerofoil
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4. Open Rotor Designs for Low Noise and High Efficiency
5. Inlet noise reduction by shielding for the blended-wing-body airplane
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