System Noise Assessment of Blended-Wing-Body Aircraft with Open Rotor Propulsion
Author:
Affiliation:
1. The Boeing Company
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1215
Reference29 articles.
1. Sound generated from the interruption of a steady flow by a supersonically moving aerofoil
2. A note on sound from the interruption of a cylindrical flow by a semi-infinite aerofoil of subsonic speed
3. Sound generation by a supersonic aerofoil cutting through a steady jet flow
4. The NASA Environmentally Responsible Aviation Project/General Electric Open Rotor Test Campaign
5. Inlet noise reduction by shielding for the blended-wing-body airplane
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1. The U.S. Air Force Next-Generation Air-Refueling System: A Resurgence of the Blended Wing Body?;Aerospace;2024-06-20
2. The Aircraft Noise Simulation Working Group (ANSWr) – V2 Aircraft Results;25th AIAA/CEAS Aeroacoustics Conference;2019-05-18
3. Current engine noise and reduction technology;CEAS Aeronautical Journal;2019-03
4. Experimental Study on Open Rotor Noise Shielding by Hybrid-Wing-Body Aircraft;AIAA Journal;2016-01
5. Open Rotor Noise Shielding by Blended-Wing-Body Aircraft;53rd AIAA Aerospace Sciences Meeting;2015-01-03
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