System Noise Assessment and the Potential for Low Noise Hybrid Wing Body Aircraft with Open Rotor Propulsion
Author:
Affiliation:
1. NASA Langley Research Center
2. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0258
Reference44 articles.
1. Liebeck, R.H. "Design of the Blended-Wing-Body Subsonic Transport," AIAA Paper No. 2002-0002.
2. Acoustic characteristics of counterrotating unducted fans from modelscale tests
3. Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7)
4. Noise of a model counterrotation propeller with reduced aft rotor diameter at simulated takeoff/approach conditions (F7/A3)
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