Experimental Study on Open Rotor Noise Shielding by Hybrid-Wing-Body Aircraft
Author:
Affiliation:
1. The Boeing Company, 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.J054243
Reference11 articles.
1. HarrisR. W.CuthbertsonR. D. “UDFTM/727 Flight Test Program,” AIAA Paper 1987-1733, 1987.
2. CzechM.ThomasR. H. “Open Rotor Aeroacoustic Installation Effects for Conventional and Unconventional Airframes,” AIAA Paper 2013-2185, 2013.
3. System Noise Assessment of Blended-Wing-Body Aircraft with Open Rotor Propulsion
4. BonetJ. T.SchellengerH. G.RawdonB. K.ElmerK. R.WakayamaS. R.BrownD.GuoY. P. “Environmentally Responsible Aviation (ERA) Project—N + 2 Advanced Vehicle Concepts Study and Conceptual Design of Subscale Test Vehicle (STV),” NASA CR-NND11AG03C, Dec. 2011.
5. Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiments
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