Experimental Study on Open Rotor Noise Shielding by Hybrid-Wing-Body Aircraft-Reference-Cited by-同舟云学术

Experimental Study on Open Rotor Noise Shielding by Hybrid-Wing-Body Aircraft

Published:2016-01 Issue:1 Volume:54 Page:242-253
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Guo Yueping¹,Thomas Russell H.²

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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