Hybrid Wing–Body Aircraft Slat Noise-Reference-Cited by-同舟云学术

Hybrid Wing–Body Aircraft Slat Noise

Published:2013-12 Issue:12 Volume:51 Page:2935-2945
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Guo Yueping¹,Brusniak Leon²,Czech Michael²,Thomas Russell H.³

Affiliation:

1. Acoustics Technology, Boeing Research and Technology, Huntington Beach, California 92647

2. Acoustics Technology, Boeing Commercial Airplane, Everett, Washington 98124

3. 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.J052540

Reference18 articles.

1. Inlet noise reduction by shielding for the blended-wing-body airplane

2. Integration of Propulsion-Airframe-Aeroacoustic Technologies and Design Concepts for a Quiet Blended-Wing-Body Transport

3. Hybrid Wing Body Aircraft System Noise Assessment with Propulsion Airframe Aeroacoustic Experiments

4. Propulsion Airframe Aeroacoustic Integration Effects for a Hybrid Wing Body Aircraft Configuration

5. 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.

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