On Noise Assessment for Blended Wing Body Aircraft-Reference-Cited by-同舟云学术

On Noise Assessment for Blended Wing Body Aircraft

Published:2014-01-10 Issue: Volume: Page:
ISSN:
Container-title:52nd Aerospace Sciences Meeting
language:
Short-container-title:

Author:

Guo Yueping¹,Burley Casey L.²,Thomas Russell H.²

Affiliation:

1. The Boeing Company

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0365

Reference30 articles.

1. Liebeck R. H. "Design of the Blended-Wing-Body Subsonic Transport" AIAA Paper 2002-0002.

2. Nickol C. L. & McCullers L. "Hybrid Wing Body Configuration System Studies" AIAA Paper 2009-931.

3. Bonet J. T., Schellenger H. G., Rawdon B. K., Elmer K. R., Wakayama S. R., Brown D. & Guo Y. P. "Environmentally Responsible Aviation (ERA) Project - N+2 Advanced Vehicle Concepts Study and Conceptual Design of Subscale Test Vehicle (STV)," NASA Contract Report 2013-216519, 2013.

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

Cited by 26 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Multidisciplinary Optimization of Aircraft Aerodynamics for Distributed Propulsion Configurations;Applied Sciences;2024-09-03

2. The U.S. Air Force Next-Generation Air-Refueling System: A Resurgence of the Blended Wing Body?;Aerospace;2024-06-20

3. Powered Low-Speed Experimental Aerodynamic Investigation of an Over-Wing-Mounted Nacelle Configuration;Journal of Aircraft;2023-11-30

4. Wind tunnel investigation of different engine layouts of a blended-wing-body transport;Chinese Journal of Aeronautics;2023-09

5. System noise assessment of conceptual tube-and-wing and blended-wing-body aircraft designs;AIAA AVIATION 2023 Forum;2023-06-08