Design and Characterization of a High-Speed Subsonic Aeroacoustic Wind Tunnel-Reference-Cited by-同舟云学术

Design and Characterization of a High-Speed Subsonic Aeroacoustic Wind Tunnel

Published:2019-01 Issue:1 Volume:56 Page:108-120
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Giardino Frank¹,Rocha Joana¹

Affiliation:

1. Carleton University, Ottawa, Ontario K1S 5B6, Canada

Funder

Natural Sciences and Engineering Research Council of Canada

Consortium for Research and Innovation in Aerospace in Quebec

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C035113

Reference43 articles.

1. Contributions of Different Aeroacoustic Sources to Aircraft Cabin Noise

2. Cruise Flight Noise Levels in a Turbojet Transport Airplane

3. HaydenR. E.MurrayB. S.TheobaldM. A. “A Study of Interior Noise Levels, Noise Sources and Transmission Paths in Light Aircraft,” NASA Langley Research Center, CR-172152, Hampton, VA, 1983, pp. 1–198.

4. WALL-PRESSURE FLUCTUATIONS BENEATH TURBULENT BOUNDARY LAYERS: SOME REFLECTIONS ON FORTY YEARS OF RESEARCH

5. Review of Turbulent Boundary Layer Models for Acoustic Analysis

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