Azimuthal Structure of Low-Frequency Noise of Installed Jet-Reference-Cited by-同舟云学术

Azimuthal Structure of Low-Frequency Noise of Installed Jet

Published:2019-05 Issue:5 Volume:57 Page:1885-1898
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Faranosov Georgy¹,Belyaev Ivan¹,Kopiev Victor²,Bychkov Oleg³

Affiliation:

1. Perm National Research Polytechnic University, 614990, Perm, Russia

2. TsAGI Moscow Research Complex, 105005, Moscow, Russia

3. Moscow Institute of Physics and Technology, 140180, Zhukovsky, Russia

Funder

Ministry of Education and Science of the Russian Federation

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057476

Reference48 articles.

1. Development of NOVA Aircraft Configurations for Large Engine Integration Studies

2. Numerical Study of Acoustic Installation Effects with a Computational Aeroacoustics Method

3. PerrinoM. “An Experimental Study into Pylon, Wing, and Flap Installation Effects on Jet Noise Generated by Commercial Aircraft,” Ph.D. Thesis, Univ. of Cincinnati, Cincinnati, OH, 2014.

4. LawrenceJ. “Aeroacoustic Interactions of Installed Subsonic Round Jets,” Ph.D. Thesis, Univ. of Southampton, Southampton, England, U.K. 2014.

5. HeffernonT. J. “Aircraft Noise Installation Effects,” Ph.D. Thesis, Univ. of Southampton, Southampton, England, U.K. 2017.

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