A parametric study of nose landing gear noise in a large-scale aeroacoustic wind tunnel-Reference-Cited by-同舟云学术

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A parametric study of nose landing gear noise in a large-scale aeroacoustic wind tunnel

Published:2022-12 Issue: Volume:201 Page:109130
ISSN:0003-682X
Container-title:Applied Acoustics
language:en
Short-container-title:Applied Acoustics

Author:

Zhao Kun,Zhang Rongping,Kopiev Victor,Belyaev Ivan,Okolo Patrick N.

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

Ministry of Education and Science of the Russian Federation

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference41 articles.

1. Almost 40 years of airframe noise research: What did we achieve?;Dobrzynski;J Aircraft,2010

2. Measurement and control of aircraft landing gear broadband noise;Li;Aerosp Sci Technol,2012

3. QTD 2 (quiet technology demonstrator 2) main landing gear noise reduction fairing design and analysis;Abeysinghe,2007

4. Bluff body noise control using perforated fairings;Boorsma;AIAA J,2009

5. Suppression of aerodynamic noise using dual-jet air curtains combined with perforated fairings;Zhao;Appl Acoust,2020

Cited by 3 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. Assessment of an Open-Source Aircraft Noise Prediction Model Using Approach Phase Measurements;Journal of Aircraft;2023-11-07

2. Intelligent prediction of acoustic performance of landing gear using deep learning;Physics of Fluids;2023-07-01

3. An Aeroacoustic Study of Full-Scale and Small-Scale Generic Landing Gear Models with Identical Geometry;Applied Sciences;2023-02-10

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