Non-Synchronous Measurements for Sound Source Localisation of a High-Lift Common Research Model in the Wind Tunnel Test-Reference-Cited by-同舟云学术

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Non-Synchronous Measurements for Sound Source Localisation of a High-Lift Common Research Model in the Wind Tunnel Test

Published:2023-09-23 Issue: Volume:40 Page:968-972
ISSN:
Container-title:2023 6th International Conference on Information Communication and Signal Processing (ICICSP)
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Author:

Jing Qiulan¹,Bao Anyu²,Yu Liang³,Xiao Youhong¹,Wang Ran⁴,Zhou Guocheng²,Chen Bao²

Affiliation:

1. College of Power and Energy Engineering, Harbin Engineering University,Harbin,China

2. Aerodynamics Research Institute,Aviation Industry Corporation of China,Harbin,China

3. School of Civil Aviation, Northwestern Polytechnical University,Xi'an,China

4. College of Logistics Engineering, Shanghai Maritime University,Shanghai,China

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10389815/10388491/10390756.pdf?arnumber=10390756

Reference15 articles.

1. Almost 40 Years of Airframe Noise Research: What Did We Achieve?

2. Airframe Noise Component Interaction Studies

3. Noise characteristic of the nacelle/pylon/slat juncture in a realistic high-lift aircraft configuration

4. Identification of the two-sources at the aircraft slat/fuselage juncture based on phased array

5. On the Alleviation of Background Noise for the High-Lift Common Research Model Aeroacoustic Test

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