Numerical analysis on the high-speed impulsive noise propagation characteristic of helicopter rotor in the presence of strong shear flow

Author:

Yang Tao,Chen Xi,Zhao Qijun,Ding Yan

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference57 articles.

1. Rotor noise measurement using a directional microphone array;Marcolini;J Am Helicopter Soc,1992

2. Low-frequency fluctuations and their suppression in the 5.5m×4m aeroacoustic wind tunnel at CARDC;Zhang;Appl Acoust,2021

3. Aeroacoustic design and characterization of the 3D-printed, open-jet, anechoic wind tunnel of Delft University of Technology;Merino-Martínez;Appl Acoust,2020

4. A study of shear-layer corrections and a tensioned fabric wall for the localization of sound sources in wind tunnel;Zhang;25th AIAA/CEAS Aeroacoustics Conference,2019

5. Investigation of the acoustic installation effects of an open-jet anechoic wind tunnel using computational aeroacoustics;Redonnet;Appl Acoust,2020

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