Structured porous blunt trailing edge with uniform and non-uniform parameters for vortex shedding noise reduction

Author:

Liu Hanru,Hu Zhijie,Chen Nanshu,Liu Yu,Fan Hengwei

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference46 articles.

1. Khorrami, M. R., Konig, B., Fares, E., Ribeiro, A., Czech, M., & Ravetta, P. A., “Airframe Noise Simulations of a Full-Scale Large Civil Transport in Landing Configuration,” In AIAA Aviation 2021 Forum (p. 2161) (2021).

2. Component-based model to predict aerodynamic noise from high-speed train pantographs;Iglesias;J Sound Vib,2017

3. Aeroacoustic design and broadband noise predictions of a fan stage with serrated outlet guide vanes;Polacsek;Phys Fluids,2020

4. Flow Control, Passive, Active, and Reactive Flow;Gad-el-Hak,2000

5. Taylor, H. D., “The elimination of diffuser separation by vortex generators,” United Aircraft Corporation Report No. R-4012-3, East Hartford, Connecticut 103 (1947).

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