Numerical Study on the Duct Noise Control of Single-Stage Axial Flow Fan with Wave Leading Edge Stator Blade Configurations

Author:

Lian Jianxin,Tong Hang,Zhang Liangji,Qiao Weiyang,Chen Weijie

Publisher

Scientific Research Publishing, Inc.

Subject

General Earth and Planetary Sciences

Reference19 articles.

1. Aeroacoustics research in Europe: The CEAS-ASC report on 2017 highlights

2. Owen, R. (1979) Energy Efficient Engine: Propulsion System—Aircraft Integration Evaluation. NASA/CR 159488.

3. Hughes, C. (2013) NASA Collaborative Research on the Ultra High Bypass Engine Cycle and Potential Benefits for Noise, Performance, and Emissions. NASA Technical Memorandum TM-2013-216345.

4. Wang, L.F. (2017) Experiment and Numerical Study on Duct Mode Identification of Fan Noise (Xi’an). Ph.D. Thesis, Northwestern Polytechnical University, Xi’an.

5. Tong, H., Li, L., Mao, L.Q., et al. (2020) Tonal Noise Reduction of a High-Speed Single Axial Fan with Wavy Leading-Edge Stator. Acta Aeronautica et Astronautica Sinica, 41, 123565. 10.7527/S1000-6893.2019.23565

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