Vane Stagger Angle and Camber Effects in Fan Noise Generation

Author:

Schulten Johan B.H.M.1

Affiliation:

1. National Aerospace Laboratory NLR, Amsterdam, the Netherlands

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 11 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. Effect of Stator Stagger Angle on Rotor-stator Interaction Noise;AIAA AVIATION 2023 Forum;2023-06-08

2. Three-dimensional effects of cascade perforations on rotor–stator interaction noise;Journal of Fluid Mechanics;2022-11-18

3. Linearized unsteady aerodynamics for aeroacoustic applications;Fundamentals of Aeroacoustics with Applications to Aeropropulsion Systems;2021

4. Noise prediction in aeroengine;Fundamentals of Aeroacoustics with Applications to Aeropropulsion Systems;2021

5. Wave response functions for a cascade of blades with an arbitrary camber;25th AIAA/CEAS Aeroacoustics Conference;2019-05-18

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