Vortex Shedding and Tonal Noise from a Sharp Bevelled Trailing Edge-Reference-Cited by-同舟云学术

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Vortex Shedding and Tonal Noise from a Sharp Bevelled Trailing Edge

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Doolan Con¹,Tetlow Matthew¹,Moreau Danielle¹,Brooks Laura¹

Affiliation:

1. University of Adelaide

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-68

Reference11 articles.

1. Vortex Noise of Isolated Airfoils

2. Discrete tones of isolated airfoils

3. Noise generated by airfoil profiles placed in a uniform laminar flow

4. Laminar boundary layer instability noise produced by an aerofoil

5. Boundary-layer instability noise on aerofoils

Cited by 3 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. On the acoustic emission characteristics of airfoils with different trailing edge configurations;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-11-30

2. On the effect of velvet structures on trailing edge noise: experimental investigation and theoretical analysis;Journal of Fluid Mechanics;2021-05-25

3. The effect of boundary layer type on trailing edge noise from sharp-edged flat plates at low-to-moderate Reynolds number;Journal of Sound and Vibration;2012-08

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