Effect of Coating Thickness on Aerodynamic Noise Reduction by Porous-Coated Cylinders
Author:
Affiliation:
1. Brandenburgische Technische Universitat Cottbus-Senftenberg
2. Southern University of Science and Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-2889
Reference32 articles.
1. Measurement of the noise generation at the trailing edge of porous airfoils
2. Numerical modelling and passive flow control using porous media
3. Steady flow around and through a permeable circular cylinder
4. Reduction in drag and vortex shedding frequency through porous sheath around a circular cylinder
Cited by 2 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. Structured Porous Coated Cylinder Modifications Based on Internal Flow Field Data;AIAA AVIATION 2023 Forum;2023-06-08
2. On the influence of porous coating thickness and permeability on passive flow and noise control of cylinders;Journal of Sound and Vibration;2023-04
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