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Experimental on self-noise control of airfoil with ridge-like structure
更新时间：2025-05-26

    • Experimental on self-noise control of airfoil with ridge-like structure

    • “Progress has been made in the acoustic performance research of NACA0012 airfoil, and it has been found that the ridge structure can effectively reduce single tone noise, providing new ideas for aviation noise control.”
    • Journal of Jilin University(Engineering and Technology Edition)   Vol. 54, Issue 8, Pages: 2385-2392(2024)
    • 作者机构：

      1.中国空气动力学研究开发中心空气动力噪声控制重点实验室，四川 绵阳 621000

      2.吉林大学 工程仿生教育部重点实验室，长春 130022

      3.威海峻铭动力科技有限公司，山东 威海 264200

      4.吉林大学 威海仿生研究院，山东 威海 264200

    • DOI：10.13229/j.cnki.jdxbgxb.20231300    

      CLC： TB53

    • Received：24 November 2023，

      Published：01 August 2024

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  • CHENG Wen,ZHANG Cheng-chun,SUN Xiao-wei,et al.Experimental on self-noise control of airfoil with ridge-like structure[J].Journal of Jilin University(Engineering and Technology Edition),2024,54(08):2385-2392. DOI： 10.13229/j.cnki.jdxbgxb.20231300.

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Related Author

SHEN Chun
LI Zhuang
MENG Jin
SUN Xiao-wei
ZHANG Cheng-chun
CHEN Zheng-wu
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Related Institution

College of Automotive Engineering， Jilin University
Key Laboratory of Engineering Bionics，Ministry of Education，Jilin University
Aero-Engine Academy of China，Aero-Engine Corporation of China
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