Rapid prediction method for airfoil trailing edge scattering noise in both water and air based on pulse pressure wavenumber-frequency spectrum

被引：0
|
作者：
Yu, Rongke [1 ,2 ]
Zhao, Kun [1 ]
Feng, Heying [2 ]
Zhang, Rongping [1 ]
Li, Yimeng [1 ,2 ]
机构：
[1] State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang,621000, China
[2] Hunan Provincial Key Laboratory of Health Maintenance for Mechanical Equipment, Hunan University of Science and Technology, Xiangtan,411201, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2024年 / 45卷 / 23期
关键词：
Compendex;
D O I：
10.7527/S1000-6893.2024.30295
中图分类号：
学科分类号：
摘要：
Gas turbines
引用
收藏
相关论文
共 5 条
  • [1] Trailing edge noise prediction based on wall pressure spectrum models for NACA0012 airfoil
    Kucukosman, Yakut Cansev
    Christophe, Julien
    Schram, Christophe
    JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2018, 175 : 305 - 316
  • [2] Prediction of airfoil trailing-edge noise using empirical wall-pressure spectrum models
    Lee, Seongkyu
    Shum, Jessica G.
    AIAA Journal, 2019, 57 (03): : 888 - 897
  • [3] Prediction of Airfoil Trailing-Edge Noise Using Empirical Wall-Pressure Spectrum Models
    Lee, Seongkyu
    Shum, Jessica G.
    AIAA JOURNAL, 2019, 57 (03) : 888 - 897
  • [4] A semi-empirical surface pressure spectrum model for airfoil trailing-edge noise prediction
    Kamruzzaman, M.
    Bekiropoulos, D.
    Lutz, Th.
    Wuerz, W.
    Kraemer, E.
    INTERNATIONAL JOURNAL OF AEROACOUSTICS, 2015, 14 (5-6) : 833 - 882
  • [5] Airfoil trailing⁃edge noise prediction based on CFD / CAA coupled boundary method
    Lu R.
    Ding Y.
    Yu P.
    Tan K.
    Pan G.
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2023, 41 (02): : 319 - 328
1