Experimental investigation into the acoustical superiority of ogee serrations in reducing leading edge noise
Author:
Funder
Laoshan Laboratory
National Natural Science Foundation of China
Qingdao National Laboratory for Marine Science and Technology
Publisher
Elsevier BV
Subject
Acoustics and Ultrasonics
Reference49 articles.
1. Predicting and reducing aircraft noise;Astley,2007
2. ACAT1 benchmark of RANS-informed analytical methods for fan broadband noise prediction: part II - influence of the acoustic models;Guérin;Acoustics,2020
3. ACAT1 benchmark of RANS-informed analytical methods for fan broadband noise prediction: part I - influence of the RANS simulation;Kissner;Acoustics,2020
4. Some aspects of non-stationary airfoil theory and its practical application;Sears;J Aeronaut Sci,1941
5. Similarity rules for thin aerofoils in non-stationary subsonic flows;Graham;J Fluid Mech,1970
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