Discrete tonal noise of NACA0015 airfoil at low reynolds
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Discrete tonal noise of NACA0015 airfoil at low reynolds number

This paper is a pilot study of the effect of external forcing and passive control on the generation of airfoil whistle noise. Interaction between instability travelling inside laminar boundary layer with the airfoil trailing edge produces discrete tonal noise. This phenomenon commonly found at lo...

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Bibliographic Details
Main Authors:	Andan, Amelda Dianne, Lee, Duck-Joo
Format:	Article
Language:	English English
Published:	Penerbit Akademia Baru 2019
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/69941/ http://irep.iium.edu.my/69941/1/69941_Discrete%20Tonal%20Noise%20of%20NACA0015.pdf http://irep.iium.edu.my/69941/7/69941_Discrete%20tonal%20noise_scopus.pdf

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