IIUM Repository

Discrete tonal noise of NACA0015 airfoil at low reynolds number

Andan, Amelda Dianne and Lee, Duck-Joo (2019) Discrete tonal noise of NACA0015 airfoil at low reynolds number. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 53 (1). pp. 129-145. ISSN 2289-7879

[img] PDF - Published Version
Restricted to Registered users only

Download (1MB) | Request a copy
Download (304kB) | Preview


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 low-to-moderate Reynolds numbers. The characteristics and behavior of tonal emissions at low Reynolds number differs from that at higher Reynolds number. Therefore, the purpose of this work is to study the discrete tonal noise generated by laminar boundary layer instability at low Reynolds number as well as at a variation of angle of attack. Experimental testing on NACA0015 was done in the anechoic wind tunnel to measure the sound spectrum at Reynolds number of Re~104 and angle of attack of 0°≤α≤5°. This work is intended to provide additional information to the tonal behavior of NACA series airfoil. Flow separation without reattachment occurs on the suction side within the selected Reynolds number and angle of attack. No tonal sound was found if fs falls below 40dB. At low Reynolds number, airfoil discrete tone consists of high intensity fs accompanied by more pronounced fn as freestream velocity increases. Airfoil tonal noise gradually decreases as angle of attack increases from α=0^° before disappearing beyond α=5°. Moreover, previously proposed empirical models to predict fs were found to have limitation in predicting tonal frequency at low Reynolds number at a variation of angle of attack. In addition, general observation shows fn has a velocity dependency of ~U0.8 while f_s is prone to exhibit ladder structure behavior with velocity dependency of ~U1.3.

Item Type: Article (Journal)
Additional Information: 8376/69941
Uncontrolled Keywords: Discrete tonal noise, flow Instabilities, anechoic wind tunnel
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > TL500 Aeronautics
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button): Kulliyyah of Engineering
Kulliyyah of Engineering > Department of Mechanical Engineering
Depositing User: Dr. Amelda Dianne Andan
Date Deposited: 28 Jan 2019 11:19
Last Modified: 09 Jul 2019 16:35
URI: http://irep.iium.edu.my/id/eprint/69941

Actions (login required)

View Item View Item


Downloads per month over past year