Please use this identifier to cite or link to this item: https://doi.org/10.1142/S0217984910023608
Title: Enhancement on propulsion performance: Modifying angle of attack profile
Authors: Xiao, Q.
Liao, W.
Dou, H.-S. 
Keywords: Effective angle of attack
Oscillating foil
Pitching motion
Propulsion performance
Issue Date: 30-May-2010
Source: Xiao, Q., Liao, W., Dou, H.-S. (2010-05-30). Enhancement on propulsion performance: Modifying angle of attack profile. Modern Physics Letters B 24 (13) : 1353-1356. ScholarBank@NUS Repository. https://doi.org/10.1142/S0217984910023608
Abstract: In this paper, numerical investigation was conducted for an oscillating NACA0012 foil combining the pitching and plunging motions. The plunging follows a sinusoidal motion while the pitching trajectory is controlled by achieving the resultant effective angle of attack (AOA) to be a harmonic cosine form. Computations were conducted over a range of the Strouhal number (St), different maximum effective AOA and different phase difference between pitching and plunging (ψ). Results show that, at higher St, significant improvement on propulsion performance has been achieved when the effective AOA profile maintains a harmonic cosine form by controlling the pitching motion of the foil. © 2010 World Scientific Publishing Company.
Source Title: Modern Physics Letters B
URI: http://scholarbank.nus.edu.sg/handle/10635/115416
ISSN: 02179849
DOI: 10.1142/S0217984910023608
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