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NACA翼周りのはく離渦と空力騒音の関係


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Title: NACA翼周りのはく離渦と空力騒音の関係
Other Titles: Relationship between Separated Vortex around NACA blade and Aerodynamic Noise
Authors: 佐々木, 壮一 / 高松, 肇一 / 林, 秀千人
Authors (alternative): Sasaki, Soichi / Takamatsu, Hajime / Hayashi, Hidechito
Issue Date: Aug-2009
Publisher: 長崎大学工学部
Citation: 長崎大学工学部研究報告 Vol.39(73), pp.15-20; 2009
Abstract: To clarify the mechanism of the aerodynamic noise generated by the separated vortex around a NACA blade is aimed. The relation between the angle of attack and the aerodynamic noise of the blade are analyzed by the wind tunnel experiment and a commercial CFD code. In the case of rear surface separation, the separated vortex that has a large scale structure in the direction of the blade chord is transformed to the vortical structure that has concentrated to the trailing edge with the increase of the angle of attack. Then the aerodynamic noise level becomes small according to the vortex scale in the blade chord. The separated vortex is formed at the vicinity of the trailing edge when the flow is separated at the leading edge. The pressure fluctuation on the blade surface at the vicinity of trailing edge becomes large by the vortex in the wake. The aerodynamic noise level becomes large with the increase of the pressure fluctuation and the expansion of the correlation length by the vortex scale when the flow is separated at the leading edge.
Keywords: Aerodynamic Noise / Wake / Shear Flow / Blade / Turbulent Flow
URI: http://hdl.handle.net/10069/22135
Relational Links: http://www.lb.nagasaki-u.ac.jp/reports/kougaku/preview.php?id=82
Type: Departmental Bulletin Paper
Text Version: publisher
Appears in Collections:Volume 39, No. 73

Citable URI : http://hdl.handle.net/10069/22135

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