DSpace university logo mark
Advanced Search
Japanese | English 

NAOSITE : Nagasaki University's Academic Output SITE > Faculty of Engineering > Bulletin > Reports of the Faculty of Engineering, Nagasaki University > Volume 29, No. 52 >


File Description SizeFormat
KJ00000136416.pdf684.89 kBAdobe PDFView/Open

Title: 離散渦法による単独翼から発生する空力騒音の予測
Other Titles: Prediction of Aerodynamic Noise Generated from Individual Blade by Discrete Vortex Method
Authors: 佐々木, 壮一 / 林, 秀千人 / 児玉, 好雄
Authors (alternative): Sasaki, Soichi / Hayashi, Hidechito / Kodama, Yoshio
Issue Date: Jan-1999
Citation: 長崎大学工学部研究報告 Vol.29(52) p.33-41, 1999
Abstract: The discrete frequency noise (DFN) which is a kind of aerodynamic noise is closely connected with Karman vortices that forms at the trailing edge into the wake. In this paper, we proposed a convenient method to predict of DFN that based not on the experiments but on the simple flow calculation, that is, discrete vortex method. From this method, the wake characteristics and the fluctuations of circulation around the body could be calculated in good agreement with experiments. The source distribution of DFN is almost gathered to the trailing edge, and at the thick blade it is extended to direction of the leading edge. The prediction of the DFN using the calculated and suggested quantities makes about ±3dB accuracy.
Keywords: Karman Vortex / Aerodynamic Acoustic / Wake / Numerical Analysis / Blade
URI: http://hdl.handle.net/10069/5051
ISSN: 02860902
Type: Departmental Bulletin Paper
Appears in Collections:Volume 29, No. 52

Citable URI : http://hdl.handle.net/10069/5051

All items in NAOSITE are protected by copyright, with all rights reserved.


Valid XHTML 1.0! Copyright © 2006-2015 Nagasaki University Library - Feedback Powerd by DSpace