A parametric study of parallel blade-vortex-interaction noise

被引：0

作者：

Tanabe, Yasutada ^{[1
]}

Saito, Shigeru ^{[1
]}

Takasaki, Keisuke ^{[2
]}

Fujita, Hajime ^{[2
]}

机构：

[1] Japan Aerosp Explorat Agcy JAXA, Tokyo, Japan

[2] Nihon Univ, Chiyoda Ku, Tokyo, Japan

来源：

NOISE CONTROL ENGINEERING JOURNAL | 2009年 / 57卷 / 05期

关键词：

10;

D O I：

10.3397/1.3197849

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

A parametric study of parallel Blade-Vortex-Interaction (BVI) has been carried out using numerical simulations. A high-resolution CFD scheme and a fine grid system are employed to capture the vortex. Along with the convection of vortex, a low dissipation of the initial vortex is observed. By locating the initial vortex far upstream of the airfoil, a parallel BVI is simulated while the vortex is convected by the flow passing through the vicinity of the blade. The results are compared with the existing experimental data with good agreement. The blade tip-to-vortex distance, airfoil incidence, and vortex rotation direction are chosen as the parameters for this parametric study. The BVI strength shows a dependency on these parameters. (C) 2009 Institute of Noise Control Engineering.

引用

页码：420 / 433

页数：14

共 10 条

[1] FALISSARD F, 2006, 4 INT C CFD ICCFD
[2] Jameson A., 1983, AIAA Paper No. 83-1929
[3] KITAPLIOGLU C, 1997, J AM HELICOPTER SOC, P272
[4] Kitaplioglu C, 1999, NASATM1999208790
[5] LEE S, 1991, 9 APPL AER C
[6] OCHI A, 1999, 55 AM HEL SOC ANN FO
[7] SHIMA E, 1999, NAL, P7
[8] AERODYNAMICS OF TWO-DIMENSIONAL BLADE-VORTEX INTERACTION
SRINIVASAN, GR
MCCROSKEY, WJ
BAEDER, JD
[J]. AIAA JOURNAL, 1986, 24 (10) : 1569 - 1576
[9] TANABE Y, 2007, 111474DSNA ONERA
[10] IMPLICIT TVD SCHEMES FOR HYPERBOLIC CONSERVATION-LAWS IN CURVILINEAR COORDINATES
YEE, HC
HARTEN, A
[J]. AIAA JOURNAL, 1987, 25 (02) : 266 - 274

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