Transonic Hovering Rotor Aeroacoustic Predictions Using Naier-Stokes/Kirchhoff Method

被引：0
|
作者：
Qi Hui [1 ]
Qu Guang-zu
Gong Bin [1 ]
机构：
[1] Shenyang Inst Chem Technol, Shenyang 110142, Peoples R China
来源：
PROCEEDINGS OF 2ND INTERNATIONAL SYMPOSIUM ON PHYSICS AND HIGH-TECH INDUSTRY, 4TH INTERNATIONAL SYMPOSIUM ON MAGNETIC INDUSTRY, 1ST SHENYANG FORUM FOR DEVELOPMENT AND COOPERATION OF HIGH-TECH INDUSTRY IN NORTHEAST ASIA | 2009年
关键词：
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
This paper focused on studying the influence of choosing Kirchhoff surface including top and bottom or not and considering the flow solution of rotor mesh or not on the result of noise prediction. As a demonstration of the overall prediction scheme, only using the integration surface with top and bottom and considering simultaneously the flow solution of rotor mesh, the computed result of far-field noise for high-speed impulsive case showed the best agreement with experimental data.
引用
收藏
页码：419 / 421
页数：3
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