空气动力学学报2012，Vol.30Issue(3)：388-393,6.
二维增升装置前缘缝翼的远场噪声分析
Far-field aeroacoustic analysis for slat of a two-dimensional high-lift configuration
刘志仁 1王福新 1宋文滨 1李亚林2
作者信息
- 1. 上海交通大学航空航天学院,上海200240
- 2. 中国商用飞机有限责任公司上海飞机设计研究院,上海200235
- 折叠
摘要
Abstract
The far-field noise of two dimensional multi-element high lift device L1T2 slat model was calculated using commercial CFD software FLUENT. LES model was used in flow field analysis to provide noise source data, while the FW-H method was used to calculate the far-field noise levels. To study the effects of gap and overlap on both maximum lift coefficient and noise levels, a total of 24 different combinations of gap and overlap were analyzed, and two response surface models were built from the results. The response surface models indicate that it is possible to find reasonable combinations of gap and overlap to achieve a balance between aerodynamic performance and noise characteristics.关键词
增升装置/缝翼/缝道参数/气动噪声Key words
high lift device/ slat/ gap and overlap/ aeroacoustics分类
航空航天引用本文复制引用
刘志仁,王福新,宋文滨,李亚林..二维增升装置前缘缝翼的远场噪声分析[J].空气动力学学报,2012,30(3):388-393,6.
