| 前体非对称涡高风速烟雾显示技术 |
| |
| 引用本文： | 柏楠,邓学蓥,王延奎.前体非对称涡高风速烟雾显示技术[J].力学学报,2007,39(2):261-266. |
| |
| 作者姓名： | 柏楠 邓学蓥 王延奎 |
| |
| 作者单位： | 北京航空航天大学流体力学重点实验室 北京航空航天大学流体所，100083 北京航空航天大学流体所，100083 |
| |
| 基金项目： | 国家自然科学基金，航空基础科学基金 |
| |
| 摘 要： | 通过在细长旋成体模型机身的不同位置设置出烟孔，使用新型发烟装置对模型注入雾化油
滴，采用激光片光法在常规风洞中高风速(60m/s)条件下得到清晰、完整而稳定的截面涡
结构图像. 并通过同状态标定法和等比例网格法发展了简易涡位定量测量技术，为前体非对
称涡Re数效应的研究提供了重要的技术平台.
|
| 关 键 词： | 高风速流场显示 定量测量 Re数效应 前体非对称涡 大迎角 |
| 文章编号： | 0459-1879（2007）02-0261-06 |
| 收稿时间： | 2006-06-14 |
| 修稿时间： | 2006-11-20 |
SMOG VISUALIZATION TECHNIQUE OF ASYMMETRIC VORTICES ON FOREBODY AT HIGH WIND SPEED |
| |
| Bo Nan,Deng Xueying,Wang Yankui.SMOG VISUALIZATION TECHNIQUE OF ASYMMETRIC VORTICES ON FOREBODY AT HIGH WIND SPEED[J].chinese journal of theoretical and applied mechanics,2007,39(2):261-266. |
| |
| Authors: | Bo Nan Deng Xueying Wang Yankui |
| |
| Affiliation: | Key Laboratory of Fluid Mechanics of Ministry of Education, Beijing University of Aeronautics and Astronautics, Beijing 100083, China |
| |
| Abstract: | We have obtained a clear, integrated and steady image of vortices at high wind speed (60 m/s) in the routine wind tunnel by setting a smoke orifice on the surface of the slender cylinder body and infusing the atomized oil with the new type of liquid droplet seeding generator. A simple technique is developed to measure the vortice position by calibrating at the same state and drawing grids in the same scale. It provides a useful technical platform for the research of Reynolds number effect on asymmetric vortices at a forebody. |
| |
| Keywords: | flow visualization at high wind speed quantitative measurment effect of Reynolds number asymmetric vortices high angle of attack |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
| 点击此处可从《力学学报》浏览原始摘要信息 |
|
点击此处可从《力学学报》下载全文 |
