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投稿时间：2012-07-09
投稿时间：2012-07-09
中文摘要: 设计了一座试验段当量直径为1.5m, 试验段长度为2.0m, 最高实验风速为50m/s的低速开口回流风洞.采用三维建模软件和计算流体力学软件, 对风洞的流场品质进行数值计算.气动设计过程表明, 收缩比、收缩曲线线形、蜂窝器、紊流网对流场品质有较大的影响.
Abstract:A test section of the equivalent diameter of 1.5m test section length of 2.0m, the highest experimental wind speed of 50m/s low-speed open return wind tunnel is designed.By using 3D modeling and computational fluid dynamics software, flow field quality is calculated by the numerical calculation.Aerodynamic design shows contraction ratio, contraction curve linear, cellular device, turbulent mesh has a greater impact on flow field qualities
文章编号：20130212 中图分类号： 文献标志码：
基金项目:国家自然科学基金项目(50706025);上海市教育委员会科研创新重点项目(11ZZ171, 11ZZ172)
| 作者 | 单位 | |
| 胡丹梅 | hudanmei@shiep.edu.cn． | |
| 张志超 | ||
| 孙凯 | ||
| 张建平 |
| Author Name | Affiliation | |
| HU Dan-mei | hudanmei@shiep.edu.cn． | |
| ZHANG Zhi-chao | ||
| SUN Kai | ||
| ZHANG Jian-ping |
引用文本：
胡丹梅,张志超,孙凯,等.低速开口回流风洞的气动设计及数值计算[J].上海电力大学学报,2013,29(2):146-150.
HU Dan-mei,ZHANG Zhi-chao,SUN Kai,et al.Low-Speed Open Return Wind Tunnel Aerodynamic Design and Numerical Calculation[J].Journal of Shanghai University of Electric Power,2013,29(2):146-150.
胡丹梅,张志超,孙凯,等.低速开口回流风洞的气动设计及数值计算[J].上海电力大学学报,2013,29(2):146-150.
HU Dan-mei,ZHANG Zhi-chao,SUN Kai,et al.Low-Speed Open Return Wind Tunnel Aerodynamic Design and Numerical Calculation[J].Journal of Shanghai University of Electric Power,2013,29(2):146-150.