| 立式风洞与立式风洞试验 |
| |
| 引用本文： | 颜,巍.立式风洞与立式风洞试验[J].民用飞机设计与研究,2016(3):52. |
| |
| 作者姓名： | 颜 巍 |
| |
| 作者单位： | 上海飞机设计研究院，上海 201210 |
| |
| 摘 要： | 尾旋是飞机的一种非正常的复杂旋转飞行状态，飞机尾旋研究在航空工程中属于比较冷门的专业。立式风洞是专门进行飞机尾旋研究等特种试验的风洞设施，这种风洞在飞机研发过程中与常规风洞相比使用率较低。对立式风洞和立式风洞试验进行简要的回顾和阐述，为相关飞机型号设计单位进行立式风洞试验、研究飞机尾旋特性与改出特性提供参考。
|
| 关 键 词： | 立式风洞 自由尾旋 旋转天平 |
Vertical Wind Tunnel and Vertical Wind Tunnel Experiments |
| |
| YAN Wei.Vertical Wind Tunnel and Vertical Wind Tunnel Experiments[J].Civil Aircraft Design and Research,2016(3):52. |
| |
| Authors: | YAN Wei |
| |
| Abstract: | Aircraft spin is a very complex rotational flight state, aircraft spin research is relatively less focused. Vertical wind tunnel is the specific wind tunnel facility for aircraft spin research, this kind of wind tunnel is less been used compare with normal wind tunnel. This paper presents the review and discussion of vertical wind tunnel and vertical wind tunnel experiments. |
| |
| Keywords: | vertical wind tunnel free spin rotary balance |
|
| 点击此处可从《民用飞机设计与研究》浏览原始摘要信息 |
| 点击此处可从《民用飞机设计与研究》下载免费的PDF全文 |
