全升力飞行器流场诱导流动现象改善效果

王林林; 高歌

全升力飞行器流场诱导流动现象改善效果

王林林¹,
高歌²

1.
广州民航职业技术学院飞机维修工程学院, 广州 510000
2. 北京航空航天大学航空发动机气动热力重点实验室, 北京 100191

详细信息

作者简介:
王林林(1982-),男,河南登封人,讲师, junjifeng@live.com.

中图分类号: V211.7
计量
- 文章访问数: 1249
- HTML全文浏览量: 79
- PDF下载量: 616
- 被引次数: 0
出版历程
- 收稿日期: 2013-04-09
- 网络出版日期: 2013-10-30

All-lifting-vehicle induced flow improvement effect

Wang Linlin¹,
Gao Ge²

1.
Aircraft Maintenance Engineering School, Guangzhou Civil Aviation College, Guangzhou 510000, China
2. National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 碟形飞行器是一种小展弦比全升力飞行器,采用一种仿生的鱼鳍型小翼对绕碟形飞行器的诱导流动现象进行改善,削弱翼尖诱导旋涡,提高整机气动效率.应用高精度风洞试验和以该风洞试验数据为校验的数值模拟,对鱼鳍型小翼的作用进行了研究,从风洞试验和数值模拟两方面给出了评判.研究结果表明:鱼鳍型小翼对碟形飞行器的诱导流动现象有较大的改善效果.
- 全升力飞行器 /
- 诱导流动 /
- 升力体 /
- 混合翼
Abstract: The saucer-shaped aircraft is a kind of all-lifting-vehicle with low aspect ratio. Bionic fin-shaped wing tips were used to improve the induced flow over the saucer-shaped aircraft and impair the induced flow separation, and then the aircraft aerodynamic efficiency could be increased. The high precision wind tunnel tests were conducted to investigate the induced flow improvement effect of the saucer-shaped lifting body, with the adopting of the fin-shaped wing tips. Numerical simulations basic on the high precision wind tunnel tests were also used. The results show that the fin-shaped wing tips could highly improve the induced flow over the saucer-shaped aircraft.
- all-lifting-vehicle /
- induced flow /
- lifting body /
- blended wing body

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参考文献(1)

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