| 用热膜法测跨音速机翼抖振边界 |
| |
| 引用本文： | 汪乔森,邱学军,张召明.用热膜法测跨音速机翼抖振边界[J].航空学报,1988,9(8):346-351. |
| |
| 作者姓名： | 汪乔森 邱学军 张召明 |
| |
| 作者单位： | 南京航空学院
(汪乔森，邱学军)，南京航空学院(张召明) |
| |
| 摘 要： | 本文给出了一种测试机翼抖振的新方法——热膜法,并描述了热膜法测量机翼抖振的原理及技术。实验结果与有关资料相比有较好的一致性。这表明热膜法是机翼抖振测量的好方法。
|
| 关 键 词： | |
| 收稿时间： | 1987-07-22; |
MEASURMENTS OF THE BUFFET BOUNDARY OF WINGS IN TRANSONIC FLOW WITH HOT-FILM METHOD |
| |
| Wang Qiaosen,Qiu Xuejun and Zhang Zhaoming.MEASURMENTS OF THE BUFFET BOUNDARY OF WINGS IN TRANSONIC FLOW WITH HOT-FILM METHOD[J].Acta Aeronautica et Astronautica Sinica,1988,9(8):346-351. |
| |
| Authors: | Wang Qiaosen Qiu Xuejun and Zhang Zhaoming |
| |
| Institution: | Nanjing Aeronautical Institute |
| |
| Abstract: | This paper presents a new method--hot film method (HFM) formeasuring the buffeting onset of wings, and describes the principle and technique for using HFM to measure wing buffeting onset. The experimental results are quite consistent with the available data. The present work indicates that the HFM can be used for measuring the buffeting onset of wings. |
| |
| Keywords: | transonic characteristics hot film anemometors buffet tests |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《航空学报》浏览原始摘要信息 |
| 点击此处可从《航空学报》下载免费的PDF全文 |
