首页 | 本学科首页   官方微博 | 高级检索  
     

大迎角细长体头涡结构演变的非定常现象研究
引用本文:马宇,刘沛清,邓学蓥,史京玲. 大迎角细长体头涡结构演变的非定常现象研究[J]. 实验流体力学, 2004, 18(4): 72-77
作者姓名:马宇  刘沛清  邓学蓥  史京玲
作者单位:北京航空航天大学流体力学研究所,北京,100083;北京航空航天大学流体力学研究所,北京,100083;北京航空航天大学流体力学研究所,北京,100083;北京航空航天大学流体力学研究所,北京,100083
基金项目:国家自然科学基金(10172017),航空基础科学基金(02A51048),翼型叶栅空气动力学国防科技重点实验室基金(00JS51.3.2HK01)
摘    要:细长旋成体绕流中位于尖部附近的一对头涡在迎角增至一定程度时,会表现出很强的非定常特征,而此时后体上为类卡门涡脱落区域。为了寻找这对头涡的非定常特征随迎角变化的规律,在两个风洞中分别用两个细长体模型进行测压和流动显示实验,得到了在很大迎角下旋成体头涡的脉动频率随迎角基本呈线性变化的规律,而后体上的卡门涡脱落频率则与迎角的正弦值成正比。

关 键 词:头涡  卡门涡脱落  压力脉动
文章编号:1007-3124(2004)04-0072-06
修稿时间:2004-01-19

The unsteadiness study of nose vortices in the flow over slender body at high angles of attack
MA Yu,LIU Pei-qing,DENG Xue-ying,SHI Jing-ling. The unsteadiness study of nose vortices in the flow over slender body at high angles of attack[J]. Experiments and Measur in Fluid Mechanics, 2004, 18(4): 72-77
Authors:MA Yu  LIU Pei-qing  DENG Xue-ying  SHI Jing-ling
Abstract:There is a strong unsteady characteristic aroused by the two vortices near the apex of cylinder when the angle of attack of it comes to a certain degree, while the Karman vortex street region is formed on the afterbody. In this paper, the pressure fluctuation characteristics of the two modes and the laws of the characteristics changed with the angle of attack increasing were proved in two different wind tunnels with two machined slender body models. In the nose vortices region, the relationship between the pressure fluctuation frequency and the cylinder attack is linear, and the frequency of the Karman vortex shedding is in proportion to the sine of the attack angle.
Keywords:nose vortex  Karman vortex shedding  pressure fluctuation characteristic
本文献已被 CNKI 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号