细长体截面绕流的稳定性及扰动的影响

李国辉; 邓学蓥

细长体截面绕流的稳定性及扰动的影响

北京航空航天大学飞行器设计与应用力学系,北京 100083

基金项目: 国家自然科学基金资助项目(10172017);航空基础科学基金资助项目(02A51048)

详细信息

作者简介:
李国辉(1966- ),男,湖南永兴人,副教授,博士生(联系人.Tel:+86-10-82317524;E-mail:ghleebh0368@sina.com.cn).

中图分类号: V211.1
计量
- 文章访问数: 2502
- HTML全文浏览量: 121
- PDF下载量: 892
- 被引次数: 0
出版历程
- 收稿日期: 2002-06-18
- 修回日期: 2004-09-10
- 刊出日期: 2004-12-15

Stability of the Crossflow Pattern Around a Slender and Influence of Disturbance

Deptartment of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, P. R. China

摘要

摘要: 应用拓扑结构的稳定性理论，分析了细长旋成体截面绕流的结构稳定性．在分析时取极限流线作为流场的内边界，并证明极限流线的鞍点-鞍点连接是拓扑结构稳定的A·D2通过分析发现，由于旋成体背涡的发展，导致截面流场拓扑结构变化，由稳定对称旋涡流态变成不稳定对称旋涡流态．此时流场中存在空间的鞍点-鞍点连接的不稳定拓扑结构，在小扰动下出现分叉，变成稳定非对称旋涡流态，形成非对称背涡．并应用开折理论分析了扰动对流场结构的影响．
- 细长体 /
- 拓扑 /
- 结构稳定性 /
- 分叉 /
- 开折
Abstract: Topological structure and stability of a slender cross flow is discussed by the stability theory of dynamic system.The inner boundary of flow field was limiting streamline and it was proved that the topological structure connected saddles by limiting streamline is stable.It is proved that the development of slender vortices leads to the change of topological structure about cross flow.And it is the change from stable and symmetrical vortices flow pattern to unstable and symmetrical vortices flow pattern,and then to stable and asymmetrical vortices flow pattern due to little disturbance which leads to the development of asymmetrical slender vortices.The influence of disturbance to flowfield structure was discussed by unfolding theory too.
- slender /
- topology /
- structure stability /
- bifurcation /
- unfolding

HTML全文

参考文献(14)

[1]	Keener E R,Chapman G T.Similarity in vortex asymmetric over slender bodies and wings[J].AIAA J,1977,12(15):1370—1372.
[2]	Ericsson L E.Sources of high alpha vortex asymmetry at zero sideslip[J].Journal of Aircraft,1992,29(6):1086—1090. doi: 10.2514/3.56864
[3]	Peake D J，Tobak M.Three dimensional interactions and vortical flow with emphasis on high speeds[R]. AGARD-AG-252,1980.
[4]	Nishioka M,Sato H.Mechanism of determination of the shedding frequency of vortices behind a cylinder at low Reynolds numbers[J].Journal of Fluid Mechanics,1978,89(1):49—60. doi: 10.1017/S0022112078002451
[5]	李国辉，邓学蓥.细长体截面流态拓扑结构演化及其稳定性分析[J].北京航空航天大学学报，2001，27(6)：674—676.
[6]	Maskell E C.Flow separation in three dimensions[R]. RAE Aero Rept,2565,1955.
[7]	陆启韶.常微分方程的定性方法和分叉[M].北京：北京航空航天大学出版社，1989.
[8]	Lowson M V，Ponton A J.Symmetry breaking in vortex flows on conical bodies[J].AIAA J,1992,30(6)：1341—1352.
[9]	Werlé H.La Tunnel hg drodgnanique au service de la recherche aerospatiale[R]. ONERA Publication, No 156，1974.
[10]	CHEN Xue-rui,DENG Xue-ying,WANG Yan-kui,et al.Influence of nose perturbations on behaviors of asymmetric vortices over slender body[J].Acta Mechanica Sinica,2002，18（6）：581—593. doi: 10.1007/BF02487960
[11]	Luo S C,Lim T T,Lua K B,et al.Flowfield around ogive/elliptic-tip cylinder at high angle of attack[J].AIAA J,1998,36(10)：1778—1787. doi: 10.2514/2.286
[12]	Bernhardt J E，Williams D R.Proportional control of asymmetric forebody vortices[J].AIAA J，1998,36(11)：2087—2093. doi: 10.2514/2.310
[13]	Bridges D H,Homung H G.Elliptic tip effects on the vortex wake of an axisymmetric body at incidence[J].AIAA J,1994,32(7)：1437—1445. doi: 10.2514/3.12213
[14]	Wardlow A B Jr,Yanta W J.Asymmetric flowfield development on a slender body at high incidence[J].AIAA J,1984,22(2)：233—245.

施引文献

资源附件(0)

访问统计

计量

文章访问数: 2502
HTML全文浏览量: 121
PDF下载量: 892
被引次数: 0

姓名
邮箱
手机号码
标题
留言内容
验证码

留言板

细长体截面绕流的稳定性及扰动的影响

作者简介:
李国辉(1966- ),男,湖南永兴人,副教授,博士生(联系人.Tel:+86-10-82317524;E-mail:ghleebh0368@sina.com.cn).

计量

Stability of the Crossflow Pattern Around a Slender and Influence of Disturbance

计量

目录

留言板

细长体截面绕流的稳定性及扰动的影响

作者简介: 李国辉(1966- ),男,湖南永兴人,副教授,博士生(联系人.Tel:+86-10-82317524;E-mail:ghleebh0368@sina.com.cn).

计量

出版历程

Stability of the Crossflow Pattern Around a Slender and Influence of Disturbance

计量

出版历程

目录

作者简介:
李国辉(1966- ),男,湖南永兴人,副教授,博士生(联系人.Tel:+86-10-82317524;E-mail:ghleebh0368@sina.com.cn).