期刊文献+

旋转钝锥高超声速绕流的数值模拟与定性分析研究

Numerical Analysis Investigation of Hypersonic Flows over a Blunt Cone with and without Spin
下载PDF
导出
摘要 本文通过数值模拟和拓扑分析,研究了以等角速旋转的钝惟有攻角绕流时垂直于物面的截面流线性状,揭示了顺流运动壁和逆流运动壁情况下截面流态的拓扑结构,定性说明了三维非定常分离的一些主要特征。 In this paper, the flows around a blunt cone with spin are simulated numerically, and the flow separation patterns are investigated. By flowfield visualization and qualitative analysis, the topological structure of the sectional flow patterns on the wall moving along or reversal to the out flow are revealed. Although it is quite difference from the cases without spin, but they have something to do with each other. In addition, the relations between a moving wall and a stationary wall, as well as the relations between the topological structure and the flow parameters on the body surface are presented.
出处 《空气动力学学报》 CSCD 北大核心 2000年第z1期1-9,共9页 Acta Aerodynamica Sinica
基金 国家自然科学基金
关键词 三维非定常分离 角速度 拓扑分析 数值模拟 three dimensional flow separation angler velocity topological analysis numerical simulation
  • 相关文献

参考文献9

  • 1[1]Moore F K. On the Separation of Unsteady Laminar Boundary Layers. Boundary Layer Research, Edited by Gortler H G, Springer Verlag, Berline, 1958.
  • 2[2]Rott N. Unsteady Viscous Flow in Vicinity ofa Stagnation Point. Quartely J. of Appl. Math., 1956, 13.
  • 3[3]Sears W R. Some Recent Development in Airfoil Theory. J. A. S., 1956, 23.
  • 4[4]O'Brien V. Stagnation Regions of Separation. The Physics of Fluid, 1981, 24(6).
  • 5[5]Wang K C. On the Current Controversy about Unsteady Separation. in Numerical and Physics Aspect of Aerodynamic Flows. Berlin: Springer-Verlag, 1982.
  • 6张涵信.二维粘性不可压缩流动的通用分离判据[J].力学学报,1983,6:559-570.
  • 7[7]Bakker P G. Bifurcations in Flow Patterns. Kluwer Academic Publishers, 1991.
  • 8[9]Hui W H. Unsteady Three-Dimensional Flow Separation. NASA CR-182412, 1988.
  • 9[10]Gad-el-Hak M and Ho C M. Unsteady Separation around an Ogive-Cylinder. J. Aircraft, 1986, 23.

共引文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部