| 三维超声速隔离段湍流内流场旋涡结构的数值模拟 |
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| 引用本文： | 范晓樯,李桦,丁猛.三维超声速隔离段湍流内流场旋涡结构的数值模拟[J].国防科技大学学报,2001,23(6):5-8. |
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| 作者姓名： | 范晓樯 李桦 丁猛 |
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| 作者单位： | 国防科技大学航天与材料工程学院, |
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| 基金项目： | 湖南省自然科学基金资助项目 ( 99JJY2 0 0 5 ) |
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| 摘 要： | 从基于雷诺平均的N S方程出发 ,采用有限体积方法离散控制方程 ,数值模拟了三维超声速隔离段湍流内流场。计算中采用了二阶OC TVD差分格式、LU隐式算法和Baldwin Lomax代数湍流模型。数值结果与实验做了对比 ,并结合隔离段中的激波串结构分析了其横截面上旋涡结构的发展过程及不同外形条件下旋涡的不同结构。计算结果表明采用本文发展的方法模拟隔离段湍流流场是可行的 ,截面为正方形与长方形的隔离段内的涡旋结构截然不同
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| 关 键 词： | 隔离段 有限体积方法 激波串 旋涡 |
| 文章编号： | 1001-2486(2001)06-0005-04 |
| 收稿时间： | 2001/4/10 0:00:00 |
| 修稿时间： | 2001年4月10日 |
Numerical Simulation of 3D Turbulent Vortex Structures in Isolator |
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| FAN Xiaoqiang,LI Hua and DING Meng.Numerical Simulation of 3D Turbulent Vortex Structures in Isolator[J].Journal of National University of Defense Technology,2001,23(6):5-8. |
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| Authors: | FAN Xiaoqiang LI Hua and DING Meng |
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| Affiliation: | College of Aerospace and Materials Engineering,National Univ. of Defense Technology, Changsha 410073,China;College of Aerospace and Materials Engineering,National Univ. of Defense Technology, Changsha 410073,China;College of Aerospace and Materials Engineering,National Univ. of Defense Technology, Changsha 410073,China |
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| Abstract: | The interaction between shock waves and boundary layer in isolator causes a very complicated flow, to simulate the turbulent flow field in it, the time dependent, implicit, finite volume, lower upper numerical method was used to solve the 3D compressible Reynolds averaged Navier Stokes equations. Numerical results are compared with experimental data and used to describe the vortex structures in different isolator shape or different location of an isolator combined shock train structures in it. The numerical results indicate that the vortex structures in square cross section and rectangular cross section is very different. |
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| Keywords: | isolator finite volume method shock train vortex |
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