| 再入飞行器高超声速三维粘性流场的数值模拟 |
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| 引用本文： | 柳军,瞿章华.再入飞行器高超声速三维粘性流场的数值模拟[J].国防科技大学学报,1996,18(2):1-4. |
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| 作者姓名： | 柳军 瞿章华 |
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| 作者单位： | 国防科技大学航天技术系 |
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| 摘 要： | 用数值方法研究大钝头倒锥体再入飞行器高超车速完全气体有攻角绕流的流场特性。控制方程为完全气体三维Ｎａｖｉｅｒ－Ｓｔｏｋｅｓ方程，数值方法采用激波捕捉的ＮＮＤ隐式算法，计算区域为含底部的全流场。文中给出了流场特性和气功力系数，并与实验结果进行了对比。
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| 关 键 词： | 高超声速，完全气体，三维流场，激波捕捉 |
| 收稿时间： | 1995/10/17 0:00:00 |
Numerical Simulation of 3-D Hypersonic Viscous Flowfield over a Capsule |
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| Liu Jun and Qu Zhanghua.Numerical Simulation of 3-D Hypersonic Viscous Flowfield over a Capsule[J].Journal of National University of Defense Technology,1996,18(2):1-4. |
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| Authors: | Liu Jun and Qu Zhanghua |
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| Abstract: | The three dimensional hypersonic viscous flow of perfect gas over a capsule is calculated numerically. The Navier-Stokes equations are taken as the governing equations. The implicit NND scheme is used for the shock capture. The computation region is involved with the full flowfíeld from the nose to the base. The flowfield properties and the areodynamic force coefficients thus obtained are good compared with the experiment results. |
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