| 战术导弹CFD软件求解器开发与应用 |
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| 引用本文： | 李斌.战术导弹CFD软件求解器开发与应用[J].战术导弹技术,2009(2):32-35. |
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| 作者姓名： | 李斌 |
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| 作者单位： | 中国空空导弹研究院,洛阳471009 |
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| 摘 要： | 介绍了战术导弹CFD软件求解器MISSsolver．该求解器采用有限体积法离散求解任意坐标系下的Euler／N—S方程，获得绕导弹的复杂流场和全弹／部件的气动特性；采用多块结构网格技术，并包含多种时间、空间差分格式，提高数值模拟的范围与精度；具有通用的前后处理接口，方便用户使用．本文主要介绍MISSsolver求解器基本结构、功能，以及应用．
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| 关 键 词： | 战术导弹 计算流体力学 CFD求解器 |
Development and Application of CFD Solver for Tactical Missile |
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| Li Bin.Development and Application of CFD Solver for Tactical Missile[J].Tactical Missile Technology,2009(2):32-35. |
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| Authors: | Li Bin |
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| Affiliation: | Li Bin (China AirBorne Missile Aeademy, Luoyang 471009, China) |
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| Abstract: | The development and application of MISSsolver for tactical missile is introduced herein. Finite volume methods were adopted to discrete the Euler/N-S equations in general coordinates. The flow field around various vehicles in supersonic range is simulated and aerodynamics characters are also obtained. The basic function of the CFD code and application in practical problem are summarized briefly. |
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| Keywords: | tactical missile computational fluid dynamic CFD solver |
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