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导弹发射过程三维非定常数值模拟
引用本文:姜毅,郝继光,傅德彬. 导弹发射过程三维非定常数值模拟[J]. 兵工学报, 2008, 29(8): 911-915
作者姓名:姜毅  郝继光  傅德彬
作者单位:北京理工大学宇航科学技术学院,北京,100081;北京理工大学宇航科学技术学院,北京,100081;北京理工大学宇航科学技术学院,北京,100081
摘    要:针对计算流体力学中的各种动网格更新技术进行了综合分析,对域动分层法动网格更新技术的原理进行了阐述。应用该方法对同心筒发射装置内导弹发射过程的三维流场分布进行了非定常数值模拟,得到全流场参数在三维空间上的时间分布,并与试验结果进行对比分析,得到了该方法正确可行、可有效保证导弹发射过程模拟的计算精度及计算效率的结论。

关 键 词:流体力学  动网格  发射  燃气射流  数值模拟

3D Unsteady Numerical Simulation of Missile Launching
JIANG Yi,HAO Ji-guang,FU De-bin. 3D Unsteady Numerical Simulation of Missile Launching[J]. Acta Armamentarii, 2008, 29(8): 911-915
Authors:JIANG Yi  HAO Ji-guang  FU De-bin
Affiliation:School of Aerospace Science and Engineering, Beijing Institute of Technology, Beijing 100081, China
Abstract:The dynamic mesh update methods of computational fluid dynamics were analyzed. A new dynamic mesh update method, i.e. zone moving and dynamic layering method, was presented, and its principle was described. The method was used for the unsteady numerical simulation of 3D flow field distribution in the launching process of missile from concentric cylinder launcher to obtain the time dis?tribution of flow field parameters in 3D space. Ihe simulation results were compared with the test re?sults .The compared result shows that the method can ensure the missile launching calculation accuracy and efficiency.
Keywords:fluid mechanics    dynamic mesh    launching    jet flow    numerical simulation  
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