采用Lagrange结构网格和Euler流场网格（L/E）耦合的数值仿真方法，对潜射航行器出筒后筒口压力场进行三维数值仿真分析。计算模型考虑海水的横向来流和航行体出筒过程对筒口气泡脉动的影响。仿真计算获得了筒口压力场气泡脉动主要特征，试验与计算的2个主要压力波峰曲线形状基本一致。通过对比计算表明，考虑横向流作用可以有效减少筒口压力场计算偏差。本文的计算方法及结论可为发射筒口压力场分析提供有益指导。
The fluid pressure field near canister outlet for underwater-launched vehicle vertical launch was simulated, using a 3D symmetric model based on the coupling of Lagrange structure mesh and Euler fluid mesh. The water horizontal relative motion and the process of vehicle motion in the launch canister were considered in the model. The characteristics of bubble pulsation were achieved through the simulation. The shape of the two primary pressure waves are approximately identical between simulation results and test results. It shows that, simulation model which consider the lateral flow can be more accurate than the model without lateral flow. The research method and its conclusions are good kind of reference to analysis of pressure field near launch canister.
2016,38(11): 151-155 收稿日期：2016-10-17
DOI：10.3404/j.issn.1672-7619.2016.11.032
分类号：TJ768.2
基金项目：“十二五”预研资助项目（1010403050102）
作者简介：张晓乐(1981-),男,博士,高级工程师,主要研究方向为水下发射技术。
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