高温燃气推进下水下航行体出筒发射数值模拟研究
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1.中国船舶集团有限公司第七一〇研究所;2.大连海事大学 船舶与海洋工程学院

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国防科工局基础科研项目“虚实结合的***多学科敏捷设计技术”(JCKY2021206B005)


Numerical Simulation Study on the Launch of Underwater Vehicle with High Temperature Gas Propulsion
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1.No.710R&2.D Institute , CSSC;3.School of Naval Architecture and Marine Engineering,Dalian Maritime University

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    摘要:

    水下航行器出筒过程往往伴随着着筒内高温高速气体的复杂流动和筒口水气多相混合流动,呈现出复杂的流动状态和变化规律,对航行器的发射动力、载荷以及出筒后的运动姿态等有着重要影响。本文以某水下航行器出筒发射为例,采用CFD方法开展高温燃气推进下水下航行体出筒发射数值模拟研究,通过不同网格密度下的水平方向位移和竖直方向位移比较,论证了本文数值模拟的收敛性。进一步,利用所建立的数值模型模拟了不同初始发射倾角、不同横向来流作用下高温燃气推进下水下航行器出筒过程,得到了航行器出筒后的偏转角度和速度,明确了筒口气泡发展变化规律、发射筒内外气体流动状态、发射过程中的速度场与温度场的典型特征等,为水下热发射系统的设计提供指导。

    Abstract:

    The process of underwater vehicles exiting the barrel is often accompanied by complex flow of high-temperature and high-speed gas inside the barrel and multiphase mixed flow of water and gas at the barrel mouth, presenting complex flow states and changing patterns, which have important impacts on the launch power, load, and motion posture of the vehicle after exiting the barrel. This article takes the launch of a certain underwater vehicle as an example and uses CFD method to conduct numerical simulation research on the launch of a high-temperature gas propulsion underwater vehicle. By comparing the horizontal and vertical displacement under different grid densities, the convergence of the numerical simulation in this article is demonstrated. Using a validated numerical model, the process of high-temperature gas propulsion for underwater vehicles exiting the barrel was simulated under different initial launch angles and lateral inflow effects. The deflection angle and velocity of the vehicle after exiting the barrel were obtained, and the development and variation law of the bubble at the barrel mouth, the flow state of gas inside and outside the launch barrel, and the typical characteristics of the velocity and temperature fields during the launch process were clarified, which provides theoretical guidance for predicting the motion posture of underwater thermal launch.

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  • 收稿日期:2024-02-01
  • 最后修改日期:2024-03-19
  • 录用日期:2024-04-03
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