On the water entry impact characteristics of high-speed vehicle with an Arbitrary Lagrangian-Eulerian method

IF 4.3 2区 工程技术 Q1 ENGINEERING, OCEAN Applied Ocean Research Pub Date : 2024-07-10 DOI:10.1016/j.apor.2024.104118
Xudong Fan , Jiazhen Zhao , Chao Qi , Xu Wang , Xujian Lyu
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Abstract

This paper investigates the fluid-structure interaction process of high-speed vehicles during water entry using the Arbitrary Lagrangian-Eulerian method. Through mesh independence verification and comparison of numerical simulation results with experimental data and empirical formulas, the reliability and accuracy of the computational method are confirmed. The study comprehensively analyzes flow field pressure distribution, cavity evolution characteristics, and vehicle force features, evaluating the impact of water-entry angle, Froude number (Fr), and cavitator dimension. The results indicate that during water entry, the instantaneous impact forces are mainly concentrated on the wetted surface at the bottom of the vehicle and the plane at the head. The peak stress at the entry point is significantly higher than at other locations, and stress waves propagate along the vehicle body, concentrating at the hollow structure due to the structural characteristics. The change in water-entry angle does not significantly affect the decay of Fr for the vehicle, but increasing the water-entry angle leads to an earlier and larger peak stress at the mid-point monitoring location of the vehicle. In addition, the study also found that the stress level increases with the increase of the Froude number, resulting in larger high-stress areas and peak stresses. However, the cavity evolution at the same water-entry depth is essentially independent of the variation in Fr. With the increase in cavitator dimension, the water-entry load and cavity profile will also significantly increase, and vehicles with larger cavitator dimension will generate larger stress waves upon impact.

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用任意拉格朗日-欧勒方法研究高速飞行器的进水冲击特性
本文采用任意拉格朗日-欧勒方法研究了高速车辆在入水时的流固耦合过程。通过网格独立性验证以及数值模拟结果与实验数据和经验公式的对比,证实了计算方法的可靠性和准确性。研究全面分析了流场压力分布、空腔演化特征和载流子受力特征,评估了入水角、弗劳德数(Fr)和空腔尺寸的影响。结果表明,在进水过程中,瞬时冲击力主要集中在飞行器底部的润湿面和头部的平面上。入水点的峰值应力明显高于其他位置,应力波沿着车体传播,由于结构特点,应力波集中在中空结构处。入水角度的变化不会对车辆 Fr 的衰减产生明显影响,但入水角度的增加会导致车辆中点监测位置的峰值应力更早、更大。此外,研究还发现,应力水平会随着 Froude 数的增加而增加,从而导致更大的高应力区域和峰值应力。然而,相同入水深度下的空腔演变与 Fr 的变化基本无关。随着空腔尺寸的增加,入水载荷和空腔轮廓也会显著增加,空腔尺寸较大的车辆在撞击时会产生较大的应力波。
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来源期刊
Applied Ocean Research
Applied Ocean Research 地学-工程:大洋
CiteScore
8.70
自引率
7.00%
发文量
316
审稿时长
59 days
期刊介绍: The aim of Applied Ocean Research is to encourage the submission of papers that advance the state of knowledge in a range of topics relevant to ocean engineering.
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