Simulation of Tail-slap Loads of Supercavitating Projectiles

Jia-zhong Zhang, Jin-Sheng Zhang, Yingjie Wei
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引用次数: 3

Abstract

To investigate the tail-slap loads on supercavitating projectiles, a simple model for cavity-fluid region is presented based on Logvinovich’s Principle. And a series of simulations of fluid - structure interaction (FSI) were done to determine the effects of the slenderness ratio of projectiles on the tail-slap loads. The results show that the impact duration increases as the slenderness ratio increases and the frequency of impacts decrease as the slenderness ratio increases. The larger the slenderness ratio is, the more obviously the body’s flexibility and vibration influent the slapping force. The results developed in this paper will provide reference for the structural dynamics research and optimization design of the supercavitating projectiles.
超空泡弹丸尾扇载荷仿真
为了研究超空泡弹丸尾扇载荷,基于Logvinovich原理建立了一个简单的空泡-流体区域模型。为了确定弹体长细比对弹尾拍打载荷的影响,进行了一系列流固耦合仿真。结果表明:冲击时间随长细比的增大而增大,冲击频率随长细比的增大而减小;长细比越大,车身的柔韧性和振动对拍打力的影响越明显。本文的研究结果将为超空泡弹的结构动力学研究和优化设计提供参考。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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