Modeling of the Tail Slap for A Supercavitating Projectile

Xuefeng Zhao, Xujian Lyu, Da Li
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引用次数: 1

Abstract

This paper presents a model for forward motion and tail slap dynamics by mathematic deduction. The MATLAB software is applied to model the above motion and the characteristics for a single slap in the water layer are analyzed, as well as several slaps in the cavitation. The duration time of single slap increases as the projectile speed decrease into a certain range and this may lead to collapse of the supercavitation and instability of the projectile moving forward. It turns out that the number of the tail slap and the reflection angle increase with the increasing of the projectile angular speed. What’s more, the differences between parameters of different slap points become smaller as the tail slap goes on under supercavitation condition.
超空泡弹丸尾翼拍打的建模
通过数学推导,建立了飞机前向运动和尾翼拍打动力学模型。利用MATLAB软件对上述运动进行建模,分析了水层中单次拍打的运动特性,以及空化过程中多次拍打的运动特性。随着弹丸速度减小到一定范围,单次拍打的持续时间增加,这可能导致超空泡的崩溃和弹丸前进的不稳定。结果表明,尾翼拍打次数和反射角随弹丸角速度的增加而增加。此外,在超空化条件下,随着尾拍打的持续进行,不同拍打点参数之间的差异逐渐变小。
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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