Underwater launching of a supercavitating projectile out of a ballistic test setup

A. Ishchenko, V. Burkin, A. S. D’yachkovskiy, Andrey V. Chupashev
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Abstract

This paper considers the investigation of the high-speed motion of specifically-shaped inert bodies (projectiles) in water. The main purpose is to determine the peculiar properties of underwater launching of supercavitating projectiles out of the bore of a test ballistic setup. Preliminary calculations of the inner ballistic parameters of a shot are per-formed for the given launcher and then compared with the corresponding experimental data. Examples of experimentally fired underwater shots are presented. The high-speed high-energy processes associated with the projectile released out of the bore and entering water are described. It is shown that during the underwater launching, the complex gas-dynamic conditions of multi-phase processes following the projectile release out of the bore can significantly affect the trajectory of its further motion in water. Using the experi-mental and calculation methods with the classical loading scheme and an acceleration bore 0.5 mm long or less under given conditions, it has been determined that the pressure at the accelerator exit increases stepwise and can significantly change the flow conditions of the projectile at the start and its further trajectory. Taking into consideration the revealed peculiarities of underwater shots and a set of technical specifications and mass-size parameters, a perspective launching ballistic setup has been designed and used to estimate the motion range of the released supercavitating projectile.
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在弹道试验装置中水下发射超空泡弹丸
本文研究了特殊形状的惰性物体(弹丸)在水中的高速运动。主要目的是确定超空泡弹丸从试验弹道装置的膛中水下发射的特殊特性。对给定发射装置的内弹道参数进行了初步计算,并与相应的实验数据进行了比较。给出了水下实验射击的实例。描述了弹丸出膛进入水中的高速高能过程。研究表明,在水下发射过程中,弹丸出膛后多相过程的复杂气动力条件会显著影响弹丸在水中进一步运动的轨迹。在给定条件下,采用经典装填方案和0.5 mm以下的加速孔进行实验和计算,确定了加速出口压力逐步增大,并能显著改变弹丸的起始流动状况和后续弹道。考虑到水下射击的特点和一套技术指标和质量尺寸参数,设计了一种透视发射弹道装置,用于估算超空泡弹丸释放的运动范围。
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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CiteScore
0.90
自引率
66.70%
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