Analyzing cavity evolution and motion characteristics of asynchronous parallel oblique water-entry super-cavitating projectile

C. Gao, Lin Lu, Xiaobin QI, Xu Yan, Chen Wang, Yanxiao Hu, Dongxia Zhang
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Abstract

Based on the volume of fluid multiphase flow model and the overset mesh technique, a numerical method for an asynchronous parallel oblique water-entry super-cavitating projectile was established. Experimental studies of the oblique water-entry of a high-speed single-launch projectile were carried out to validate the viability of the numerical method. The paper performed the numerical simulations and analyses of cavity evolution and motion characteristics of the front and rear projectiles in different initial intervals and in two sequences of top-side water-entry projectile first and bottom-side water-entry projectile first. The results show that when the initial interval of the first launch projectile is 0.5 time the projectile length, the first launch projectile cannot produce a cavity to completely encapsulate the projectile due to the violent squeezing of the following launch projectile cavity, and its movement is seriously affected and eventually loses its trajectory stability. At the same time, the first launch projectile that enters water from top side is squeezed to a larger degree than the one from bottom side, and the wetting phenomenon occurs earlier and loses stability faster. As the initial interval increases, the influence of the following launch projectile cavity near the first launch projectile is weakened, and the first launch projectile in both water entry sequences move steadily. For the following launch projectile, due to the continuous influence of the first launch projectile cavity, its cavity is always asymmetrical, and its motion stability is affected. The following launch projectile deflects to the inner side and destabilizes when the initial interval is 0.5 times the projectile length. When the initial interval is 1 time the projectile length, it moves steadily. It deflects to the outer side and destabilizes when the initial interval is 2 and 3 times the projectile length. In addition, the motion characteristics of the following launch projectile are basically identical in two water-entry sequences.
分析异步平行斜入水超空化弹丸的空腔演化和运动特性
基于流体体积多相流模型和超集网格技术,建立了异步平行斜入水超空化弹丸的数值方法。为了验证数值方法的可行性,还对高速单发弹丸的斜入水实验进行了研究。论文对不同初始间隔和上侧先入水和下侧先入水两种顺序下前后弹体的空腔演化和运动特性进行了数值模拟和分析。结果表明,当先发射弹丸的初始间隔为弹丸长度的 0.5 倍时,由于后发射弹丸空腔的剧烈挤压,先发射弹丸无法产生空腔将弹丸完全包裹,其运动受到严重影响,最终失去弹道稳定性。同时,从上侧入水的第一枚发射弹比从下侧入水的第一枚发射弹受到的挤压程度更大,湿化现象发生得更早,失去稳定性的速度更快。随着初始间隔的增大,第一个发射弹附近的后续发射弹空腔的影响减弱,两个入水序列中的第一个发射弹都会稳定移动。对于后续发射弹而言,由于受到第一个发射弹空腔的持续影响,其空腔总是不对称的,运动稳定性受到影响。当初始间隔为弹丸长度的 0.5 倍时,后发射弹丸会向内侧偏转并失稳。当初始间隔为弹丸长度的 1 倍时,弹丸稳定运动。当初始间隔为弹丸长度的 2 倍和 3 倍时,弹丸向外侧偏转并失稳。此外,在两个入水序列中,后续发射弹丸的运动特性基本相同。
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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