超空泡航行器20°角倾斜入水冲击载荷特性试验研究

doi:10.3969/j.issn.1000-1093.2018.06.016

兵工学报 ›› 2018, Vol. 39 ›› Issue (6): 1159-1164.doi: 10.3969/j.issn.1000-1093.2018.06.016

超空泡航行器20°角倾斜入水冲击载荷特性试验研究

陈诚，袁绪龙，党建军，徐强

(西北工业大学航海学院，陕西西安 710072)

收稿日期:2017-08-17 修回日期:2017-08-17 上线日期:2018-07-29
通讯作者: 袁绪龙（1977—），男，副教授，硕士生导师 E-mail:yuanxulong@nwpu.edu.cn
作者简介:陈诚（1990—），男，博士研究生。E-mail:chencheng1990@mail.nwpu.edu.cn；
党建军（1965—），男，教授，博士生导师。E-mail:janjund@nwpu.edu.cn
基金资助:
武器装备预先研究基金项目（9140A13050215HK03015）

Experimental Investigation into Impact Load during Oblique Water-entry of a Supercavitating Vehicle at 20°

CHEN Cheng, YUAN Xu-long, DANG Jian-jun, XU Qiang

(School of Marine Science and Technology, Northwestern Polytechnical University, Xi'an 710072, Shaanxi, China)

Received:2017-08-17 Revised:2017-08-17 Online:2018-07-29

摘要/Abstract

摘要： 为探究带圆盘空化器的超空泡航行器倾斜入水过程冲击载荷特性，开展了20°入水角条件下的试验研究。超空泡航行器由空气炮加速获得入水初速度，采用内置惯性测量单元记录载荷变化，试验完成后提取数据进行分析；试验设定了典型入水工况，分析了航行器入水冲击过程轴向载荷的变化特性，进行了入水速度和空化器面积对入水冲击载荷影响的系列试验，分析了各参数下的冲击载荷特性。研究结果表明：航行器入水冲击载荷峰值时刻侵彻距离为空化器直径的1.89倍，阻力系数为稳定航行阶段的1.33倍；在所研究的范围内入水速度和空化器面积对阻力系数峰值无影响。

关键词: 超空泡航行器, 圆盘空化器, 入水试验, 冲击载荷

Abstract: In order to investigate the impact load characteristics of a supercavitating vehicle with a disk cavitator during oblique water-entry, a series of experiments were carried out at the water-entry angle of 20° . An air cannon is set up to provide the initial velocity of supercavitating vehicle. An inertial measurement unit is embedded at the center of gravity of supercavitating vehicle to record the variation of axial impact load, and the data is extracted and analyzed after the experimental test. A typical research case is set up, and the impact load characteristics varying with time are obtained and described in detail. Subsequently, a series of experiments for different entry speeds and cavitator areas are carried out, and the effects of the influence factors on the impact load characteristics are analyzed. The investigation shows that, when the impact load reaches the peak, the penetration distance is 1.89 times of the diameter of cavitator as a reference dimension, and the resistance coefficient is 1.33 times of that in the steady stage. The resistance coefficient is shown to be independent of entry velocity and cavitator area over a wide range of test conditions. Key

Key words: supercavitatingvehicle, diskcavitator, waterentryexperiment, impactload

中图分类号:

TJ630.1

陈诚，袁绪龙，党建军，徐强. 超空泡航行器20°角倾斜入水冲击载荷特性试验研究[J]. 兵工学报, 2018, 39(6): 1159-1164.

CHEN Cheng, YUAN Xu-long, DANG Jian-jun, XU Qiang. Experimental Investigation into Impact Load during Oblique Water-entry of a Supercavitating Vehicle at 20°[J]. Acta Armamentarii, 2018, 39(6): 1159-1164.

参考文献

［1］ Seddon C M, Moatamedi M. Review of water entry with applications to aerospace structures［J］. International Journal of Impact Engineering, 2006, 32(7):1045-1067.
［2］秦洪德, 赵林岳, 申静. 入水冲击问题综述［J］. 哈尔滨工业大学学报, 2011, 43(增刊1):152-157.
QIN Hong-de, ZHAO Lin-yue, SHEN Jing. Review of water entry problem［J］. Journal of Harbin Institute of Technology, 2011, 43(S1): 152-157. (in Chinese)
［3］魏卓慧, 王树山, 马峰. 刚性截锥形弹体入水冲击载荷［J］. 兵工学报, 2010, 31(增刊1):118-120.
WEI Zhuo-hui, WANG Shu-shan, MA Feng. Diving impact load of rigid truncated conical projectile［J］. Acta Armmamentarii, 2010, 31(S1):118-120. (in Chinese)
［4］何春涛, 王聪, 闵景新,等. 回转体匀速垂直入水早期空泡数值模拟研究［J］. 工程力学, 2012, 29(4):237-243.
HE Chun-tao, WANG Cong, MIN Jing-xin, et al. Numerical simulation of early air-cavity of cylinder cone with vertical water-entry［J］. Engineering Mechanics, 2012, 29(4):237-243. (in Chinese)
［5］ Xu B W, Li Y L, Feng J F, et al. Research on the water-entry attitude of a submersible aircraft［J］. SpringerPlus, 2016, 5(1):1933.
［6］路中磊, 魏英杰, 王聪,等. 开放空腔壳体入水扰动流场结构及空泡失稳特征［J］. 物理学报, 2017, 66(6):150-163.
LU Zhong-lei, WEI Ying-jie, WANG Cong, et al. Experimental and numerical investigation on the flow structure and instability of water-entry cavity by a semi-closed cylinder［J］. Acta Physica Sinica , 2017, 66(6):150-163. (in Chinese)
［7］ Park M S, Jung Y R, Park W G. Numerical study of impact force and ricochet behavior of high speed water-entry bodies［J］. Computers & Fluids, 2003, 32(7):939-951.
［8］王永虎, 石秀华. 空投雷弹斜入水初始弹道数值分析［J］. 弹道学报, 2012, 24(2):92-95.
WANG Yong-hu, SHI Xiu-hua. Numerical analysis for initial hydroballistics of airborne missile during oblique water-entry impact［J］. Journal of Ballisticas, 2012, 24(2):92-95. (in Chinese)
［9］ Nguyen V T, Vu D T, Park W G, et al. Navier-Stokes solver for water entry bodies with moving Chimera grid method in 6DOF motions［J］. Computers & Fluids, 2016, 140:19-38.

［10］ Guo Z T, Zhang W, Xiao X K, et al. An investigation into horizontal water entry behaviors of projectiles with different nose shapes［J］. International Journal of Impact Engineering, 2012, 49(2):43-60.
［11］ Tveitnes T, Fairlie-Clarke A C, Varyani K. An experimental investigation into the constant velocity water entry of wedge-shaped sections［J］. Ocean Engineering, 2008, 35(14):1463-1478.
［12］ Bodily K G, Carlson S J, Truscott T T. The water entry of slender axisymmetric bodies［J］. Physics of Fluids, 2014, 26(7):45-78.
［13］ Alaoui A E M, Nême A, Tassin A, et al. Experimental study of coefficients during vertical water entry of axisymmetric rigid shapes at constant speeds［J］. Applied Ocean Research, 2012, 37:183-197.
［14］ Yuan X L, Xing T. Hydrodynamic characteristics of a supercavitating vehicle's aft body［J］. Ocean Engineering, 2016, 114:37-46.

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超空泡航行器20°角倾斜入水冲击载荷特性试验研究

Experimental Investigation into Impact Load during Oblique Water-entry of a Supercavitating Vehicle at 20°

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