Development of gas guns combined with a water tank for launching high-velocity projectiles into water obliquely and horizontally
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摘要: 为开展模型高速斜入水和水中高速航行的水流场实验研究，研制了立式和卧式气炮与水箱组合的实验系统。通过快速阀和活塞阀控制气炮激发和驱动状态，一级气炮采用高压空气直接驱动弹托和模型，二级气炮采用高压空气驱动重活塞压缩使集气腔中产生高压气体，再驱动弹托和模型达到预定速度。通过调节水箱和发射管角度，使高速模型斜入水或水平入水。其中，立式可变发射角二级气炮可发射质量1～1000 g的模型至2500 m/s最大速度，卧式一级气炮可发射质量1～100 kg的模型至300 m/s最大速度。和小气室、高燃气压力火药驱动方式相比，新型气炮采用大体积、中低驱动压力气室，高压气体更接近等熵膨胀做功，调节高压气体压力，能较好地满足模型质量和速度的宽范围要求。结合光反射通断法测速、高速摄影和阴影流场显示等测量技术，得到立式气炮压缩管重活塞运动速度、压缩管末端压力时间曲线和模型倾斜与水平入水的流场阴影图像。结果表明：重活塞速度在膜片破裂前和理论计算值符合较好，但破膜后差异较大。立式气炮流场阴影图像反映了模型斜入水产生的空中和水中激波以及在气水界面的反射激波、空泡形成和侧向气水界面的破碎与飞溅等现象。从卧式气炮的模型水平入水阴影图像提取气泡轮廓，清楚地看出尾部气泡气水界面的波动和失稳。和商业计算软件Fluent计算结果相比，空泡上游区域基本重合，但尾流区域强湍流导致两者存在明显差异。和水洞实验相比，气炮水箱实验系统近真实地再现高速入水过程伴随的冲击和动态空化等物理现象和模型尺度效应。Abstract: Gas guns with a water tank assembly, were developed for launching projectiles into water obliquely and horizontally. The burst of gas guns was controlled by the quick valve and the piston valve. The cartridges and models in the one-stage gas gun were directly driven by high-pressure air. The heavy piston in the two-stage gas gun was driven by high-pressure air first, and then compressed the air in the gas-gathered chamber to drive the cartridges and models to the predetermined high-speed. By adjusting the angle between the water tank and the launching tube, the high-speed model can entry into water either obliquely or horizontally. The vertical gas gun with variable launch angles, is capable of launching a projectile with mass ranged from several to hundreds of grams at speed ranged from hundreds to thousands of meters per second. The horizontal gas gun can launch the projectile with mass ranged from several to tens kilograms at speed ranged from several to hundreds of meters per second. In contrast to a powder gas gun using small chamber filled with vitiated gas at high pressure and temperature, these gas guns are distinguished for the large volume air reservoir run at medium even low pressure, and characterized by a wide range of mass and speed of the projectile by adjusting the air pressure, which is close to isentropic expansion. Based on light reflection and beam on-off methodology, high-speed photography and shadowgraphy measurements, the results including the piston velocity in compression tube, the pressure time history at the end of the compression tube and the shadowgraph images of water entry and underwater navigation, were obtained. The results show that the piston velocities are in good agreement with the theoretical calculation before the diaphragm bursting, after which the difference increases. The high-speed shadowgraphs in the vertical gas gun clearly indicate the shock waves in the air and water generated by the oblique impacting of the projectile into the water, as well as the reflection of the shock wave on the gas-water interface, where the formation of cavitation, the break and splash of the interface are observed either. A gas bubble induced by water and enrolled air envelopes, which is extracted from the images in the horizontal gas gun, clearly indicates the fluctuation or instability along the gas-water interface close to the bubble rear. Compared with the numerical results by the commercial software fluent, the obtained bubble lineament basically coincides except at rear due to strongly wake turbulence attached to the projectile. In contrast to the water tunnel, the test rigs in this paper are superior in wide range of mass and speed, as well as reproducing real conditions such as impacting phenomenon and dynamic cavitation during the process of high-speed water entry.
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图 1 立式可变发射角二级气炮示意图
Figure 1. Schematic of the vertical two-stage gas gun with a rotated launch tube
图 2 立式气炮可变发射角侧视图
Figure 2. Profiles of variable incident angle of the vertical gas gun
图 3 卧式一级气炮总体结构示意图
Figure 3. Schematic diagram of the global structure of the horizontal one-stage gas gun
图 4 光反射测速法示意图
Figure 4. Schematic diagram of velocity measurement with light reflection
图 5 立式气炮阴影测量系统光路示意图
Figure 5. Schematic diagram of optical path of shadow measurement of the vertical gas gun
图 6 卧式气炮实验舱和阴影测量系统光路示意图
Figure 6. Schematic diagram of optical paths of shadow measurement of the horizontal gas gun
图 7 破膜工况重活塞沿压缩管轴线速度分布
Figure 7. Piston velocity distribution along the axis of the compression tube under diaphragm burst condition
图 8 破膜工况集气腔压力时间曲线
Figure 8. Pressure history in the gas collection chamber under diaphragm burst condition
图 9 未破膜工况重活塞速度沿压缩管轴线分布和随时间变化
Figure 9. Piston velocity distribution along the axis of compression tube and history with time marching under non-burst condition
图 10 模型入水前后阴影照片
Figure 10. Shadow graphs captured before and after the oblique water-entry of the model
图 11 不同头形模型斜入水流场阴影图像
Figure 11. Shadow graphs with projectiles of different head models inclined into the water
图 12 气泡轮廓实验和计算结果对比
Figure 12. Comparison of bubble contours between experimental and computational results
表 1 不同工况模型参数
Table 1. Parameters of different models
头部形状 锥角/（°） 柱身长度/mm 总体长度/mm 质量/g 尖头 60 50 67 53.4 尖头 90 50 60 52.8 平头 90 50 55 52.6 
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[1] 何肇雄, 郑震山, 马东立, 等. 国外跨介质飞行器发展历程及启示 [J]. 舰船科学技术, 2016, 38(5): 152–157. DOI: 10.3404/j.issn.1672-7619.2016.05.032.HE Z X, ZHENG Z S, MA D L, et al. Development of foreign trans-media aircraft and its enlightenment to China [J]. Ship Science and Technology, 2016, 38(5): 152–157. DOI: 10.3404/j.issn.1672-7619.2016.05.032. [2] LEXOW B, WICKERT M, THOMA K, et al. The extra-large light-gas gun of the Fraunhofer EMI: applications for impact cratering research [J]. Meteoritics and Planetary Science, 2012, 48(1): 3–7. DOI: 10.1111/j.1945-5100.2012.01427.x. [3] 王金贵. 气体炮原理及技术 [M]. 北京: 国防工业出版社, 2001: 65−70. [4] 张德志, 唐润棣, 林俊德, 等. 新型气体驱动二级轻气炮研制 [J]. 兵工学报, 2004, 25(1): 14–18. DOI: 10.3321/j.issn:1000-1093.2004.01.004.ZHANG D Z, TANG R D, LIN J D, et al. Development of a new type gas-driven two-stage light gas gun [J]. Acta Armamentarii, 2004, 25(1): 14–18. DOI: 10.3321/j.issn:1000-1093.2004.01.004. [5] 冯建宁, 彭炎午, 林俊德. 新型非火药驱动二级轻气炮内弹道诸问题的研究 [J]. 西北工业大学学报, 1994, 12(3): 477–481.FENG J N, PENG Y W, LIN J D, et al. On some problems of interior ballistics in a new type two-stage light gas gun with non-powder projection [J]. Journal of Northwestern Polytechnical University, 1994, 12(3): 477–481. [6] 林俊德, 张向荣, 朱玉荣, 等. 超高速撞击实验的三级压缩气炮技术 [J]. 爆炸与冲击, 2012, 32(5): 483–489. DOI: 10.11883/1001-1455(2012)05-0483-07.LIN J D, ZHANG X R, ZHU Y R, et al. The technique of three-stage compressed-gas gun for hypervelocity impact [J]. Explosion and Shock Waves, 2012, 32(5): 483–489. DOI: 10.11883/1001-1455(2012)05-0483-07. [7] THORNHILL T F, CHHABILDAS L C, REINHART W D, et al. Particle launch to 19km/s for micro-meteoroid simulation using enhanced three-stage light gas gun hypervelocity launcher techniques [J]. International Journal of Impact Engineering, 2006, 33(1): 799–811. [8] PIEKUTOWSKI A J, POORMON K L. Development of a three-stage, light-gas gun at the University of Dayton Research Institute [J]. International Journal of Impact Engineering, 2006, 33(1): 615–624. [9] MORITOH T, KAWAI N, NAKAMURA K G, et al. Three-stage light-gas gun with a preheating stage [J]. Review of Scientific Instruments, 2004, 75(2): 537–540. DOI: 10.1063/1.1641155. [10] 张庆明, 龙仁荣, 郑克勤, 等. 基于氢氧混合爆轰驱动的三级轻气炮: CN201710137286.1 [P]. 2017-06-27. [11] WANG X, DAI C D, WANG Q S, et al. Development of a three-stage gas gun launcher for ultrahigh-pressure Hugoniot measurements [J]. Review of Scientific Instruments, 2019, 90(1): 013903. DOI: 10.1063/1.5035502. [12] 董石, 孟川民, 肖元陆, 等. 反应气体驱动二级轻气炮技术的初步研究 [J]. 高压物理学报, 2017, 31(2): 182–186. DOI: 10.11858/gywlxb.2017.02.011.DONG S, MENG C M, XIAO Y L, et al. Preliminary study of two-stage light gas gun using reactive gas as driving energy [J]. Chinese Journal of High Pressure Physics, 2017, 31(2): 182–186. DOI: 10.11858/gywlxb.2017.02.011. [13] 张向荣, 朱玉荣, 林俊德, 等. 压缩氮气驱动的高速气炮实验技术 [J]. 航天器环境工程, 2015, 32(4): 343–348. DOI: 10.3969/j.issn.1673-1379.2015.04.001.ZHANG X R, ZHU Y R, LIN J D, et al. Experimental technique of high velocity gas gun driven by compressed nitrogen [J]. Spacecraft Environment Engineering, 2015, 32(4): 343–348. DOI: 10.3969/j.issn.1673-1379.2015.04.001. [14] 黄振贵, 王瑞琦, 陈志华, 等. 90°锥头弹丸不同速度下垂直入水冲击引起的空泡特性 [J]. 爆炸与冲击, 2018, 38(6): 1189–1199. DOI: 10.11883/bzycj-2018-0115.HUANG Z G, WANG R Q, CHEN Z H, et al. Experimental study of cavity characteristic induced by vertical water entry impact of a projectile with a 90° cone-shaped head at different velocities [J]. Explosion and Shock Waves, 2018, 38(6): 1189–1199. DOI: 10.11883/bzycj-2018-0115. [15] 罗驭川, 黄振贵, 高建国, 等. 截锥体头型弹丸低速斜入水实验研究 [J]. 爆炸与冲击, 2019, 39(11): 113902. DOI: 10.11883/bzycj-2018-0498.LUO Y C, HUANG Z G, GAO J G, et al. Experiment research of low-speed oblique water-entry of truncated cone-shaped projectile [J]. Explosion and Shock Waves, 2019, 39(11): 113902. DOI: 10.11883/bzycj-2018-0498. [16] 时素果, 杨晓光, 王亚东, 等. 细长体高速入水过程压力特性试验研究 [J]. 应用力学学报, 2018, 35(2): 223–227. DOI: 10.11776/cjam.35.02.A009.SHI S G, YANG X G, WANG Y D, et al. Experimental study on the pressure characteristic of high-speed slender body water entry [J]. Chinese Journal of Applied Mechanics, 2018, 35(2): 223–227. DOI: 10.11776/cjam.35.02.A009. [17] 陈诚, 袁绪龙, 邢晓琳, 等. 预置舵角下超空泡航行体倾斜入水弹道特性研究 [J]. 兵工学报, 2018, 39(9): 1780–1785. DOI: 10.3969/j.issn.1000-1093.2018.09.015.CHEN C, YUAN X L, XING X L, et al. Research on the trajectory characteristics of supercavitating vehicle obliquely entering into water at preset rudder angle [J]. Acta Armamentarii, 2018, 39(9): 1780–1785. DOI: 10.3969/j.issn.1000-1093.2018.09.015. [18] 张伟, 郭子涛, 肖新科, 等. 弹体高速入水特性实验研究 [J]. 爆炸与冲击, 2011, 31(6): 579–584. DOI: 10.11883/1001-1455(2011)06-0579-06.ZHANG W, GUO Z T, XIAO X K, et al. Experimental investigations on behaviors of projectile high-speed water entry [J]. Explosion and Shock Waves, 2011, 31(6): 579–584. DOI: 10.11883/1001-1455(2011)06-0579-06. [19] CHEN T, HUANG W, ZHANG W, et al. Experimental investigation on trajectory stability of high-speed water entry projectiles [J]. Ocean Engineering, 2019, 175: 16–24. DOI: 10.1016/j.oceaneng.2019.02.021. -
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