Numerical simulation of two-phase flow in a side spray gun considering piston reset motion
-
摘要: 为研究活塞回复运动对火药燃气流动的影响，基于两相流理论对活塞控制侧向后喷武器的发射过程进行了数值模拟研究。考虑控制侧向后喷通道开闭的活塞-弹簧系统的往复运动，建立了结合膛内气固两相流、活塞腔内流固耦合和侧向排气管内气体瞬态流动的武器发射过程数学模型，并将数值模拟结果与相关文献进行了比较验证。得到了该武器发射过程中膛内流场分布与稀疏波传播特性，并与普通武器的膛内流场进行了对比分析。进一步研究了活塞回复运动对火药燃气流动和减后坐效率的影响。结果表明：相对于不考虑活塞的回复运动，在弹丸初速都降低1.52%的情况下，因为活塞回复关闭后喷通道，其减后坐效率由38.86%下降到32.88%，说明在此类武器研究中，不可忽视活塞回复运动。Abstract: In order to study the effect of the piston reset motion on the flow of propellant gas in a piston-controlled side spray gun, the propulsion process of the gun was modeled and simulated based on the one-dimensional two-phase flow interior ballistic theory. First, by considering the reciprocating motion of the piston-spring system that controls the opening and closing of the rear spray channel, a mathematical model of the gun propulsion process was established. It combines the gas-solid two-phase flow in the barrel, the fluid-solid coupling between the piston and the gas in the piston cavity, and the transient gas flow in the exhaust pipe. The flow field coupling between the barrel and the piston cavity, and the flow field coupling between the piston cavity and the exhaust pipe were modeled, respectively, and the solution procedure was displayed. The MacCormack scheme and the Runge-Kutta method were used in the simulations, and the accuracy of the numerical method was validated by the published data. Next, the propagation law of the rarefaction wave in the barrel during the firing cycle was gained. The projectile velocity and the pressure at the projectile base and the breech were presented. Then, the distributions of the pressure, the gas velocity, and the solid velocity in the barrel of the piston-controlled side spray gun were compared with those in the traditional gun. Finally, the effects of the piston reset motion on the propellant gas flow and the recoil reduction efficiency were analyzed. The results show that compared with the situation ignoring the piston reset motion, when the muzzle velocity is reduced by 1.52%, the recoil reduction efficiency of the case considering the reset motion drops from 38.86% to 32.88% because the piston closes the rear spray channel during the reset process. Therefore, the reset motion of the piston cannot be ignored in the numerical simulation on the gun firing process.
-
Key words:
- recoil reduction /
- piston motion /
- two-phase flow /
- fluid-solid coupling
-
图 1 活塞控制侧向后喷减后坐武器原理图
Figure 1. Structural diagrams of the piston-controlled side spray gun
图 2 排气孔导通面积随弹丸位移变化
Figure 2. Change of barrel vent conducting area with projectile displacement
图 7 普通火炮和活塞控制侧向后喷武器的膛内压力
Figure 7. Pressures of the traditional gun and the piston-controlled side spray gun
图 8 普通火炮和活塞控制侧向后喷武器的弹丸速度
Figure 8. Projectile velocities of the traditional gun and the piston-controlled side spray gun
图 14 流入活塞腔内气体的总质量
Figure 14. Total mass of the propellant gasflowing into the piston cavity
图 15 侧向后喷排气管内流场
Figure 15. Flow field along the axis of the sideways rear-spraying exhaust pipe
图 16 活塞回复对武器发射过程后坐冲量的影响
Figure 16. Effect of piston reset motion on recoil momentum during the propulsion process
表 2 已知参数
Table 2. Known parameters
A/mm2 ρp/（kg·m−3） k ep/（kJ·kg−1） R/（J·kg−1·K） K0 αc/（J·m·kg−1·s−1·K−1） 706.5 1 600 1.25 3 600 350 0.588 6 619 
下载: 导出CSV
表 3 计算参数
Table 3. Calculation parameters
mh/kg Sh/mm2 kh/（N·mm−1） Vho/mm3 xb/m r1/mm Ac/mm2 0.3588 314 10 628 0.45 10 314
下载: 导出CSV
-
[1] OUYANG Q, ZHENG J J, LI Z C, et al. Controllability analysis and testing of a novel magnetorheological absorber for field gun recoil mitigation [J]. Smart Materials and Structures, 2016, 25(11): 115041. DOI: 10.1088/0964-1726/25/11/115041. [2] KATHE E L. Sonic rarefaction wave recoilless gun system: US 6460446 B1 [P]. 2002-10-08. [3] ZHANG X B, WANG Y Z. Analysis of dynamic characteristics for rarefaction wave gun during the launching [J]. Journal of Applied Mechanics, 2010, 77(5): 051601. DOI: 10.1115/1.4001289. [4] 张帆, 廖振强, 刘国鑫, 等. 基于两相流理论的膨胀波枪炮内弹道机理 [J]. 弹道学报, 2007, 19(4): 9–12. DOI: 10.3969/j.issn.1004-499X.2007.04.003.ZHANG F, LIAO Z Q, LIU G X, et al. Interior ballistic study on rarefaction wave gun based on theory of two-phase flow [J]. Journal of Ballistics, 2007, 19(4): 9–12. DOI: 10.3969/j.issn.1004-499X.2007.04.003. [5] 廖振强, 邱明. 自动武器气体动力学[M]. 北京: 国防工业出版社, 2015. [6] 陈杨, 廖振强, 刘国鑫, 等. 两种拉瓦尔喷管减后坐结构效能对比分析 [J]. 弹道学报, 2008, 20(4): 88–91.CHEN Y, LIAO Z Q, LIU G X, et al. Performance comparison of two recoilless structures with Laval nozzles [J]. Journal of Ballistics, 2008, 20(4): 88–91. [7] CHENG C, WANG C, ZHANG X B. A prediction method for the performance of a low-recoil gun with front nozzle [J]. Defence Technology, 2019, 15(5): 703–712. DOI: 10.1016/j.dt.2019.06.005. [8] 张帆, 廖振强, 刘国鑫, 等. 喷孔前置式膨胀波枪炮发射过程数值仿真与分析 [J]. 系统仿真学报, 2008, 20(18): 5032–5034, 5039.ZHANG F, LIAO Z Q, LIU G X, et al. Numerical simulation and analysis on front orifice rarefaction wave gun propulsion [J]. Journal of System Simulation, 2008, 20(18): 5032–5034, 5039. [9] 肖俊波, 杨国来, 李洪强, 等. 身管武器时延式喷管减后坐动力学建模仿真 [J]. 兵工学报, 2017, 38(10): 1909–1917. DOI: 10.3969/j.issn.1000-1093.2017.10.005.XIAO J B, YANG G L, LI H Q, et al. Dynamics modeling and simulation of recoil reduction of automatic weapon by time-delay nozzle device [J]. Acta Armamentarii, 2017, 38(10): 1909–1917. DOI: 10.3969/j.issn.1000-1093.2017.10.005. [10] 翁春生, 王浩. 计算内弹道学[M]. 北京: 国防工业出版社, 2006. [11] NUSSBAUM J, HELLUY P, HÉRARD J M, et al. Numerical simulations of gas-particle flows with combustion [J]. Flow, Turbulence and Combustion, 2006, 76(4): 403–417. DOI: 10.1007/s10494-006-9028-4. [12] RASHAD M M, ZHANG X B, EL SADEK H, et al. Two-phase flow interior ballistics model of naval large caliber guided projectile gun system [J]. Applied Mechanics and Materials, 2013, 465−466: 592–596. DOI: 10.4028/www.scientific.net/AMM.465-466.592. [13] JANG J S, OH S H, ROH T S. Development of three-dimensional numerical model for combustion-flow in interior ballistics [J]. Journal of Mechanical Science and Technology, 2016, 30(4): 1631–1637. DOI: 10.1007/s12206-016-0319-y. [14] MONREAL-GONZÁLEZ G, OTÓN-MARTÍNEZ R A, VELASCO F J S, et al. One-dimensional modelling of internal ballistics [J]. Journal of Energetic Materials, 2017, 35(4): 397–420. DOI: 10.1080/07370652.2016.1265613. [15] MENSHOV I S, NEMTSEV M Y, SEMENOV I V. Numerical modeling of wave processes accompanying combustion of inhomogeneously distributed composite propellant [J]. Computational Mathematics and Mathematical Physics, 2019, 59(9): 1528–1541. DOI: 10.1134/S0965542519090148. [16] HU C B, ZHANG X B. A Riemann problem based coupling method for predicting the combustion of propellant in a gun launching process [J]. Propellants, Explosives, Pyrotechnics, 2019, 44(6): 751–758. DOI: 10.1002/prep.201800293. [17] CHENG C, ZHANG X B. Numerical investigation of two-phase reactive flow with two moving boundaries in a two-stage combustion system [J]. Applied Thermal Engineering, 2019, 156: 422–431. DOI: 10.1016/j.applthermaleng.2019.04.061. [18] CAO R D, ZHANG X B. Design optimization for a launching system with novel structure [J]. Defence Technology, 2019, 15(5): 680–689. DOI: 10.1016/j.dt.2019.08.005. [19] 张帆. 膨胀波火炮发射原理及其在常规结构枪炮中的应用[D]. 南京: 南京理工大学, 2008: 103−106. [20] 陈杨. 喷管气流反推减后坐武器系统关键技术研究[D]. 南京: 南京理工大学, 2010: 10−11. [21] 王颖泽. 基于膨胀波发射技术的火炮内弹道与发射动力学分析[D]. 南京: 南京理工大学, 2009: 57−58. -
点击查看大图
计量
- 文章访问数: 468
- HTML全文浏览量: 267
- PDF下载量: 47
- 被引次数: 0