固相颗粒在C1xb固体火箭发动机中的运动规律

doi:10.12382/bgxb.2021.0136

兵工学报 ›› 2022, Vol. 43 ›› Issue (3): 489-502.doi: 10.12382/bgxb.2021.0136

固相颗粒在C1xb固体火箭发动机中的运动规律

顾兴鹏¹，李军伟¹，乔文生²，武胜²，韩磊¹，汪琪¹，王宁飞¹

（1.北京理工大学宇航学院，北京 100081； 2.内蒙古动力机械研究所，内蒙古呼和浩特 010010）

上线日期:2022-04-07
作者简介:顾兴鹏（1993—），男，博士研究生。E-mail:1975564047@qq.com
基金资助:
国防基础科研项目（JCKY2019204B020）

Motion Trajectory of Solid Particles in C1xb Solid Rocket Motor

GU Xingpeng¹， LI Junwei¹， QIAO Wensheng²， WU Sheng²， HAN Lei¹， WANG Qi¹， WANG Ningfei¹

(1.School of Aerospace Engineering，Beijing Institute of Technology，Beijing 100081，China；2.Inner Mongolia Power Machinery Research Institute，Hohhot 010010，Inner Mongolia，China)

Online:2022-04-07

摘要/Abstract

摘要： 基于C1xb型固体火箭发动机内流场，对发动机内的凝相颗粒进行受力分析，并获得固相颗粒运动过程中的速度和加速度。建立二维颗粒运动轨迹模型，并在该模型下获得固相颗粒在发动机内的运动空间分布规律。研究颗粒注入位置、粒径及发动机转速对凝相颗粒运动的影响规律。结果表明：从含铝丁羟推进剂上游端和下游端表面离开的颗粒，有着较大概率与壁面发生碰撞；较大尺寸粒径颗粒会增大颗粒运动过程中与壁面发生碰撞的概率；旋转相对于轴向过载更能对颗粒在发动机内的空间分布产生影响。所得固体发动机内两相流流动规律及颗粒沉积分布沉积规律，可为提高固体发动机性能提供理论指导。

关键词: C1xb固体火箭发动机, 固相颗粒, 颗粒受力, 颗粒运动轨迹, 颗粒粒径

Abstract: The force of condensed-phase particles in C1xb solid rocket motor (SRM) is analyzed based on internal flow field of motor. The velocity and acceleration of particle at different moments are obtained，and a two-dimensional particle motion trajectory model is established. Based on this model，the spatial distribution rule of particles in SRM is obtained. On this basis，the effects of motor rotation，initial position of particle and particle size on the movement of condensed-phase particles are studied. Results show that the particles leaving the upstream and downstream surfaces of aluminized hydroxyl-terminated-polybutadiene propellant have a greater probability of colliding with inner wall. Larger size particles increase the probability of collision with inner wall during particle movement. Rotation has more influence on spatial distribution of particles in motor in comparison with axial overload.

Key words: C1xbsolidrocketmotor, condensed-phaseparticle, forceonparticle, particlemotiontrajectory, particlesize

中图分类号:

TJ763

顾兴鹏，李军伟，乔文生，武胜，韩磊，汪琪，王宁飞. 固相颗粒在C1xb固体火箭发动机中的运动规律[J]. 兵工学报, 2022, 43(3): 489-502.

GU Xingpeng， LI Junwei， QIAO Wensheng， WU Sheng， HAN Lei， WANG Qi， WANG Ningfei. Motion Trajectory of Solid Particles in C1xb Solid Rocket Motor[J]. Acta Armamentarii, 2022, 43(3): 489-502.

参考文献［1］

［1］

晁侃，王健儒，陆贺建.残余限燃环对大型分段式固体火箭发动机凝相沉积的影响[J].固体火箭技术，2021，44(1):9-15.CHAO K，WANG J R，LU H J. Influence of residual annular insulator on slag accumulation in segmented SRM[J].Journal of Solid Rocket Technology，2021，44(1):9-15.(in Chinese)[2］晁侃，王健儒，陆贺建. 喷管斜置对固体发动机燃烧室熔渣沉积影响数值分析[J]. 固体火箭技术，2013，36(5):594-597.CHAO K，WANG J R，LU H J.Numerical analysis on influence of sloped nozzle on slag accumulation in SRM[J].Journal of Solid Rocket Technology，2013，36(5):594-597.(in Chinese)[3］ SALITA M.Deficiencies and requirements in modeling of slag generation in solid rocket motors[J].Journal of Propulsion & Power，1995，11(1):10-23.[4］ SALITA M.Predicted slag deposition histories in eight solid rocket motors using the CFD model ‘EVT’[C]∥Proceedings of the 31st Joint Propulsion Conference and Exhibit.San Diego，CA，US:AIAA，1995.[5］刘佩进，李强.非壅塞固冲发动机补燃室内凝相颗粒运动规律研究[J].固体火箭技术，2007，30(1):17-20.LIU P J，LI Q.Study on collision law of condensed particles in secondary combustor of unchoked solid ducted motor[J].Journal of Solid Rocket Technology，2007，30(1):17-20.(in Chinese) [6］胡建新，夏志勋，刘君，等.非壅塞火箭冲压发动机补燃室两相流数值模拟[J]. 推进技术，2004，25(3):193-195，240.HU J X，XIA Z X，LIU J，et al.Two phase flow combustion modeling of secondary combustion chamber in a unchoked ducted rocket[J].Journal of Propulsion Technology，2004，25(3):193-195，240.(in Chinese) [7］袁亚雄，杨均匀.内弹道颗粒轨道模型及数值计算[J].弹道学报，1995，7(4):7-11.YUAN Y X，YANG J Y.The interior ballistic particle trajectory model and its numerical calculation[J].Journal of Ballistics，1995，7(4):7-11.(in Chinese) [8］程诚，张小兵.内弹道两相流三维并行数值模拟[J].兵工学报，2019，40(4):769-776.CHENG C，ZHANG X B.Parallel numerical simulation on three-dimensional two-phase flow of interior ballistic trajectory[J].Acta Armamentarii，2019，40(4):769-776.(in Chinese) [9］程诚，张小兵.某制导炮弹二维两相流内弹道性能分析与数值模拟研究[J].兵工学报，2015，36(1):58-63.CHENG C，ZHANG X B. Two-dimensional numerical simulation on two-phase flow interior ballistic performance of a guided projectile[J].Acta Armamentarii，2015，36(1):58-63.(in Chinese)[10］杨文婧，匡亮，褚开维，等.基于CFD-DEM算法的固体火箭发动机气-固两相流模拟[J].推进技术，2019，40(7):1546-1553.YANG W J，KUANG L，CHU K W, et al. Study of gas-particle flow in solid rocket motor based on computational fluid method-discrete element method[J].Journal of Propulsion Technology，2019，40(7): 1546-1553.(in Chinese)[11］ BERNARDINI M，CIMINI M，STELLA F，et al.Large-eddy simulation of vortex shedding and pressure oscillations in solid rocket motors[J].AIAA Journal，2020，58(10):1-11.[12］ DUPAYS J，PREVOST M，TARRIN P，et al.Effects of particulate phase on vortex shedding driven oscillations in solid rocket motors[C]∥Proceedings of the 32nd Joint Propulsion Conference and Exhibit. Lake Buena Vista，FL，US：AIAA，1996.[13］ HALOULAKOS V E.Slag mass accumulation in spinning solid rocket motors[J]. Journal of Propulsion and Power， 1991，7(1): 14-21.[14］ MORSI S A，ALEXANDER A J.An investigation of particle trajectories in two-phase flow systems[J].Journal of Fluid Mechanics，1972，55(2):193-208.[15］李桢.横向过载下固体火箭发动机工作过程研究[D].长沙：国防科学技术大学，2005.LI Z. Investigation of the work process of solid rocket motor under lateral overload [D].Changsha：National University of Defense Technology，2005.(in Chinese)[16］崔立堃.过载状态下固体火箭发动机内流场数值计算[J].战术导弹技术，2017(3):98-103.CUI L K. Numerical simulation of flow field in the solid rocket motor under overload conditions[J].Tactical Missile Technology，2017(3):98-103.(in Chinese)

固相颗粒在C1xb固体火箭发动机中的运动规律

Motion Trajectory of Solid Particles in C1xb Solid Rocket Motor

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献［1］

相关文章 0

编辑推荐

Metrics

本文评价

固相颗粒在C1xb固体火箭发动机中的运动规律

Motion Trajectory of Solid Particles in C1xb Solid Rocket Motor

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献 ［1］

相关文章 0

编辑推荐

Metrics

本文评价

参考文献［1］