[1]王学智,刘少伟,王 伟,等.倾斜发射导弹燃气流对发射箱前盖冲击数值仿真[J].弹箭与制导学报,2017,37(5):95-98.[doi:10.15892/j.cnki.djzdxb.2017.05.001]
 WANG Xuezhi,LIU Shaowei,WANG Wei,et al.Numerical Simulation about the Impact of Inclined Launching Missile Jet Flow on the Front Covers of Launch Canisters[J].,2017,37(5):95-98.[doi:10.15892/j.cnki.djzdxb.2017.05.001]
点击复制

倾斜发射导弹燃气流对发射箱前盖冲击数值仿真

参考文献/References:

[1] 苗瑞生. 发射气体动力学 [M]. 北京: 国防工业出版社, 2006: 318-323.
[2] 马艳丽, 姜毅, 郝继光, 等. 固体发动机燃气射流对发射平台冲击效应研究 [J]. 固体火箭技术, 2010, 33(4): 373-376.
[3] 姚昌仁, 张波. 火箭导弹发射装置 [M]. 北京: 北京理工大学出版社, 1998: 132-134.
[4] 王伟, 王学智, 刘少伟. 导弹燃气射流对多联装发射箱前盖影响数值模拟 [J]. 计算机测量与控制, 2013, 21(10): 2747-2749.
[5] 王汉平, 吴菊华. 基于CFD的潜射导弹筒口压力场预测 [J]. 弹道学报, 2011, 20(4): 73-76.
[6] 姜毅, 郝继光, 傅德彬. 导弹发射过程三维非定常数值模拟 [J]. 兵工学报, 2008, 29(8): 911-915.
[7] 杨风波, 马大为, 任杰, 等. 新型车载同心筒流场机理与热环境研究 [J]. 固体火箭技术, 2014, 37(3): 301-306.

相似文献/References:

[1]刘 群,姜 毅,郝继光.燃气射流对发射车天线影响分析[J].弹箭与制导学报,2007,(3):187.
 LIU Qun,JIANG Yi,HAO Ji-guang.The Affection Analysis of Jet Flow to Launch Vehicle[J].,2007,(5):187.
[2]陈树伟,毕世华,陈 阵,等.某导弹发射箱箱盖开盖角度优化研究[J].弹箭与制导学报,2007,(4):201.
 CHEN Shu-wei,BI Shi-hua,CHEN Zhen,et al.Research on Optimization of Opening Angle for Lid of Some Missile Launching Container[J].,2007,(5):201.
[3]周 帆,姜 毅,张学文,等.火箭发动机射流复杂噪声测量数据时频分析[J].弹箭与制导学报,2012,(3):145.
 ZHOU Fan,JIANG Yi,ZHANG Xuewen,et al.Time-frequency Analysis of Test Data from Complex Noise of Rocket Engine Jet[J].,2012,(5):145.
[4]周 强,李 强,刘 杰.集束武器射击方式对弹丸姿态的影响分析[J].弹箭与制导学报,2013,33(3):146.
 ZHOU Qiang,LI Qiang,LIU Jie.The Analysis of Influence on Projectile Based on Firing Method of Cluster Weapon[J].,2013,33(5):146.
[5]王 芳,龚军锋.CFD/CSD与机弹分离的耦合模拟技术[J].弹箭与制导学报,2013,33(6):193.
 WANG Fang,GONG Junfeng.CFD/CSD and Missile Separation Integrative Simulation Method[J].,2013,33(5):193.
[6]刘小军,傅德彬,王新星.弹筒间隙及壁面条件对火箭弹燃气射流的影响分析[J].弹箭与制导学报,2014,34(3):119.
 LIU Xiaojun,FU Debin,WANG Xinxing.Effects of Small Gaps and Wall Thermal Conditions on Exhausted Gas Jet for Rockets[J].,2014,34(5):119.
[7]张 赢,刘超峰.导弹自翻转的超大攻角非定常气动特性研究[J].弹箭与制导学报,2015,35(5):112.[doi:10.15892/j.cnki.djzdxb.2015.05.028]
 ZHANG Ying,LIU Chaofeng.Unsteady Aerodynamics Characteristics on Self-turning of Missile at Extra-wide Angle-of-attack[J].,2015,35(5):112.[doi:10.15892/j.cnki.djzdxb.2015.05.028]
[8]郑无计,张登成,张艳华,等.基于动网格对内装式空射火箭分离过程的仿真[J].弹箭与制导学报,2015,35(5):119.[doi:10.15892/j.cnki.djzdxb.2015.05.029]
 ZHENG Wuji,ZHANG Dengcheng,ZHANG Yanhua,et al.Simulation of Internally Carried Air-launched Launch Vehicle Separation from Aircraft by Dynamic Grid[J].,2015,35(5):119.[doi:10.15892/j.cnki.djzdxb.2015.05.029]
[9]白涛涛,孙振华,张泽远.三维双燃速装药固体火箭发动机工作过程研究[J].弹箭与制导学报,2015,35(6):91.[doi:10.15892/j.cnki.djzdxb.2015.06.023]
 BAI Taotao,SUN Zhenhua,ZHANG Zeyuan.Study of Work Process in Three-dimension Dual-burning Rate Grain Solid Rocket Motor[J].,2015,35(5):91.[doi:10.15892/j.cnki.djzdxb.2015.06.023]
[10]曹军伟,何国强,单睿子,等.高温燃气射流对固冲发动机二次燃烧效率影响研究[J].弹箭与制导学报,2016,36(2):87.[doi:10.15892/j.cnki.djzdxb.2016.02.021]
 CAO Junwei,HE Guoqiang,SHAN Ruizi,et al.Research on Effect of High Temperature Gas Injection on Secondary Combustion Efficiency of Solid Rocket Ramjet[J].,2016,36(5):87.[doi:10.15892/j.cnki.djzdxb.2016.02.021]
[11]王 伟,王学智,刘少伟.倾斜发射导弹燃气流场数值模拟[J].弹箭与制导学报,2013,33(4):127.
 WANG Wei,WANG Xuezhi,LIU Shaowei.Numerical Simulation of Jet Flow for Incline-launched Missile[J].,2013,33(5):127.

备注/Memo

作者简介:王学智(1965-),男,辽宁沈阳人,教授,博士,研究方向:兵器发射理论与技术。

更新日期/Last Update:

2017-08-15