[1] 冯金富, 杨松涛, 刘文杰. 战斗机武器内埋关键技术综述 [J]. 飞航导弹, 2010(7): 71-74. FENG J F, YANGS T, LIU W J. Summary of key technologies for embedding fighter weapons [J]. Aerodynamic Missile Journal, 2010 (7): 71-74. (in Chinese) [2] 常超, 丁海河. 内埋弹射武器机弹安全分离技术综述 [J]. 现代防御技术, 2012, 40(5): 67-74. CHANG C, DING H H.Review on missile store safety separation technology of embedded ejection weapons [J]. Modern Defence Technology, 2012, 40(5): 67-74. (in Chinese) [3] 刘乐卿, 张全, 刘浩. F/A-22隐身战机武器投放仿真与试验技术 [J]. 兵器装备工程学报, 2016, 37(10): 8-12. LIU L Q, ZHANG Q, LIU H.Weapon separation modeling simulation and test of F/A-22 stealth fighter [J]. Journal of Ordnance Equipment Engineering, 2016, 37(10): 8-12. (in Chinese) [4] LIJEWSKI L E, SUHS N E. Time-accurate computational fluid dynamics approach to transonic store separation trajectory prediction [J]. Journal of Aircraft, 1994, 31(4): 886-891. [5] PREWITT N C, BELK D M, SHYY W. Parallel computing of overset grids for aerodynamic problems with moving objects [J]. Progress in Aerospace Sciences, 2000, 36(2): 117-172. [6] SNYDER D, KOUTSAVDIS E, ANTTONEN J. Transonic store separation using unstructured CFD with dynamic meshing [C]∥Proceedings of the 33rd AIAA Fluid Dynamics Conference And Exhibit. Orlando, FL, US: AIAA, 2003: 3919. [7] KOOMULLIL R, CHENG G, SONI B, et al. Moving-body simulations using overset framework with rigid body dynamics [J]. Mathematics & Computers in Simulation, 2008, 78(5/6): 618-626. [8] PREWITT N C, BELK D M, MAPLE R C. Multiple-body trajectory calculations using the Beggar Code [J]. Journal of Aircraft, 2012, 36(5): 802-808. [9] OSMAN A A, ALY A M, KHALIL E E, et al. Numerical analysis of an external store separation from an airplane [C]∥Proceedings of AIAA Modeling and Simulation Technologies Conference. San Diego, CA, US: AIAA, 2016: 2143. [10] BAYSAL O, FOULADI K, LEUNG W, et al. Interference flows past cylinder-fin-sting-cavity assemblies [J]. Journal of Aircraft, 1992, 29(2): 194-202. [11] FOULADI K, BAYSAL O. Viscous simulation method for unsteady flows past multicomponent configurations [J]. Journal of Fluids Engineering, 1992, 114(2): 161-169. [12] LAWSON S J, BARAKOS G N. Review of numerical simulations for high-speed, turbulent cavity flows [J]. Progress in Aerospace Sciences, 2011, 47(3): 186-216. [13] ANANDHANARAYANAN K, ARORA K, SHAH V, et al. Se-paration dynamics of air-to-air missile using a grid-free Euler solver [J]. Journal of Aircraft, 2013, 50(3): 725-731. [14] JOHNSON M W. A novel Cartesian CFD cut cell approach [J]. Computers & Fluids, 2013, 79: 105-119. [15] MERRICK J D. Influence of Mach number and dynamic pressure on cavity tones and freedrop trajectories [D]. Wright-Patterson AFB, OH, US: Air Force Institute of Technology, 2014. [16] 沈琼, 余雄庆. 无人机机载导弹分离轨迹的数值仿真 [J]. 弹箭与制导学报, 2009, 29(5): 99-102. SHEN Q, YU X Q. Numerical simulation of trajectory of missile separated from UAV [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2009, 29(5): 99-102. (in Chinese) [17] 李杰, 纪秀玲, 孙超. 不同释放力组合下小型外挂物投放的数值模拟 [J]. 北京理工大学学报, 2010, 30(3): 23-26. LI J, JI X L, SUN C. Computational studies of light stores separation with various ejector forces [J]. Transactions of Beijing Institute of Technology, 2010, 30(3): 23-26. (in Chinese) [18] 段旭鹏, 常兴华, 张来平. 基于动态混合网格的多体分离数值模拟方法 [J]. 空气动力学学报, 2011, 29(4): 447-452. DUAN X P, CHANG X H, ZHANG L P. A CFD-and-6DOF-coupled solver for multiple moving object problems based on dynamic hybrid grids [J]. Acta Aerodynamica Sinica, 2011, 29(4): 447-452. (in Chinese) [19] 唐上钦, 黄长强, 翁兴伟. 考虑气动干扰的导弹内埋式发射弹道研究 [J]. 弹箭与制导学报, 2013, 33(3): 138-142. TANG S Q, HUANG C Q, WENG X W. The Study ontrajectory of missile separating from cavity with aerodynamic interference considered [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013, 33(3): 138-142. (in Chinese) [20] 曾铮, 王刚, 叶正寅. RBF整体网格变形技术与多体轨迹仿真 [J]. 空气动力学学报, 2015, 33(2): 170-177. ZENG Z, WANG G, YE Z Y. Enhanced RBF mesh deformation method and multi-body trajectory simulation [J]. Acta Aerodynamica Sinica, 2015, 33(2): 170-177. (in Chinese) [21] 郭少杰, 王斌, 周培培, 等. 隐身无人机内埋武器分离安全性数值研究 [J]. 机械科学与技术, 2017, 36(增刊1): 1-7. GUO S J, WANG B, ZHOU P P, et al. Numerical analysis for internal weapon separation performance of a stealth UAV [J]. Mechanical Science and Technology for Aerospace Engineering, 2017, 36(S1): 1-7. (in Chinese) [22] 范晶晶, 张海瑞, 管飞, 等. 外挂式导弹机弹分离气动干扰特性研究 [J]. 国防科技大学学报, 2018, 40(2): 13-21. FAN J J, ZHANG H R, GUAN F, et al. Studies of aerodynamic interference characteristics for external store separation [J]. Journal of National University of Defense Technology, 2018, 40(2): 13-21. (in Chinese) [23] 朱世权, 李海元, 陈志华, 等. 攻角对空空导弹与载机分离过程的影响 [J]. 工程力学, 2018, 35(9): 248-256. ZHU S Q, LI H Y, CHEN Z H, et al. Influences of angles of attack during the separation of an air-to-air missile from the aircraft [J]. Engineering Mechanics, 2018, 35(9): 248-256. (in Chinese) [24] 雷娟棉, 牛健平, 王锁柱, 等. 初始分离条件对航弹与载机分离安全性影响的数值模拟研究 [J]. 兵工学报, 2016, 37(2): 357-366. LEI J M, NIU J P, WANG S Z, et al. Numerical simulation about the effect of initial separation condition on safety of aerial bomb separated from an aircraft [J]. Acta Armamentarii, 2016, 37(2): 357-366. (in Chinese) [25] 朱收涛, 曹林平, 封普文, 等. 平飞时内埋导弹弹射分离仿真与研究 [J]. 电光与控制, 2012, 19(9): 67-71,75. ZHU S T, CAO L P, FENG P W, et al.Simulation of missile separation from internal weapon bay [J]. Electronics Optics & Control, 2012, 19(9): 67-71,75. (in Chinese) [26] 郭亮, 王纯, 叶斌, 等. 采用流动控制的超声速内埋物投放特性研究 [J]. 航空学报, 2015, 36(6): 1752-1761. GUO L, WANG C, YE B, et al. Investigation on characteristics of store release from internal bay in supersonic flow under flow control [J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(6): 1752-1761. (in Chinese) [27] 闫盼盼, 张群峰, 金明, 等. 内埋武器发射参数对下落轨迹的影响 [J]. 工程力学, 2018, 35(1): 246-256. YAN P P, ZHANG Q F, JIN M, et al. Effects of launching parameters on the separation trajectory of internal weapons [J]. Engineering Mechanics, 2018, 35(1): 246-256. (in Chinese) [28] 艾邦成, 宋威, 董垒, 等. 内埋武器机弹分离相容性的研究进展综述 [J/OL]. 航空学报, 2020. [2020-03-27]. http:∥kns.cnki.net/kcms/detail/11.1929.V. 20200223.2144.004.html. AI B C, SONG W, DONG L, et al. Review on aircraft-store se-paration compatibility for the internal weapons [J/OL]. Acta Aeronautica et Astronautica Sinica, 2020. [2020-03-27]. http:∥kns.cnki.net/kcms/detail/ 11.1929.V.20200223.2144.004.html. (in Chinese) [29] HEIM E R. CFD wing/pylon/finned store mutual interference wind tunnel experiment:AEDC-TSR-91-P4 [R]. Arnold AFB, TN, US: Arnold Engineering Development Center, 1991.
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