[1] 边金尧, 徐松林, 钱海鹰. 同心发射筒研究现状[J]. 舰船科学技术, 2012, 34(11):1-5,51. BIAN J Y, XU S L, QIAN H Y. Research progress of concentric launching canister[J]. Ship Science and Technology, 2012, 34(11): 1-5,51. (in Chinese) [2] 于勇, 母云涛. 新型变截面同心筒发射装置及其热环境气动原理研究[J]. 宇航学报, 2013, 34(9): 1281-1287. YU Y,MU Y T. Configuration and gas dynamics analysis for a new variable cross-section concentric canister launcher [J]. Journal of Astronautics, 2013, 34(9): 1281-1287. (in Chinese) [3] 苗佩云, 袁曾凤. 同心筒式发射时筒内流场机理及内外筒间隙的影响[J]. 战术导弹技术, 2006, 29(1): 8-13. MIAO P Y, YUAN Z F. The effect of flow mechanism and annular sizes on concentric canister launcher[J]. Tactical Missile Technology January, 2006, 29(1): 8-13. (in Chinese) [4] 袁绪龙, 王亚东, 刘维. 同心筒水下发射内弹道建模与仿真研究[J]. 弹道学报, 2013, 25(2): 48-53. YUAN X L, WANG Y D, LIU W. Interior ballistic modeling and simulation of underwater launched missile using concentric canister launcher [J]. Journal of Ballistics, 2013, 25(2): 48-53. (in Chinese) [5] 于勇, 母云涛. 同心筒式发射装置附加弹射力影响因素分析[J]. 航空动力学报, 2014, 29(4):980-986. YU Y, MU Y T. Influential factors analysis to additional ejection force in concentric canister launcher [J]. Journal of Aerospace Power, 2014, 29(4): 980-986. (in Chinese) [6] 郑榆淇,傅德彬,王新星,等. 异形截面同心筒燃气流动特性数值研究[J]. 固体火箭技术, 2016, 39(5): 729-734. ZHENG Y Q, FU D B, WANG X X, et al. Numerical investigation of exhaust flows for missile launching in an irregular section concentric canister launcher [J]. Journal of Solid Rocket Technology, 2016, 39(5): 729-734. (in Chinese) [7] 马艳丽, 姜毅, 王伟臣,等. 湿式独立自排导垂直发射技术研究[J]. 导弹与航天运载技术, 2011(2): 29-33,51. MA Y L, JIANG Y, WANG W C, et al. Research on the wet-type concentric canister launcher [J]. Missiles and Space Vehicles, 2011(2): 29-33,51. (in Chinese) [8] 马艳丽, 姜毅, 王伟臣,等. 同心筒发射过程燃气射流冲击效应研究[J]. 固体火箭技术, 2011, 34(2): 140-145. MA Y L, JIANG Y, WANG W C, et al. Study on impact effect of combustion gas jet during concentric canister launching process [J]. Journal of Solid Rocket Technology, 2011, 34(2): 140-145. (in Chinese) [9] 傅德彬, 姜毅, 陈建伟,等. 同心筒自力发射燃气排导优化设计[J]. 弹箭与制导学报, 2004, 24(3): 42-45. FU D B, JIANG Y, CHEN J W, et al. Optimization design for concentric canister launcher combustion gas exhaust [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2004, 24(3): 42-45. (in Chinese) [10] 刘琦, 傅德彬, 姜毅,等. 同心筒发射装置燃气射流流场非定常数值模拟[J]. 弹箭与制导学报, 2004, 24(3): 161-163. LIU Q, FU D B, JIANG Y, et al. Unsteady simulation of jet flow in concentric canister launcher [J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2004, 24(3): 161-163. (in Chinese) [11] 谭大成. 弹射内弹道学[M]. 北京: 北京理工大学出版社, 2015:84-102. TAN D C. Interior ballistics of catapults[M]. Beijing: Beijing Institute of Technology Press, 2015: 84-102. (in Chinese) [12] 唐垚,姜毅,王成德,等. 多级活塞缸式燃气弹射内弹道的研究[J]. 固体火箭技术, 2018, 41(4): 524-531. TANG Y, JIANG Y, WANG C D, et al. Research on the internal trajectory of multi-stage piston cylinder gas ejection [J]. Journal of Solid Rocket Technology, 2018, 41(4): 524-531. (in Chinese) [13] SHIH T H, LIOU W W, SHABBIR A, et al. A new κ-ε eddy viscosity model for high reynolds number turbulent flows[J]. Computers Fluids, 1995, 24(3): 227-238. [14] LAMONT P J. The impingement of underexpanded, axisymmetric jets on perpendicular and inclined flat plates[J]. Journal of Fluid Mechanics, 2006, 100(3): 471-511. [15] CINNELLA P, TONG X L, WU J X, et al. Comprehensive numerical study of jet-flow impingement over flat plates[J]. Journal of Spacecraft & Rockets, 2002, 39(3): 357-366. [16] 杨桦,姜毅,陶倩楠, 等.复燃现象对导流器排导流场影响数值分析[J].固体火箭技术,2020,43(3):393-399. YANG H, JIANG Y, TAO Q N, et al. Numerical analysis of afterburning's influence on division flow field with deflector [J]. Journal of Solid Rocket Technology, 2020, 43(3): 393-399. (in Chinese) [17] 郝继光, 姜毅, 韩书永, 等. 一种新的动网格更新技术及其应用[J]. 弹道学报, 2007, 19(2): 88-92. HAO J G, JIANG Y, HAN S Y, et al. A New dynamic mesh update method and its apllications [J]. Journal of Ballistics, 2007, 19(2): 88-92. (in Chinese)
第43卷第7期2022 年7月 兵工学报ACTA ARMAMENTARII Vol.43No.7Jul.2022
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