[1] 陶如意,张丁山,赵润翔,等.超声速子母弹分离干扰流场数值模拟与试验研究[J].空气动力学学报,2010,28(3):310-315. TAO R Y, ZHANG D S, ZHAO R X, et al. Numerical and experimental study of interference flow field on separation of supersonic cluster munition [J]. Journal of Aerodynamics, 2010, 28(3): 310-315. (in Chinese) [2] 黄凯.子母弹抛撒过程射流流场对子弹运动的影响[D].南京:南京理工大学,2015:8-11. HUANG K. The jet flow field of submunition dispersal process and its influence on the projectile motion [D]. Nanjing: Nanjing University of Science and Technology, 2015: 8-11. (in Chinese) [3] 林靖明,安复兴,于德滨.母弹激波对子弹气动特性影响的研究[J].兵工学报,2000,21(4):334-337. LIN J M, AN F X, YU D B. Shock effects from the dispenser on the aerodynamic characteristics of submunitions [J]. Acta Armamentarii, 2000, 21(4): 334-337. (in Chinese) [4] STALMAEH C J, ROMERO S. Dynamie tests of a submissile dispensing system in a supersonic wind tunnel [C]∥Proceedings of the 11th AIAA Aerodynamic Testing Conference. Reno,NV, US: AIAA, 1980: 0452. [5] RIZK M, JOLLY B. Aerodynamic simulation of bodies with moving components using CFD overset gird methods [C]∥Proceedings of the 44th AIAA Aerospace Sciences Meeting & Exhibit 2006. Reno, NV, US: AIAA, 2006: 1252. [6] BHANGE N P,SEN A,GHOSH A K.Technique to improve precision of kinetic energy projectiles through motion study[C]∥Proceedings of Atmospheric Flight Mechanics Conference. Chicago, IL, US: AIAA,2009:5720. [7] WOODEN P A, BROOKS W,JUBARAJ S B.Calibrating CFD predictions for use in multiple store separation analysis [C]∥Proceedings of the 36th AIAA Aerospace Sciences Meeting & Exhibit. Reno, NV, US: AIAA, 1998:0754. [8] PERKINS S C, DILLENIUS M F E. Supersonic submunition aerodynamics during dispense [C]∥Proceedings of the 26th Aerospace Sciences Meeting. Reno, NV, US: AIAA, 1988:0335. [9] CAVALLO P, LEE R, HOSANGADI A. Simulation of weapons bay separation flow fields using unstructured grids [C]∥Proceedings of the 19th Applied Aerodynamics Conference. Norfolk, VA, US: AIAA, 1999:33412.
[10] 郭正.包含运动边界的多体非定常流场数值模拟方法研究[D].长沙:国防科学技术大学,2002: 4-20. GUO Z. Study on numerical simulation of multibody unsteady flow field with motion boundary [D]. Changsha: National University of Defense Technology, 2002: 4-20. (in Chinese) [11] 张玉东,纪楚群.子母弹分离非定常气动特性数值模拟[C]∥近代空气动力学研讨会论文集. 北京:中国宇航出版社,2005:333-338. ZHANG Y D, JI C Q. Numerical simulation of the unsteady aerodynamic characteristics of the submunition separation[C]∥Proceedings of Modern Aerodynamics Symposium. Beijing:China Astonautic Publishing House, 2005: 333-338. (in Chinese) [12] 王金龙,王浩,陶如意,等.子母弹不同舱段分离流场特性及运动特性研究[J].空气动力学报,2016,34(4):490-496. WANG J L, WANG H, TAO R Y, et al. Themoment characteristics analysis of interference flow field on the separation of multi-bay cluster munition[J]. Acta Aerodynamica Sinica,2016,34(4): 490-496. (in Chinese) [13] 陶如意,张丁山,赵润祥,等.超声速子母弹分离干扰流场数值模拟与试验研究[J].空气动力学学报,2010,28(3):310-315. TAO R Y, ZHANG D S, ZHAO R X, et al. Numerical and experimental study of interference flow field on separation of supersonic cluster munition[J].Acta Aerodynamica Sinica, 2010,28(3): 310-315.(in Chinese) [14] 赵承庆,姜毅. 气体射流动力学[M].北京:北京理工大学出版社,1998:30-35. ZHAO C Q,JIANG Y. The kinetics of gas jet [M]. Beijing: Beijing Institute of Technology Press, 1998: 30-35.(in Chinese) [15] 陈永辉,王强,朴明波.湍流模型的发展及其研究现状[J].能源与环境,2009 (2):4-6. CHEN Y H, WANG Q, PU M B. Development and research status of turbulence model [J]. Energy and Environment, 2009 (2): 4-6. (in Chinese) [16] WU Q, ZHAO Q J, WANG Q. Highly-efficient aerodynamic option design of rotor airfoil using viscous adjoint method [J]. Transactions of Nanjing University of Aeronautics & Astronautics, 2017, 34(2):134-142. [17] 贾沛然,沈为异.弹道导弹弹道学[M].长沙:国防科技大学出版社,1980. JIA P R, SHEN W Y. Ballistic missile ballistics [M]. Changsha: National University of Defense Technology Press, 1980. (in Chinese) [18] POPE S P. Turbulent flows [M]. Cambridge, UK: Cambridge University Press, 2000. [19] THOMAS J P, DOWELL E H, HALL K C. Nonlinear inviscid aerodynamic effects on transonic divergence, flutter, and limit-cycle oscillations[J].AIAA Journal, 2002, 40(4):638-646.
第40卷第1期 2019 年1月兵工学报ACTA ARMAMENTARIIVol.40No.1Jan.2019
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