[1] Rainey G. Progress on the launch-vehicle buffeting problem [J]. Journal of Spacecraft and Rockets, 1965, 2(3): 289-299. [2] 唐伟, 江定武, 桂业伟, 等. 旋成体导弹头部母线线性的选择问题研究[J]. 空气动力学学报, 2010, 28(2): 218-221. TANG Wei, JIANG Ding-wu, GUI Ye-wei, et al. Study on generatrix curvetypes of axis-symmetric missiles [J]. Acta Aerodynamica Sinica, 2010, 28(2): 218-221. (in Chinese) [3] Perkins E W, Jorgensen L H. Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 3.67, A52H28[R]. US:NACA, 1952. [4] Stoney Jr WE. Transonic drag measurements of eight-body nose shapes, L53K17[R]. US: NACA, 1954. [5] Perkins E W, Jorgensen L H, Sommer S C. Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 7.4, A52H28[R]. US:NACA, 1958. [6] Lee J W, Min B Y, Byun Y H, et al. Multi-point nose shape optimization of space launcher using response surface method[C]∥40th AIAA Aerospace Sciences Meeting & Exhibit. Reno, NV, US:AIAA, 2002: 2002-0106. [7] Gusman M R, Housman J A, Kiris C C. Adjoint-based adaptive meshing in a shape trade study for rocket ascent[C]∥6th International Conference on Computational Fluid Dynamics (ICCFD6). St Petersburg, Russia:Springer, 2010: 391-400. [8] Engblom W A. Numerical simulation of Titan IVB transonic buffet environment[J]. Journal of Spacecraft and Rockets, 2003, 40(5): 648-656. [9] Tsutsumi S, Takaki R, Takama Y, et al. Hybrid LES/RANS simulations of transonic flowfield around a rocket fairing[C]∥30th AIAA Applied Aerodynamics Conference. New Orleans, LA, US:AIAA, 2012: 2012-2900.
[10] Brauckmann G J, Streett C L, Kleb W L, et al. Computational and experimental unsteady pressures for alternate SLS booster nose shapes[C]∥AIAA, Aerospace Sciences Meeting. Kissimmee, FL, US: AIAA, 2015: 2015-0559. [11] 赵瑞, 荣吉利, 任方, 等. 火箭整流罩外气动噪声环境的大涡模拟研究[J].宇航学报, 2015, 36(9) : 988-994. ZHAO Rui, RONG Ji-li, REN Fang, et al. Large eddy simulation of the aeroacoustic environment of a rocket fairing[J]. Journal of Astronautics, 2015, 36(9): 988-994. (in Chinese)
[12] 赵瑞, 荣吉利, 任方, 等. 一种改进的跨声速旋成体壁面脉动压力预测方法[J]. 宇航学报, 2016, 37(10):1179-1184. ZHAO Rui, RONG Ji-li, REN Fang, et al. Improvement of the fluctuating pressure empirical functions around rotated aircraft at transonic Mach numbers[J]. Journal of Astronautics, 2016, 37(10): 1179-1184. (in Chinese) [13] Matsukawa Y. Implicit large eddy simulation of a supersonic flat-plate boundary layer flow by weighted compact nonlinear scheme[J]. International Journal of Computational Fluid Dynamic, 2011, 25(2): 47-57. [14] Shen Y Q, Zha G C, Chen X Y. High order conservative differencing for viscous terms and the application to vortex-induced vibration flows [J]. Journal of Computational Physics, 2008, 228(22): 8283-8300. [15] Dubuc L, Cantariti F, Woodgate M, et al. Solution of unsteady Euler equations using an implicit dual time step method [J]. AIAA Journal, 1998, 36(8): 1417-1424. [16] Jameson A, Yoon S. Lower-upper implicit schemes with multiple grids for the Euler equations[J]. AIAA Journal, 1987, 25(7): 929-935. [17] Plotkin K J, Robertson J E. Prediction of space shuttle fluctuating pressure environment, including rocket plume effects, NASA-CR-124347[R]. WA, US: NASA, 1973.
第38卷 第5期 2017 年5月兵工学报ACTA ARMAMENTARIIVol.38No.5May2017
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