[1] Wang Y X. Axial-symmetric vectoring exhaust nozzle for jet-thrust-aircraft. Beijing: National Defense Industry Press, 2006: 282. (in Chinese) 王玉新. 喷气发动机轴对称推力矢量喷管. 北京: 国防工业出版社, 2006: 282. [2] Ashley S. Thrust vectoring: a new angle to air superiority. Mechanical Engineering Journal, 1995, 17(1): 58-64. [3] Kowal H J. Advances in thrust vectoring and the application of flow-control technology. Canadian Aeronautics and Space Journal, 2002, 48(2): 145-151. [4] Deere K A. Summary of fluidic thrust vectoring research conducted at NASA Langley research center. AIAA-2003-3800, 2003. [5] Flamm J D, Deere K A. Design enhancements of the two-dimensional, dual throat fluidic thrust vectoring nozzle concept. AIAA-2006-3701, 2006. [6] Tan H J, Chen Z. A computational study of 2-D dual-throat fluidic thrust-vectoring nozzles. Journal of Aerospace Power, 2007, 22(10): 1678-1684. (in Chinese) 谭慧俊, 陈智. 二元双喉道射流推力矢量喷管的数值模拟研究. 航空动力学报, 2007, 22(10): 1678-1684. [7] Strykowski P J. Counterflow thrust vectoring of supersonic jets. AIAA Journal, 1996, 34(11): 2306-2314. [8] Yang J J, Wang M S. Numerical research on basic flow characteristics of counterflow thrust vectoring nozzle. Acta Aeronautica et Astronautica Sinica, 2008, 29(4):769-775. (in Chinese) 杨建军, 汪明生. 逆流推力矢量喷管基本流动特征的数值研究. 航空学报, 2008, 29(4): 769-775. [9] Smith B L, Glezer A. Jet vectoring using synthetic jets. Journal of Fluid Mechanics, 2002, 458(1): 1-34. [10] Luo Z B, Xia Z X. Advances in synthetic jet technology and applications in flow control. Advances in Mechanics, 2005, 35(2): 221-234. (in Chinese) 罗振兵, 夏智勋. 合成射流技术及其在流动控制中应用的进展. 力学进展, 2005, 35(2): 221-234. [11] Zhang P F, Wang J J, Feng L H. Review on the zero-net-mass-flux jet and the application in separation flow control. Science in China E: Technological Sciences, 2008, 51(9): 1315-1344. [12] Gu Y S, Li B B, Chen K M. Cross flow transfer characteristics of a new beveled synthetic jet actuator and its applications to boundary layer control. Acta Aeronautica et Astronautica Sinica, 2010, 31(2): 231-237. (in Chinese) 顾蕴松, 李斌斌, 程克明. 斜出口合成射流激励器横流输运特性及边界层控制. 航空学报, 2010, 31(2): 231-237. [13] Rumsey C L, Sanetrik M D. Efficiency and accuracy of time-accurate turbulent Navier-Stokes computations. AIAA-1995-1835, 1995. [14] Menter F. Zonal two equation turbulence models for aerodynamic flows. AIAA-1993-2906, 1993. [15] Tang Z G, Liu G. Effects of turbulence models on the numerical simulation of nozzle jets. Acta Aerodynamica Sinica, 2010, 28(2): 188-195. [16] Eggers J M. Velocity profiles and eddy viscosity distributions downstream of a Mach 2.22 nozzle exhausting to quiescent air. NASA TN D-3601, 1966. [17] Tong B G, Yin X Y. Gas dynamics. Beijing: High Education Press, 1990: 415. (in Chinese) 童秉纲, 尹协远. 气体动力学. 北京: 高等教育出版社, 1990: 415. |