Citation: | Zhang Yongsheng, Wang Yankui, Yu Xiaowei, et al. Design of secondary-divergent vectoring nozzle based on secondary fluidic injection[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(03): 261-264. (in Chinese) |
[1] Hamed A, Laskowski G. A parametric study of slot injection thrust vectoring in a 2DCD nozzle . AIAA-97-3154, 1997 [2] Deere K A. Computational investigation of the aerodynamic effects on fluidic thrust vectoring . AIAA -2000-3598, 2000 [3] 王强,付尧明,额日其太.流体注入的轴对称矢量喷管三维流场计算[J].推进技术,2002,23(6):441-444 Wang Qiang, Fu Yaoming, Eri Qitai. Computation of three dimensional nozzle flow field with fluidic injection [J]. Journal of Propulsion Technology, 2002, 23(6):441-444(in Chinese) [4] 张群峰,吕志咏,王戈一,等.轴对称射流矢量喷管的试验与数值模拟[J].推进技术,2004,25(2):139-143 Zhang Qunfeng, Lu Zhiyong, Wang Geyi, et al. Numerical simulation of an axisymmetric fluidic vectoring nozzle [J]. Journal of Propulsion Technology, 2004, 25(2):139-143(in Chinese) [5] 邓远灏,钟梓鹏,宋文艳.收敛 - 扩张喷管中运用次流推力矢量控制技术的计算研究[J].固体火箭技术,2004,28(1):29-32 Deng Yuanhao, Zhong Zipeng, Song Wenyan. Computational investigation of secondary flow thrust vector control technology used in a convergent-divergen nozzle [J]. Journal of Solid Rocket Technology, 2004, 28(1):29-32(in Chinese) [6] 乔渭阳,蔡元虎.基于次流喷射控制推力矢量喷管的实验及数值研究[J].航空动力学报,2001,16(3):273-278 Qiao Weiyang, Cai Yuanhu. A study on the two-dimensional thrust vectoring nozzle with secondary flow injection [J]. Journal of Aerospace Power, 2001, 16(3):273-278(in Chinese)
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