[1] Deere K A, Berrier B L, Flamm J D.A Computational Study of a New Dual Throat Fluidic Thrust Vectoring Nozzle Concept[R].AIAA 2005-3502. [2] Waithe K A, Deere K A.Experimental and Computational Investigation of Multiple Injection Ports in a Convergent-Divergent Nozzle for Fluidic Thrust Vectoring[R].AIAA 2003-3802. [3] Deere K A.Summary of Fluidic Thrust Vectoring Research Conducted at NASA Langley Research Center[R].AIAA 2003-3800. [4] Deere K A.Computational Investigation of the Aerodynamic Effects on Fluidic Thrust Vectoring[R].AIAA 2000-3598. [5] Hamed A, Laskowski G.A Parametric Study of Slot Injection Thrust Vectoring in a 2DCD Nozzle[R].AIAA 1997-3154. [6] Gogoi A, Siddesha H, Vivek K G.Navier Stokes Computation on Nozzle with Secondary Jet Injection[R].AIAA 2005-4847. [7] Eric Gamble, Dan Haid.Improving Off-Design Nozzle Performance Using Fluidic Injection[R].AIAA 2004-1206. [8] Dan Haid, Eric Gamble.Nozzle Aftbody Drag Reduction Using Fluidics[R].AIAA 2004-3921. [9] 王占学, 李志杰.喷管气动参数对推力矢量影响的数值模拟[J].推进技术,8,9(2).(WANG Zhan-xue, LI Zhi-jie.Effect of Aerodynamic Parameters of Main and Secondary Flow Path on Thrust Vectoring [J].Journal of Propulsion Technology, 8,9(2).) [10] 李志杰, 王占学, 蔡元虎.二次流喷射位置对流体推力矢量喷管气动性能影响的数值模拟[J].航空动力学报,8,3(9). [11] 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,2,3(6).(WANG Qiang, FU Yao-ming, Eriqitai.Computation of There Dimensional Nozzle Flow Field with Fluidic Injection [J].Journal of Propulsion Technology, 2,3(6).) [12] 王占学, 王玉男, 李志杰,等.基于激波控制的流体推力矢量喷管试验[J].推进技术,0,1(6).(WANG Zhan-xue, WANG Yu-nan, LI Zhi-jie, et al.Experiment on Fluidic Thrust-vectoring Nozzle Based on Shock Control Concept [J].Journal of Propulsion Technology, 0,1(6).)
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