[1] |
Kowal H J.Advances in thrust vectoring and the application of flow-control technology[J].Canadian Aeronautics and Space Journal,2002,48(2):145-151.
|
[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-2003-3802,2003.
|
[3] |
张群锋,吕志咏,王戈一,等.轴对称射流矢量喷管的试验和数值模拟[J].推进技术,2004,25(2):139-143. ZHANG Qunfeng,LÜ 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)
|
[4] |
金捷,雷金春,廖华琳,等.激波诱导轴对称气动矢量喷管壁面静压分布的试验[J].航空动力学报,2007,22(10):1700-1703. JIN Jie,LEI Jinchun,LIAO Hualin,et al.Experimental investigation of wall static pressure distributions of shock induced axisymmetric fluidic vectoring nozzle[J].Journal of Aerospace Power,2007,22(10):1700-1703.(in Chinese)
|
[5] |
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,2008,29(2):187-193. WANG Zhanxue,LI Zhijie.Effect of aerodynamic parameters of main and secondary flow path on thrust vectoring[J].Journal of Propulsion Technology,2008,29(2):187-193.(in Chinese)
|
[6] |
Miller D N,Yagle P J,Hamstra J W.Fluidic throat skewing for thrust vectoring in fixed-geometry nozzles [R].AIAA 99-0365,1999.
|
[7] |
Williams R G,Vittal B R.Fluidic thrust vectoring and throat control exhaust nozzle [R].AIAA-2002-4060,2002.
|
[8] |
王庆伟,刘波,王如根.二元喷管气动喉道控制的数值模拟[J].航空学报,2009,30(2):226-231. WANG Qingwei,LIU BO,WANG Rugen.Numerical simulation of two-dimensional nozzle using fluidic injection for throat area control[J].Acta Aeronautica et Astronautica Sinica,2009,30(2):226-231.(in Chinese)
|
[9] |
Deere K A,Berrier B L,Flamm J D,et al.Computational study of fluidic thrust vectoring using separation control in a nozzle [R].AIAA-2003-3803,2003.
|
[10] |
Deere K A,Berrier B L,Flamm J D.A computational study of a new dual-throat fluidic thrust vectoring nozzle concept [R].AIAA-2005-3502,2005.
|
[11] |
Flamm J D,Deere K A.Experimental study of a dual-throat fluidic thrust-vectoring nozzle concept [R].AIAA-2005-3503,2005.
|
[12] |
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[J].航空动力学报,2007,22(10):1679-1684. TAN Huijun,CHEN Zhi.A computational study of 2-D dual-throat fluidic thrust-vectoring nozzles[J].Journal of Propulsion Technology,2007,22(10):1678-1684.(in Chinese)
|
[13] |
Flamm J D.Experimental study of a nozzle using fluidic counterflow for thrust vectoring[R].AIAA 98-3255,1998.
|
[14] |
Lim M,Kim H D,Setoguchi T.Studies on thrust vector control using a fluidic counter-flow concept [R].AIAA-2006-5204,2006.
|
[15] |
汪明生,杨建军.逆流推力矢量喷管基本流动特征的数值研究[J].航空学报,2008,29(4):769-775. WANG Mingsheng,YANG Jianjun.Numerical research on basic flow characteristics of counterflow thrust vectoring nozzle[J].Acta Aeronautica et Astronautica Sinica,2008,29(4):769-775.(in Chinese)
|
[16] |
周慧晨,谭慧俊,孙姝,等.一种矢量增强型双喉道射流推力矢量喷管的数值模拟[J].航空动力学报,2010,25(9):2070-2076. ZHOU Huichen,TAN Huijun,SUN Shu,et al.Numerical investigation of a vector-enhanced dual-throat thrust-vectoring nozzle[J].Journal of Propulsion Technology,2010,25(9):2070-2076.(in Chinese)
|