| Citation: | WANG Meng-jie, Eriqitai, WANG Qiang. Transient response of startup process for fluidic control vector nozzle[J]. Journal of Aerospace Power, 2012, 27(10): 2364-2370.
|
| [1] |
吴雄.固体发动机燃气二次喷射理论与试验研究 . 长沙:国防科技大学,2007. WU Xiong.Theoretical and experimental research on Hot gas secondary injection for solid rocket motor .Changsha:National University of Defence Technology,2007.(in Chinese)
|
| [2] |
Deere K A.Summary of fluidic thrust vectoring research conducted at NASA Langley Research Center .AIAA-2003-3800,2003.
|
| [3] |
Erdem E,Albayrak K,Tinaztepe H T,et al. Numerical investigation of flowfield inside a conical rocket nozzle in the presence of transverse injection .AIAA-2008-359,2008.
|
| [4] |
Miller D N,Catt J A.Conceptual development of fixed-geometry nozzles using fluidic injection for throat area control .AIAA-1995-2603,1995.
|
| [5] |
Deere K A,PAB3D simulations of a nozzle with fluidic injection for yaw thrust-vector control .AIAA-1998-3254,1998.
|
| [6] |
Patrick J Y,Daniel N M,Ginn K B,et al.Demonstration of fluidic throat skewing for thrust vectoring in structrally fixed nozzles .GT-2000-0013,2000.
|
| [7] |
Anderson C J,Giuliano V J,Wing D J.Investigation of hybrid fluidic mechanical thrust vectoring forfixed exit exhaust nozzles .AIAA-97-36559,1997.
|
| [8] |
Sadiq M U.Performance analysis and flowfield characterization of secondary injection thrust vector control (SITVC) for a 2DCD nozzle .California:University of Southern California,2007.
|
| [9] |
李杰.自适应多用途发动机与变循环发动机[J].航空制造技术,2011(21):38-41. LI Jie.Adaptive versatile engine and varible cycle engine[J].Aeronautical Manufacturing Technology,2011(21):38-41.(in Chinese)
|
| [10] |
ANSYS Incorporate.ANSYS CFX-solver theory guide release 13.0[M].Pennsylvania:ANSYS Incorporate,2010.
|
| [11] |
DelBello T,Georgiadis N,Yoder D,et al.Computational study of axisymmetric off-design nozzle flows .NASA/TM-2003-212876,2003.
|
| [12] |
Saha S,Chakraborty D.Numerical exploration of starting process in supersonic nozzle[J].Aeronautical Journal,2007,111(1115):51-58.
|
| [13] |
Amann H O.Experimental study of the starting process in reflection nozzle[J].Physics of Fluids,1969,12(5):150-153.
|
| [14] |
Dickmann D A.On the near field mean flow structure of transverse jets issuing into a supersonic freestream .Arlington:The University of Texas,2007.
|
| [15] |
Ostlund J,Damgaard T,Frey M,et al.Side-load phenomena in highly overexpa-nded rocket nozzles .AIAA-2001-3684,2001.
|
DownLoad: