| Citation: | GUO Chang-chao, YU Xin-yu, LI Bo, XIE Kan, WEI Zhi-jun, WANG Ning-fei. Experiment on thrust adjustment characteristics of fluidic nozzle throat[J]. Journal of Aerospace Power, 2015, 30(4): 999-1007. doi: 10.13224/j.cnki.jasp.2015.04.029 |
| [1] |
Martin A I.The aerodynamic variable nozzle[J].Journal of Aeronautical Sciences, 1957, 24(5):357-362.
|
| [2] |
McArdle J G.Internal characteristics and performance of an aerodynamically controlled, variable discharge convergent nozzle[R].NACA TN4312, 1958.
|
| [3] |
McAulay J E.Cold-air investigation of three variable throat area convergent-divergent nozzles[R].NASA TM X-42, 1959.
|
| [4] |
Blaszak J J, Fahrenholz F E.Rocket thrust control by gas injection[R].Cambridge:Massachusetts Institute of Technology, Naval Supersonic Laboratory, Technical Report 430, 1960.
|
| [5] |
Gunter F L, Fahrenholz F E.Final report on a study of rocket thrust control by gas injection[R].Cambridge:Massachusetts Institute of Technology, Naval Supersonic Laboratory, Technical Report 448, 1961.
|
| [6] |
Zumwalt G W, Jackomis W N.Aerodynamic throat nozzle for thrust magnitude control of solid fuel rockets[R].New York:American Rocket Society, 1962.
|
| [7] |
谢侃, 刘宇, 王一白.固体火箭发动机气动喉部的两相流数值模拟[J].推进技术, 2010, 31(1):56-60. XIE Kan, LIU Yu, WANG Yibai.Simulation for the two-phase flow aerodynamic throat of solid rocket motors[J].Journal of Propulsion Technology, 2010, 31(1):56-60.(in Chinese)
|
| [8] |
Miller D N, Catt J A.Conceptual development of fixed geometry nozzles using fluidic injection for throat-area control[R].AIAA 95-2603, 1995.
|
| [9] |
Richard J Z.Thrust vector control by liquid injection for solid propellant rockets[R].AIAA 75-1225, 1975.
|
| [10] |
Green C J.Liquid injection thrust vector control[J].AIAA Journal, 1963, 1(3):573-578.
|
| [11] |
Deer K A.Summary of fluidic thrust vectoring research conducted at NASA Langley Research Center[R].AIAA-2003-3800, 2003.
|
| [12] |
Ali A, Rodriguez C, Andrew N, et al.Combination of fluidic thrust modulation and vectoring in a 2D nozzle[R].AIAA-2012-3780, 2012.
|
| [13] |
Damiel Y, Miller N, Patrick J Y, et al.Fluidic throat skewing for thrust vectoring in fixed-geometry nozzles[R].AIAA 99-0365, 1999.
|
| [14] |
Baruzzini D, Domel N, Daniel M.Pulsed injection flow control for throttling in supersonic nozzles:a computational fluid dynamics design study[R].AIAA-2007-4215, 2007.
|
| [15] |
谢侃, 刘宇, 王一白.固体火箭发动机流体喉部非定常过程[J].推进技术, 2011, 32(1):103-108. XIE Kan, LIU Yu, WANG Yibai.Unsteady process of aerodynamic throat for solid rocket motor[J].Journal of Propulsion Technology, 2011, 32(1):103-108.(in Chinese)
|
| [16] |
张建华, 谢侃.流体喉部喷管二次流矢量控制方案[J].北京航空航天大学学报, 2012, 38(3):309-313. ZHANG Jianhua, XIE Kan.Secondary flow thrust vector control study for fluidic throat nozzle[J].Journal of Beijing University of Aeronautics and Astronautics, 2012, 38(3):309-313.(in Chinese)
|
| [17] |
甘舜仙.六分力试验台静态误差分析与调整[J].推进技术, 1987(6):73-81. GAN Shunxian.Static error analysis and adjustment of six-component force test stand[J].Journal of Propulsion Technology, 1987(6):73-81.(in Chinese)
|
| [18] |
刘宏璇.六分力测试方法研究[D].南京:南京理工大学, 2008.
|