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Journal of Propulsion Technology
1001-4055
2005 Issue 1
Study on outer loading about interweaved fibers composite case by experiments
WANG Ming-jian;HE Hong-qing;YU Jian
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page:93-96
Preparation of waterborne polyurethane latex and study on its cladding of RDX
LU Ming;CHEN Yu;LUO Yun-jun;TAN Hui-min
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page:89-92
Increasing the burning rate of nitramine modified double-base propellant with ACP
LIAO Lin-quan;QIN Guang-ming;LI Xiao-jiang;WAN Guo-qiang;LI Jun-qiang
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page:84-88
Application of improved FSQP algorithm to turbofan engine multivariable nonlinear control
QI Xue-feng;FAN Ding
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page:58-61,67
Adaptive inverse control based on filtered-ε LMS algorithm for aeroengines
HUANG Jin-quan;HU Wen-fei
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page:54-57
Fixed-order robust control for a engine based on Homotopy algorithm
SUN Hu-guo;LI Hua-cong;FAN Si-qi
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page:50-53
Modified method of establishing the state space model of aeroengine
ZHENG Tie-jun;WANG Xi;LUO Xiu-qin;LI Qi-han
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page:46-49
Control of separation losses on turbine blade with low Reynolds number
Qiao Wei-yang;WANG Zhan-xue;YI Jin-bao
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page:42-45
Numerical analysis of non-equilibrium scale effects in hypersonic nozzle
ZENG Ming;LIN Zhen-bin;FENG Hai-tao;QU Zhang-hua
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page:38-41
Experimental investigation on caret inlet's total pressure distortion controlled by vortex break fence
ZHONG Yi-cheng;YU Shao-zhi;CHEN Xiao
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page:34-37
Modeling of N2O monopropellant thruster pre-heating
HUO Xue-liang;WEI Di;LI Lu-ming
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page:80-83
Preliminary experimental investigation on detonation wave ignition technique
Guo Hong-jie;LIANG Guo-zhu;MA Bin;ZHANG Zhen-peng
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page:76-79
Temperature measurement of arcjet plume with emission spectrum
SHEN Yan;ZHAO WEN-HUA;SHI Yong;CHEN Li-ming
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page:72-75
Numerical solution for electromagnetic field within arcjet thruster flow region
XIAO Ying-chao
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page:68-71,96
Mechanism of fuel self-fit control in pulse detonation engine
FAN Yu-xin;WANG Jia-hua;LI Jian-zhong;ZHANG Yi-ning;ZHANG Jing-Zhou
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page:62-67
Effect of porosity of holes array on cooling effectiveness of effusion cooling
HU Ya-ping;JI Hong-hu
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page:28-33
A method for discharge coefficients computation of film cooling holes on blade surface of turbine cascade
XIANG An-ding;LIU Song-ling;ZHU Hui-ren
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page:24-27
Numerical simulation of isolation rotor internal flowfield in axial flow compressor
SHANG Xu-sheng;CAI Yuan-hu;HOU Le-yi;CHEN Yu-chun
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page:20-23
Application of control technology based on Venturi in kerosene fueled scramjet
DING Meng;WU Ji-ping;LIANG Jian-han;LIU Wei-dong;WANG Zhen-guo
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page:16-19
Numerical investigation on combustion flow of a kerosene-fueled scramjet with 3D cavity(Ⅱ) Preliminary investigation on fuel/air mixing and flame stabilization enhanced by 3D cavity
HUANG Sheng-hong;Xu Sheng-li;LIU Xiao-yong
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page:10-15
Numerical simulations of flowfields in a scramjet combustor with a strut
WANG Xiao-dong;SONG Wen-yan
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page:5-9
Numerical and experimental studies for temperature field of monopropellant hydrazine thruster
WANG Chao;ZHOU Xu-dong;TANG Jian-hua;SUN Lei;HUA Wei;YANG Jian-hui;YANG Ling-qin
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page:1-4