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Journal of Rocket Propulsion
1672-9374
2011 Issue 1
Implementation of FEA program for vibration characteristics of bladed disk system
CHEN Hong-yu;TIAN Ai-mei
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page:40-45
Automatic control technology of tank pressure based on pressure transmitter and intelligent instrument
LI Chang-min
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page:57-60
Heat transfer analysis of platelet transpiration cooling thrust chamber
HUANG Chun-tao;SUN Bing
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page:17-21,39
Calculation of jet stream flow field of reverse jet engine during landing with dynamic mesh technology
ZHAO Chun-mei;ZHU Cheng-min
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page:28-33
Stress analysis of filament-wound composite gas cylinders with metal liner
YAN Fei
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page:46-50,56
Numerical simulation of combustion chamber flow field for solid-liquid rocket ramjet
HAN Hong-wei;LIU Yu;REN Jun-xue
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page:22-27
Design and simulation research of seal configuration in flashboard-type normally open pyro-valve
ZHANG Xiao-dong;LI Lu-lu;LIU Shan;TANG Mei-fang
..............
page:51-56
Analysis of error factor in vibration measurement
CHEN Hai-feng;ZHANG Shao-bo;LIU Ying-yuan
..............
page:61-64
Research on power system of heavy launch vehicle in China
TAN Yong-hua
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page:1-6
New method of experimental study on supercritical characteristic of single droplet fuel
ZHANG Meng-zheng;XU Sheng-li
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page:7-16,45
Numerical analysis of instable cavitation phenomenon in 2D blade cascade of inducer
TANG Fei;LI Jia-wen
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page:34-39