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Journal of Propulsion Technology
1001-4055
2002 Issue 4
Development and expectation of performance simulation in aviation engine
huang jia zuo ; feng guo tai
..............page:346-351
Experimental investigation on the combustion behavior of aluminium-magnesium based fuel-rich propellant
liu pei jin ; chen jing ping ; li zuo zuo
..............page:342-345
Thermal decomposition characteristics of AP/KP/GAP fuel-rich propellant
zhu hui ; zhang zuo ; wu pai ; wang chun hua ; zhao feng qi ; yuan chao ; yin cui mei ; qiu gang
..............page:339-341
Stability analysis of the crack in solid rocket motor grain
meng shang yang ; tang guo jin ; lei yong jun
..............page:335-338
Image analysis system for goodness of mixing of solid propellants
he ji yu ; chen zuo ; dai jian wu ; wang bo zuo ; chen shao zhen
..............page:332-334
Effect of nanometer-sized lanthanum oxide on catalyzing decomposition of cyclotrimethylenetriamine
xu hong ; liu jian hong ; chen pei ; zhao feng qi ; tian de yu
..............page:329-331
Effects of blade positive curving on aerodynamic performance of compressor cascades
wang hui she ; zhong jing jun ; wang zhong qi ; liu yan ming ; yuan xin
..............page:321-324
Experimental study of near field rocket noise in exhausted flow field
xu qiang ; liao guang zuo ; li jun ; cao cong yong
..............page:318-320
Numerical approach for turbine blade with trailing edge ejection
wang yan gang ; mei yun huan ; liu bo ; cao zhi peng
..............page:315-317
Investigation of flow in isolator of hypersonic inlet
zhang yuan ; wang cheng peng ; yang jian jun ; xu jing lei
..............page:311-314
Influence of the clapboard on electromagnetic field and resonant frequency within the resonant cavity of microwave plasma thruster
tang jin lan ; he hong qing ; han xian wei ; mao gen wang ; yang zuo ; wan wei
..............page:303-306
Flow analysis and validation of rocket ejector mode for rocket based combined cycle
wang guo hui ; cai ti min ; he guo qiang ; liu pei jin ; huang sheng hong ; qin fei
..............page:298-302
Numerical and experimental study of tile-shaped aerospike nozzles
dai wu ye ; liu yu ; ma bin ; cheng xian chen
..............page:292-297
Angle properties of the primary nozzle of plug nozzle
zuo li zi ; liu yu ; wang yi bai
..............page:287-291
Effect of temperature profile at entrance on flow-fields of nozzle
wang xiao dong ; le jia ling
..............page:283-286
Flow performance analysis in an axial compressor rotor with splitter
yan ming ; chen zuo zhang
..............page:280-282
Effection of structural parameters of tripropellant injector on twophase flow in the mixer
tian zhang fu ; li qing lian ; shen chi bing ; zhou jin ; wang zhen guo
..............page:276-279
Adiabatic film cooling effectiveness downstream of primary jet in combustion chamber
lin yu zhen ; yuan zuo xiang ; liu gao en ; xie chuan hua
..............page:273-275,331
Experimental study of import pass ways for model tripropellant injector
li qing lian ; tian zhang fu ; wang zhen guo
..............page:268-272
Numerical simulation on the stage-separation flow fields of the multi-stage rocket
liu jun ; xu chun guang ; guo zheng
..............page:265-267