1001-4055
2002 Issue 5
..............page:424-424
..............page:414-414
..............page:386-386
Effects of plug contour simplification and truncation on linear plug nozzle
wang chang hui ; liu yu ; dai wu ye
wang chang hui ; liu yu ; dai wu ye
..............page:438-440
Optimization design of two dimensional scramjet nozzle based on N-S equations
chen bing ; xu xu ; cai guo zuo
chen bing ; xu xu ; cai guo zuo
..............page:433-437
Experimental mensuration and analysis of aerospike nozzles and bell nozzle performance
wang yi bai ; liu yu ; zuo li zi
wang yi bai ; liu yu ; zuo li zi
..............page:428-432
Numerical simulation of two-phase flow for a tail-pipe nozzle
dan lin peng ; zhang zhen peng ; he da jun ; zuo jun feng ; li jia yu
dan lin peng ; zhang zhen peng ; he da jun ; zuo jun feng ; li jia yu
..............page:425-427
Computation of ablation of thermal-protection layer in solid rocket ramjet combustor
sun bing ; liu xiao yong ; lin xiao shu ; cai guo zuo
sun bing ; liu xiao yong ; lin xiao shu ; cai guo zuo
..............page:375-378
Numerical calculation on low power arcjet thrusters
tang hai bin ; liu yu ; zhang zheng ke
tang hai bin ; liu yu ; zhang zheng ke
..............page:370-374
Numerical simulation of slag accumulation for solid rocket motors
xiang hong jun ; fang guo yao
xiang hong jun ; fang guo yao
..............page:366-369,374
Method for calculation model establishment in liquid propellant rocket engine numerical simulation
li jia wen ; zhang li hui ; zhang zhen peng
li jia wen ; zhang li hui ; zhang zhen peng
..............page:363-365
Integrated design and optimization method for scramjet
xu da jun ; sun bing ; xu xu ; wang yuan guang ; chen bing
xu da jun ; sun bing ; xu xu ; wang yuan guang ; chen bing
..............page:360-362
Fundamental study of fault monitoring and diagnostic technology of liquid rocket engine
zhang zhen peng
zhang zhen peng
..............page:353-359
Cold-flow tests on tile-shaped aerospike nozzle
dai wu ye ; liu yu ; ma bin
dai wu ye ; liu yu ; ma bin
..............page:420-424
Altitude performance prediction of perigee kick motor nozzle
liang guo zhu ; zhang zhong qin ; an lian ; liu ze ming
liang guo zhu ; zhang zhong qin ; an lian ; liu ze ming
..............page:415-419
Experimental study of flow coefficient and spray characteristics of spatter platelet injector
yang li jun ; hu ze bao ; cai guo zuo ; zhang zhen peng
yang li jun ; hu ze bao ; cai guo zuo ; zhang zhen peng
..............page:410-414
Computation based on the Simons model for vacuum plume
zhang jian hua ; cai guo zuo
zhang jian hua ; cai guo zuo
..............page:406-409
Research on gas dynamic resonance igniters of multi-thruster
tong xiao yan ; zhang guo zhou ; ma bin ; liang guo zhu ; song ya na
tong xiao yan ; zhang guo zhou ; ma bin ; liang guo zhu ; song ya na
..............page:402-405
Numerical simulation on combustion of hydrogen/hydrocarbon in supersonic airstream
xu xu ; cai guo zuo
xu xu ; cai guo zuo
..............page:398-401
Numerical and experimental investigation on supersonic secondary combustion
ma chao zuo ; xu xu ; cai guo zuo
ma chao zuo ; xu xu ; cai guo zuo
..............page:394-397
Numerical simulation of C-H-O-N system liquid rocket engine nozzle flow
cai guo zuo ; ma chao zuo ; zhang hua zhao
cai guo zuo ; ma chao zuo ; zhang hua zhao
..............page:391-393
Numerical simulation of flow in the absorption chamber of laser propulsion rocket engine
zheng li ming ; zhu ding qiang ; xu xu ; cai guo zuo
zheng li ming ; zhu ding qiang ; xu xu ; cai guo zuo
..............page:387-390
Research of rotor attacking angle for liquid rocket reaction turbine
zhang guo zhou ; yu nan jia ; wei mo
zhang guo zhou ; yu nan jia ; wei mo
..............page:383-386
Computation of combustion in hybrid rocket motor using a boundary layer theory
tian hui ; cai guo zuo ; wang hui yu ; zhang zhen peng
tian hui ; cai guo zuo ; wang hui yu ; zhang zhen peng
..............page:379-382