Journal of Propulsion Technology 2002 Issue 6 tui jin ji shu di 23 juan (2002 nian ) zhu zhe suo yin

tui jin ji shu di 23 juan (2002 nian ) zhu zhe suo yin

..............page:A4-A6

tui jin ji shu di 23 juan (2002 nian ) zhu ti fen lei suo yin

..............page:A1-A3

zhi xie 2002 nian du shen gao zhuan jia

..............page:517-517

gao xing neng rl60 fa dong ji bu jian re shi che

..............page:508-508

Numerical study for turbulent flow inside rotating disc cavities
zhang jing zhou ; ji hong hu

..............page:472-476

Study for the mathematical model of supersonic inlet
lu yan ; fan si qi ; ma hui min

..............page:468-471

Design and experimental investigation on a new grooved treated casing with forward-step in an axial-flow compressor
wu yan hui ; zhu jun qiang ; liu zhi wei

..............page:463-467

Numerical simulation of effects of leading edge on the performance of inlet
wang xiao dong ; le jia ling

..............page:460-462

Distilling character parameter method investigation for space aerocraft propulsion system using improving time-series method
zhang chun liang ; zhang zhen peng ; zhu gang

..............page:457-459,467

Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine
qi shao jun ; cai yuan hu ; wang zhan xue ; ge ai xue

..............page:453-456

Transient heat conduction and temperature field characteristics of a propellant
liu qing cai ; zhou yan huang ; yu yong gang

..............page:448-452

Numerical simulation of effects of heat transfer on the transient performance of gas turbine engines
wu hu ; lian xiao chun

..............page:445-447

Computation of three dimensional nozzle flow field with fluidic injection
wang qiang ; fu yao ming ; e ri qi tai

..............page:441-444

Effect of pretreatment of cotton cellulose by steam explosion on properties of nitrocellulose
shao zi qiang ; xu kun ; wang fei jun ; wang ji xun ; zuo fan geng

..............page:525-528

Ammonium nitrate surface modification through spraying and drying technology
zhang jie ; yang rong jie ; liu yun fei ; tan hui min

..............page:521-524

Combustion characteristics of boron-based fuel-rich propellant at low pressure
hu song qi ; li zuo zuo ; wang ying hong ; wei qing

..............page:518-520

Thermal cracking and catalytic cracking of endothermic hydrocarbon fuel on mixture catalyst
zhang bo ; wang bin cheng ; lin rui sen

..............page:513-517

Research on the constitutive equations of HTPB composite solid propellant with damage and aging
yang jian hong ; yu mao hong ; hou gen liang ; wang you jun ; lv qiu juan

..............page:509-512

Resonace regulation of microwave plasma thruster under the low signal
yang zuo ; han xian wei ; he hong qing ; mao gen wang

..............page:505-508

Method of characteristics for vacuum plume simulation
chen bing ; cai guo zuo

..............page:500-504

Influence of injection angle on the thermodynamic aspects of endwall film-cooling in a turbine cascade
liu gao wen ; liu song ling

..............page:496-499,512

Nonlinear acoustic wave in combustors
huang yu hui ; wang zhen guo ; zhou jin

..............page:492-495

Real-time intelligent diagnosis system for missile propellant filling equipment
zhang zuo ; zhang yu xiang ; huang xian xiang

..............page:489-491

Application of global variable structure control method in aeroengine control system
fan ding ; zhao qing rong

..............page:485-488

Numerical simulation of internal flow field of swirl nozzle
zhou li xin ; zhang hui qiang ; lei fan pei ; huang chong xi ; chen jian hua

..............page:480-484

Effect of suction hole on heat transfer characteristic of internal passage
zuo yun ; zhu hui ren ; xu du chun ; liu song ling

..............page:477-479,508