Journal of Propulsion Technology 2003 Issue 3 zeng cheng dao dan xuan yong wo pen ( shan ) fa dong ji

zeng cheng dao dan xuan yong wo pen ( shan ) fa dong ji

..............page:227-227

FEM creep damage study for nickel-base single crystal structure under multiaxial stress conditions
yue zhu feng ; lv zhen zhou ; yang zhi guo ; yin ze yong

..............page:285-288

Mechanism of the deteriorated processability in boron-fuel-rich HTPB propellants
zheng jian ; wang ai hua ; pang ai min

..............page:282-284,288

Measurement on catalytic cracking heat sink of endothermic hydrocarbon fuels
he long ; guo yong sheng ; wang bin cheng ; lin rui sen

..............page:278-281

Experimental studies for plasmas ignition of solid propellants
xie yu shu ; zhang xiao bing ; yuan ya xiong ; zhou yue

..............page:275-277

Identification of turbojet ignition based on neural network with a prior
yu da ren ; niu jun ; he bao cheng ; shi xin xing

..............page:272-274

Overview of flame holders of cavities in supersonic combustion
liu ou zi ; hu yu li ; cai yuan hu ; liu jing hua ; ling wen hui

..............page:265-271

Combustion flow in ejecting mode of strutjet engine (Ⅱ) Effects of secondary combustion and configuration
huang sheng hong ; he hong qing ; he guo qiang

..............page:259-264

Experimental investigation of microwave plasma thruster in vacuum
han xian wei ; he hong qing ; mao gen wang ; qu ; tang jin lan ; yang zuo

..............page:208-211

Effect of primary rocket parameters on the performance of RBCC(rocket based combined cycle) in ejector mode
wang guo hui ; he guo qiang ; cai ti min

..............page:204-207

Numerical simulation for temperature in a monopropellant thrust chamber on the orbit
shen jun ; liu wei qiang ; tang jian hua

..............page:201-203,281

Performance monitoring and fault diagnosis of engines based genetic algorithm
hu jin hai ; xie shou sheng

..............page:198-200

Hybrid knowledge model and reasoning strategy based on intelligent fault diagnosis for liquid-propellant rocket engines
liu hong gang ; wu jian jun ; chen qi zhi

..............page:193-197

Numerical analysis of combustion and heat transfer in dual-operation LOX/hydrogen engine
lin zhi yong ; luo shi bin ; tian zhang fu ; zhou jin

..............page:254-258

Local tomography inspecting investigation for inner crack of SRM
lu hong yi ; yang xing gen ; cheng wei ping

..............page:251-253

Effect of twin jets shielding on screech tones
he feng ; zhang dong dong

..............page:247-250

Calculation and determination for the channel of a channel surface tension tank
li zhi ; shen chi bing ; zhou jin

..............page:244-246

Numerical simulation of flow field and thermal analysis for stage separation of multistage missile
zhang wen pu ; feng zhen ping

..............page:240-243

μ synthesis control with robust performance for missile turbojet engine
wang zuo ; yao hua

..............page:236-239

Starting and acceleration control law design for a missile turbojet engine
xie guang hua ; niu tian hua ; wang yi jun ; su xiang rong

..............page:232-235

A system configuration of tripropellant rocket engine with linear plug nozzle
li bing ke ; shen chi bing ; zhou jin

..............page:228-231

Numerical simulation of underexpanded jet from inclined nozzles
le gui gao ; ma da wei ; li zi yong ; li zhi gang

..............page:225-227

Chemical kinetics analysis for nozzle performance
sun de chuan ; chen jie ; lin qing guo

..............page:222-224

Coupled compressor-diffuser flow model for predicting response of a twin-spool turbine engine to inlet pressure distortion
wu hu ; huang zhi tao ; lian xiao chun

..............page:219-221,235

Discharge coefficient measurements for film cooling holes on blade surface in a turbine cascade
xiang an ding ; zhu hui ren ; liu song ling ; xu du chun ; guo wen

..............page:216-218,239

Large eddy simulation on scalar transport in ramjet dump combustor
wang bing ; zhang hui qiang ; wang xi zuo ; guo yin cheng ; lin wen zuo

..............page:212-215