Journal of Propulsion Technology 2004 Issue 6 Independent component analysis for the fault features of liquid propellant rocket engine

Independent component analysis for the fault features of liquid propellant rocket engine
ren hai feng ; hu xiao ping ; wu jian jun

..............page:481-483,490

Numerical investigation on two phase flow of a kerosene-fueled scramjet with 3D cavity(Ⅰ) Numerical calibration and characteristics of general flow
huang sheng hong ; xu sheng li ; liu xiao yong

..............page:484-490

Ducted rocket secondary chamber optimization with response surface methodology
hu jian xin ; xia zhi xun ; zhao jian min ; guo jian ; zhang zuo ; luo zhen bing ; zuo wan bo

..............page:491-494

System capability estimating for a metal/water reaction fuel ramjet system
luo kai ; dang jian jun ; wang yu cai ; zhang yu wen

..............page:495-498

Experiment of aerodynamic performance for hypersonic vehicle integrated with sidewall compression inlet
fan xiao zuo ; li zuo ; yi shi he ; pan sha

..............page:499-502

Numerical study of the throttle characteristic about the ramjet inlet and mixing section
bai peng ; zhu shou mei ; meng yu peng ; li wen xu ; ma han dong ; zhou wei jiang

..............page:503-507

Effects of axial spacing on compressor performance in all flow range
li chuan peng ; hu jun ; zhang liao yuan ; wang ying feng

..............page:508-511

Effects of swept blade on the aerodynamic performance of turbine cascade
yue guo qiang ; han wan jin

..............page:512-516

Experimental and numerical investigation on the effect of hot streak on the 2nd vane in turbine
zuo chao ; nei tian cheng sheng ; zuo yuan kang lang ; xu jian zhong

..............page:517-520

Influence of incidences on the distribution of static pressure of swept-curved compressor cascades
chen fu ; zhao gui jie ; song yan ping ; wang zhong qi

..............page:521-525

A digital electronic control system design and test for a certain small turbojet engine
yang yu wu

..............page:526-529

PI output feedback control for aero-engine based on LMI
wang zuo ; zuo dao liang

..............page:530-534

Aero-engine multivariable learning fuzzy decouple control
ren xin yu ; fan si qi

..............page:535-537,560

Experimental investigation on working process of pulse detonation engine (PDE)
fan yu xin ; wang jia zuo ; li jian zhong ; zhang jing zhou

..............page:538-542

Maximal net thrust and optimal frequency of pulse detonation engine
li jian zhong ; wang jia zuo ; fan yu xin ; zhang jing zhou ; zhang yi ning

..............page:543-548

Effects of parameters of turbulence generator on the detonation wave in air-breathing gasoline-air pulse detonation engine
zheng dian feng ; wang jia zuo ; zhang hui qiang ; lin wen zuo

..............page:549-552

A numerical simulation on the nozzle flow of pulse detonation engine
li hui huang ; yang ji ming ; xu li gong

..............page:553-556

An MDO approach for engine nozzle design
fang jie ; tong xiao yan ; mao xiao fang ; cai guo zuo

..............page:557-560

Numerical simulation on aerospike nozzle flowfield with chemical non-equilibrium reaction
wang chang hui ; liu yu

..............page:561-565

Experimental investigation of ignition technology in liquid hydrocarbon fueled scramjet combustor
ding meng ; yu yong ; liang jian han ; liu wei dong ; wang zhen guo

..............page:566-569

Study on the composite modified double base propellant containing 3,4-dinitrofurazanfuroxan (DNTF)
zhao feng qi ; chen pei ; luo yang ; zhang rui e ; zhang zhi zhong ; zhou yan shui ; li shang wen

..............page:570-572,576

Swabbing technology characteristics of solid rocket motor liner
tang han xiang ; wu zuo ; chen jiang

..............page:573-576

tui jin ji shu di 25 juan (2004 nian ) zong mu ci

..............page:A1-A4

tui jin ji shu di 25 juan (2004 nian ) zhu zhe suo yin

..............page:A5-A7

hang tian ke gong ji tuan ke ji qi kan lian he zheng ding qi shi

..............page:A8-A10