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Current Issue

  • 2003,Vol 24,No. 3

    15 March 2003

Hybrid knowledge model and reasoning strategy based on intelligent fault diagnosis for liquid-propellant rocket engines

2003, 24 (3): 193-197   

Performance monitoring and fault diagnosis of engines based genetic algorithm

2003, 24 (3): 198-200   

Numerical simulation for temperature in a monopropellant thrust chamber on the orbit

2003, 24 (3): 201-203   

Effect of primary rocket parameters on the performance of RBCC (rocket based combined cycle) in ejector mode

2003, 24 (3): 204-207   

Experimental investigation of microwave plasma thruster in vacuum

2003, 24 (3): 208-211   

Large eddy simulation on scalar transport in ramjet dump combustor

2003, 24 (3): 212-215   

Discharge coefficient measurements for film cooling holes on blade surface in a turbine cascade

2003, 24 (3): 216-218   

Coupled compressor-diffuser flow model for predicting response of a twin-spool turbine engine to inlet pressure distortion

2003, 24 (3): 219-221   

Chemical kinetics analysis for nozzle performance

2003, 24 (3): 222-224   

Numerical simulation of underexpanded jet from inclined nozzles

2003, 24 (3): 225-227   

A system configuration of tripropellant rocket engine with linear plug nozzle

2003, 24 (3): 228-231   

Starting and acceleration control law design for a missile turbojet engine

2003, 24 (3): 232-235   

μ synthesis control with robust performance for missile turbojet engine

2003, 24 (3): 236-239   

Numerical simulation of flow field and thermal analysis for stage separation of multistage missile

2003, 24 (3): 240-243   

Calculation and determination for the channel of a channel surface tension tank

2003, 24 (3): 244-246   

Effect of twin jets shielding on screech tones

2003, 24 (3): 247-250   

Local tomography inspecting investigation for inner crack of SRM

2003, 24 (3): 251-253   

Numerical analysis of combustion and heat transfer in dual-operation LOX/hydrogen engine

2003, 24 (3): 254-258   

Combustion flow in ejecting mode of strutjet engine(Ⅱ)Effects of secondary combustion and configuration

2003, 24 (3): 259-264   

Overview of flame holders of cavities in supersonic combustion

2003, 24 (3): 265-271   

Identification of turbojet ignition based on neural network with a prior

2003, 24 (3): 272-274   

Experimental studies for plasmas ignition of solid propellants

2003, 24 (3): 275-277   

Measurement on catalytic cracking heat sink of endothermic hydrocarbon fuels

2003, 24 (3): 278-281   

Mechanism of the deteriorated processability in boron-fuel-rich HTPB propellants

2003, 24 (3): 282-284   

FEM creep damage study for nickel-base single crystal structure under multiaxial stress conditions

2003, 24 (3): 285-288