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Current Issue

  • 2002,Vol 23,No. 1

    15 January 2002

Prospect for neural networks used aeroengine fault diagnosis technology

2002, 23 (1): 1-4   

Optimizing modification on parameter of solid rocket engine

2002, 23 (1): 5-7   

Digital electronic control system of a liquid fuel ramjet engine

2002, 23 (1): 8-10   

Fault detection and diagnosis system based on the rule and time variation for spacecraft propulsion system

2002, 23 (1): 11-14   

Numerical simulation on three-dimensional subsonic impinging jet

2002, 23 (1): 15-18   

Adaptive unstructured grid for two-dimensional Euler equations

2002, 23 (1): 19-23   

Performance investigation by wind tunnel for S-shaped subsonic inlet

2002, 23 (1): 24-26   

Numerical investigation of aerospike nozzle configuration on its performance

2002, 23 (1): 27-32   

Improved method of two-phase flow simulation

2002, 23 (1): 33-35   

Influence of non-axisymmetric endwall profile on the flow field of a turbine cascade

2002, 23 (1): 36-39   

Numerical simulation on unsteady flow with turbulence intensity effects in a turbine stage

2002, 23 (1): 40-44   

Numerical simulation of exhausted flow field in closed launch tube

2002, 23 (1): 45-48   

Effect of double-nozzle engine jet flow on vehicle aerodynamic characteristics

2002, 23 (1): 49-51   

Preliminary experimental investigation on gas dynamic resonance tube heating effect

2002, 23 (1): 52-56   

Structure of dynamic seal used in the lubricating system of a missile turbojet engine

2002, 23 (1): 57-59   

Internal radiation effects in semitransparent high-temperature coatings

2002, 23 (1): 60-62   

Numerical simulation on supersonic combustion of methane

2002, 23 (1): 63-66   

Effect of urethane groups on processing behaviour of composite solid propellants

2002, 23 (1): 67-70   

Analyses of theory and experiment for void damage of solid propellant

2002, 23 (1): 71-73   

Flame structure of NC/TMETN insensitive propellant containing different secondary flame suppressors

2002, 23 (1): 74-78   

Linkage-mutualism" mechanism for interactions between AP and HMX

2002, 23 (1): 79-83   

Viscous pressure forming of super-alloy super-thin wall corrugated parts applied to ramjet engine

2002, 23 (1): 84-88