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Current Issue

  • 2000,Vol 21,No. 3

    15 March 2000

Dynamic characteristics of priming process in spacecraft propulsion systems (Ⅱ)experimental results and reliability analysis

2000, 21 (3): 1-5   

Acceleration effects on internal ballistics performance of solid rocket motor

2000, 21 (3): 6-8   

Flowfield computation in rocket ramjet with complex boundary

2000, 21 (3): 9-12   

Multimedia real-time data simulation for a turbojet engine

2000, 21 (3): 13-15   

Experimental study on mechanism of initial shock wave in jet flow

2000, 21 (3): 16-18   

Performance computation for blunt body scheme of microwave electrothermal thruster

2000, 21 (3): 19-22   

Effects of vector nozzle deflection on engine thrust

2000, 21 (3): 23-25   

Measurement and analysis for shock due to the secondary gas injection

2000, 21 (3): 26-29   

Numerical simulation on internal and external flow fields of nozzle with complex geometry

2000, 21 (3): 30-33   

Cold gas simulation on aft-end internal flow for solid rocket motor with submerged nozzle

2000, 21 (3): 34-37   

Effect of spool coupling on compressor stability

2000, 21 (3): 38-39   

Critical rotational speed of turopump rotors (V)finite element method for critical rotation speed calculation

2000, 21 (3): 40-42   

Calculation for rotor stability in turbopumps

2000, 21 (3): 43-45   

Modeling the rotating behavior of an augmented turbofan engine

2000, 21 (3): 46-48   

Experimental research of casing treatment on single stage transonic fan

2000, 21 (3): 49-52   

Numerical simulation of performeance and jet flowfield of the nozzle

2000, 21 (3): 53-55   

Effect of spray characteristic on the liquid rocket combustion stability

2000, 21 (3): 56-59   

Grain design for hybrid rocket engine with cluster type thrust chamber

2000, 21 (3): 60-62   

Theoretical prediction of storage life for HTPB propellant

2000, 21 (3): 63-66   

Acoustic emission experimental study on meso-damage mechanism of HTPB propellant

2000, 21 (3): 67-70   

Propagating process of cracks on polysulfide propellant during combustion

2000, 21 (3): 71-74   

Catalytic mechanism of fullerene in RDX-CMDB propellants

2000, 21 (3): 75-78   

Leveling properties of the composite solid propellants slurry

2000, 21 (3): 79-82   

Numerical control milling for aeroengine integrated impeler of TC6 titanium alloy

2000, 21 (3): 83-85   

Thrust vector measurement for small engine

2000, 21 (3): 86-88