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Current Issue

  • 2000,Vol 21,No. 6

    15 June 2000

Prospect for solid propellant technologies at the beginning of the 21st century

2000, 21 (6): 1-5   

Research on accelerated reliability growth test (I)presentment of a new direction

2000, 21 (6): 6-9   

Primary analysis of deep cooled turbojet liquid rocket engine combined cycle

2000, 21 (6): 10-13   

Influence of outward radiation of parallel four thrust chambers on wall temperature

2000, 21 (6): 14-17   

Gear method for calculation of one dimensional chemical reaction nozzle flow

2000, 21 (6): 21-24   

Improving acceleration dynamic performance of a two-spool turbojet using variable nozzle area controls

2000, 21 (6): 25-27   

Mixed H2/H output feedback control of aeroengine based on LMI

2000, 21 (6): 28-31   

Unsteady effects on isolated rotor exit of an axial flow compressor

2000, 21 (6): 32-35   

Two types of bowed blades in turbine stage

2000, 21 (6): 36-39   

3-D viscous numerical investigation on flow field of a transonic axial-flow fan rotor

2000, 21 (6): 40-43   

Transient response of rotors system with surge

2000, 21 (6): 44-47   

Application of SIMPLE algorithm with domain decomposition in tube viscous flow field

2000, 21 (6): 48-51   

Comparison of two multi-grid schemes for radial turbo-machinery compressible flow

2000, 21 (6): 52-55   

Characteristic of the entry of niche-like preburner in the hypersonic inlet

2000, 21 (6): 56-58   

Finite elemant calculation of crack combustion flow field in solid propellant

2000, 21 (6): 59-61   

Gas filling phenomena in fin-slot region during ignition transient

2000, 21 (6): 62-64   

Measurement and analysis for spectrum of iron in kerosene-oxygen flame

2000, 21 (6): 65-69   

Interaction of ammonium perchlorate with HMX and RDX during decomposition

2000, 21 (6): 70-73   

High pressure thermal decomposition behavior and relation to burning rate of catalyzed nitrate propellant

2000, 21 (6): 74-78   

Estimation of formation enthalpy of thermoplastic polyurethane binder for novel thermoplastic propellant

2000, 21 (6): 79-82   

CCD cross-correlation particle image velocimetry and its application to counterflow flowfield measurements

2000, 21 (6): 83-88