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  • 2002,Vol 23,No. 4

    15 April 2002

Numerical simulation on the stage-separation flow fields of the multi-stage rocket

2002, 23 (4): 265-267   

Experimental study of import pass ways for model tripropellant injector

2002, 23 (4): 268-272   

Adiabatic film cooling effectiveness downstream of primary jet in combustion chamber

2002, 23 (4): 273-275   

Effection of structural parameters of tripropellant injector on twophase flow in the mixer

2002, 23 (4): 276-279   

Flow performance analysis in an axial compressor rotor with splitter

2002, 23 (4): 280-282   

Effect of temperature profile at entrance on flow-fields of nozzle

2002, 23 (4): 283-286   

Angle properties of the primary nozzle of plug nozzle

2002, 23 (4): 287-291   

Numerical and experimental study of tile-shaped aerospike nozzles

2002, 23 (4): 292-297   

Flow analysis and validation of rocket ejector mode for rocket based combined cycle

2002, 23 (4): 298-302   

Influence of the clapboard on electromagnetic field and resonant frequency within the resonant cavity of microwave plasma thruster

2002, 23 (4): 303-306   

Computation of the integrated flow field around missile and mixed compression intake

2002, 23 (4): 307-310   

Investigation of flow in isolator of hypersonic inlet

2002, 23 (4): 311-314   

Numerical approach for turbine blade with trailing edge ejection

2002, 23 (4): 315-317   

Experimental study of near field rocket noise in exhausted flow field

2002, 23 (4): 318-320   

Effects of blade positive curving on aerodynamic performance of compressor cascades

2002, 23 (4): 321-324   

Experiment study for platelet slab flow channel control performance of platelet transpiration cooled thrust chamber

2002, 23 (4): 325-328   

Effect of nanometer-sized lanthanum oxide on catalyzing decomposition of cyclotrimethylenetriamine

2002, 23 (4): 329-331   

Image analysis system for goodness of mixing of solid propellants

2002, 23 (4): 332-334   

Stability analysis of the crack in solid rocket motor grain

2002, 23 (4): 335-338   

Thermal decomposition characteristics of AP/KP/GAP fuel-rich propellant

2002, 23 (4): 339-341   

Experimental investigation on the combustion behavior of aluminium-magnesium based fuel-rich propellant

2002, 23 (4): 342-345   

Development and expectation of performance simulation in aviation engine

2002, 23 (4): 346-351