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  • 2002,Vol 23,No. 6

    15 June 2002

Computation of three dimensional nozzle flow field with fluidic injection

2002, 23 (6): 441-444   

Numerical simulation of effects of heat transfer on the transient performance of gas turbine engines

2002, 23 (6): 445-447   

Transient heat conduction and temperature field characteristics of a propellant

2002, 23 (6): 448-452   

Application of after-burning between high and low turbines to improve performance of two-spool turbofan engine

2002, 23 (6): 453-456   

Distilling character parameter method investigation for space aerocraft propulsion system using improving time-series method

2002, 23 (6): 457-459   

Numerical simulation of effects of leading edge on the performance of inlet

2002, 23 (6): 460-462   

Design and experimental investigation on a new grooved treated casing with for ward-step in an axial-flow compressor

2002, 23 (6): 463-467   

Study for the mathematical model of supersonic inlet

2002, 23 (6): 468-471   

Numerical study for turbulent flow inside rotating disc cavities

2002, 23 (6): 472-476   

Effect of suction hole on heat transfer characteristic of internal passage

2002, 23 (6): 477-479   

Numerical simulation of internal flow fleld of swirl nozzle

2002, 23 (6): 480-484   

Application of global variable structure control method in aeroengine control system

2002, 23 (6): 485-488   

Real-time intelligent diagnosis system for missile propellant filling equipment

2002, 23 (6): 489-491   

Nonlinear acoustic wave in combustors

2002, 23 (6): 492-495   

Influence of injection angle on the thermodynamic aspects of end wall film-cooling in a turbine cascade

2002, 23 (6): 496-499   

Method of characteristics for vacuum plume simulation

2002, 23 (6): 500-504   

Resonace regulation of microwave plasma thruster under the low signal

2002, 23 (6): 505-508   

Research on the constitutive equations of HTPB composite solid propellant with damage and aging

2002, 23 (6): 509-512   

Thermal cracking and catalytic cracking of endothermic hydrocarbon fuel on mixture catalyst

2002, 23 (6): 513-517   

Combustion characteristics of boron-based fuel-rich propellant at low pressure

2002, 23 (6): 518-520   

Ammonium nitrate surface modification through spraying and drying technology

2002, 23 (6): 521-524   

Effect of pretreatment of cotton cellulose by steam explosion on properties of nitrocellulose

2002, 23 (6): 525-528