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Current Issue

  • 2003,Vol 24,No. 4

    15 April 2003

Research on accelerated reliability growth test (Ⅵ) Step stress test schemes

2003, 24 (4): 289-291   

Numerical simulation and experimental validation for viscous flow field in rocket engine chamber

2003, 24 (4): 292-295   

Numerical study for CH4/air supersonic combustion

2003, 24 (4): 296-299   

Influence of tangential rotational jet on the mixing effect in additional chamber of solid ram rocket

2003, 24 (4): 300-302   

Design of channel surface tension tank propellant management device

2003, 24 (4): 303-305   

Influence of thrust chamber parameters on nozzle chemical kinetic performance

2003, 24 (4): 306-309   

Particle simulation model for the inner flow field in solid rocket motor with crack

2003, 24 (4): 310-314   

Study of experimental method for ablation of insulator of SRM with high acceleration (Ⅰ)

2003, 24 (4): 315-318   

Numerical studies in axial compressor cascades using partial deposition model

2003, 24 (4): 319-322   

Matching between supersonic inlet and aero-engine

2003, 24 (4): 323-325   

Computation for the effect of turbulence models on internal performance for axisymmetric vectoring exhaust nozzles

2003, 24 (4): 326-329   

Base pressure model of plug nozzle

2003, 24 (4): 330-333   

Comparative investigation of the infrared characteristics for two exhaust systems of a turbofan engine

2003, 24 (4): 334-336   

Aerodynamic investigation of flow fields in the channel with ejection through the holes on the wall

2003, 24 (4): 337-340   

Pressure loss of the internal passage with rib turbulators and suction holes

2003, 24 (4): 341-343   

Numerical investigation of turbulence parameter on flow field of rotating disc cavity with complex geometry

2003, 24 (4): 344-347   

Studies on spray characteristics of barbotaged atomizer

2003, 24 (4): 348-352   

Hardware-in-loop studies for integrated flight/propulsion control modes at subsonic flight conditions

2003, 24 (4): 353-356   

Optimal acceleration control of turbofan engine with genetic algorithm

2003, 24 (4): 357-360   

Fault simulation and analysis of turbojet oil-supplied regulating system

2003, 24 (4): 361-363   

Robust H_∞/PI state feedback control for aeroengine

2003, 24 (4): 364-367   

Effect of turbine efficiency changing on turbo-engine’s accelerating characteristic under closed-loop control mode

2003, 24 (4): 368-372   

Photochemical ignition characteristic of H2-O2-Cl2 mixtures

2003, 24 (4): 373-375   

Influence of nano-/micro- powder filler on properties of propellant slurry

2003, 24 (4): 376-379   

CAD/CAM of rimed blisks

2003, 24 (4): 380-383