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Current Issue

  • 2003,Vol 24,No. 6

    15 June 2003

Research on accelerated reliability growth test (Ⅷ) Organization and performance of the test

2003, 24 (6): 481-483   

Intelligent damage-mitigating and life-extending control techniques for reusable liquid-propellant rocket engines

2003, 24 (6): 484-487   

Optimal control analysis on gradual tripropellant engine for SSTO

2003, 24 (6): 488-490   

Experimental and numerical study for cold flow of plug nozzle

2003, 24 (6): 491-494   

Numerical study of jet interaction flows in the two-dimensional transitional regime by DSMC/EPS method

2003, 24 (6): 495-499   

Conceptual design of multi-cycle pulse detonation engines

2003, 24 (6): 500-504   

Numerical analysis on the performance of dual-bell nozzle

2003, 24 (6): 505-508   

Numerical simulation and performance analysis of the linear clustered plug nozzles

2003, 24 (6): 509-513   

Measurement of pressure and temperature in exhaust jet during launching stage of rocket

2003, 24 (6): 514-516   

Neural network PID adaptive control in pilotless aircraft turbojet engine

2003, 24 (6): 517-520   

Numerical simulation for flow in a supersonic combustor with cavity flame holders

2003, 24 (6): 521-523   

Experimental study on the mean flow behind EBMC flameholder

2003, 24 (6): 524-527   

An experimental investigation of film cooling effectiveness on the surface of turbine blade

2003, 24 (6): 528-531   

Circular leading edge with a flat for compressor blades

2003, 24 (6): 532-536   

Three-dimensional pressure distribution of the cascades with aft-loading profile and the influence of loss development

2003, 24 (6): 537-542   

Numerical investigation for the influence of buoyancy on heat transfer in an annulus between rotating cylinders with turbulent axial flow

2003, 24 (6): 543-546   

An engine-starting test on the highland ground

2003, 24 (6): 547-549   

Data synthesis of simulated altitute test cell versus ground test cell for turbojet engine

2003, 24 (6): 550-552   

Investigation of helium resonance ignitor and kerosene/oxygen ignitor

2003, 24 (6): 553-556   

Influence of microconvexities of aluminium particle surface on agglomeration

2003, 24 (6): 557-559   

Synthesis of nanometer-CuFe2O4 and its catalysis on thermal decomposition of RDX

2003, 24 (6): 560-562   

Improvement of low temperature elongation ratio of high-burning rate HTPB propellant

2003, 24 (6): 563-566   

Study on boron-based solid propellants for integrated motor

2003, 24 (6): 567-570   

Combustion property of Nitramine/AP/HTPB propellant under high pressures

2003, 24 (6): 571-572   

Viscous pressure forming for aluminum alloy bowl-type parts of turbofan engine

2003, 24 (6): 573-576