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Current Issue

  • 2010,Vol 31,No. 3

    15 March 2010

Numerical simulation on the flow field of solid fuel ramjet with inner bypass

2010, 31 (3): 257-260   

Supersonic with counter-flowing jets on drag and heat-transfer reduction

2010, 31 (3): 261-264   

Effect of design parameters and boundary layer correction on performance of jaws inlet

2010, 31 (3): 265-269   

Experimental investigation on combustion efficiency of the ramjet model at low pressure

2010, 31 (3): 270-275   

Transient burning rate model for pressurization of a pulsed solid rocket motor

2010, 31 (3): 276-280   

A quasi-steady model of immobile droplet evaporation with pressure oscillation

2010, 31 (3): 281-288   

Numerical simulation on accumulation and breaking of Al2O3 particles for solid rocket engine

2010, 31 (3): 289-295   

Comparison on aerodynamic damping between subsonic blade and transonic blade

2010, 31 (3): 296-300   

Flow mechanisms of improving compressor performance through self recirculation casing treatment

2010, 31 (3): 301-308   

Effects of turbofan exhaust system geometry parameters on sound pressure level

2010, 31 (3): 309-313   

Aerodynamic investigation on retrofit for turbine of a turbo-shaft engine

2010, 31 (3): 314-319   

Effect of aspect ratio on flow characteristics in a confined channel with staggered jet array impingement

2010, 31 (3): 320-324   

Experiments on heat transfer enhancement with vortex in a double-decker jet/film cooling structure

2010, 31 (3): 325-330   

Experiment on fatigue/creep life of turbine components

2010, 31 (3): 331-334   

Investigations on flutter characteristics of rotor blade with IGV/fan interactions

2010, 31 (3): 335-339   

Investigation on flow instability of transonic compressor rotor and the effects of CGCT on stall margin at low Reynolds number

2010, 31 (3): 340-344   

Study on the mechanical properties of NGEC and NGEC based propellants

2010, 31 (3): 345-350   

Experimental invetigation for hygrothermal aging law and damage mode of HTPB composite solid propellant

2010, 31 (3): 351-355   

Study on combustion rate prediction model of CMDB propellant with fine grained AP

2010, 31 (3): 356-360   

Computational investigation on axisymmetric nozzles with fluidic injection for throat area control

2010, 31 (3): 361-365   

Friction thermal effect on rubbing response of a high pressure rotor system

2010, 31 (3): 366-371   

Measurement method for microgram amounts laser ablation mass

2010, 31 (3): 372-376   

Effects on aerodynamic drag of incident laser energy in technology of laser plasma point source drag reduction

2010, 31 (3): 377-380   

A method of real time measurement for transient microthrust

2010, 31 (3): 381-384