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Current Issue

  • 2010,Vol 31,No. 6

    15 June 2010

Progress in air-breathing hypersonic technology

2010, 31 (6): 641-649   

French contribution to hypersonic airbreathing propulsion technology development

2010, 31 (6): 650-659   

Research status and perspective of rocket based combined cycle propulsion system

2010, 31 (6): 660-665   

A review on the research development of Gao-Yong equations of turbulent flows

2010, 31 (6): 666-675   

Unsteady start/unstart characteristics of 2-D hypersonic inlet caused by oscillating angle-of-attack

2010, 31 (6): 676-680   

Mechanism of plasma effect on the performance of highly-turning compressor cascade

2010, 31 (6): 681-688   

Aerodynamics design of two-stage vaneless counter-rotating turbine

2010, 31 (6): 689-695   

Fire test on a gas-gas injector with hydrogen-rich/oxygen-rich gas

2010, 31 (6): 696-700   

Passive control of combustion instability through an acoustic valve

2010, 31 (6): 701-709   

Mechanism,prediction and control method of combustion instability in propulsion system

2010, 31 (6): 710-720   

Studies on kerosene injection and mixing with cavity in supersonic flow

2010, 31 (6): 721-729   

Experimental study and analysis of thermo-acoustic instabilities in natural gas premixed flames

2010, 31 (6): 730-744   

Infrared characteristics calculating of turbofan engine exhaust system

2010, 31 (6): 745-750   

Experiment on fluidic thrust-vectoring nozzle based on shock control concept

2010, 31 (6): 751-756   

Flow characteristic of a dual synthetic jets actuator with different beveled exit and boundary layer control

2010, 31 (6): 757-763   

Control method of scramjet engines

2010, 31 (6): 764-772   

Effect of oxidizers in magnesium fuel-rich propellant for water-ramjet engine

2010, 31 (6): 773-776   

Experimental investigation on nitrous oxide/propane ignition characteristics

2010, 31 (6): 777-782   

Numerical simulation on pulse detonation engine

2010, 31 (6): 783-788