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Current Issue

  • 2010,Vol 31,No. 2

    15 February 2010

Coupled numerical simulation for the later period of the stage separation of a multi-stage rocket

2010, 31 (2): 129-133   

Experimental investigation for hydrogen/oxygen engine using gas dynamic resonance ignition technique

2010, 31 (2): 134-138   

Parametric cycle analysis of mixed exhaust turbofan with inter-stage turbine burner

2010, 31 (2): 139-142   

Investigation on flow distortion control of a subsonic inlet

2010, 31 (2): 143-146   

3D inward turning inlet design basing on axisymmetric nozzle and its preliminary assessment

2010, 31 (2): 147-152   

Rocket jet effect on the performance of a RBCC inlet

2010, 31 (2): 153-160   

Numerical investigations on the combustion instability for a ramjet engine

2010, 31 (2): 161-164   

Analysis and optimization of vortex configuration for vortex-cooled combustion chamber

2010, 31 (2): 165-169   

Experimental investigation on dual shear coaxial gas-gas injector

2010, 31 (2): 170-173   

Flutter prediction method applied in turbomachinery design

2010, 31 (2): 174-180   

Mechanism of stall margin improvement of two stages transonic fan with two-portion axial slot casing treatment

2010, 31 (2): 181-186   

Experimental investigations for the flow structures on the concave surface with inclined impingement in small distance

2010, 31 (2): 187-192   

Multidisciplinary probabilistic and robust design optimization for turbine blade

2010, 31 (2): 193-197   

Effect of stator-rotor interactions on the blades surface pressure

2010, 31 (2): 198-203   

Numerical investigation on starting performance of zero-secondary flow ejectors

2010, 31 (2): 204-209   

Integral wind-up protection PI control for turbofan engine based on LMI

2010, 31 (2): 210-215   

Acceleration control law optimization in aero engine based on SQP

2010, 31 (2): 216-218   

Application of active disturbance rejection control method in aeroengines afterburning transition state control

2010, 31 (2): 219-225   

Analysis on properties of catalytic combustion of composite BAMO-THF propellants

2010, 31 (2): 226-229   

Experiment on convective heat transfer of aviation kerosene under supercritical pressures

2010, 31 (2): 230-234   

Effects of gas-phase speed on EPDM insulator ablation

2010, 31 (2): 235-239   

Primary analysis for performance of laser propulsion with water propellant

2010, 31 (2): 240-242   

Numerical study on the propagation properties of laser-induced shock wave

2010, 31 (2): 243-246   

Thrust performance study on laser plasma micro ablation with transmission mode

2010, 31 (2): 247-251   

Theoretical analysis of energy law of similitude of conical nozzles for laser propulsion in repetitively-pulsed mode

2010, 31 (2): 252-256