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Current Issue

  • 2002,Vol 23,No. 3

    15 March 2002

Review on the models and numerical methods for simulation of precooling and starting process of LOX/LH2 rocket engine

2002, 23 (3): 177-181   

Numerical simulation on 3-D two-phase flow field in SRM with acceleration load

2002, 23 (3): 182-185   

Choose of the supersonic cruising engine’s design parameters

2002, 23 (3): 186-188   

Numerical simulation of turbofan engine with mixer afterburning under transient conditions

2002, 23 (3): 189-192   

Numerical simulation on 3-D turbulent flow and combustion process (Ⅱ) Results and analysis

2002, 23 (3): 193-197   

Experimental investigation of the effects of ignition energy on pressures in a pulse detonation combustor

2002, 23 (3): 198-201   

Numerical simulation of 3-D complex cold flow field of a gas generator

2002, 23 (3): 202-206   

Experimental for a like-doublet injector with 40°impingement angle

2002, 23 (3): 207-208   

3-D viscous numerical investigation on the overall aerodynamic performance of a transonic axial-flow compressor stage

2002, 23 (3): 209-212   

Integrated treatments on certain engine surge and experimental study on surge margin enlargement

2002, 23 (3): 213-215   

Modeling surge and recovery of the axial compression system in a turbine engine

2002, 23 (3): 216-218   

Numerical study of flow past hypersonic research vehicle with detaching booster

2002, 23 (3): 219-222   

Mixing process in symmetry trailing edge slot for a turbine blade

2002, 23 (3): 223-225   

Pressure fields measurements and flow losses around a row of short cylinder with jet impingement

2002, 23 (3): 226-229   

Heating transfer of longitudinal ripple heat shield tunnel

2002, 23 (3): 230-232   

Several issues in the implementation of vibration analysis of bladed disk

2002, 23 (3): 233-236   

Establishment of correlation equation about impingement heat transfer from rib roughened surface within arrays of circular jets

2002, 23 (3): 237-239   

Design and numerical analysis of the magnetic field of stationary plasma thruster

2002, 23 (3): 240-244   

Low temperature mechanical properties of high-burning rate HTPB/IPDI propellants (Ⅱ) Design and application of surfactants

2002, 23 (3): 245-248   

Study on the thermal decomposition of NEPE propellant (Ⅰ)Thermal decomposition of binder

2002, 23 (3): 249-251   

Crystallization of polyethylene glycol in NEPE propellants

2002, 23 (3): 252-257   

Effect of nano metal powder on the thermal decomposition characteristics of HMX

2002, 23 (3): 258-261   

Effect of GAP coating boron on the ignition performance and combustion residues for boron-based propellants

2002, 23 (3): 262-264