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Current Issue

  • 2000,Vol 21,No. 1

    15 January 2000

Adaptive thresholds algorithm for fault detection of liquid rocket engine in ground test

2000, 21 (1): 1-4   

Frequency characteristic for liquid propellant staged combustion cycle rocket engine

2000, 21 (1): 5-7   

Theoretical computation on the contamination of vacuum plume in the backflow region

2000, 21 (1): 8-11   

Numerical study on normal fuel injection in scramjet

2000, 21 (1): 12-14   

SFD method simulation on interactions of shock waves with boundary layers in the hypersonic inlet

2000, 21 (1): 15-19   

Numerical simulation and utilization of inner flow field for solid ramjet

2000, 21 (1): 20-22   

Numerical simulation of the turbulent flow in a 3D afterburner

2000, 21 (1): 23-25   

Experimental investigation on heat transfer within a rotating ribber serpenting passage

2000, 21 (1): 26-29   

Numerical simulation of impinging jet produced by missile

2000, 21 (1): 30-32   

Experimental study on high mixture ratio torch ignitor

2000, 21 (1): 33-35   

Malfunction analysis to nozzle guide component of turbofan engine

2000, 21 (1): 36-38   

Modeling technique for stage by stage axial flow compression system

2000, 21 (1): 39-41   

Cavitation in fuel limitor of fuel adjusting system of turbojet

2000, 21 (1): 42-44   

Internal turbulent flow and generation of “jet wake”structure at outlet of a centrifugal impeller

2000, 21 (1): 45-48   

Bayesian inferance on AMSAA BISE model and in application to engine

2000, 21 (1): 49-53   

Numerical investigation of zonal multigrid method in complex regions

2000, 21 (1): 54-56   

Experimental research on spray properties of unlike impinging injectors

2000, 21 (1): 57-59   

Secondary flow measurements and flow losses near the endwall of linear turbine cascade

2000, 21 (1): 60-63   

Application of surface and interface chemistry principles to solid propellant

2000, 21 (1): 64-66   

Optimization of grain design for hybrid rocket engine

2000, 21 (1): 67-70   

Kinetic extension of the solid propellant cracks simulated by the equivalent forces working on the virtual new surfaces

2000, 21 (1): 71-74   

Micromechanics analysis on the viscoelastics constitutive law of composite solid propellent (Ⅱ)reinforce effects of non spherical particles

2000, 21 (1): 75-78   

Storage life prediction for HTPB propellant under constant strain

2000, 21 (1): 79-81   

Effects of nanometer PbCO 3 on combustion behavior of NEPE propellant

2000, 21 (1): 82-85   

Advanced system of monitor and measurement for the combusti on process and rate of solid propellants

2000, 21 (1): 86-88