Research and development of afterburner control system for military aeroengine

Abstract ( ) PDF (1258KB) ( )

2001, 22 (2)： 89-91   

Research on accelerated reliability growth testing (Ⅲ)Graphical methods for grouped data

Abstract ( ) PDF (1180KB) ( )

2001, 22 (2)： 92-96   

Review of catalytic cracking of endothermic hydrocarbon fuel

Abstract ( ) PDF (1435KB) ( )

2001, 22 (2)： 97-100   

Modular simulation on the start process for staged combustion cycle liquid propellant rocket engine

Abstract ( ) PDF (761KB) ( )

2001, 22 (2)： 101-103   

Approach to dynamic data processing for liquid rocket engine based on wavelet analysis

Abstract ( ) PDF (1278KB) ( )

2001, 22 (2)： 104-107   

Experimental study on two-phase pulse detonation engine model

Abstract ( ) PDF (825KB) ( )

2001, 22 (2)： 108-110   

Performance monitoring and diagnosis system for missile turbojet engine

Abstract ( ) PDF (957KB) ( )

2001, 22 (2)： 111-113   

Fault diagnosis for turboengine based on wavelet and fuzzy neural network

Abstract ( ) PDF (1146KB) ( )

2001, 22 (2)： 114-117   

Numerical analysis on three-dimensional flow in 2-D mixed-compression supersonic inlet

Abstract ( ) PDF (933KB) ( )

2001, 22 (2)： 118-121   

Effect of tabs fixed on a convergent nozzle to the infra-red radiation of the exhausting hot jet

Abstract ( ) PDF (1117KB) ( )

2001, 22 (2)： 122-125   

Simulation research for radiation heat transfer of engine group by model nozzles

Abstract ( ) PDF (695KB) ( )

2001, 22 (2)： 126-128   

Numerical simulation of turbulent flow in a turn-around duct

Abstract ( ) PDF (1033KB) ( )

2001, 22 (2)： 129-132   

LTR control for aeroengines

Abstract ( ) PDF (936KB) ( )

2001, 22 (2)： 133-136   

Effect of inlet on the engine performance and platform point for aircraft

Abstract ( ) PDF (826KB) ( )

2001, 22 (2)： 137-138   

Nonlinear continuum damage mechanics model on high temperature creep analysis

Abstract ( ) PDF (997KB) ( )

2001, 22 (2)： 139-142   

Power density optimization of an endoreversible brayton cycle coupled to variable-temperature heat reservoirs

Abstract ( ) PDF (983KB) ( )

2001, 22 (2)： 143-146   

Effecting parameters of supersonic flowfield with secondary injection

Abstract ( ) PDF (1006KB) ( )

2001, 22 (2)： 147-150   

Experimental study of remains of poisonous propellant on the ground after explosion of liquid rocket

Abstract ( ) PDF (1136KB) ( )

2001, 22 (2)： 151-154   

Numerical assessment of MMH/NTO rocket engine combustion instability

Abstract ( ) PDF (804KB) ( )

2001, 22 (2)： 155-156   

Investigation on supersonic combustion of kerosene using fuel-rich hot gas as pilot flame

Abstract ( ) PDF (1502KB) ( )

2001, 22 (2)： 157-161   

High burning rate propellant formulation used in broad temperature range

Abstract ( ) PDF (827KB) ( )

2001, 22 (2)： 162-164   

Catalysis combustion property and mechanism of PDADN-RDX-CMDB propellant

Abstract ( ) PDF (1789KB) ( )

2001, 22 (2)： 165-170   

Determining poisson’s ratio of solid propellant by means of cylindrical motors

Abstract ( ) PDF (860KB) ( )

2001, 22 (2)： 171-173   

A small thrust measurement system of electric thruster

Abstract ( ) PDF (782KB) ( )

2001, 22 (2)： 174-176