Propulsion system stability control for super-maneuvering flight

Abstract ( ) PDF (963KB) ( )

2000, 21 (4)： 1-4   

Starting and accelarating the missle turbojet engine by ground test

Abstract ( ) PDF (1159KB) ( )

2000, 21 (4)： 5-8   

Numerical investigation of the flow field inside the liquid hydrogen inducer

Abstract ( ) PDF (769KB) ( )

2000, 21 (4)： 9-11   

One-dimensional finite element solutions for liquid transients in propellant feedlines

Abstract ( ) PDF (993KB) ( )

2000, 21 (4)： 12-15   

New sealing structure of high pressure liquid rocket engine

Abstract ( ) PDF (1185KB) ( )

2000, 21 (4)： 16-19   

Effect of mixing tube area and position on performances for lobed ejector

Abstract ( ) PDF (1069KB) ( )

2000, 21 (4)： 20-23   

Numerical simulation of plug nozzle flow field

Abstract ( ) PDF (769KB) ( )

2000, 21 (4)： 24-26   

Numerical simulation of 3-D unsteady turbulent flow in SRM chamber with finocyl grain

Abstract ( ) PDF (1380KB) ( )

2000, 21 (4)： 27-31   

Numerical simulation of nonlinear gas oscillations in closed pipe

Abstract ( ) PDF (917KB) ( )

2000, 21 (4)： 32-35   

Numerical study on flow field in 2-D segment compression supersonic intake for an air-to-air missile

Abstract ( ) PDF (964KB) ( )

2000, 21 (4)： 36-39   

Numerical calculation for flow and heat transfer of a shrouded rotating disk with high-positioned air-inlet

Abstract ( ) PDF (942KB) ( )

2000, 21 (4)： 40-43   

Identification of nonlinear mathematic model of Air pressure buffer

Abstract ( ) PDF (808KB) ( )

2000, 21 (4)： 44-46   

Study for flow resistance characteristics of the modelled laminated porous wall

Abstract ( ) PDF (967KB) ( )

2000, 21 (4)： 47-50   

Effect of temperature and rotational speed on radial clearance of turbine blade tip

Abstract ( ) PDF (830KB) ( )

2000, 21 (4)： 51-53   

Turbine engine composite route flight loading spectrum derivation

Abstract ( ) PDF (959KB) ( )

2000, 21 (4)： 54-56   

Calculating Hopf bifurcation point of a nonlinear rotor-bearing system

Abstract ( ) PDF (682KB) ( )

2000, 21 (4)： 57-59   

Calculation for effect of variable specific heat capacity on nozzle flow field and performance

Abstract ( ) PDF (773KB) ( )

2000, 21 (4)： 60-62   

Hypergolic propellant rocket engine combustion instability studies

Abstract ( ) PDF (984KB) ( )

2000, 21 (4)： 63-65   

Incomplete combustion test for solid rocket motors

Abstract ( ) PDF (763KB) ( )

2000, 21 (4)： 66-68   

Non-linear constitutive equation of HTPB composite solid propellant

Abstract ( ) PDF (959KB) ( )

2000, 21 (4)： 69-72   

Chelated titanate aids used in nitrate plasticized polyether propellant

Abstract ( ) PDF (1018KB) ( )

2000, 21 (4)： 73-76   

Effect of ethanolamine derivative aids on rheological properties of HTPB propellant slurry

Abstract ( ) PDF (1035KB) ( )

2000, 21 (4)： 77-80   

Fibre-optic image viewing system applied to combustion test

Abstract ( ) PDF (824KB) ( )

2000, 21 (4)： 81-83   

Simulated tests and data acquisition system for aerospike nozzle

Abstract ( ) PDF (1179KB) ( )

2000, 21 (4)： 85-88