Conceptual design model of rocket base combined cycle propulsion system

Abstract ( ) PDF (1402KB) ( )

2003, 24 (1)： 1-5   

Transient characteristics during shutdown operation of liquid feed line for attitude control propulsion subsystem

Abstract ( ) PDF (760KB) ( )

2003, 24 (1)： 6-8   

Prediction of acceleration and stability for variable nozzle turbofan engine

Abstract ( ) PDF (826KB) ( )

2003, 24 (1)： 9-11   

Analysis of installation performance of the missile turbojet engine

Abstract ( ) PDF (1340KB) ( )

2003, 24 (1)： 12-16   

Multi-fault diagnosis for turbo-pump based on neural network

Abstract ( ) PDF (1491KB) ( )

2003, 24 (1)： 17-20   

Aerodynamic stability analysis of inlet total pressure distortion for turbofan

Abstract ( ) PDF (854KB) ( )

2003, 24 (1)： 21-23   

High-accuracy software for misalignment-thrust calculation in rocket nozzle

Abstract ( ) PDF (1072KB) ( )

2003, 24 (1)： 24-27   

Experimental and numerical investigation of a swirl atomizer

Abstract ( ) PDF (1398KB) ( )

2003, 24 (1)： 28-32   

Turbulent flow calculation for a tail-pipe nozzle using multiblock algorithm and finite volume method

Abstract ( ) PDF (758KB) ( )

2003, 24 (1)： 33-35   

Numerical study on the flowfields of the zero second-flow annular supersonic air ejectors

Abstract ( ) PDF (1148KB) ( )

2003, 24 (1)： 36-39   

Influence of propellant crack on turbulence flow in solid rocket motor

Abstract ( ) PDF (777KB) ( )

2003, 24 (1)： 40-42   

Numerical simulation on three-dimensional separation of cooling jet in cascade

Abstract ( ) PDF (1260KB) ( )

2003, 24 (1)： 43-46   

Spray characteristics of transverse unlike impinging platelet injector

Abstract ( ) PDF (1390KB) ( )

2003, 24 (1)： 47-50   

New model to calculate the film cooling effectiveness

Abstract ( ) PDF (1175KB) ( )

2003, 24 (1)： 51-54   

Detection of compressor stall based on wavelet analysis

Abstract ( ) PDF (864KB) ( )

2003, 24 (1)： 55-57   

Flamelet modeling of turbulent jet non-premixed flame

Abstract ( ) PDF (1485KB) ( )

2003, 24 (1)： 58-62   

Investigation of deflagration to detonation transition distance in a tube with mixture

Abstract ( ) PDF (1071KB) ( )

2003, 24 (1)： 63-66   

Numerical study on chemical mechanism in supersonic H₂/Air mixture gas flow

Abstract ( ) PDF (1213KB) ( )

2003, 24 (1)： 67-70   

Experimental investigation on combustion instability of tripropellant rocket engine

Abstract ( ) PDF (1117KB) ( )

2003, 24 (1)： 71-73   

Effect of chain extender on the mechanical properties of NEPE propellant

Abstract ( ) PDF (1862KB) ( )

2003, 24 (1)： 74-79   

Effect of the burning rate regulator on the thermal behavior of RDX/AP/HTPB propellant

Abstract ( ) PDF (898KB) ( )

2003, 24 (1)： 80-82   

Catalysis of nanocomposite CuO·Cr₂O₃ on thermal decomposition of RDX

Abstract ( ) PDF (1157KB) ( )

2003, 24 (1)： 83-86   

Technological methods on increasing storage life of HTPB propellants

Abstract ( ) PDF (814KB) ( )

2003, 24 (1)： 87-89   

High resolution inspecting investigation for inner defect of SRM.

Abstract ( ) PDF (856KB) ( )

2003, 24 (1)： 90-92   

CAD/CAM software for integrated blade of missile turbine engine

Abstract ( ) PDF (1072KB) ( )

2003, 24 (1)： 93-96