Journal of Propulsion Technology 2003 Issue 1 2002 nian xiao wo pen ( shan ) fa dong ji ying yong yan jiu jin zhan

2002 nian xiao wo pen ( shan ) fa dong ji ying yong yan jiu jin zhan

..............page:66

tui jin ji shu rong huo " bai zhong zhong guo jie chu xue shu qi kan " cheng hao

..............page:46

CAD/CAM software for integrated blade of missile turbine engine
shao jin wen ; zhang zhen jia ; ma yu lin

..............page:93-96

High resolution inspecting investigation for inner defect of SRM.
lu hong yi ; yang xing gen ; sun you tian

..............page:90-92

Technological methods on increasing storage life of HTPB propellants
wang chun hua ; peng wang da ; weng wu jun ; zhang ren

..............page:87-89

Catalysis of nanocomposite CuO·Cr2O3 on thermal decomposition of RDX
hong wei liang ; liu jian hong ; tian de yu ; gui yang ; ren xiang zhong ; zhao feng qi

..............page:83-86

Effect of the burning rate regulator on the thermal behavior of RDX/AP/HTPB propellant
zhao feng qi ; chen pei ; li shang wen ; yin cui mei ; liu zi ru

..............page:80-82

Effect of chain extender on the mechanical properties of NEPE propellant
zhao xiao bin ; zhang xiao ping ; zheng jian ; du lei

..............page:74-79

Experimental investigation on combustion instability of tripropellant rocket engine
huang yu hui ; wang zhen guo ; zhou jin

..............page:71-73,89

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

..............page:67-70

Investigation of deflagration to detonation transition distance in a tube with mixture
han qi xiang ; wang jia zuo ; wang bo

..............page:63-66

Flamelet modeling of turbulent jet non-premixed flame
wang hai feng ; chen yi liang ; cai xiao dan ; li yi

..............page:58-62

Detection of compressor stall based on wavelet analysis
jiang tao ; jia zhi wei ; li ying hong

..............page:55-57

New model to calculate the film cooling effectiveness
zhu hui ren ; liu song ling

..............page:51-54

Spray characteristics of transverse unlike impinging platelet injector
cao yong ; guo zhi hui ; huang yong

..............page:47-50,86

Numerical simulation on three-dimensional separation of cooling jet in cascade
yang ke ; wang song tao ; wang zhong qi ; feng guo tai

..............page:43-46

Influence of propellant crack on turbulence flow in solid rocket motor
hu chun bo ; he guo qiang ; wei jin jia ; liu pei jin ; cai ti min

..............page:40-42

Numerical study on the flowfields of the zero-second-flow annular supersonic air ejectors
xu wan wu ; wang zhen guo

..............page:36-39

Turbulent flow calculation for a tail-pipe nozzle using multiblock algorithm and finite volume method
dan lin peng ; zhang zhen peng ; zhao yong zhong ; jia yong gang

..............page:33-35

Experimental and numerical investigation of a swirl atomizer
wang guo hui ; cai ti min ; he guo qiang ; hu chun bo

..............page:28-32

High-accuracy software for misalignment-thrust calculation in rocket nozzle
chen jun ; dong shi yan ; ji zong de

..............page:24-27

Aerodynamic stability analysis of inlet total pressure distortion for turbofan
cheng bang qin ; tao zeng yuan ; li jun

..............page:21-23

Multi-fault diagnosis for turbo-pump based on neural network
zhang zuo ; zhang yu xiang ; huang xian xiang

..............page:17-20,39

Analysis of installation performance of the missile turbojet engine
wang zhan xue ; qiao wei yang ; cai yuan hu

..............page:12-16

Prediction of acceleration and stability for variable nozzle turbofan engine
wang jin ; lin hong zhen

..............page:9-11

Transient characteristics during shutdown operation of liquid feed line for attitude control propulsion subsystem
nie wan sheng ; chen xin hua ; dai de hai ; xia peng ; zhuang feng chen

..............page:6-8

Conceptual design model of rocket base combined cycle propulsion system
huang sheng hong ; he hong qing ; he guo qiang ; liu pei jin ; qin fei ; wang guo hui

..............page:1-5