Journal of Propulsion Technology 2008 Issue 1 tui jin ji shu tou gao xu zhi

..............page:封4

Influence of thermoplastic polyurethane on mechanical properties of modified double base propellants
FAN Xi-ping;TAN Hui-min;ZHANG Lei;CHU Li-qiu

..............page:124-128

Preparation of NiO/CNTs composites and their effects on the thermal decomposition of AP and AP/HTPB
LIU Jian-xun;LIU Yong;ZHANG Xiao-juan;JIANG Wei;WANG Zuo-shan;LI Feng-sheng

..............page:119-123

Modeling for mechanical properties of HTPB solid propellants
TIAN De-yu;HONG Wei-liang;LIU Jian-hong;LI Shao-ning;LIU Jing-feng;CAI Hong-hua;CHEN Zhou-wu

..............page:114-118

Improvement of combustion heat testing equipment of fuel-rich propellant based on boron
WANG Ying-hong;DENG Yong-feng;ZHANG Xiao-hong;PAN Kuang-zhi

..............page:110-113

Properties of a fast-burning ballistic modifier coated by polyurethane and its effect on propellant combustion
RAN Xiu-lun;YANG Rong-jie;LIU Chun;WANG Xiao-fei

..............page:105-109

Ignition characteristics of boron-based fuel-rich propellants
FAN Hong-jie;WANG Ning-fei;FAN Xue-zhong;GUAN Da-lin

..............page:102-104

Combustion physical model of the ethylene oxide-tetrahydrofuran copolymers type gas generating propellant
TANG Gen;DENG Kang-qing

..............page:98-101

Numerical simulation of hall thruster plume
QIAN Zhong;WANG Ping-yang;DU Zhao-hui;KANG Xiao-lu

..............page:93-97

Analysis for fracture characteristic of pre-cracked directionally solidified turbine blades
WEI Da-sheng;WANG Yan-rong;LI Wei

..............page:89-92

Application of immune feedback mechanism on aeroengine control
ZHOU Wen-xiang;HUANG Jin-quan;ZHANG Jun-feng

..............page:84-88

An aeroengine fault detection method based 0n kernel principal component analysis
HU Jin-hai;XIE Shou-sheng;CHEN Wei;HOU Sheng-li;CAI Kai-long

..............page:79-83

Flight test investigation for an integrated ducted rocket
GU Yan-wu

..............page:75-78

Numerical simulation of the vortex generator jets for low-pressure turbine separation control
ZHANG Man;QIAO Wei-yang

..............page:67-74

Basic analysis Of a counter-rotating turbine
JI Lu-cheng;SHAO Wei-Wei;WANG Bao-chen

..............page:62-66

Effect of jet flow distribution on fluidic throat skewing nozzle
ZHOU Min;WANG Ru-gen;ZHANG Xiang-yi;XU Xue-miao

..............page:58-61

Influence of back pressure on location of shock train in isolator
JIN Liang;WU Xian-yu;LUO Shi-bin;WANG Zhen-guo

..............page:54-57

Curved surface structure of internal contraction tunnel/isolator of two-dimensional hypersonic inlet
ZHANG Xiao-jia;LIANG De-wang;HUANG Guo-ping

..............page:49-53

Concept of a Varied geometry scramjet inlet with rotatable cowl
JIN Zhi-guang;ZHANG Kun-yuan

..............page:43-48

Dynamic analysis on extendible exit cone nozzle of solid rocket motor during extending
YOU Jun-feng;XIAO Jin-you;ZHANG Duo;GAN Xiao-song;REN Quan-bin

..............page:37-42

Large-eddy simulation of premixed combustion and validation of the combustion model
WANG Fang;ZHOU Li-xing;XU Chun-xiao;HUANG Yong

..............page:33-36

2D numerical simulation for detonation wave
LUO Jun;HE Li-ming;CHEN Deng

..............page:29-32

An experiment on flow structures of a round jet impinging on concave surfaces
LIU Zhen-xiong;MAO jun-kui;BU Ji-Xing

..............page:25-28

Test of unlike impinging injector atomization characteristic with gelled water
ZHANG Meng-zheng;YANG Wei-dong;WANG Mei

..............page:22-24,61

Numerical simulation of particle collision and impingement for a model SRM
LI Qiang;LI Jiang;LIU Pei-jin;HE Guo-qiang

..............page:18-21

Ultrasonic image diagnoses for multi-layered adhesive structure in solid rocket motor
ZHANG Ji-tang;LU Hong-nian;CAO Fu-qi

..............page:13-17

Preliminary analysis of spinning solid rocket motor dynamics stability
YANG Dan;GAO Ye;XIONG Yong-liang

..............page:8-12

Solid rocket motor structure selection based 0n knowledge reuse
GU Jian-guang;ZHANG Wei-hua;WANG Zhong-wei

..............page:1-7