Journal of Propulsion Technology 2000 Issue 4 srmu xin pen guan cai liao shi che cheng gong

srmu xin pen guan cai liao shi che cheng gong

..............page:62

tech56 xiang mu zhong de wo lun shi yan
feng yong hong

..............page:35

ge yu pw gong si wei mei jun yan zhi zhi sheng ji fa dong ji
feng yong hong

..............page:23

1999 nian yun zai huo jian de yi wai shi gu

..............page:19

xi qi shi huo jian fa dong ji de gai jin
feng yong hong

..............page:4

ba dun han jie yan jiu suo de pen tu ji shu
pan li hua

..............page:83-84

Simulated tests and data acquisition system for aerospike nozzle
DAI Wu-ye;LIU Yu;CHENG Xian-Chen

..............page:85-88

Fibre-optic image viewing system applied to combustion test
LI Ming;SONG Wen-yan;JI Zhong-ying

..............page:81-83

Effect of ethanolamine derivative aids on rheological properties of HTPB propellant slurry
LU Guo-lin;WANG Bei-hai

..............page:77-80

Chelated titanate aids used in nitrate plasticized polyether propellant
LI Hong-xu;DENG Jian-ru;TANG Han-xiang

..............page:73-76

Non-linear constitutive equation of HTPB composite solid propellant
ZHANG Yong-jing;ZHAO Guang-hui;YANG Jian-hong;QIANG Hong-fu

..............page:69-72

Incomplete combustion test for solid rocket motors
HAN Yu

..............page:66-68

Hypergolic propellant rocket engine combustion instability studies
NIE Wan-sheng;ZHUANG Feng-chen

..............page:63-65,76

Calculation for effect of variable specific heat capacity on nozzle flow field and performance
WANG Zhan-xue;WANG Jian-feng;TANG Di-yi

..............page:60-62

Calculating Hopf bifurcation point of a nonlinear rotor-bearing system
ZHANG Xin-jiang;XIA Song-bo;WU Xin-hua;HAN Wan-jin

..............page:57-59

Turbine engine composite route flight loading spectrum derivation
SONG Ying-dong;GAO De-ping

..............page:54-56,72

Effect of temperature and rotational speed on radial clearance of turbine blade tip
GUO Shu-fen;XU Bo

..............page:51-53

Study for flow resistance characteristics of the modelled laminated porous wall
YU Xin-hua;DONG Zhi-rui;LIU Song-ling;YOU Shao-kun

..............page:47-50

Identification of nonlinear mathematic model of Air pressure buffer
YU Da-ren;YAN Zhi-gang;BAO Wen;SHI Xin-xing;HE Bao-cheng

..............page:44-46

Numerical calculation for flow and heat transfer of a shrouded rotating disk with high-positioned air-inlet
XU Guo-qiang;ZHAN Guo-zhi;DING Shui-ting;TAO Zhi;LUO Xiang

..............page:40-43

Numerical study on flow field in 2-D segment compression supersonic intake for an air-to-air missile
WANG Guo-hui;LI Jin-xian;CAI Ti-min

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

Numerical simulation of nonlinear gas oscillations in closed pipe
LIU Jun;GUO Zheng;QU Zhang-hua

..............page:32-35

Numerical simulation of 3-D unsteady turbulent flow in SRM chamber with finocyl grain
XIANG Hong-jun;FANG Guo-yao

..............page:27-31

Numerical simulation of plug nozzle flow field
GUO Zheng;LIU Jun;QU Zhang-hua

..............page:24-26

Effect of mixing tube area and position on performances for lobed ejector
WANG Guang-zhen;WU Shou-sheng;WANG Zhi-shan;WEI Fu-qing

..............page:20-23

New sealing structure of high pressure liquid rocket engine
DU Tian-en

..............page:16-19

One-dimensional finite element solutions for liquid transients in propellant feedlines
CHENG Mou-sen;LIU Kun;ZHANG Yu-lin

..............page:12-15

Numerical investigation of the flow field inside the liquid hydrogen inducer
YI Tong-xun;CHENG Fang-zhen;SUO Yi-sheng;JIANG Zi-kang

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

Starting and accelarating the missle turbojet engine by ground test
ZHENG Yan

..............page:5-8

Propulsion system stability control for super-maneuvering flight
WANG Li-feng;ZHANG Jin

..............page:1-4