1672-9374
2015 Issue 4
Research progress about rocket based combined cycle combustion organization
CUI Peng;,XU Wanwu;,CHEN Jian;,SONG Changqing;
CUI Peng;,XU Wanwu;,CHEN Jian;,SONG Changqing;
..............page:1-7
Development of 1 000 N bipropellant orbit control engine with light weight and high specific impulse
LIU Xiaowei;,YAO Mingming;,LI Jiaming;,CAO Jing;,QU Haijun;
LIU Xiaowei;,YAO Mingming;,LI Jiaming;,CAO Jing;,QU Haijun;
..............page:8-12,42
Numerical simulation of flow process in screw centrifugal nozzle
WU Gaoyang;,ZHENG Gang;,NIE Wansheng;,QIAO ye;
WU Gaoyang;,ZHENG Gang;,NIE Wansheng;,QIAO ye;
..............page:13-18
Study on dynamic response characteristics of droplet evaporation in pressure oscillation environment
YIN Ting;,WU Gaoyang;,NIE Wansheng;
YIN Ting;,WU Gaoyang;,NIE Wansheng;
..............page:19-28
Simulated analysis on nozzle dynamic characteristics based on high-order WENO scheme
LIANG Junlong;,ZHANG Guitian;,QIN Yanping;
LIANG Junlong;,ZHANG Guitian;,QIN Yanping;
..............page:29-36
Research on formation mechanism of negative pressure phenomenon in propellant pipeline
CAO Wei;,WANG Rui;,CHEN Jian;,WEI Yanxiang;,JIN Guangming;,LIU Feng;
CAO Wei;,WANG Rui;,CHEN Jian;,WEI Yanxiang;,JIN Guangming;,LIU Feng;
..............page:37-42
Impact of sidewall rocket on engine nozzle
LIU Xiaowei;,LI Yongzhou;
LIU Xiaowei;,LI Yongzhou;
..............page:43-47
Analysis on thermodynamic cycle characteristics of air-turbo-rocket engine
LI Wen-long;,GUO Hai-bo;,NAN Xiang-yi;
LI Wen-long;,GUO Hai-bo;,NAN Xiang-yi;
..............page:48-54
A rapid optimization design method for frame structure of double thrust chambers
HUO Shihui;,YUAN Junshe;,XU Xuejun;,YANG Sa;
HUO Shihui;,YUAN Junshe;,XU Xuejun;,YANG Sa;
..............page:55-60
Mass calculation of key assembly units in LH2/LOX rocket engine based on visual interface
XUE wei;,CAI Zhenyu;,CAO Hongjuan;,GE Qingming;
XUE wei;,CAI Zhenyu;,CAO Hongjuan;,GE Qingming;
..............page:61-66,73
Physicochemical characteristic analysis on shoulder ring flaw of pressure boost gas valve in liquid oxygen supply system
QIN Yongtao;,GAO Qiang;,WU Rongyan;,YANG Zhanwei;,TIAN Baoyun;
QIN Yongtao;,GAO Qiang;,WU Rongyan;,YANG Zhanwei;,TIAN Baoyun;
..............page:67-73
Influence of temperature on tank pressurization system
MU Penggang;,TONG Fei;,PU Guangrong;,MA Jian;
MU Penggang;,TONG Fei;,PU Guangrong;,MA Jian;
..............page:74-78
Integration design system for turbo pump in rocket engine
ZHANG Chenxi;,MA Xiaodan;
ZHANG Chenxi;,MA Xiaodan;
..............page:79-83
International standard minimization improvement of horizontal miniwatt high-speed pump
ZHANG Liqiang;,LIU Haili;,GAO Hong;
ZHANG Liqiang;,LIU Haili;,GAO Hong;
..............page:84-89,104
Design and calculation of casting head for high strength stainless steel centrifugal impeller
JI Yanqing;,CHEN Pengrong;
JI Yanqing;,CHEN Pengrong;
..............page:90-94
Analysis of effects of bellows in front of pump on thrust measurement
SHEN Jibin;,ZENG Xiaojun;,CAO Qinghong;
SHEN Jibin;,ZENG Xiaojun;,CAO Qinghong;
..............page:95-99
..............page:封3
Method of valve fault detection based on sound pressure measurement
ZHANG Shaobo;,WANG Naishi;,CHEN Haifeng;,ZHANG Junfeng;
ZHANG Shaobo;,WANG Naishi;,CHEN Haifeng;,ZHANG Junfeng;
..............page:100-104
Discussion of analytic technique for LRE test data storage
DONG Dong;,QIAO Jianghui;,ZHU Chengliang;,LIU Xiao;,BAI Wenyi;
DONG Dong;,QIAO Jianghui;,ZHU Chengliang;,LIU Xiao;,BAI Wenyi;
..............page:105-108,112
A flow calibration system for orbit-control engine of satellite
LIU Wanlong;,TIAN Guohua;,XU Xin;,SUN Shujiang;,ZHU Haowei;
LIU Wanlong;,TIAN Guohua;,XU Xin;,SUN Shujiang;,ZHU Haowei;
..............page:109-112