Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Journal of Rocket Propulsion》 2011-03
Add to Favorite Get Latest Update

Application of AMESim in dynamic characteristic simulation of liquid rocket engine system

PAN Hui,ZHANG Li-hui(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)  
According to the modular modeling idea and general simulation requirements,a general engine system simulation module library was developed on the basis of the secondary development of the AMESet platform in AMESim.The dynamic characteristic simulation of different types of liquid rocket engine systems was conducted.The research results show that the modeling process is simple and feasible.The correctness and reliability of adopted simulation method were preliminarily validated through comparison of calculated results and testing curves.The research work lays a good foundation for the general simulation of future liquid rocket engine systems.
【CateGory Index】: V434
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
Chinese Journal Full-text Database 1 Hits
1 SU Long-fei~1,ZHANG Li-hui~1,PAN Hai-lin~2 (1.School of Astronautics, Beijing University of Aeronautics and Astronautics,Beijing100083,China; 2.Beijing Control Engineering Inst,Beijing100080,China);Numerical Simulation on the Starting Process of Satellite Propulsion System[J];Journal of Aerospace Power;2005-04
Chinese Journal Full-text Database 10 Hits
1 Chen Yang Cai Guobiao Zhang Zhenpeng(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191,China)Xia Jixia(Beijing Institute of Control Engineering,Beijing 100190,China);Numerical simulation on dynamic stability of pressure reducing regulator in integral bipropellant propulsion system[J];Journal of Beijing University of Aeronautics and Astronautics;2010-10
2 Dou Wei(Beijing Aerospace Propulsion Institute,Beijing,100076);Pressure Drop and Experiment of Liquid Rocket Engine Filter[J];Missiles and Space Vehicles;2011-01
3 YIN Jiawa1,LIAO Ying 2,JIN Guangming 3,HU Xiaoping 2,ZHANG Shaoyong 1(1 College of Information Engineering,Xiangtan University,Hunan Xiangtan 411105,China;2 College of Aerospace and Material Engineering,NUDT,Changsha 410073,China;3 Shanghai Institute of Space Propulsion,Shanghai 200233,China);The Research on Influence of Low Freezing Point Propellant on Performance of Liquid-propellant Rocket Engine[J];Journal of Projectiles,Rockets,Missiles and Guidance;2009-04
4 FAN Zhong-ze1,HUANG Min-chao2,YU Yong3,ZHU Heng-wei3(1.College of Electric and Information Engineering,Xi'an Jiaotong University,Xi'an 710049,China;2.College of Aerospace and Material Engineering,National Univ.of Defense Technology,Changsha 410073,China;3.Equipment Academe of the Second Artillery,Beijing 100085,China);Modular Model of Space Propulsion System in the Whole Operation Process[J];Journal of National University of Defense Technology;2007-02
5 LIU Jing-hua,TAN Jian-guo,YANG Tao,WANG Zhen-guo(College of Aerospace and Material Engineering,National Univ.of Defense Technology,Changsha 410073,China);Research on Low-frequency Oscillation in Hydrogen Peroxide Engine[J];Journal of National University of Defense Technology;2007-05
6 FAN Zhong-ze1,HUANG Min-chao2(1.School of Electric and Information Engineering,Xi'an Jiaotong Univ.,Xi'an 710049,China;2.College of Aerospace and Material Engineering,National Univ.of Defense Technology,Changsha 410073,China);Fault Simulation of Space Power System in the Operation Process[J];Journal of National University of Defense Technology;2008-02
7 YANG Shi-lin,GAO Bo,DONG Xin-gang(National Key Laboratory of Combustion,Flow and Thermo-structure,The 41st Institute of the Fourth Academy of CASC,Xian 710025,China);Analysis on dynamic characteristics of regulable flow gas generator with sliding discal valve[J];Journal of Solid Rocket Technology;2009-05
8 Li Longfei,Chen Jianhua,Liu Zhanguo(Xi'an Aerospace Propulsion Institute,Xi'an,710100);Control Techniques of High Frequency Combustion Instability for High Thrust LOX/Kerosene Staged Combustion Cycle Engine[J];Missiles and Space Vehicles;2011-03
9 Liu Feng, Zhou Jin (College of Astronautics and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China);Analysis of the unbalanced depletion of the propellant for the metal diaphragm tank[J];Journal of Rocket Propulsion;2006-05
10 1Chen Yang, 1Gao Fang, 1Zhang Zhenpeng, 2Zhu Zihuan(1 School of Astronautics,Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;2 Beijing Institute of Aerospace Testing Technology, Beijing 100074, China );Dynamic simulation of working process for control system of a pneumatic diaphragm control valve[J];Journal of Rocket Propulsion;2006-06
【Secondary Citations】
Chinese Journal Full-text Database 6 Hits
1 ZHANG Li-hui~1,LI Jia-wen~1,ZHANG Xue-mei~1, JIN Guang-ming~2,WEI Yan-xiang~2 (1.School of Astronautics,Beijing University of Aeronautics and Astronautics, Beijing100083,China; 2.Shanghai Institute of Power Machinery,Shanghai200233, China);Dynamic Characteristics Study of Spacecraft Propulsion System Engine[J];Journal of Aerospace Power;2004-04
2 CHENG Mou-sen,LIU Kun,ZHANG Yu-lin(Inst.of Aerospace and Material Engineering,National Univ. of Defence Technology, Changsha 410073,China);One-dimensional finite element solutions for liquid transients in propellant feedlines[J];JOURNAL OF PROPULSION TECHNOLOGY;2000-04
3 NIE Wan sheng 1,CHEN Xin hua 1,DAI De hai 2,XIA Peng 1,ZHUANG Feng chen 1(1 Inst. of Equipment Command and Technology, Beijing 101416, China; 2 Shanghai Inst. of Power Machinery, Shanghai 200233, China);Transient characteristics during shutdown operation of liquid feed line for attitude control propulsion subsystem[J];Journal of Propulsion Technology;2003-01
4 LI Jia-wen~1, ZHANG Li-hui~1, ZHANG Xue-mei~1, JIN Guang-ming~2, WEI Yan-xiang~2(1.School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083, China;2.Shanghai Inst. of Space Propulsion, Shanghai 200233, China);Simulation software for the static and dynamic characteristics of space propulsion system[J];Journal of Propulsion Technology;2004-02
5 CHEN Xin hua 1, NIE Wan sheng 1, DAI De hai 2 (1.Department of Test Engineering,the Academy of Equipment Command & Technology, Beijing 10416, China; 2.801 Research Institute of China Aerospace Science and Technology Corporation,Shanghai 200233,China);Numerical Simulation of Pulse Operation for Small Thrust Liquid Rocket Propulsion System[J];Journal of Institute of Command and Technology;2003-01
6 Shen Chibing Chen Qizhi (Dept of Astronautical Technology, National University of Defense Technology·Changsha·410073);ANALYSIS OF THE STARTING PROCESS OF LOW THRUST PROPULSION SYSTEM[J];JOURNAL OF ASTRONAUTICS;1997-03
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved