|Table of Contents|

Research progress on numerical simulation technology of liquid rocket engine dynamic characteristics(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2017年05期
Page:
1-6
Research Field:
专论与综述
Publishing date:

Info

Title:
Research progress on numerical simulation technology of liquid rocket engine dynamic characteristics
Author(s):
LI Yuanqi; LIU Hongjun; XU Haohai; CHEN Hongyu
Science and Technology on Liquid Rocket Engine Laboratory, Xi'an 710100, China
Keywords:
research progress;  liquid rocket engine;  dynamic characteristic;  simulation technology
PACS:
V430-34
DOI:
-
Abstract:
The numerical simulation technology is one of the important methods to investigate the dynamic characteristics of liquid rocket engine(LRE).A review on numerical simulation technology of LRE dynamic characteristics is done in this paper.Development of the technology can be divided into three stages: special simulation program phase,general simulation software phase and multidisciplinary collaborate simulation phase.Key work of each developing phase is summarized and evaluated.Main characteristics of the simulation technology in each stage are analyzed.Based on summary of the research progress,the development direction of the future numerical simulation technology of LRE dynamic characteristics is proposed.

References:

[1] POWELL M F, BUTLER P T. Ground test simulation of rocket engine start transients: AIAA 75-1273 [R]. USA: AIAA, 1975.
[2] MEYER C M, MAUL W A. The application of neural networks to the SSME startup transient: NASA CR-187138 [R]. USA: NASA, 1991.
[3] KANMURI A, KANDA T, WAKAMATSU Y, et al. Transient analysis of LOX/LH2 rocket engine(LE-7): AIAA 89-2736 [R]. USA: AIAA, 1989.
[4] BAUDART P A, DUTHOIT V, HARLAY J C. Numerical simulation of cryotechnic rocket engine ignition: AIAA 91-2290 [R]. USA: AIAA, 1991.
[5] 徐浩海. 液氧煤油补燃发动机起动过程研究[D]. 西安: 中国航天科技集团公司第六研究院第十一研究所, 2003.
[6] 杨永强. 液氧煤油补燃发动机强迫起动过程研究[D]. 西安: 中国航天科技集团公司六院11所, 2005.
[7] MASON J R, SOUTHWICK R D. Large liquid rocket engine transient performance simulation system final report: NASA-CR-184099 [R]. USA: NASA, 1991.
[8] BINDER M P. An RL 10A-3-3A rocket engine model using the rocket engine transient simulator(ROCETS)software: AIAA 93-2357 [R]. USA: AIAA, 1993.
[9] FOLLETT R F, TAYLOR R P. Liquid rocket propulsion dynamic flow modeling using the ROCETS engineering modules in the EASY5x environment: AIAA 93-2599 [R]. USA: AIAA, 1993.
[10] ORDONNEAU G, ALBANO G, MASSE J. CARINS: A future versatile and flexible tool for engine transient prediction [C]// Proceedings of 4th International Conference on Launcher Technology. Liege Belgium: [s.n.], 2002: 111-120.
[11] YAMANISHI N, KIMURA T, TAKAHASHI M, et al. Transient analysis of the LE-7A rocket engine using the rocket engine dynamic simulator(REDS): AIAA 2004-3850 [R]. USA: AIAA, 2004.
[12] ISSELHORST A. HM7B simulation with ESPSS tool on Ariane 5 ESC-A upper stage: AIAA 2010-7047 [R]. USA: AIAA, 2010.
[13] DI MATTEO F, DE ROSA M, ONOFRIX M. Start-up transient simulation of a liquid rocket engine: AIAA 2011-6032 [R]. USA: AIAA, 2011.
[14] DI MATTEO F, DE ROSA M. Steady state library for liquid rocket engine cycle design: AIAA 2011-6033 [R]. USA: AIAA, 2011.
[15] 潘辉, 张黎辉. AMESim软件在液体火箭发动机系统动态仿真上的应用[J]. 火箭推进, 2011,37(3): 6-11.
PAN Hui, ZHANG Lihui. Application of AMESim in dynamic characteristic simulation of liquid rocket engine system [J]. Journal of rocket propulsion, 2011, 37(3): 6-11.
[16] 李锦江. 一种低温发动机系统动态仿真的快捷方法[J]. 导弹与航天运载技术, 2012(1): 13-17.
[17] 晏政, 刘泽军, 程玉强, 等. 航天器推进系统模块化建模方法[J]. 国防科技大学学报, 2012,34(4): 28-32.
[18] 尤裕荣, 赵双龙, 吴宝元, 等. 基于AMESim的冲压发动机燃油调节器动态特性仿真[J]. 火箭推进, 2010,36(4): 12-15.
YOU Yurong, ZHAO Shuanglong, WU Baoyuan. A simulation on dynamic characteristics of ramjet fuel regulator based on AMESim [J]. Journal of rocket propulsion, 2010,36(4): 12-15.
[19] 黄敏超, 王新建, 王楠. 补燃循环液体火箭发动机启动过程的模块化仿真[J]. 推进技术, 2001,22(2): 101-103.
[20] 樊忠泽, 黄敏超, 余勇, 等. 空间推进系统工作过程的模块化建模[J]. 国防科技大学学报, 2007,29(2): 29-33.
[21] 魏鹏飞, 吴建军, 刘洪刚, 等. 液体火箭发动机一种通用模块化仿真方法[J]. 推进技术, 2005,26(2): 147-150.
[22] 刘昆, 张育林, 程谋森. 液体火箭发动机系统瞬变过程模块化建模与仿真[J]. 推进技术, 2003,24(5): 401-405.
[23] 张黎辉, 李伟, 段娜. 液体火箭发动机模块化通用仿真[J]. 航空动力学报, 2011,26(3): 687-691.
[24] 刘红军. 补燃循环发动机静态特性与动态响应特性研究[D]. 西安: 航天工业总公司第十一研究所, 1998.
[25] 吕鹏翾. 液体火箭发动机工作过程数值仿真[J]. 火箭推进, 2004,30(5):10-17.
LÜ Pengxuan. Numerical simulation of operation process of liquid rocket engine [J]. Journal of rocket propulsion, 2004, 30(5): 10-17.
[26] 肖立明, 罗巧军. 膨胀循环发动机起动过程研究[J]. 火箭推进, 2007,33(1):7-11.
XIAO Liming, LUO Qiaojun. Investigation on start-up process of expander cycle liquid propellant rocket engine [J]. Journal of rocket propulsion, 2007, 33(1): 7-11.
[27] HONGYU C, HONGJUN L, LIU H. A tool for simulation and analysis of space propulsion systems transient performance [C]// 6th CSA-IAA Conference. Shanghai, China: CSA, 2015: 211-216.
[28] 陈宏玉, 刘红军, 陈建华. 补燃循环发动机强迫起动过程[J]. 航空动力学报, 2015,30(12):3010-3016.
[29] LYTLE J K. The numerical propulsion system simulation: an overview: NASA/TM- 2000-209915 [R]. USA: NASA, 2000.
[30] FOLLEN G, AUBUCHON M. Numerical zooming between a NPSS engine system simulation and a one-dimensional high compressor analysis code: NASA/TM-2000-209913 [R]. USA: NASA, 2000.

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Last Update: 2017-11-10