PDF下载 分享
[1]闫 松,李 斌,李 锋,等.联合静力和动力试验数据修正机架的有限元模型[J].火箭推进,2021,47(05):56-64.
 YAN Song,LI Bin,LI Feng,et al.Finite element model updating of thrust frame combining static and dynamic test data[J].Journal of Rocket Propulsion,2021,47(05):56-64.
点击复制

联合静力和动力试验数据修正机架的有限元模型

参考文献/References:

[1] FRADY G,JENNINGS J,MIMS K,et al.Engine system loads analysis compared to hot-fire data[C]//43rd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference.Denver,Colorado.Reston,Virginia:AIAA,2002:1510. [2] CHRISTENSEN E,BROWN A,FRADY G. Calculation of dynamic loads due to random vibration environemnts in rocket engine systems[C]//48th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference. Honolulu,Hawaii. Reston,Virginia:AIAA,2007:1784. [3] CHRISTENSEN E,FRADY G,MIMS K,et al.Structural dynamic analysis of the X-34 rocket engine[C]//39th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics,and Materials Conference and Exhibit. Long Beach,CA. Reston,Virginia:AIAA,1998:2012. [4] BROWN A M. Temperature-dependent modal test/analysis correlation of X-34 FASTRAC composite rocket nozzle[J].Journal of Propulsion and Power,2002,18(2):284-288. [5] MULLER G R.Finite element models of the space shuttle main engine[R].NASA TM-78260,1980. [6] BAKER M,PRAY C. Understanding critical dynamic loads for nozzle and nozzle extension design[C]//47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. San Diego,California. Reston,Virginia:AIAA,2011:5686. [7] 杜飞平,谭永华,陈建华. 基于子结构试验建模综合的火箭发动机结构动力分析[J].推进技术,2015,36(10):1547-1553. [8] 叶莺樱.某新型发动机结构振动特性分析[D].北京:中国运载火箭技术研究院,2019. [9] 李斌.构建基础研究平台,推动液体动力技术创新发展[J].火箭推进,2014,40(1):1-9.LI B. Establishment of fundamental research platform for promoting innovative development of liquid propulsion technology[J].Journal of Rocket Propulsion,2014,40(1):1-9. [10] BERMAN A,NAGY E J.Improvement of a large analytical model using test data[J].AIAA Journal,1983,21(8):1168-1173. [11] MOTTERSHEAD J E,FRISWELL M I.Model updating in structural dynamics:a survey[J].Journal of Sound and Vibration,1993,167(2):347-375. [12] MARWALA T,SIBISI S.Finite element model updating using Bayesian framework and modal properties[J].Journal of Aircraft,2005,42(1):275-278. [13] 张安平,陈国平.基于混合人工鱼群算法的结构有限元模型修正[J].航空学报,2010,31(5):940-945. [14] 杨智春,王乐,李斌,等.结构动力学有限元模型修正的目标函数及算法[J].应用力学学报,2009,26(2):288-296. [15] XIAO F,HULSEY J L,CHEN G S.Multi-direction bridge model updating using static and dynamic measurement[J].Applied Physics Research,2015,7(1):47. [16] CATBAS F N,CILOGLU S K,HASANCEBI O,et al.Limitations in structural identification of large constructed structures[J].Journal of Structural Engineering,2007,133(8):1051-1066. [17] HORTA L G,REAVES M C,LDW J S.A procedure for static and dynamic model update of finite element models:application to an inflated/rigidized torus[C]//Proceeding of the IMAC XXIV:Conference and Exposition on Structural Dynamic.St Louis,Missouri:[s.n.],2006. [18] SCHLUNE H,PLOS M,GYLLTOFT K.Improved bridge evaluation through finite element model updating using static and dynamic measurements[J].Engineering Structures,2009,31(7):1477-1485. [19] SOL? M,HE L,LOMBAERT G,et al.Finite element model updating of a footbridge based on static and dynamic measurements[C]//Proceedings of the 4th International Conference on Computational Methods in Structural Dynamics and Earthquake Engineering(COMPDYN 2013).Kos Island,Greece.Athens:Institute of Structural Analysis and Antiseismic Research School of Civil Engineering National Technical University of Athens(NTUA)Greece,2014. [20] 闫松,李斌,李斌潮,等.三维扫描测振技术在液体火箭发动机模态试验中的应用[J].宇航学报,2017,38(1):97-103. [21] MOTTERSHEAD J E,LINK M,FRISWELL M I.The sensitivity method in finite element model updating:a tutorial[J].Mechanical Systems and Signal Processing,2011,25(7):2275-2296.

备注/Memo

基金项目:科工局稳定支持项目(HTKJ2020KL011007)
作者简介:闫松(1988—),男,博士,研究领域为结构动力学模型修正、载荷识别,非接触测试。

更新日期/Last Update: 1900-01-01