Dynamic Similarity Design Method for Vibration Response of Impact Test of Straight Blades
HE Fengxia1,2, LUO Zhong1,2,3, LI Lei1,2, LI Yuqi1,2
1. School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819; 2. Key Laboratory of Vibration and Control of Aero-Propulsion System Ministry of Education, Northeastern University, Shenyang 110819; 3. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian Universityf Technology, Dalian 116024
HE Fengxia, LUO Zhong, LI Lei, LI Yuqi. Dynamic Similarity Design Method for Vibration Response of Impact Test of Straight Blades[J]. Journal of Mechanical Engineering, 2021, 57(9): 71-77.
[1] 陈兆林,杨智春,王用岩,等. 基于能量有限元法和虚拟模态综合法的高频冲击响应分析方法[J]. 航空学报. 2018,39(8):182-191. CHEN Zhaolin,YANG Zhichun,WANG Yongyan,et al. A high-frequency shock response analysis method based on energy finite element and virtual mode synthesis and simulation[J]. Acta Aeronautica et Astronautica Sinica,2018,39(8):182-191. [2] SHORTER P J,LANGLEY R S. Vibro-acoustic analysis of complex systems[J]. Journal of Sound and Vibration,2005,288(3):669-699. [3] MACE B R,SHORTER P J. Energy flow models from finite element analysis[J]. Journal of Sound and Vibration,2000,233(3):369-389. [4] DALTON E C. Ballistic shock response by an extension of statistical energy analysis[C]//63rd Shock and Vibration Symposium,VA:AIAA,1992. [5] DALTON E,CHAMBERS N S I B,CHAMBERS N S I I. Analysis and validation testing of impulsive load response in complex,multi-compartmented structures[S]. Los Angeles:American Institute of Aeronautics and Astronautics,1995. [6] DALTON E C. High frequency shock prediction in multiply-connected plate structures[C]//64rd Shock and Vibration Symposium,VA:AIAA,1993. [7] 彭志刚. 基于统计能量法的星箭解锁冲击响应谱分析[D]. 哈尔滨:哈尔滨工业大学,2015. PENG Zhigang. Shock response spectrum analysis of unlocking about separation between satellite and rovket based on statistical energy analysis[D]. Harbin:Harbin Institute of Technology,2015. [8] SHOKRIEH M M,ASKARI A. Similitude study of impacted composite laminates under buckling loading[J]. Journal of Engineering Mechanics,2013,139(10):1334-1340. [9] MAZZARIOL L M,OSHIRO R E,ALVES M. A method to represent impacted structures using scaled models made of different materials[J]. International Journal of Impact Engineering,2016,90:81-94. [10] 张玮,韩晨健,杜志鹏,等. 集成桅杆缩比模型冲击试验方法研究[J]. 兵工学报,2015,36(S1):206-212. ZHANG Wei,HAN Chenjian,DU Zhipeng,et al. Research on impact experimental method for synthesis mast scaling model[J]. Acta Armamentarii,2015,36(S1):206-212. [11] 张文笛,罗忠,于清文,等. 直板叶片振动响应试验的相似关系确定方法[J]. 航空发动机. 2019,45(5):63-69. ZHANG Wendi,LUO Zhong,YU Qingwen,et al. Determination method for similarity relationship of straight-plate blade vibration response test[J]. Aeroengine,2019,45(5):63-69. [12] MACE B. Statistical energy analysis,energy distribution models and system modes[J]. Journal of Sound and Vibration,2003,264(2):391-409. [13] 张国军,闫云聚,李鹏博. 基于统计能量法的飞行器结构声振响应分析[J]. 噪声与振动控制,2014(3):92-96. ZHANG Guojun,YAN Yunju,LI Pengbo. Analysis of vibro-acoustic response of aircrafts based on statistical energy method[J]. Noise and Vibration Control. 2014(3):92-96. [14] 林华刚,闫云聚,李鹏博. 飞行器结构在高强宽频噪声环境下的响应预示分析与试验研究[J]. 机械工程学报,2016,52(3):71-78. LIN Huagang,YAN Yunju,LI Pengbo. Aircraft structure’s response prediction analysis and experimental study in high-strength broadband noise environments[J]. Journal of Mechanical Engineering,2016,52(3):71-78. [15] 姚德源,王其政. 统计能量分析原理及其应用[M]. 北京:北京理工大学出版社,1995. YAO Deyuan,WANG Qizheng. Statistical energy analysis theory and its application[M]. Beijing:Beijing Institute of Technology Press,1995 [16] 王军评,毛勇建,黄含军,等. 统计能量分析法在爆炸分离冲击响应预示中的应用[J]. 航天器环境工程. 2011,28(5):414-420. WANG Junping,MAO Yongjian,HUANG Hanjun,et al. Application of statistical energy analysis method in prediction of pyro-shock responses[J]. Spacecraft Environment Engineering,2011,28(5):414-420. [17] ZHAO H,DING J,ZHU W,et al. Shock response prediction of the typical structure in spacecraft based on the hybrid modeling techniques[J]. Aerospace Science and Technology,2019,89:460-467.