TY - JOUR
T1 - 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
AU - Chen, Zhaolin
AU - Yang, Zhichun
AU - Wang, Yongyan
AU - Zhang, Xinping
N1 - Publisher Copyright:
© 2018, Press of Chinese Journal of Aeronautics. All right reserved.
PY - 2018/8/25
Y1 - 2018/8/25
N2 - To analyze the transient response of structures under high-frequency shock load, a new method based on Energy Finite Element Method (EFEM) and Virtual Mode Synthesis and Simulation (VMSS) is proposed. The frequency band average of the Frequency Response Function (FRF) is obtained from steady-state analysis by energy finite element method, and then the virtual mode coefficients are calculated by virtual mode synthesis and simulation. Finally, the shock response of structures under high-frequency shock load is evaluated by Duhamel integral. Numerical simulations of a pinned-pinned beam are performed. The results obtained by the method proposed are compared with those obtained by the Finite Element Method (FEM) and Statistical Energy Analysis (SEA), showing that the proposed method is valid, and has the advantages of simple model, low computational cost, etc.
AB - To analyze the transient response of structures under high-frequency shock load, a new method based on Energy Finite Element Method (EFEM) and Virtual Mode Synthesis and Simulation (VMSS) is proposed. The frequency band average of the Frequency Response Function (FRF) is obtained from steady-state analysis by energy finite element method, and then the virtual mode coefficients are calculated by virtual mode synthesis and simulation. Finally, the shock response of structures under high-frequency shock load is evaluated by Duhamel integral. Numerical simulations of a pinned-pinned beam are performed. The results obtained by the method proposed are compared with those obtained by the Finite Element Method (FEM) and Statistical Energy Analysis (SEA), showing that the proposed method is valid, and has the advantages of simple model, low computational cost, etc.
KW - Energy finite element method
KW - High-frequency shock
KW - Shock response spectrum
KW - Transient response
KW - Virtual mode synthesis and simulation
UR - http://www.scopus.com/inward/record.url?scp=85056186188&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2018.21893
DO - 10.7527/S1000-6893.2018.21893
M3 - 文章
AN - SCOPUS:85056186188
SN - 1000-6893
VL - 39
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 8
M1 - 221893
ER -