Vibration of a laminated composite plate with closing delamination

被引：0
作者：
Zak, A. [1 ]
Krawczuk, M. [1 ]
Ostachowicz, W. [1 ]
机构：
[1] Inst. of Fluid Flow Machinery PASci, ul. Gen. J.Fiszera 14, PL-80-952 Gdańsk, Poland
来源：
Key Engineering Materials | 1999年 / 167卷
关键词：
Boundary conditions - Delamination - Failure (mechanical) - Fast Fourier transforms - Finite element method - Interfaces (materials) - Laminated composites - Loads (forces) - Mathematical models - Natural frequencies - Structural analysis - Vibrations (mechanical);
D O I：
暂无
中图分类号：
学科分类号：
摘要：
The vibration of a laminated composite plate with closing delamination is analysed in the present paper using the finite element method. The effect of delaminated layers is modelled by using additional boundary conditions in the delamination front. Contact forces between delaminated layers are also considered in the model. The influence of delamination length and position on changes in natural frequencies of the plate is investigated. The plate is vibrated by a harmonic force or by a force impulse and the resulting time series are analysed using FFT. Results of the numerical calculations are compared against experimental data for laminated composite plates.
引用
收藏
页码：17 / 26
相关论文
共 50 条
  • [41] Vibration and acoustic response of an orthotropic composite laminated plate in a hygroscopic environment
    Zhao, Xin
    Geng, Qian
    Li, Yueming
    [J]. JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 2013, 133 (03) : 1433 - 1442
  • [42] Spectral element modeling and analysis of the transverse vibration of a laminated composite plate
    Park, Ilwook
    Lee, Usik
    [J]. COMPOSITE STRUCTURES, 2015, 134 : 905 - 917
  • [43] Active vibration control of a laminated composite plate subjected to blast load
    Uyanik, Haydar
    Mecitoglu, Zahit
    [J]. AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, 2009, 81 (04) : 308 - 315
  • [44] FREE VIBRATION OF RECTANGULAR PLATE WITH DELAMINATION
    Shiau, L-C.
    Zeng, J. -Y.
    [J]. JOURNAL OF MECHANICS, 2010, 26 (01) : 87 - 93
  • [45] Application of folded plate formulation in analyzing stiffened laminated composite and sandwich folded plate vibration
    Pal, Sreyashi
    Niyogi, A. Guha
    [J]. JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2008, 27 (07) : 693 - 710
  • [46] Vibration characteristics of generally laminated composite curved beams with single through-the-width delamination
    Jafari-Talookolaei, Ramazan-Ali
    Abedi, Maryam
    Hajianmaleki, Mehdi
    [J]. COMPOSITE STRUCTURES, 2016, 138 : 172 - 183
  • [47] Delamination tolerance studies in laminated composite panels
    K L Singh
    B Dattaguru
    T S Ramamurthy
    P D Mangalgiri
    [J]. Sadhana, 2000, 25 : 409 - 422
  • [48] Delamination tolerance studies in laminated composite panels
    Singh, K.L.
    Dattaguru, B.
    Ramamurthy, T.S.
    Mangalgiri, P.D.
    [J]. Sadhana - Academy Proceedings in Engineering Sciences, 2000, 25 (04) : 409 - 422
  • [49] Delamination tolerance studies in laminated composite panels
    Singh, KL
    Dattaguru, B
    Ramamurthy, TS
    Mangalgiri, PD
    [J]. SADHANA-ACADEMY PROCEEDINGS IN ENGINEERING SCIENCES, 2000, 25 (4): : 409 - 422
  • [50] Dynamic behavior of laminated composite plates with delamination
    Hong, Ming
    Chen, Hao-ran
    [J]. Chuan Bo Li Xue/Journal of Ship Mechanics, 2000, 4 (06): : 28 - 38
12345