항공우주시스템공학회지 (Journal of Aerospace System Engineering)

  • 제13권4호
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  • Pages.10-17
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  • 2019
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  • 1976-6300(pISSN)
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  • 2508-7150(eISSN)
항공우주시스템공학회 (The Society for Aerospace System Engineering)
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Effect of delamination on vibration characteristic of smart laminated composite plate

  • Shankar, Ganesh (Department of Mechanical Engineering, Ramgarh Engineering College Ramgarh) ;
  • Varun, Jayant Prakash (Department of Mechanical Engineering, Indian Institute of Technology(Indian School of Mines)) ;
  • Mahato, P.K. (Department of Mechanical Engineering, Indian Institute of Technology(Indian School of Mines))
  • 투고 : 2018.10.13
  • 심사 : 2019.02.17
  • 발행 : 2019.08.31
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초록

This study is concerned with a numerical analysis based on the finite element method to describe the effect of midplane delamination in smart laminated composite plate structures. A new finite element model for centrally located delamination and healthy section was developed and coded in Matlab. The transient analysis of delaminated composite plate with integrated Active Fiber Composite (AFC) was investigated in the present article. The formulation of the governing equation was based on the minimum total potential energy approach. The Newmark time integration technique was employed to solve the differential equations. A parametric study on the effects of boundary conditions and AFC patch location, in presence of delamination on the laminated plate were studied.

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참고문헌

  1. C.N. Della, D. Shu, Vibration of delaminated composite laminates: A review, Appl. Mech. Revie. 60, 1-20, 2007. https://doi.org/10.1115/1.2375141
  2. F. Ju, H.P. Lee, K.H. Lee, Finite element analysis of free vibration of delaminated composite plates, Compos. Eng.5 195-209, 1995. https://doi.org/10.1016/0961-9526(95)90713-L
  3. A. K. Acharyya, D. Chakravorty, & A. Karmakar, Natural frequencies and mode shapes of composite cylindrical delaminated shells by finite element. Journal of Reinforced Plastics and Composites, 29(2), 226-237 2010. https://doi.org/10.1177/0731684408097012
  4. M. H. Noh, S. Y. Lee, Dynamic instability of delaminated composite skew plates subjected to combined static and dynamic loads based on HSDT. Composites Part B: Engineering, 58, 113-121 2014. https://doi.org/10.1016/j.compositesb.2013.10.073
  5. S. K. Kumar, M. Cinefra, E.Carrera, R. Ganguli, D. Harursampath, Finite element analysis of free vibration of the delaminated composite plate with variable kinematic multilayered plate elements. Composites Part B: Engineering, 66, 453-465 2014. https://doi.org/10.1016/j.compositesb.2014.05.031
  6. J. Chen, H. Wang, G. Qing, Modeling vibration behavior of delaminated composite laminates using meshfree method in Hamilton system. Applied Mathematics and Mechanics, 36(5), 633-654 2015. https://doi.org/10.1007/s10483-015-1933-7
  7. M. Hammami, A. El Mahi, C. Karra, M. Haddar, Experimental analysis of the linear and nonlinear behaviour of composites with delaminations. Applied Acoustics, 108, 31-39 2016. https://doi.org/10.1016/j.apacoust.2015.10.026
  8. E.F. Crawley, J. De Luis, Use of piezoelectric actuators as elements of intelligent structures, AIAA J. 25 (1987) 1373-1385. https://doi.org/10.2514/3.9792
  9. H.S Tzou, C.I. Tseng, Distributed piezoelectric sensor/actuator design for dynamic measurement/control of distributed parameter systems: a piezoelectric finite element approach. Journal of sound and vibration 138(1) :17-34, 1990. https://doi.org/10.1016/0022-460X(90)90701-Z
  10. W.S. Hwang, W. Hwang, H.C Park, Vibration control of laminated composite plate with piezoelectric sensor/actuator: active and passive control methods. Mechanical Systems and Signal Processing 8(5):571-83, 1994. https://doi.org/10.1006/mssp.1994.1040
  11. N.W. Hagood, A.A. Bent, Development of piezoelectric fiber composites for structural actuation. AIAA/ASME/ASCE/AHS/ASC 34th Struct. Dynamics and Mater. Conference 3625-3638, 1993.
  12. P.K. Mahato, D.K. Maiti, Aeroelastic analysis of smart composite structures in hygro-thermal environment. Compos. Struct. 92 :1027-1038, 2010. https://doi.org/10.1016/j.compstruct.2009.09.050
  13. P.K.Mahato, D.K. Maiti, Flutter control of smart composite structures in hygrothermal environment, J. Aerospace Eng. 23: 317-326, 2010. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000046
  14. A.J. Brunner, M. Barbezat, C. Huber, P.H. Flueler, The potential of active fiber composites made from piezoelectric fibers for actuating and sensing applications in structural health monitoring. Mater. and struct38: 561-567, 2005. https://doi.org/10.1007/BF02479548
  15. P.J.Guruprasad, A.K Tamrakar, D. Harursampath, Modeling of active fiber composite for delamination sensing. Smart Mater. Nano-and Micro-Smart Syst. 641305-641305, 2006.
  16. M. Martinez, A. Artemev, Finite element analysis of broken fiber effects on the performance of active fiber composites. Compos. Struct. 88 :491-496, 2009. https://doi.org/10.1016/j.compstruct.2008.06.004
  17. Bathe KJ, Wilson EL. Numerical methods in finite element analysis. Englewood Cliffs, NJ: Prentice-Hall; 1976.