Nothing Special   »   [go: up one dir, main page]

 

 
[ Log In | Register]
! Skip Navigation Links
Skip Navigation Links
Image of Journal of Applied Nonlinear Dynamics
ISSN:2164-6457 (print)
ISSN:2164-6473 (online)
Journal of Applied Nonlinear Dynamics
Miguel A. F. Sanjuan (editor), Albert C.J. Luo (editor)
Miguel A. F. Sanjuan (editor)

Department of Physics, Universidad Rey Juan Carlos, 28933 Mostoles, Madrid, Spain

Email: miguel.sanjuan@urjc.es

Albert C.J. Luo (editor)

Department of Mechanical and Industrial Engineering, Southern Illinois University Ed-wardsville, IL 62026-1805, USA

Fax: +1 618 650 2555 Email: aluo@siue.edu

Simulations of Post-impact Skin/core Debond Growth in Sandwich Plates Under Impulsive Loading

Journal of Applied Nonlinear Dynamics 3(4) (2014) 369--379 | DOI:10.5890/JAND.2014.12.008

Vyacheslav N. Burlayenko$^{1}$; Tomasz Sadowski$^{2}$

$^{1}$ Department of Applied Mathematics, National Technical University ’KhPI’,Kharkiv, 61002,Ukraine

$^{2}$ Department of Solid Mechanics, Lublin University of Technology, Lublin, 20-618, Poland

Download Full Text PDF

 

Abstract

In this study, the transient dynamics of a sandwich plate with post impact zone is examined. The dynamic response of the sandwich plate is simulated by using the finite element code ABAQUS. The damage mechanics approach implemented into ABAQUS via cohesive elements is applied to model the debonding propagation under impulsive loading. To demonstrate the effectiveness of the FE model developed, a foam-cored sandwich plate with an initial penny-shaped impacted region is modelled. The influence of the skin-to-core debond on the global nonlinear dynamics of the sandwich plate is studied in detail.

Acknowledgments

The main results of this paper have been previously presented by the authors as an oral presentation “Effects of a skin/core debond on the dynamics of impacted sandwich plates” at the 12th Conference on Dynamical Systems - Theory and Applications, DSTA-2013, December 2-5 Lodz, Poland and they contributed as an extended abstract to the conference proceedings. The second author would like to mention that this research was co-financed by Ministry of Science and Higher Education within the statutory research number S/20/2013.

References

  1. [1]  Zenkert, D. (1996), An Introduction to Sandwich Construction, Chameleon Press Ltd, London.
  2. [2]  Gibson, L.J. and Ashby, M.F. (1997), Cellular Solids, Structure and Properties, Cambridge University Press, Cambridge.
  3. [3]  Ashby, M.F., Evans, A.G., Fleck, N.A., Gibson, L.J., Hutchinson, J.W., and Wadley, H.N. (2000), Metal Foams: a Design Guide, Butterworth-Heinemann, Boston MA.
  4. [4]  Abrate, S. (1998), Impact on Composite Structures, Cambridge University Pressm, Cambridge.
  5. [5]  Olsson, R. (2002), Engineering method for prediction of impact response and damage in sandwich panels, Journal of Sandwich Structures and Materials, 4, 3-29.
  6. [6]  Herup, E. and Palazotto, A. (1998), Low-velocity impact damage initiation in graphite/epoxy/Nomex honeycomb-sandwich plates, Composites Science and Technology, 57, 1581-1598.
  7. [7]  Mines, R. (1998), Low velocity perforation behaviour of polymer composite sandwich panels, International Journal of Impact Engineering, 21, 855-879.
  8. [8]  Olsson, R., Donadon, M., and Falzon, B. (2006), Delamination threshold load for dynamic impact on plates, International Journal of Solids and Structures, 43, 3124-3141.
  9. [9]  Xu, L. and Rosakis, A.J. (2002), Impact failure characteristics in sandwich structures. Part II: effects of impact speed and interfacial strength, International Journal of Solids and Structures, 39, 215-235.
  10. [10]  Xu, L. and Rosakis, A.J. (2002), Impact failure characteristics in sandwich structures Part I: basic failure mode selection, International Journal of Solids and Structures, 439, 4237-4248.
  11. [11]  Foo, C.C., Chai, G.B., and Seah, L.K. (2008), A model to predict low-velocity impact response and damage in sandwich composites, Composites Science and Technology, 68, 1348-1356.
  12. [12]  Shokrieh, M.M. and Fakhar, M.N. (2012), Experimental, analytical, and numerical studies of composite sandwich panels under low-velocity impact loadings, Mechanics of Composite Materials, 47, 643-658.
  13. [13]  Zhang, G., Wang, B., Ma, L., Xiong, J., Yang, J., and Wu, L. (2013), The residual compressive strength of impact-damaged sandwich structures with pyramidal truss cores, Composite Structures, 105, 188-198.
  14. [14]  Burlayenko, V.N. and Sadowski, T. (2011), Post-impact dynamic response of sandwich plates with foam and non-metallic honeycomb cores, In: Proceedings of the 7th European Nonlinear Dynamics Conference ENOC 2011, 24 - 29 July 2011, Rome, Italy, Bernardini, D., Rega, G. and Romeo, F. (eds.) ISBN:978-88-906234-2-4.
  15. [15]  Burlayenko, V.N. and Sadowski, T. (2012), A numerical study of the dynamic response of sandwich plates initially damaged by low-velocity impact, Computational Materials Science, 52, 212-216.
  16. [16]  Elder, D.J., Thomson, R.S., Nguyen, M.W., and Scott, M.L. (2004), Review of delamination predictive methods for low speed impact of composite laminates, Composite Structures, 66, 677-683.
  17. [17]  Aymerich, F., Dore, F., and Priolo, P. (2009), Simulation of multiple delaminations in impacted crossply laminates using a finite element model based on cohesive interface elements, Composite Science and Technology, 69, 1699-1709.
  18. [18]  Belytschko, T., Liu, W.K., and Moran, B. (2002), Nonlinear finite elements for continua and structures, John Wiley and Sons, Chichester.
  19. [19]  Turon, A., Costa, J., Camanho, P.P., and Maimi, P. (2008,) Analytical and numerical investigation of the length of the cohesive zone in delaminated composite materials, Computational Methods in Applied Sciences, 10, 77-97.
  20. [20]  Camanho, P.P. and Davila, C.G. (2002) Mixed-mode Decohesion Finite Elements for the Simulation of Delamination in Composite Materials, NASA/TM-2002-211737.
  21. [21]  Benzeggagh, M.L. and Kenane, V. (1996), Measurement of mixed-mode delamination fracture toughness of unidirectional Glass/Epoxy composites with mixed-mode bending apparatus, Composites Science and Technology, 56, 439-449.
  22. [22]  Wriggers, P. (2006), Computational Contact Mechanics, Springer-Verlag, Berlin.
  23. [23]  Awrejcewicz, J. and Olejnik, P. (2005), Analysis of dynamic systems with various friction laws, Applied Mechanics Reviews - Transactions of ASME, 58, 389-411.
  24. [24]  Tomblin, J., Lacy, T., Smith, B., Hooper, S., Vizzini, A., and Lee, S. (1999), Review of damage tolerance for composite sandwich airframe structures, Report DOT/FAA/AR-99/49.
  25. [25]  ABAQUS (2009), User's Manual Version 9EF-1, Dassault Systèmes Simulia Corp., Providence, RI, USA.
  26. [26]  Zenkert, D., Shipsha, D., Bull, P. and Hayman, P. (2005), Damage tolerance of composite sandwich panels with localized damage, Composites Science and Technology, 65, 2597-2611.
  27. [27]  Li, Q.M., Mines, R.A.W. and Birch, R.S. (2000), The crush behavior of Rohacell-51WF structural foam, International Journal of Solids and Structures, 37, 6321-6341.
  28. [28]  Burlayenko, V.N. and Sadowski, T. (2012), Finite element nonlinear dynamic analysis of sandwich plates with partially detached facesheet and core, Finite Elements in Analysis and Design, 62, 49-64.

Copyright © 2011-2024 L & H Scientific Publishing. All rights reserved. Wildcard SSL Certificates