PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Numerical and experimental verification of impact response of laminated aluminum composite structure

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Laminated Aluminum Composite Structure (LACS) has shown great potential for replacing traditional bulk aluminum parts, due to its ability to maintain low manufacturing costs and create complex geometries. In this study, a LACS, that consists of 20 aluminum layers joined by a structural tape adhesive, was fabricated and tested to understand its impact performance. Three impact tests were conducted: axial drop, normal and transverse three-point bending drop tests. Numerical simulations were performed to predict the peak loads and failure modes during impacts. Material models with failure properties were used to simulate the cohesive failure, interfacial failure, and aluminum fracture. Various failure modes were observed experimentally (large plastic deformation, axial buckling, local wrinkling, aluminum fracture and delamination) and captured by simulations. Cross-section size of the axial drop model was varied to understand the LACS buckling direction and force response. For threepoint bending drop simulations, the mechanism causing the maximum plastic strain at various locations in the aluminum and adhesive layers was discussed. This study presents an insight to understand the axial and flexural responses under dynamic loading, and the failure modes in LACS. The developed simulation methodology can be used to predict the performance of LACS with more complex geometries.
Rocznik
Strony
127--147
Opis fizyczny
Bibliogr. 25 poz., rys., tab., wykr.
Twórcy
autor
  • General Motors Global Technical Center, 29360 William Durant Boulevard, Warren, Michigan 48092-2025, USA.
  • General Motors Global Technical Center, 29360 William Durant Boulevard, Warren, Michigan 48092-2025, USA.
autor
  • General Motors Global Technical Center, 29360 William Durant Boulevard, Warren, Michigan 48092-2025, USA.
autor
  • General Motors Global Technical Center, 29360 William Durant Boulevard, Warren, Michigan 48092-2025, USA.
Bibliografia
  • [1] D. Zangani, M. Robinson, and A.G. Gibson. Evaluation of stiffness terms for z-cored sandwich panels. Applied Composite Materials, 14:159–175, 2007. doi: 10.1007/s10443-007-9038-y.
  • [2] J. Yu, E. Wang, J. Li, and Z. Zheng. Static and low-velocity impact behavior of sandwich beams with closed-cell aluminum-foam core in three-point bending. International Journal of Impact Engineering, 35(8):885–894, 2008. doi: 10.1016/j.ijimpeng.2008.01.006.
  • [3] Q. Sun, Z. Meng, G. Zhou, S.-P. Lin, H. Kang, S. Keten, H. Guo, and X. Su. Multi-scale computational analysis of unidirectional carbon fiber reinforced polymer composites under various loading conditions. Composite Structures, 196:30–43, 2018. doi: 10.1016/j.compstruct.2018.05.025.
  • [4] G.S. Dhaliwal and G.M. Newaz. Modeling low velocity impact response of carbon fiber reinforced aluminum laminates (CARALL). Journal of Dynamic Behavior of Materials, 2:181–193, 2016. doi: 10.1007/s40870-016-0057-3.
  • [5] G.-C. Yu, L.-Z. Wu, L. Ma, and J. Xiong. Low velocity impact of carbon fiber aluminum laminates. Composite Structures, 119:757–766, 2014. doi: 10.1016/j.compstruct.2014.09.054.
  • [6] M. Koc, F.O. Sonmez, N. Ersoy, and K. Cinar. Failure behavior of composite laminates under four-point bending. Journal of Composite Materials, 50(26): 3679–3697, 2016. doi: 10.1177/0021998315624251.
  • [7] A. Shojaei, G. Li, P.J. Tan, and J. Fish. Dynamic delamination in laminated fiber reinforced composites: A continuum damage mechanics approach. International Journal of Solid and Structures, 71:262–276, 2015. doi: 10.1016/j.ijsolstr.2015.06.029.
  • [8] J. Wang, R. Bihamta, T.P. Morris, and Y.-C. Pan. Numerical and experimental investigation of a laminated aluminum composite structure. Applied Composite Materials, 26:1177–1188, 2019. doi: 10.1007/s10443-019-09773-7.
  • [9] D. Zangani, M. Robinson, and A.G. Gibson. Energy absorption characteristics of web-core sandwich composite panels subjected to drop-weight impact. Applied Composite Materials, 15:139–156, 2008. doi: 10.1007/s10443-008-9063-5.
  • [10] Q.-R. Yang, J.-X. Liu, S.-K. Li, and T.-T. Wu. Bending mechanical property and failure mechanisms of woven carbon fiber-reinforced aluminum alloy composite. Rare Metals, 35(12): 915–919, 2016. doi: 10.1007/s12598-014-0271-x.
  • [11] M. Kinawy, R. Butler, and G.W. Hunt. Bending strength of delaminated aerospace composites. Philosophical Transactions of The Royal Society, 370:1780–1797, 2012. doi: 10.1098/rsta.2011.0337.
  • [12] C. Kabogu, I. Mohagheghian, J. Zhou, Z. Guan, W. Cantwell, S. John, B.R.K. Blackman, A.J. Kinloch, and J.P. Dear. High-velocity impact deformation and perforation of fibre metal laminates. Journal of Materials Science, 53:4209–4228, 2018. doi: 10.1007/s10853-017-1871-2.
  • [13] X. Wang, X. Zhao, Z. Wu, Z. Zhu, and Z. Wang. Interlaminar shear behavior of basalt FRP and hybrid FRP laminates. Journal of Composite Materials, 50(8):1073–1084, 2016. doi: 10.1177/0021998315587132.
  • [14] C. Liu, D. Du, H. Li, Y. Hu, Y. Xu, J. Tian, G. Tao, and J. Tao. Interlaminar failure behavior of GLARE laminates under short-beam three-point-bending load. Composites Part B: Engineering, 97:361–367, 2016. doi: 10.1016/j.compositesb.2016.05.003.
  • [15] A. Yapici and M. Metin. Effect of low velocity impact damage on buckling properties. Engineering, 1:161–166, 2009. doi: 10.4236/eng.2009.13019.
  • [16] J. Sarkar, T.R.G. Kutty, D.S. Wilkinson, J.D. Embury, and D.J. Lloyd. Tensile properties and bendability of T4 treated AA6111 aluminum alloys. Materials Science and Engineering: A, 369(1-2):258–266, 2004. doi: 10.1016/j.msea.2003.11.022.
  • [17] 3M Automotive Division, 3M TM Structureal Adhesive Tape SAT1010M Technical Data Sheet, 3M, St. Paul, 2019.
  • [18] C.J. Corbett, L. Laszczyk, and O. Rebuffet. Assessing and validating the crash behavior of Securalex HS, a high-strength crashworthy aluminum alloy, using the GISSMO model. In 14th International LS-Dyna Users Conference, Detroit, 2016.
  • [19] G. Falkinger, N. Sotirov, and P. Simon. An investigation of modeling approaches for material instability of aluminum sheet metal using the GISSMO-model. In 10th European LS-DYNA Conference, Wurzburg, 2015.
  • [20] Livermore Softwar Technology Corporation (LSTC), LS-DYNA ® KEYWORD USER’S MANUAL VOLUME II Material Models, 2012.
  • [21] A. Mostafa, K. Shankar, and E.V. Morozov. Experimental, theoretical and numerical investigation of the flexural behaviour of the composite sandwich panels with PVC foam core. Applied Composite Materials, 21:661–675, 2014. doi: 10.1007/s10443-013-9361-4.
  • [22] G.A.O. Davies and I. Guiamatsia. The problem of the cohesive zone in numerically simulating delamination/debonding failure modes. Applied Composite Materials, 19:831–838, 2012. doi: 10.1007/s10443-012-9257-8.
  • [23] F. Dogan, H. Hadavinia, T. Donchev, and P.S. Bhonge. Delamination of impacted composite structures by cohesive zone interface elements and tiebreak contact. Central European Journal of Engineering, 2(4):612–626, 2012. doi: 10.2478/s13531-012-0018-0.
  • [24] C. Hesch and P. Betsch. Continuum mechanical considerations for rigid bodies and fluidstructure interaction problems. Archive of Mechanical Engineering, 60(1):95–108, 2013. doi: 10.2478/meceng-2013-0006.
  • [25] J.J.C. Remmers and R. de Borst. Delamination buckling of fibre-metal laminates. Composites Science and Technology, 61(15):2207–2213, 2001. doi: 10.1016/S0266-3538(01)00114-2.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a39f82c8-4924-4327-b66b-45bb1973d920
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.