Available Relevant Study on Stress Analysis and Static Strength Prediction of Fiber Metal Laminates

Zhang, Xiaochen; Meng, Weiying; Guo, Jiancheng; Zhang, Yu

doi:https://doi.org/10.1155/2020/8874830

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Volume 2020 | Article ID 8874830 | https://doi.org/10.1155/2020/8874830

Available Relevant Study on Stress Analysis and Static Strength Prediction of Fiber Metal Laminates

Xiaochen Zhang,¹Weiying Meng,¹Jiancheng Guo,¹and Yu Zhang¹

Academic Editor: Jian Chen

Received01 Oct 2020

Revised13 Oct 2020

Accepted14 Oct 2020

Published09 Dec 2020

Abstract

Fiber metal laminates (FMLs) are a novel type of structural material that has been extensively applied in the aerospace field. These laminates are sandwich-type composite materials that comprise alternate metal and fiber-reinforced resin layers. Because of the structural characteristics of the material, it has high-impact resistance from the metal layer and increased fracture toughness and excellent fatigue and damage tolerance properties from the fiber layer. To further develop and apply this new composite material, it is essential to understand the research status on the stress analysis of each component in FMLs and the tensile strength properties of FMLs. Therefore, in this study, the current research status on the residual stress and applied stress of the component materials in FMLs and the tensile strength of the laminates is summarized. The relationship between the applied stress of each layer and the remote stress of laminates and the relationship between the tensile properties of laminates and the component material properties in laminates are clarified. Additionally, the theoretical basis and direction of development of the related models are analyzed and studied. Consequently, all of the above are aimed at laying a foundation for further investigations of the laminate theory and for the improvement of the theoretical research system.

References

A. Vlot, L. B. Vogelesang, and T. J. de Vries, “Towards application of fibre metal laminates in large aircraft,” Aircraft Engineering and Aerospace Technology, vol. 71, no. 6, pp. 558–570, 1999.
View at: Publisher Site | Google Scholar
A. Vlot and J. W. Gunnink, Eds., Fibre Metal Laminates: An Introduction, Kluwer Academic Publishers, Dordrecht, 2001.
S. Y. Wang, Preparation and Mechanical Properties of Fiber Metal Laminates [Dissertation], Harbin Institute of Technology, Harbin, 2012.
J. Tao, H. G. Li, L. Pan, and Y. B. Hu, “Review on research and development of fiber metal laminates,” Nanjing University of Aeronautics and Astronautics, vol. 47, pp. 626–636, 2015.
View at: Publisher Site | Google Scholar
L. P. Jiang, “Research of glare laminate fatigue performance comprehensive evaluation,” Materials Research, vol. 36, pp. 113–118, 2012.
View at: Google Scholar
C. A. J. R. Vermeeren, T. Beumler, J. L. C. G. de Kanter, O. C. van der Jagt, and B. C. L. Out, “Glare design aspects and philosophies,” Applied Composite Materials, vol. 10, no. 4/5, pp. 257–276, 2003.
View at: Publisher Site | Google Scholar
Y. J. Guo and X. R. Wu, “Phenomenological model for predicting fatigue crack growth in fiber reinforced metal laminates,” Acta Aeronaut et Astronaut Sinica, vol. 19, pp. 275–282, 1998.
View at: Google Scholar
P. Y. Chang, P. C. Yeh, and J. M. Yang, “Fatigue crack initiation in hybrid boron/glass/aluminum fiber metal laminates,” Materials Science and Engineering: A, vol. 496, no. 1-2, pp. 273–280, 2008.
View at: Publisher Site | Google Scholar
R. M. Frizzell, C. T. Mccarthy, and M. A. Mccarthy, “An experimental investigation into the progression of damage in pin-loaded fibre metal laminates,” Composites Part B: Engineering, vol. 39, no. 6, pp. 907–925, 2008.
View at: Publisher Site | Google Scholar
Y. M. Fu, J. Zhong, and Y. Chen, “Thermal postbuckling analysis of fiber–metal laminated plates including interfacial damage,” Composites Part B: Engineering, vol. 56, pp. 358–364, 2014.
View at: Publisher Site | Google Scholar
R. Marissen, Fatigue Crack Growth in ARALL: A Hybrid Aluminum-Aramid Composite Material Crack Growth Mechanisms and Quantitative Predictions of the Crack Growth Rates, Report LR-574, Delft University of Technology, Delft, 1988.
J. J. Homan, “Fatigue initiation in fibre metal laminates,” International Journal of Fatigue, vol. 28, no. 4, pp. 366–374, 2006.
View at: Publisher Site | Google Scholar
Y. J. Guo, Fatigue Damage and Life Prediction of Fiber Reinforced Metal Laminates [Dissertation], Institute of Aeronautical Materials, Beijing, 1997.
O. Kieboom, Fatigue Crack Initiation and Early Crack Growth in Glare at Different Temperatures [Dissertation], Delft University of Technology, Delft, 2000.
I. Sen, R. C. Alderliesten, and R. Benedictus, “Design optimisation procedure for fibre metal laminates based on fatigue crack initiation,” Composite Structures, vol. 120, pp. 275–284, 2015.
View at: Publisher Site | Google Scholar
Y. Huang, J. Z. Liu, X. Huang, J. Z. Zhang, and G. Q. Yue, “Delamination and fatigue crack growth behavior in fiber metal laminates (Glare) under single overloads,” International Journal of Fatigue, vol. 78, pp. 53–60, 2015.
View at: Publisher Site | Google Scholar
S. U. Khan, R. C. Alderliesten, and R. Benedictus, “Post-stretching induced stress redistribution in fibre metal laminates for increased fatigue crack growth resistance,” Fibre Science and Technology, vol. 69, no. 3-4, pp. 396–405, 2009.
View at: Publisher Site | Google Scholar
A. Vasek, J. Polak, and V. Kozak, “Fatigue crack initiation in fibre-metal laminate GLARE 2,” Materials Science and Engineering A, vol. 234-236, pp. 621–624, 1997.
View at: Publisher Site | Google Scholar
R. C. Alderliesten, “On the available relevant approaches for fatigue crack propagation prediction in GLARE,” International Journal of Fatigue, vol. 29, no. 2, pp. 289–304, 2007.
View at: Publisher Site | Google Scholar
S. Oken and R. R. June, Analytical and Experimental Investigation of Aircraft Metal Structures Reinforced with Filamentary Composites [Report], NASA CR-1859, 1971.
H. J. Hu, H. Y. Li, and R. Q. Zheng, “Modifying residual stresses in ARALL laminates by prestressing,” Acta Mater Compos Sinica, vol. 10, pp. 9–12, 1993.
View at: Publisher Site | Google Scholar
H. J. Hu, H. Y. Li, R. Q. Zheng, and W. Qiang, “Method of modifying residual stresses of aramid-aluminum laminates (ARALL) by prestrain,” Acta Mater Compos Sinica, vol. 13, pp. 123–126, 1995.
View at: Publisher Site | Google Scholar
M. Abouhamzeh, J. Sinke, K. M. B. Jansen, and R. Benedictus, “Closed form expression for residual stresses and warpage during cure of composite laminates,” Composite Structures, vol. 133, pp. 902–910, 2015.
View at: Publisher Site | Google Scholar
H. Y. Li, H. J. Hu, and R. Q. Zheng, “Analysis and measurement on residual stress of aramid aluminum laminates,” Acta Aeronaut et Astronaut Sinica, vol. 15, pp. 596–600, 1994.
View at: Google Scholar
W. H. Zhong, Z. Q. Gao, Z. G. Zhang, and H. C. Yang, “Study of residual stress in super-hybrid composite Ti/CFRP,” New carbon Maternité, vol. 15, pp. 18–22, 2000.
View at: Google Scholar
A. R. Ghasemi and M. M. Mohammadi, “Residual stress measurement of fiber metal laminates using incremental hole-drilling technique in consideration of the integral method,” International Journal of Mechanical Sciences, vol. 114, pp. 246–256, 2016.
View at: Publisher Site | Google Scholar
Z. F. Gu, D. Y. Cui, W. H. Zhong, H. Y. Li, H. J. Hu, and R. Q. Zheng, “Analysis of residual stresses for fiber reinforced alumimium laminate,” Acta Mater Compos Sinica, vol. 12, pp. 75–80, 1995.
View at: Publisher Site | Google Scholar
Z. H. Hu, G. R. Wang, X. D. He, and W. B. Liu, “The effect of metal mould on residual stress of composite laminated during cure process,” J Astronaut, vol. 28, pp. 816–818, 2007.
View at: Google Scholar
Y. J. Guo and R. Q. Zheng, “The residual stresses in glass fiber reinforced aluminium laminates (GLARE),” Journal of Materials Engineering, no. 1, pp. 28–30, 1998.
View at: Google Scholar
J. Brunbauer and G. Pinter, “Fatigue life prediction of carbon fibre reinforced laminates by using cycle-dependent classical laminate theory,” Composites Part B: Engineering, vol. 70, pp. 167–174, 2015.
View at: Publisher Site | Google Scholar
C. H. Park and A. Baz, “Comparison between finite element formulations of active constrained layer damping using classical and layer-wise laminate theory,” Finite Elements in Analysis and Design, vol. 37, no. 1, pp. 35–56, 2001.
View at: Publisher Site | Google Scholar
P. Chaphalkar and A. D. Kelkar, “Classical laminate theory model for twill weave fabric composites,” Composites. Part A, Applied Science and Manufacturing, vol. 32, no. 9, pp. 1281–1289, 2001.
View at: Publisher Site | Google Scholar
Q. Wang, L. L. Liang, and C. N. Peng, “Analysis of the mechanical properties of TC4-6061 composite plate based on classical laminate theory,” Applied Mechanics and Materials, vol. 724, pp. 12–16, 2015.
View at: Publisher Site | Google Scholar
V. S. Kale and N. K. Chhapkhane, “Analysis of the response of a laminate to imposed forces using classical lamination theory and finite element technique,” Int J Eng Sci Tec, vol. 5, pp. 1419–1426, 2013.
View at: Google Scholar
H. Fukunag and G. N. Vanderplaats, “Stiffness optimization of orthotropic laminated composites using lamination parameters,” AIAA Journal, vol. 29, pp. 641–646, 1991.
View at: Publisher Site | Google Scholar
T. Nowal, “Elastic-plastic behavior and failure analysis of selected fiber metal laminates,” Composite Structures, vol. 183, pp. 450–456, 2018.
View at: Publisher Site | Google Scholar
J. Y. Zheng and P. F. Liu, “Elasto-plastic stress analysis and burst strength evaluation of Al-carbon fiber/epoxy composite cylindrical laminates,” Computational Materials Science, vol. 42, no. 3, pp. 453–461, 2008.
View at: Publisher Site | Google Scholar
W. Y. Meng, L. Y. Xie, J. X. Hu, X. Lv, B. Qin, and B. W. Wang, “Strain measurement and stress prediction methods of metal layer in fiber metal laminates,” J B Univ Aeronaut Astronaut, vol. 44, pp. 142–150, 2018.
View at: Publisher Site | Google Scholar
E. C. Botelho, R. A. Silva, L. C. Pardini, and M. C. Rezende, “A review on the development and properties of continuous fiber/epoxy/aluminum hybrid composites for aircraft structures,” Materials Research, vol. 9, no. 3, pp. 247–256, 2006.
View at: Publisher Site | Google Scholar
J. W. Gunnink and L. B. Vogelesang, “Aerospace ARALL-the advancement in aircraft materials,” in Proceedings of the 35th International SAMPE Symposium, pp. 1708–1721, Anaheim, California, April 1990.
View at: Google Scholar
J. W. Gunnink and L. B. Vogelesang, “Aerospace ARALL: a challenger for aircraft designer,” in Proceedings of the 36th International SAMPE Symposium and Exhibition, pp. 1509–1522, San Diego, California, April 1991.
View at: Google Scholar
G. C. Wu and J. M. Yang, “Analytical modelling and numerical simulation of the nonlinear deformation of hybrid fibre–metal laminates,” Modelling Simul Mater Sci Eng, vol. 13, no. 3, pp. 413–425, 2005.
View at: Publisher Site | Google Scholar
H. Y. Ma, D. Mackay, S. Chi Lee, and W. Ying Shiu, “Aliphatic and cyclic hydrocarbons,” Journal of Materials Engineering, no. 7, pp. 61–64, 2006.
View at: Publisher Site | Google Scholar
Y. J. Wang, B. Wang, L. Zhang, and H. Y. Ma, “Tensile properties of glass fiber reinforced aluminum orthorhombic laminate,” Journal of Materials Engineering, vol. 43, pp. 60–65, 2015.
View at: Google Scholar
P. Cortés and W. J. Cantwell, “The prediction of tensile failure in titanium-based thermoplastic fibre-metal laminates,” Composites Science and Technology, vol. 66, no. 13, pp. 2306–2316, 2006.
View at: Publisher Site | Google Scholar
P. Iaccarino, A. Langella, and G. Caprino, “A simplified model to predict the tensile and shear stress–strain behaviour of fibreglass/aluminium laminates,” Composites Science and Technology, vol. 67, no. 9, pp. 1784–1793, 2007.
View at: Publisher Site | Google Scholar
J. L. Chen and C. T. Sun, “Modeling of orthotropic elastic-plastic properties of ARALL laminates,” Composites Science and Technology, vol. 36, no. 4, pp. 321–337, 1989.
View at: Publisher Site | Google Scholar
M. Kawai, M. Morishita, S. Tomura, and K. Takumida, “Inelastic behavior and strength of fiber-metal hybrid composite: glare,” International Journal of Mechanical Sciences, vol. 40, no. 2-3, pp. 183–198, 1998.
View at: Publisher Site | Google Scholar
A. S. Tong, L. Y. Xie, E. J. Bai, X. Bai, S. J. Zhang, and B. W. Wang, “Test and prediction model of statics property of fiber metal laminates,” Acta Aeronautica Et Astronautica Sinica, vol. 39, p. 221193, 2017.
View at: Google Scholar
P. M. Rao and V. Subba Rao, “Estimating the failure strength of fiber metal laminates by using a hybrid degradation model,” Journal of Reinforced Plastics and Composites, vol. 29, no. 20, pp. 3058–3063, 2010.
View at: Publisher Site | Google Scholar

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Copyright © 2020 Xiaochen Zhang et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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