Numerical simulation of low-velocity impact damage behaviour of composite laminates based on SMA superelasticity

被引：0
|
作者：
Zhang L. [1 ]
Hu D. [1 ,2 ,3 ]
Jia A. [1 ]
Wang R. [1 ,2 ,3 ]
机构：
[1] College of Energy and Power Engineering, Beihang University, Beijing
[2] Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing
[3] Collaborative Innovation Center of Advanced Aero-Engine, Beijing
来源：
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2017年 / 34卷 / 02期
关键词：
Composite laminates; Compression-after-impact; FEA; Low-velocity impact; SMA;
D O I：
10.13801/j.cnki.fhclxb.20160413.004
中图分类号：
学科分类号：
摘要：
This study established 3D finite element analysis models of composite laminates containing SMA wires of different angles and different distance intervals by combing ABAQUS software platform and VC++6.0 program designing. The SMA piecewise linear model derived from Brinson constitutive model to describe the SMA superelasticity and the 3D HASHIN failure criterion to predict intralaminar damage of composite laminates were compiled as ABAQUS/VUMAT subroutines. Interlaminar damage was modeled with cohesive element. Numerical simulation method of the low-velocity impact damage behaviour of composite laminates containing SMA wires and compression-after-impact was proposed. This study compared the damage behaviour of laminates with and without SMA wires, as well as ordinary metal wires at different impact energy. Compression-after-impact (CAI) simulation results indicate that the CAI strength of laminates containing SMA wires with volume friction of 25% and diameter of 0.5 mm, is increased by 5.78% compared with laminates not containing SMA wires, and by 4.69% compared with laminates containing ordinary metal wires at impact energy of 16 J. Furthermore, computation results of SMA wires volume friction and diameter value effecting on the impact behaviour show that laminates' anti-impact ability becomes stronger when volume friction increases. When volume friction keeps constant, the enhancing effect on the laminates' anti-impact ability with SMA wires of smaller diameter (0.3 mm) is better than that with larger diameter (0.6 mm). © 2017, Chinese Society for Composite Materials. All right reserved.
引用
收藏
页码：364 / 373
页数：9
相关论文
共 26 条
  • [1] Abrate S., Impact on Composite Structures, pp. 135-160, (2005)
  • [2] Kreculj D., Rasauo B., Review of impact damages modelling in laminated composite aircraft structures, Tehniki Vjesnik, 20, 3, pp. 485-495, (2013)
  • [3] Angioni S.L., Meo M., Foreman A., Impact damage resistance and damage suppression properties of shape memory alloys in hybrid composites-A review, Smart Materials and Structures, 20, 1, pp. 1424-1428, (2010)
  • [4] Pappada S., Ramette R., Toia L., Et al., Embedding of superelastic SMA wires into composite structures: Evaluation of impact properties, Journal of Materials Engineering and Performance, 18, 5-6, pp. 522-530, (2009)
  • [5] Pappada S., Ramette R., Largo A., Et al., Low-velocity impact response in composite plates embedding shape memory alloy wires, Polymer Composites, 33, 5, pp. 655-664, (2012)
  • [6] Rim M., Kim E., Lee I., Et al., Low-velocity impact characteristics of composite plates with shape memory alloy wires, Journal of Theoretical and Applied Mechanics, 49, 3, pp. 841-857, (2011)
  • [7] Zhu Y.G., Lu H.X., Yang D.Z., Mechanical properties of elastoplastic matrix composite reinforced by long SMA fibers, Acta Materiae Compositae Sinica, 19, 2, pp. 89-93, (2002)
  • [8] Zhu Y.P., Dui G.S., Micromechanical modeling of mechanical property for SMA reinforced composite, Acta Materiae Compositae Sinica, 25, 2, pp. 156-160, (2008)
  • [9] Kim E., Lee I., Roh J., Et al., Effects of shape memory alloys on low velocity impact characteristics of composite plate, Composite Structures, 93, 11, pp. 2903-2909, (2011)
  • [10] Meo M., Marulo F., Guida M., Et al., Shape memory alloy hybrid composites for improved impact properties for aeronautical applications, Composite Structures, 95, pp. 756-766, (2013)
123