Tensile Test Performance of Fibre Reinforced SMATed Aluminium Laminates
Authors
Yun Wan, Zhen-Qing Wang, Li-Min Zhou, Meng-Zhou Chang
Corresponding Author
Yun Wan
Available Online June 2014.
- DOI
- 10.2991/icmsa-15.2015.175How to use a DOI?
- Keywords
- FML, SMAT, Metal Volume Fraction Theory, Tensile Test.
- Abstract
Fiber metal laminates (FMLs) are hybrid structures consisting of metal sheets and fiber reinforced plastic layers. Glass reinforced aluminum laminates (GLARE) reflects the combination of aluminum alloy layers and glass fiber reinforced layers. It is utilized in the aircraft upper fuselage and the leading edge surfaces of the vertical and horizontal tail planes at present. Surface mechanical attrition treatment (SMAT) is a technology which can improve the ultimate stress of metal. The SMATed aluminum alloy layers are introduced to the fabrication of new GLARE. After tensile test and theoretical calculation, the results show that the SMATed aluminum can improve the strength of GLARE obviously.
- Copyright
- © 2015, the Authors. Published by Atlantis Press.
- Open Access
- This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).
Cite this article
TY - CONF AU - Yun Wan AU - Zhen-Qing Wang AU - Li-Min Zhou AU - Meng-Zhou Chang PY - 2014/06 DA - 2014/06 TI - Tensile Test Performance of Fibre Reinforced SMATed Aluminium Laminates BT - Proceedings of the 2015 International Conference on Material Science and Applications PB - Atlantis Press SP - 943 EP - 947 SN - 2352-541X UR - https://doi.org/10.2991/icmsa-15.2015.175 DO - 10.2991/icmsa-15.2015.175 ID - Wan2014/06 ER -