Tensile Test Performance of Fibre Reinforced SMATed Aluminium Laminates

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/).

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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  -