EXPERIMENTAL ANALYSIS OF FIBER METAL LAMINATE WITH ALUMINIUM ALLOY FOR AIRCRAFT STRUCTURES

Abstract

 The objective is to examine the methods of testing on FIBER/METAL LAMINATE (FML) WITH ALUMINIUM ALLOY to obtain empirical estimates of Load capacity under various loads.FML is the combination of metal and polymer composite laminates. The main objective is Weight reduction and improved damage tolerance characteristics. Mechanical properties of FML shows improvements over the properties of both aluminum alloys and composite materials individually. Moisture absorption in FML composites is slower when compared with polymer composites. Load tests are of interest because such tests are commonly used to determine the suitability of a fiber used in aircraft components. This analysis has focused on experimental obstacles to the reliable determination of post-crack load capacity.

Authors and Affiliations

Mr. Hariharan E *

Keywords

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  • EP ID EP90630
  • DOI 10.5281/zenodo.50999
  • Views 79
  • Downloads 0

How To Cite

Mr. Hariharan E * (30).  EXPERIMENTAL ANALYSIS OF FIBER METAL LAMINATE WITH ALUMINIUM ALLOY FOR AIRCRAFT STRUCTURES. International Journal of Engineering Sciences & Research Technology, 5(5), 94-102. https://europub.co.uk/articles/-A-90630