Abstract
Laminate structures are used in the automobile, aerospace, and display industries. The advantages of fiber metal laminates are well known. Fiber metal laminates are useful for reducing the weight and improving impact resistance. However, currently, the mechanical properties of fiber metal laminates are not derived. In this paper, we use thickness as a factor for comparing the properties of laminates of various thickness combinations. The properties fiber metal laminates are analyzed using design of experiments. In addition, the finite element method is used to analyze elastic and plastic strains of fiber metal laminates and aluminum plates. The final goal of this paper is to find a suitable finite element model of fiber metal laminates under bending.
| Original language | English |
|---|---|
| Pages (from-to) | 963-970 |
| Number of pages | 8 |
| Journal | Transactions of the Korean Society of Mechanical Engineers, A |
| Volume | 39 |
| Issue number | 10 |
| DOIs | |
| Publication status | Published - 2015 Oct |
Bibliographical note
Publisher Copyright:© 2015 The Korean Society of Mechanical Engineers.
All Science Journal Classification (ASJC) codes
- Mechanical Engineering