Abstract
The MTS810 and SHPB were used to experimentally study the quasi-static and dynamic mechanical properties of Kevlar/epoxy composite laminates. Effects of the strain rate and lay-up types of fiber on the mechanical behaviors of laminated Kevlar were discussed. Based on the strain-rate curves of laminated Kevlar, an empirical constitutive equation was proposed in which the strain-rate hardening and damage softening effects of the material were taken into consideration. A stiffness-strengthened factor was introduced into the proposed constitutive equation to describe the influences of fiber lay-up types on the mechanical properties of the laminates. Results show that the introduced factor is reasonable in the fitted and experimental stress-stain curves.
Original language | English |
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Pages (from-to) | 200-206 |
Number of pages | 7 |
Journal | Baozha Yu Chongji/Expolosion and Shock Waves |
Volume | 28 |
Issue number | 3 |
State | Published - May 2008 |
Externally published | Yes |
Scopus Subject Areas
- General Physics and Astronomy
Keywords
- Constitutive equation
- Kevlar/epoxy composite laminates
- SHPB
- Solid mechanics