journal article·2004-04

Dynamic damage initiation of composite beams subjected to axial impact

Zheng Zhang, Farid Taheri

Composites Science and Technology· Volume 64· Issue 5
Publisher page

Abstract

Abstract The dynamic damage behavior of carbon-epoxy laminated beams, having initial geometric imperfections, subject to an axial impulse was investigated numerically and experimentally. The study focused on investigating the damage initiation and damage mechanism in the beams impacted axially by a moving mass. The dynamic equilibrium equations were developed based on the Timoshenko beam assumption with the consideration of beam's transverse inertia, transverse shear deformation and the cross section's rotational inertia effects. The Higher-Order Shear Deformation Theory was adopted to model the nonlinear distributed shear strain across the beam thickness. The von-Karman Strain–Displacement nonlinear relationship was used to model the deformation of the beam. Hashin's failure criteria was used to predict the damage of beams. The experiments were conducted using a horizontal linear bearing impact setup. Scanning Electron Microscopy results showed that delamination and matrix crack were the primary damage mechanisms in the beams. Effect of fiber angle, lay-up sequence and initial geometric imperfection on critical energy of damage initiation was also investigated.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Response to Dynamic Loads · Structural Analysis of Composite Materials

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (23)

Show source-provided references
1. Effect of laminate configuration and impactor's mass on trhe initial impact damage of graphite/epoxy composite plates due to line-loading impact
2. Normalized impact response and damage in a thin thin composite laminate supported by a rigid substrate10.1177/002199839402801603 ↗
3. Experimental techniques for the investigation of the effects of impact damage on carbon-fiber composites10.1016/0266-3538(95)00097-6 ↗
4. Damage mechanisms in composite laminates impacted by a flat-ended impactor10.1016/0266-3538(95)80019-0 ↗
5. Impact damage characterization of carbon fiber/epoxy exompoasite with multi-layer reinfotrcement10.1016/S1359-8368(00)00028-7 ↗
6. Time-resolved impact response and damage of fiber-reinforced composite laminates10.1177/002199830003401003 ↗
7. Photoelastic study of the mechanic behavior of orthotropic composite plates subject to impact10.1016/S0263-8223(01)00086-1 ↗
8. Impact behavior of cross-ply laminated composite plates under low velicities10.1016/S0263-8223(00)00134-3 ↗
9. An approach to evaluate the impact damage initiation and propagation in composite plates10.1016/S1359-8368(01)00031-2 ↗
10. Analytical prediction of large mass impact damage in composite laminates10.1016/S1359-835X(01)00073-2 ↗
11. Numerical studies on dynamic pulse buckling of FRP composite laminated beams subject to an axial impact10.1016/S0263-8223(02)00012-0 ↗
12. Strain rate behavior of composite materials10.1016/S1359-8368(98)00008-0 ↗
13. Initial and progressive failure analysis of laminated composite structures under dynamic loading10.1016/0263-8223(94)90270-4 ↗
14. Modeling of impacts on comosite structures10.1016/S0263-8223(00)00138-0 ↗
15. Experimental and theoretical studies of columns under axial impact10.1016/0020-7683(82)90044-0 ↗
16. Dynamic pulsebuckling and postbuckling of composite laminated beam using higher order shear deformation theory10.1016/S1359-8368(02)00134-8 ↗
17. A simple higher-order theory for laminated composite plates10.1115/1.3167719 ↗
18. Failure criteria for unidirectional fiber composites10.1115/1.3153664 ↗
19. Rosen BW. Mechanics of composite strengthening, Ch. 3. In: Fiber composite materials, ASM, Metal Park, OH, 1965.
20. A theory of the yielding and plastic flow of anisotropic metals
21. Lindberg · 1987
22. Dynamic elastic buckling of a slender beam with geometric imperfection subject to an axial impulse10.1016/S0168-874X(99)00067-0 ↗
23. J.W. Lemmens, Inc., Operating instructions for the GrindoSonic MK5 “Industrial” instrument. Avaialble: http://www.grindosonic.com.