Finite Element Analysis of Low-Velocity Impact Damage on Stiffened Composite Panels
Commenced in January 2007
Frequency: Monthly
Edition: International
Paper Count: 33123
Finite Element Analysis of Low-Velocity Impact Damage on Stiffened Composite Panels

Authors: Xuan Sun, Mingbo Tong

Abstract:

To understand the factors which affect impact damage on composite structures, particularly the effects of impact position and ribs. In this paper, a finite element model (FEM) of low-velocity impact damage on the composite structure was established via the nonlinear finite element method, combined with the user-defined materials subroutine (VUMAT) of the ABAQUS software. The structural elements chosen for the investigation comprised a series of stiffened composite panels, representative of real aircraft structure. By impacting the panels at different positions relative to the ribs, the effect of relative position of ribs was found out. Then the simulation results and the experiments data were compared. Finally, the factors which affect impact damage on the structures were discussed. The paper was helpful for the design of stiffened composite structures.

Keywords: Stiffened, Low-velocity, Impact, Abaqus, Impact Energy.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1093920

Procedia APA BibTeX Chicago EndNote Harvard JSON MLA RIS XML ISO 690 PDF Downloads 2528

References:


[1] E. Greenhalgh, S. M. Bishop, Characterisation of impact damage in skin-stringer composite structures. Elsevier Science Ltd. Composite Structures 36 (1996) 187-207.
[2] A.N. Palazotto, Finite element analysis of low-velocity impact on composite sandwich plates. Elsevier Science Ltd. Composite Structures 49 (2000) 209±227.
[3] Joshi S P, Sun C T. Impact induced fracture in a laminated composite (J). J. Comps. Mater.,1985, 19: 51-66.
[4] Choi H Y, Chang F K. A model for p redicting damage in graphite / epoxy laminate composites resulting from low2velocity point impact (J). J. Compos. Mater. , 1992, 26: 2134-69.
[5] Chang F.K., Lessard L.B. Damage Tolerance of Laminated Composites Containing an Open Hole and Subjected to Compressive Loadings: I-Analysis. Journal of Composite Materials. 1991, 25(1):2-43.
[6] Maimía P., Camanhob P.P., Mayugoa J.A., et al. A continuum damage model for composite laminates: Part I - Constitutive model. Mechanics of Materials. 2007, 39(10):897-908.
[7] Soutis C., Fleck N.A. Static Compression Failure of Carbon Fibre T800/924C Composite Plate with a Single Hole. Journal of Composite Materials. 1990, 24:536-558.