journal article·2003-01

Failure Mechanisms and Modelling of Impact Damage in Sandwich Beams - A 2D Approach: Part II - Analysis and Modelling

Andrey Shipsha, Stefan Hallström, Dan Zenkert

Publisher page

Abstract

This study addresses the effect of low velocity impact damage on the post-impact residual strength and failure mechanisms of sandwich beams with Rohacell WF51 foam core. The considered impact damage has a form of a subinterface cavity surrounded by crushed core while the face sheet remains virtually undamaged. Part I of this study deals with experimental investigation of impact-damaged beams tested in transverse shear, bending and edgewise compression. It is shown that the crushed core and the bridging condition in the peripheral regions of the impact damage exert a significant effect on the post-impact critical loads and failure mechanisms. In this paper, parameterised finite element (FE) models of impact damage with implemented crushed core properties are developed for numerical analyses of post-impact failure. In the analysis of the shear case, a model for II bridging condition in the peripheral regions of impact damage is introduced. A point-stress criterion is applied for predictions of failure loads and crack kink angle. Geometrically nonlinear FE analysis is employed for evaluation of critical loads for local buckling in the beams with impact damage. The FE analyses demonstrate good agreement with experimental results.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Mechanical Behavior of Composites · Cellular and Composite Structures · Structural Analysis of Composite Materials

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

Affiliations

Department of Aeronautics, Royal Institute of Technology, S-100 44, Stockholm, Sweden,

Department of Aeronautics, Royal Institute of Technology, S-100 44, Stockholm, Sweden

References (22)

Show source-provided references
1. Shipsha, A. · Journal of Sandwich Structures and Materials · 2002 · 5 · 5
2. 10.1115/1.310168910.1115/1.3101689 ↗
3. Wiese, M. · 807
4. 10.1016/S0263-8223(98)00133-010.1016/S0263-8223(98)00133-0 ↗
5. 10.1016/S0263-8223(98)00058-010.1016/S0263-8223(98)00058-0 ↗
6. 10.1016/0734-743X(94)80031-410.1016/0734-743X(94)80031-4 ↗
7. 10.1016/0010-4361(94)90003-510.1016/0010-4361(94)90003-5 ↗
8. Olsson, R. · 1997
9. 10.1177/10996362990010040210.1177/109963629900100402 ↗
10. 10.1177/00219983980320040210.1177/002199839803200402 ↗
11. 10.1177/00219983920260040310.1177/002199839202600403 ↗
12. 12. Tsang, P.H.W. (1994). Impact resistance and damage tolerance of composite sandwich panels. PhD Thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology (MIT). Cambridge, MA.
13. Zenkert, D. · 1995
14. 10.1002/nme.162038130210.1002/nme.1620381302 ↗
15. 10.1016/S0022-5096(98)00107-010.1016/S0022-5096(98)00107-0 ↗
16. 10.1007/978-94-017-2260-5_510.1007/978-94-017-2260-5_5 ↗
17. Bueckner, H.F. · Transactions of the ASME · 1958 · 1225
18. 10.1177/00219983740080030310.1177/002199837400800303 ↗
19. 10.1016/0013-7944(95)00231-610.1016/0013-7944(95)00231-6 ↗
20. 10.1023/A:100743940962510.1023/A:1007439409625 ↗
21. 10.1016/0013-7944(94)90061-210.1016/0013-7944(94)90061-2 ↗
22. Bathe, K.-J. · 1996