Numerical analysis of low-velocity rigid-body impact response of composite panels
dc.contributor.author | Yazdani Nezhad, Hamed | |
dc.contributor.author | Merwick, F. | |
dc.contributor.author | Frizzell, R. M. | |
dc.contributor.author | Carthy, C. T. | |
dc.date.accessioned | 2016-07-25T09:22:56Z | |
dc.date.available | 2016-07-25T09:22:56Z | |
dc.date.issued | 2014-09-29 | |
dc.description.abstract | This paper investigates various modelling strategies to identify the most suitable approach for modelling the low-velocity impact response of laminated composite panels. The purpose of this paper is to thoroughly investigate a dropped tool scenario or a ground vehicle impact on an aircraft fuselage panel using detailed numerical models. Three-dimensional meso-scale finite element models have been developed and implemented with user-defined material subroutines in ABAQUS/Standard. The models predict the simultaneous evolution of inter-laminar and intra-laminar damage mechanisms that occur in composite panels during impact. The paper describes the implementation of the combined inter/intra-laminar models and assesses their performance. User-defined material models developed in previous work for quasistatic problems have been further developed in this paper for damage analysis under impact loading. Experimental dropweight impact tests, representative of low-velocity high-energy rigid-body impacts, have been carried out for model validation. Impact energy levels were varied from 10 to 40 J to evaluate the damage threshold and damage area that develops within the laminate. The results of the combined inter/intra-laminar model are in excellent agreement with experimental data, especially in terms of energy absorbed during impact. Numerical results provide an accurate description of the threshold at which a significant change in laminate stiffness occurs. It is shown conclusively that the combined inter/ intra-laminar damage model developed in this work can be employed as an accurate predictive tool for low-velocity impact events. | en_UK |
dc.identifier.citation | Yazdani Nezhad, H. et al. (2014) Numerical analysis of low-velocity rigid-body impact response of composite panels, International Journal of Crashworthiness, Vol. 20, Iss. 1, pp. 27-43 | en_UK |
dc.identifier.issn | 1358-8265 | |
dc.identifier.uri | http://dx.doi.org/10.1080/13588265.2014.96337 | |
dc.identifier.uri | https://dspace.lib.cranfield.ac.uk/handle/1826/10162 | |
dc.language.iso | en | en_UK |
dc.publisher | Taylor & Francis | en_UK |
dc.subject | Composite | en_UK |
dc.subject | Low-velocity impact | en_UK |
dc.subject | Impact | en_UK |
dc.subject | In-plane damage | en_UK |
dc.subject | Delamination | en_UK |
dc.subject | Finite element analysis | en_UK |
dc.title | Numerical analysis of low-velocity rigid-body impact response of composite panels | en_UK |
dc.type | Article | en_UK |
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