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Please use this identifier to cite or link to this item: https://dspace.lboro.ac.uk/2134/21059

Title: Experimental study of impact damage resistance and tolerance of composite sandwich panels
Authors: Zhou, Gang
Nash, Peter
Gahlay, S.
Burt, M.
Keywords: Unsymmetrical sandwich
Impact damage
Damage tolerance
CAI strength
Issue Date: 2013
Publisher: © Canadian Association for Composite Structures and Materials
Citation: ZHOU, G. ...et al., 2013. Experimental study of impact damage resistance and tolerance of composite sandwich panels. IN: Van Hoa, S. and Hubert, P. (eds.), 19TH International Conference on Composite Materials (ICCM 19), Montreal, Canada, July 28th-2nd Aug. Paper 2844.
Abstract: An experimental study of in-plane compressive behaviour of carbon/epoxy-skinned and E-glass/epoxy-skinned sandwich panels was conducted. For the former, two carbon/epoxy skin thickness combinations were 8/6 plies and 16/12 plies. Both cross ply (CP) and quasi-isotropic (QI) lay-ups were used in each combination. For the latter, two E-glass/epoxy skin thickness combinations of 8/8 and 16/16 plies were used with both being in a cross ply lay-up. The majority of sandwich panels were impact-damaged with their dominant damage mechanisms being characterised. All impact-damaged and baseline panels were in-plane compression tested. The effects of impact damage, lacking symmetry, skin thickness, skin lay-up and core density on CAI strength were examined.
Description: This is a conference paper.
Version: Published
URI: https://dspace.lboro.ac.uk/2134/21059
Publisher Link: http://www.iccm-central.org/Proceedings/ICCM19proceedings/
Appears in Collections:Conference Papers and Contributions (Aeronautical and Automotive Engineering)

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