Experimental study of impact damage resistance and tolerance of composite sandwich panels

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...

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Bibliographic Details
Main Authors: Peter Nash, Gang Zhou, S. Gahlay, M. Burt
Format: Default Conference proceeding
Published: 2013
Subjects:
Other engineering not elsewhere classified
Unsymmetrical sandwich
Impact damage
Damage tolerance
CAI strength
Engineering not elsewhere classified
Online Access:https://hdl.handle.net/2134/15231
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