ID 1483


Development of a Hybrid Material for Aerospace Application,

Made of C/E Sandwich Panels with GlareÔ Protection and

Experimental Evaluation of the Impact Behaviour



Ad Vlot and Gianfranco La Rocca

Delft University of Technology, The Netherlands

Aldo Frediani

University of Pisa, Italy


Keywords: C/E composite laminates, glare, sandwich panels, impact test,

impact damage, damage resistance, inspectability, delamination