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