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