Abstract:
Sandwich structures comprising para-aramid paper honeycomb core and carbon fiber epoxy matrix composite facesheets were fabricated for aerospace applications. For the adh...Show MoreMetadata
Abstract:
Sandwich structures comprising para-aramid paper honeycomb core and carbon fiber epoxy matrix composite facesheets were fabricated for aerospace applications. For the adhesion of honeycomb core and composite facesheets, two different types of adhesive films were used. The curing parameters for adhesive films, including temperature and time, were optimized for maximum bonding strength.
Date of Conference: 21-23 August 2013
Date Added to IEEE Xplore: 10 April 2014
Electronic ISBN:978-1-4799-0993-3