Optimization of the manufacturing parameters of honeycomb composite sandwich structures for aerospace application

Please use this identifier to cite or link to this item: http://localhost:80/xmlui/handle/123456789/1762

Title:	Optimization of the manufacturing parameters of honeycomb composite sandwich structures for aerospace application
Authors:	Farooq, U. Khurram, A. A. Ahmad, M. S. Rakha, S. A. Munir, A. Ali, N. Subhani, T.
Keywords:	Engineering and Technology Sandwich structure Para-aramid honeycomb Mechanical testing
Issue Date:	21-Aug-2013
Publisher:	IEEE 2013 International Conference on Aerospace Science & Engineering (ICASE)
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.
URI:	http://142.54.178.187:9060/xmlui/handle/123456789/1762
ISBN:	978-1-4799-0993-3
Appears in Collections:	Proceedings

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