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

Farooq, U.; Khurram, A. A.; Ahmad, M. S.; Rakha, S. A.; Munir, A.; Ali, N.; Subhani, T.

dc.contributor.author	Farooq, U.
dc.contributor.author	Khurram, A. A.
dc.contributor.author	Ahmad, M. S.
dc.contributor.author	Rakha, S. A.
dc.contributor.author	Munir, A.
dc.contributor.author	Ali, N.
dc.contributor.author	Subhani, T.
dc.date.accessioned	2019-11-22T10:44:47Z
dc.date.available	2019-11-22T10:44:47Z
dc.date.issued	2013-08-21
dc.identifier.isbn	978-1-4799-0993-3
dc.identifier.uri	http://142.54.178.187:9060/xmlui/handle/123456789/1762
dc.description.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.	en_US
dc.language.iso	en_US	en_US
dc.publisher	IEEE 2013 International Conference on Aerospace Science & Engineering (ICASE)	en_US
dc.subject	Engineering and Technology	en_US
dc.subject	Sandwich structure	en_US
dc.subject	Para-aramid honeycomb	en_US
dc.subject	Mechanical testing	en_US
dc.title	Optimization of the manufacturing parameters of honeycomb composite sandwich structures for aerospace application	en_US
dc.type	Proceedings	en_US