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.


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    Title :

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


    Contributors:
    Farooq, U. (author) / Khurram, A. A. (author) / Ahmad, M. S. (author) / Rakha, S. A. (author) / Ali, N. (author) / Munir, A. (author) / Subhani, T. (author)


    Publication date :

    2013-08-01


    Size :

    499392 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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