Preprint Article Version 1 Preserved in Portico This version is not peer-reviewed

Development of Aluminum Honeycomb Cored Carbon Fiber Reinforced Polymer Composite Based Sandwich Structure

Version 1 : Received: 16 December 2018 / Approved: 17 December 2018 / Online: 17 December 2018 (10:59:35 CET)

How to cite: Okur, M.Z.; Kangal, S.; Tanoğlu, M. Development of Aluminum Honeycomb Cored Carbon Fiber Reinforced Polymer Composite Based Sandwich Structure. Preprints 2018, 2018120195. https://doi.org/10.20944/preprints201812.0195.v1 Okur, M.Z.; Kangal, S.; Tanoğlu, M. Development of Aluminum Honeycomb Cored Carbon Fiber Reinforced Polymer Composite Based Sandwich Structure. Preprints 2018, 2018120195. https://doi.org/10.20944/preprints201812.0195.v1

Abstract

Lightweight composite sandwich structures are laminated composite structures that are composed of thin stiff face sheets bonded to a thicker lightweight core in between. These structures have high potential to be used in marine, aerospace, defense and civil engineering applications due to their high strength to weight ratios and energy absorption capacity.In this study, composite sandwich structures were developed with carbon fiber reinforced polymer composite face sheets and aluminum honeycomb core materials with various thicknesses. Carbon fiber/epoxy composite face sheets were fabricated with lamination of [0/90]s carbon fabrics by vacuum infusion technique. Al honeycomb layers were sandwiched together with the face sheets using a thermosetting adhesive. Mechanical tests were carried out to determine the mechanical behavior of face sheets, Al cores and the composite structure. Effect of core thickness on the mechanical properties of the sandwich was investigated.

Keywords

Sandwich structures, carbon fiber, epoxy, aluminum honeycomb, mechanical properties, vacuum infusion

Subject

Engineering, Mechanical Engineering

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