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Mustafa Özgür Bora
Researcher at Kocaeli University
Publications - 45
Citations - 1346
Mustafa Özgür Bora is an academic researcher from Kocaeli University. The author has contributed to research in topics: Composite number & Adhesive. The author has an hindex of 12, co-authored 40 publications receiving 999 citations.
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A review: Fibre metal laminates, background, bonding types and applied test methods
TL;DR: In this article, the most commercially available fiber metal laminates (FMLs) are ARALL (Aramid Reinforced Aluminium Laminate), based on aramid fibres, GLARE (Glass Reinforced Aluminum Laminate) based on high strength glass fibres and CARALL (Carbon Reinforced Alloy Laminate, based on carbon fibres).
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The influence of low velocity repeated impacts on residual compressive properties of honeycomb sandwich structures
TL;DR: In this article, the authors describe the low velocity impact behavior of repeatedly impacted honeycomb sandwich structures which are used in aircraft interiors comprising of unidirectional glass fiber reinforced epoxy composite face sheets and aluminum honeycomb core.
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Experimental investigation of single and repeated impacts for repaired honeycomb sandwich structures
TL;DR: In this paper, single and repeated impact behaviors of repaired honeycomb sandwich structures which are used in cargo panels at A319/A320/A321 Airbus were examined and it was determined that the impact behavior of repaired composite is sufficient to be used in aircrafts.
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Effect of Fiber Orientation on Scratch Resistance in Unidirectional Carbon-Fiber-Reinforced Polymer Matrix Composites
TL;DR: In this paper, scratch resistance of continuous carbon-fiber- reinforced polyetherimide composites were investigated as a function of fiber orientations by means of CSM microscratch tester machine.
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On the life time prediction of repeatedly impacted thermoplastic matrix composites
Mustafa Özgür Bora,Onur Çoban,Tamer Sinmazçelik,Tamer Sinmazçelik,İsmail Cürgül,Volkan Günay +5 more
TL;DR: In this article, the impact fatigue properties of unidirectional carbon fiber reinforced polyetherimide (PEI) composites were investigated by using pendulum type instrumented impact tester (Ceast, Resil 25) at energy levels ranging 0.54-0.94 J.