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Şükrü Karakaya

Researcher at Afyon Kocatepe University

Publications -  18
Citations -  220

Şükrü Karakaya is an academic researcher from Afyon Kocatepe University. The author has contributed to research in topics: Reflector (antenna) & Finite element method. The author has an hindex of 8, co-authored 18 publications receiving 196 citations.

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Buckling optimization of laminated composite plates using genetic algorithm and generalized pattern search algorithm

TL;DR: In this paper, genetic algorithm and generalized pattern search algorithm are used for optimal stacking sequence of a composite panel, which is simply supported on four sides and is subject to biaxial in-plane compressive loads.
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Natural frequency and buckling optimization of laminated hybrid composite plates using genetic algorithm and simulated annealing

TL;DR: In this article, genetic algorithm and simulated annealing are used to maximize the natural frequency and buckling loads of simply supported hybrid composite plates, and the best configurations are identified for different plate aspect ratios.
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Simulation of lightning strike damage in carbon nanotube doped CFRP composites

TL;DR: In this article, the authors investigated the damage behavior caused by a lightning strike on carbon fiber reinforced plastic (CFRP) composites, and showed that the damage area in each ply and the depth of the damage are not linear under the effect of either different waveforms or maximum strike currents.
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Curved large tape springs for an ultra-thin shell deployable reflector

TL;DR: In this paper, a study of large tape springs to be used as ribs of an ultra-thin shell space deployable reflector is presented, both longitudinally and transversely curved.
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Structural Optimization of Laminated Composite Plates for Maximum Buckling Load Capacity Using Genetic Algorithm

TL;DR: In this paper, the structural optimization of laminated composite plates for maximum buckling load capacity is performed by using genetic algorithm, and the composite plate under consideration is a 64-ply laminate made of graphite/epoxy, is simply supported on four sides, and subject to in-plane compressive static loads.