Flutter Optimization of a Wing–Engine System with Passive and Active Control Approaches von Asadi, Davood, Farsadi, Touraj, Kayran, Altan

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A Comparative Study on the Efficiencies of Aerodynamic Reduced Order Models of Rigid and Aeroelastic Sweptback Wings von Özkaya Yılmaz, Özge, Kayran, Altan

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Development of a prediction model using fully connected neural networks in the analysis of composite structures under bird strike von Hasılcı, Zehra, Boǧoçlu, Muharrem Erdem, Dalkılıç, Ahmet Selim, Kayran, Altan

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Improvement of structural characteristics of composite thin-walled beams using variable stiffness concept via curvilinear fiber placement von Farsadi, Touraj, Bozkurt, Mirac Onur, Coker, Demirkan, Kayran, Altan

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Surrogate model based optimization of variable stiffness composite wingbox for improved buckling load with manufacturing and failure constraints von İnci, Hasan, Kayran, Altan

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High Aspect Ratio Composite Wings: Geometrically Nonlinear Aeroelasticity, Multi-Disciplinary Design Optimization, Manufacturing, and Experimental Testing von Farsadi, Touraj, Ahmadi, Majid, Sahin, Melin, Haddad Khodaparast, Hamed, Kayran, Altan, Friswell, Michael I

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Classical flutter analysis of composite wind turbine blades including compressibility von Farsadi, Touraj, Kayran, Altan

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Küssner's Function in the Sharp Edged Gust Problem-A Correction von Kayran, Altan

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Geometrically nonlinear aeroelastic behavior of pretwisted composite wings modeled as thin walled beams von Farsadi, Touraj, Rahmanian, Mohammad, Kayran, Altan

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Flight flutter testing and aeroelastic stability of aircraft von Kayran, Altan

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Flight flutter testing and aeroelastic stability of aircraft von Kayran, Altan

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Reduced order nonlinear aeroelasticity of swept composite wings using compressible indicial unsteady aerodynamics von Farsadi, Touraj, Rahmanian, Mohammad, Kayran, Altan

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Aircraft vulnerability assessment against fragmentation warhead von Konokman, Hüseyin Emrah, Kayran, Altan, Kaya, Mustafa

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Free-Vibration Analysis of Ring-Stiffened Branched Composite Shells of Revolution von Kayran, Altan, Yavuzbalkan, Erdem

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Design, analysis and optimization of thin walled semi-monocoque wing structures using different structural idealization in the preliminary design phase von DABABNEH, ODEH, KAYRAN, ALTAN

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Semi-analytical study of free vibration characteristics of shear deformable filament wound anisotropic shells of revolution von Kayran, Altan, Yavuzbalkan, Erdem

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Experimental and numerical study of process-induced total spring-in of corner-shaped composite parts von Çiçek, K Furkan, Erdal, Merve, Kayran, Altan

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Implementation of Dirlik’s damage model for the vibration fatigue analysis von Demirel, Gürzap İ., Kayran, Altan

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Accurate equivalent models of sandwich laminates with honeycomb core and composite face sheets via optimization involving modal behavior von Çınar, Okan, Erdal, Merve, Kayran, Altan

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Flutter qualification of transport aircraft with store suspension von Kayran, Altan

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