Prof. ALTAN KAYRAN

Publication Network

Published journal articles indexed by SCI, SSCI, and AHCI

Surrogate model based optimization of variable stiffness composite wingbox for improved buckling load with manufacturing and failure constraints

Inci H., KAYRAN A.

COMPOSITE STRUCTURES , vol.351, 2025 (SCI-Expanded)

A Comparative Study on the Efficiencies of Aerodynamic Reduced Order Models of Rigid and Aeroelastic Sweptback Wings

Özkaya Yılmaz Ö., KAYRAN A.

Aerospace , vol.11, no.8, 2024 (SCI-Expanded)

High Aspect Ratio Composite Wings: Geometrically Nonlinear Aeroelasticity, Multi-Disciplinary Design Optimization, Manufacturing, and Experimental Testing

Farsadi T., Ahmadi M., ŞAHİN M., Haddad Khodaparast H., KAYRAN A., Friswell M. I.

Aerospace , vol.11, no.3, 2024 (SCI-Expanded)

Development of a prediction model using fully connected neural networks in the analysis of composite structures under bird strike

Hasilci Z., BOĞOÇLU M. E., DALKILIÇ A. S., KAYRAN A.

JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY , vol.36, no.2, pp.709-722, 2022 (SCI-Expanded)

Improvement of structural characteristics of composite thin-walled beams using variable stiffness concept via curvilinear fiber placement

Farsadi T., Bozkurt M. O., ÇÖKER D., KAYRAN A.

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering , vol.235, no.14, pp.2017-2032, 2021 (SCI-Expanded)

Flutter Optimization of a Wing-Engine System with Passive and Active Control Approaches

Asadi D., Farsadi T., KAYRAN A.

AIAA JOURNAL , vol.59, no.4, pp.1422-1440, 2021 (SCI-Expanded)

Flutter study of flapwise bend-twist coupled composite wind turbine blades

Farsadi T., KAYRAN A.

WIND AND STRUCTURES , vol.32, no.3, pp.267-281, 2021 (SCI-Expanded) Sustainable Development

Classical flutter analysis of composite wind turbine blades including compressibility

Farsadi T., KAYRAN A.

WIND ENERGY , vol.24, no.1, pp.69-91, 2021 (SCI-Expanded) Sustainable Development

Reduced order nonlinear aeroelasticity of swept composite wings using compressible indicial unsteady aerodynamics

Farsadi T., Rahmanian M., KAYRAN A.

JOURNAL OF FLUIDS AND STRUCTURES , vol.92, 2020 (SCI-Expanded)

Development of Bolted Flange Design Tool Based on Artificial Neural Network

Yildirim A., Akay A. A., Gülasik H., Çöker D., Gürses E., Kayran A.

Journal of Pressure Vessel Technology, Transactions of the ASME , vol.141, 2019 (SCI-Expanded)

Geometrically nonlinear aeroelastic behavior of pretwisted composite wings modeled as thin walled beams

Farsadi T., Rahmanian M., KAYRAN A.

JOURNAL OF FLUIDS AND STRUCTURES , vol.83, pp.259-292, 2018 (SCI-Expanded)

Evaluation of the Effect of Spar Cap Fiber Angle of Bending-Torsion Coupled Blades on the Aero-Structural Performance of Wind Turbines

Şener Ö., Farsadi T., Gozc M. O., Kayran A.

Journal of Solar Energy Engineering, Transactions of the ASME , vol.140, 2018 (SCI-Expanded)

Aircraft vulnerability assessment against fragmentation warhead

Konokman H. E., KAYRAN A., KAYA M.

AEROSPACE SCIENCE AND TECHNOLOGY , vol.67, pp.215-227, 2017 (SCI-Expanded)

Experimental and numerical study of process-induced total spring-in of corner-shaped composite parts

Cicek K. F., Erdal Erdoğmuş M., Kayran A.

JOURNAL OF COMPOSITE MATERIALS , vol.51, pp.2347-2361, 2017 (SCI-Expanded)

Accurate equivalent models of sandwich laminates with honeycomb core and composite face sheets via optimization involving modal behavior

Cinar O., ERDAL ERDOĞMUŞ M., KAYRAN A.

JOURNAL OF SANDWICH STRUCTURES & MATERIALS , vol.19, no.2, pp.139-166, 2017 (SCI-Expanded)

Two-stage fatigue life evaluation of an aircraft fuselage panel with a bulging circumferential crack and a broken stringer

Sayar B., KAYRAN A.

FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES , vol.37, no.5, pp.494-507, 2014 (SCI-Expanded)

Non-linear progressive failure analysis of open-hole composite laminates under combined loading

Gunel M., KAYRAN A.

JOURNAL OF SANDWICH STRUCTURES & MATERIALS , vol.15, no.3, pp.309-339, 2013 (SCI-Expanded)

Effect of Semi-Geodesic Winding on the Vibration Characteristics of Filament Wound Shells of Revolution

KAYRAN A., Ibrahimoglu C. S.

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME , vol.78, no.6, 2011 (SCI-Expanded)

Computational and experimental study of high-speed impact of metallic Taylor cylinders

Konokman H. E., Coruh M. M., KAYRAN A.

ACTA MECHANICA , vol.220, pp.61-85, 2011 (SCI-Expanded)

Free-Vibration Analysis of Ring-Stiffened Branched Composite Shells of Revolution

KAYRAN A., Yavuzbalkan E.

AIAA JOURNAL , vol.48, no.4, pp.749-762, 2010 (SCI-Expanded)

An Approach for the Evaluation of Effective Elastic Properties of Honeycomb Cores by Finite Element Analysis of Sandwich Panels

Aydincak I., KAYRAN A.

JOURNAL OF SANDWICH STRUCTURES & MATERIALS , vol.11, no.5, pp.385-408, 2009 (SCI-Expanded)

Semi-analytical study of free vibration characteristics of shear deformable filament wound anisotropic shells of revolution

KAYRAN A., Yavuzbalkan E.

JOURNAL OF SOUND AND VIBRATION , vol.319, pp.260-281, 2009 (SCI-Expanded)

Flight flutter testing and aeroelastic stability of aircraft

Kayran A.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY , vol.79, no.2, pp.150-162, 2007 (SCI-Expanded)

Flight flutter testing and aeroelastic stability of aircraft

Kayran A.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY , vol.79, no.5, pp.494-506, 2007 (SCI-Expanded)

Kuessner's function in the sharp-edged gust problem - A correction

Kayran A.

JOURNAL OF AIRCRAFT , vol.43, no.5, pp.1596-1599, 2006 (SCI-Expanded)

Kuessner's function in the sharp-edged gust problem - A correction

Kayran A.

Journal Of Aircraft , vol.43, no.5, pp.1596-1599, 2006 (SCI-Expanded)

Flutter qualification of transport aircraft with store suspension

Kayran A.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY , vol.76, no.1, pp.19-28, 2004 (SCI-Expanded)

Effect of stacking sequence on free vibration frequencies of laminated composite circular cylindrical shells

Kayran A., Anlas G.

JOURNAL OF VIBRATION AND CONTROL , vol.5, no.3, pp.355-372, 1999 (SCI-Expanded)

A method of strain and stress analysis for failure prediction in laminated composites

Ardiç E., Bolcan C., Kayran A.

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering , vol.209, no.1, pp.43-51, 1995 (SCI-Expanded)

A METHOD OF STRAIN AND STRESS-ANALYSIS OF COMPOSITES FOR NONLINEAR STRAIN DISTRIBUTION CASE

ARDIC E., BOLCAN C., KAYRAN A.

INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES , vol.31, no.24, pp.3457-3473, 1994 (SCI-Expanded)

A METHOD FOR THE CALCULATION OF NATURAL FREQUENCIES OF ORTHOTROPIC AXISYMMETRICALLY LOADED SHELLS OF REVOLUTION

KAYRAN A., VINSON J., ARDIC E.

JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME , vol.116, no.1, pp.16-25, 1994 (SCI-Expanded)

THE EFFECT OF TRANSVERSE-SHEAR DEFORMATION ON THE NATURAL FREQUENCIES OF LAYERED COMPOSITE PARABOLOIDAL SHELLS

KAYRAN A., VINSON J.

JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME , vol.112, no.4, pp.429-439, 1990 (SCI-Expanded)

TORSIONAL VIBRATIONS OF LAYERED COMPOSITE PARABOLOIDAL SHELLS

KAYRAN A., VINSON J.

JOURNAL OF SOUND AND VIBRATION , vol.141, no.2, pp.231-244, 1990 (SCI-Expanded)

FREE-VIBRATION ANALYSIS OF LAMINATED COMPOSITE TRUNCATED CIRCULAR CONICAL SHELLS

KAYRAN A., VINSON J.

AIAA JOURNAL , vol.28, no.7, pp.1259-1269, 1990 (SCI-Expanded)

Articles Published in Other Journals

Implementation of Dirlik's damage model for the vibration fatigue analysis

Demirel G., Kayran A.

Procedia Structural Integrity , vol.21, pp.101-111, 2019 (Conference Book)

Development of a regression model for the life assessment of open-hole specimens with double through cracks utilizing stress intensity factor calculations via XFEM

Heıdarı S., Kayran A.

Procedia Structural Integrity , vol.21, pp.154-165, 2019 (Peer-Reviewed Journal)

Load Reduction in Wind Turbines with Bend-Twist CoupledBlades without Power Loss at Underrated Wind Speeds

Atalay O., Kayran A.

Journal of Physics: Conference Series , vol.1037, no.42015, pp.1-10, 2018 (Peer-Reviewed Journal)

Investigation of the effect of bending twisting coupling on the loads in wind turbines with superelement blade definition

Gözcü M. O., Kayran A.

Journal of Physics: Conference Series , vol.524, no.12040, pp.1-10, 2014 (Peer-Reviewed Journal)

Preliminary study on the applicability of semi-geodesic winding in the design and manufacturing of composite towers

Kayran A., İbrahimoğlu C. S.

Journal of Physics: Conference Series , vol.555, no.12059, pp.1-12, 2014 (Peer-Reviewed Journal)

Comparison of transient and quasi-steady aeroelastic analysis of wind turbine blade in steady wind conditions

Sargın H., Kayran A.

Journal of Physics: Conference Series , vol.524, no.12051, pp.1-11, 2014 (Peer-Reviewed Journal)

Investigation of the effect of bending twisting coupling on the load in wind turbines with superelement blade definition

GÖZCÜ M. O., KAYRAN A.

Journal of Physics Conference Series , vol.524, no.12040, 2014 (Peer-Reviewed Journal)

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

Dababneh O., KAYRAN A.

International Journal of Structural Integrity , vol.5, no.3, pp.214-226, 2014 (ESCI)

Assessment of effective elastic properties of honeycomb cores by finite element analysis of sandwich panels

KAYRAN A., Aydincak I.

ICCM International Conferences on Composite Materials , 2009 (Scopus)

Effect of anisotropy on the vibration characteristics of composite shells of revolution

KAYRAN A., Yavuzbalkan E.

ICCM International Conferences on Composite Materials , 2007 (Scopus)

Refereed Congress / Symposium Publications in Proceedings

Topology-Lattice Optimization of an Extendable Wing

KAYRAN A., Aksoy B.

10th World Congress on Mechanical, Chemical, and Material Engineering, MCM 2024, Barcelona, Spain, 22 - 24 August 2024

Performance Comparison of RBF and ANN Based Surrogate Models for the Static Aeroelastic Behavior of a Wing

Yılmaz Ö. Ö., KAYRAN A.

AIAA Aviation Forum and ASCEND, 2024, Nevada, United States Of America, 29 July - 02 August 2024

Implementation of Through the Thickness Compressive Stress on the Retardation of Delamination Initiation in Ply-Drop Off Regions

Ergin F., Kayran A.

International Workshop on Plasticity, Damage and Fracture of Engineering Materials, İstanbul, Turkey, 4 - 06 October 2023

STRUCTURAL DESIGN, TOPOLOGY AND MULTI-OBJECTIVE OPTIMIZATION OF A PRISMATIC STRUCTURE UTILIZING STRUT BASED LATTICE CELL STRUCTURES

Aksoy B., Kayran A.

12th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 13 - 15 September 2023, pp.1-18

Numerical Investigation of Delamination in Highly Tapered Laminates

Ergin F., Kayran A.

Eccomass COMPOSITES 2023, Palermo, Italy, 12 - 14 September 2023

Investigation of the Effects of Varying Stagger Distances on Load Carrying Capacity of Tapered Laminates

Ergin F., Kayran A.

Wind Energy Science Conference, Glasgow, England, 23 - 26 May 2023

Improving the Load Carrying Capacity of Highly Tapered Laminates

ERGİN F., KAYRAN A.

ASME International Mechanical Engineering Congress and Exposition (IMECE), Louisiana, United States Of America, 29 October - 02 November 2023 Sustainable Development

EFFICIENT MODELING OF BLADES VIA BEAM ELEMENT IN THE MULTI-OBJECTIVE OPTIMIZATION OF SMALL WIND TURBINE BLADES

KAYRAN A., ÇÖKER D., Muyan C., Batmaz O. A., Pourrajabian A., Wood D.

ASME International Mechanical Engineering Congress and Exposition (IMECE), Louisiana, United States Of America, 29 October - 02 November 2023 Sustainable Development

Boşta Hareket Davranışı İçeren Kontrol Yüzeylerine Sahip Bir Uçağın Doğrusal Olmayan Aeroservoelastik Modellenmesi ve Analizi

Yurtsever U., Kayran A., Şahin M.

Otomatik Kontrol Ulusal Kongresi (TOK), Elazığ, Turkey, 15 - 18 September 2022, pp.1-7

INVESTIGATION OF LOAD CARRYING CAPACITIES OF HIGHLY TAPERED LAMINATES

Ergin F., Kayran A.

Ulusal Havacılık ve Uzay Konferansı, İzmir, Turkey, 14 - 16 September 2022, pp.1-9

Aeroelastic Model Corrections of a Very Light Aircraft; Implications on Static Trim, Flutter and Gust Response

Demirer G., Kayran A.

AIAA AVIATION 2022 Forum, Illinois, United States Of America, 27 June - 01 July 2022

TENSILE TESTING OF REPAIRED COMPOSITE SPECIMENS WITH DIC MEASUREMENT AND FEM CORRELATION

Ekren M., KAYRAN A.

11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 08 September 2021, pp.1-10

DESIGN OPTIMIZATION OF VARIABLE STIFFNESS COMPOSITE LAMINATES USING SURROGATE MODELS FOR MINIMUM COMPLIANCE OF CURVED WING PANELS

İNCİ H., KAYRAN A.

11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 08 September 2021, pp.1-20

INVESTIGATION OF THE EFFECT OF LAMINATE STIFFNESS ON BEARING/BYPASS LOADS FOR BOLTED COMPOSITE JOINTS

Candan K., KAYRAN A.

11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 08 September 2021, pp.1-19

NURBS BASED OPTIMIZATION OF VARIABLE STIFNESS COMPOSITE STRUCTURES

ÇİMEN K., KAYRAN A.

11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 08 September 2021, pp.1-16

Static and Dynamic Aeroelastic Analysis of a Very Light Aircraft

Demirer H. G., Kayran A.

Ankara International Aerospace Conference, Ankara, Turkey, 8 - 10 September 2021, no.2021057, pp.1-14

Homogenization of Unidirectional Composites with Brittle Fracture Modeled by the Phase-Field Approach

Atasoy M., Kayran A., Göktepe S.

6th International Virtual Conference of Engineering Against Failure, Patras, Greece, 23 - 25 June 2021, no.115, pp.100

COMPARATIVE STRUCTURAL OPTIMIZATION STUDY OF COMPOSITE AND ALUMINUM HORIZONTAL TAIL PLANE OF A HELICOPTER

Arpacıoğlu B., KAYRAN A.

ASME 2019International Mechanical Engineering Congress and Exposition, 11 - 14 November 2019

AEROELASTIC MODELING AND ANALYSIS OF HIGH ASPECT RATIO WINGS WITH DIFFERENT FIDELITY STRUCTURAL MODELS

Çiçek G., KAYRAN A.

ASME 2019 International Mechanical Engineering Congress and Exposition, 11 - 14 November 2019

Multibody Simulation of Helicopter Rotor with Structural Flexibility

Turan B. İ., KAYRAN A.

8th Asian/Australian Rotorcraf t Forum, 30 October - 02 November 2019

AN INVESTIGATION ON DEVELOPMENT OF A PREDICTION MODEL FOR FATIGUE LIFE OF OPEN HOLE SPECIMENS WITH DOUBLE THROUGH THE THICKNESS CRACKS USING RESPONSE SURFACE METHODOLOGY

Shabestari S. H., Kayran A.

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 18 - 20 September 2019, no.2019046, pp.1-15

A COMPARISON STUDY ON STRENGTH ANALYSIS OF COMPOSITE REPAIR ADHESIVE ZONE BY ANALYTICAL METHODS AND ABAQUS COHESIVE ZONE MODELLING TECHNIQUES

Ekren M., Kayran A.

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 18 - 20 September 2019, pp.1-10

Experimental Assessment of Bend-Twist Coupling Potentials of Composite Materials via Digital Image Correlation Method

ŞENER Ö., ATALAY O., KAYRAN A.

AIAA SciTech Forum, 7 - 11 January 2019

Implementation of Dirlik's damage model for the vibration fatigue analysis

Demirel G. I., KAYRAN A.

1st International Workshop on Plasticity, Damage and Fracture of Engineering Materials, IWPDF 2019, Ankara, Turkey, 22 - 23 August 2019, vol.21, pp.101-111

Development of a regression model for the life assessment of open-hole specimens with double through cracks utilizing stress intensity factor calculations via XFEM

Shabestari S. S. H., KAYRAN A.

1st International Workshop on Plasticity, Damage and Fracture of Engineering Materials, IWPDF 2019, Ankara, Turkey, 22 - 23 August 2019, vol.21, pp.154-165

Implementation of Dirlik s damage model for the vibration fatigue analysis

Demirel İ. G., Kayran A.

1st International Workshop on Plasticity, Damage and Fracture of Engineering Materials, IWPDF 2019, Ankara, Turkey, 22 - 23 August 2019, pp.101-111

ENERGY ABSORPTION MECHANISMS AND CRASH ANALYSIS OF HELICOPTER SEATS

Öztürk G., KAYRAN A.

International Mechanical Engineering Congress and Exposition IMECE2018, United States Of America, 9 - 15 November 2018

EVALUATION OF TRANSVERSE SHEAR MODULI OF COMPOSITE SANDWICH BEAMS THROUGH THREE-POINT BENDING TESTS

ŞENER Ö., Dede O., ATALAY O., ATASOY M., KAYRAN A.

International Mechanical Engineering Congress and Exposition IMECE2018, United States Of America, 9 - 15 November 2018

COMPARATIVE STUDY OF POST-BUCKLING LOAD REDISTRIBUTION IN STIFFENED AIRCRAFT PANEL WITH AND WITHOUT MATERIAL NONLINEARITY

AYDIN E., KAYRAN A.

International Mechanical Engineering Congress and Exposition IMECE2018, United States Of America, 9 - 15 November 2018

KANAT SUPERSONİK FLUTTER HIZININ İKİ BOYUTLU KANAT AERODİNAMİĞİ İLE TAHMİNİ

Okumuş B., Kayran A.

VII. ULUSAL HAVACILIK VE UZAY KONFERANSI, Samsun, Turkey, 12 - 14 September 2018, no.20181040, pp.1-11

Determination of Transverse Shear Moduli of Composite Core Materials Through Sandwich Beam Tests

ŞENER Ö., Dede O., ATALAY O., ATASOY M., KAYRAN A.

12th International Conference on Sandwich Structures ICSS-12, Switzerland, 19 - 22 August 2018

Load Reduction in Wind Turbines with Bend-Twist Coupled Blades without Power Loss at Underrated Wind Speeds

Atalay O., Kayran A.

7th Science of Making Torque from Wind, TORQUE 2018, Milan, Italy, 20 - 22 June 2018, vol.1037

Optimization of Variable Stiffness Composite Laminates by Particle Swarm and Whale Optimization Algorithms Utilizing Surrogate Models

İNCİ H., KAYRAN A.

AIAA SciTech Forum 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Kissimmee, United States Of America, 8 - 12 January 2018

Structural Performance and Power Production of Wind Turbine Systems with Bend-Twist Coupled Blades in Underrated Wind Conditions

ŞENER Ö., KAYRAN A.

AIAA SciTech Forum 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, United States Of America, 8 - 12 January 2018

Nonlinear Static Aeroelastic Behavior of Composite Missile Fin with Interlaminar and Intralaminar Damage

ÖZKAYA Ö., KAYRAN A.

AIAA SciTech Forum 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, United States Of America, 8 - 12 January 2018

Coupling of a multibody simulation tool for rotary systems with an unsteady viscous flow solver

Soğancı S., KAYRAN A., TUNCER İ. H.

AIAA Aerospace Sciences Meeting, 2018, Florida, United States Of America, 8 - 12 January 2018

EXPERIMENTAL STUDY AND FINITE ELEMENT ANALYSIS OF DOVETAIL ATTACHMENTS

Akay A. A., Çöker D., Kayran A., Gürses E.

ASME 2017 International Mechanical Engineering Congress & Exposition, Florida, United States Of America, 3 - 09 November 2017, pp.1-8

FREE VIBRATION ANALYSIS OF UNIFORM AND ASYMMETRIC COMPOSITE PRETWISTED ROTATING THIN WALLED BEAM

Farsadi T., ŞENER Ö., KAYRAN A.

ASME International Mechanical Engineering Congress and Exposition, Tama, Japan, 3 - 09 November 2017

EXPERIMENTAL STUDY AND FINITE ELEMENT ANALYSIS OF DOVETAIL ATTACHMENTS

Akay A. A., Çöker D., Kayran A., Gürses E.

ASME International Mechanical Engineering Congress and Exposition, Tama, Japan, 3 - 09 November 2017

DEVELOPMENT OF ARTIFICIAL NEURAL NETWORK BASED DESIGN TOOL FOR AIRCRAFT ENGINE BOLTED FLANGE CONNECTION SUBJECT TO COMBINED AXIAL AND MOMENT LOAD

Sanli T. V., Gürses E., Çöker D., Kayran A.

ASME International Mechanical Engineering Congress and Exposition, Tama, Japan, 3 - 09 November 2017

Damage Analysis in Blast Loaded Concrete Columns Using Single Degree of Freedom Approach

ERDOLU Ö., KAYRAN A.

17th International Symposium on the Interaction of the Effects of Munitions with Structures- ISIEMS, Germany, 16 - 20 October 2017