Yayınlar & Eserler

Yayın Ağı
SCI, SSCI ve AHCI İndekslerine Giren Dergilerde Yayınlanan Makaleler

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

Inci H., KAYRAN A.
COMPOSITE STRUCTURES , cilt.351, 2025 (SCI-Expanded) identifier identifier

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

Özkaya Yılmaz Ö., KAYRAN A.
Aerospace , cilt.11, sa.8, 2024 (SCI-Expanded) Creative Commons License identifier

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 , cilt.11, sa.3, 2024 (SCI-Expanded) Creative Commons License identifier identifier

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 , cilt.36, sa.2, ss.709-722, 2022 (SCI-Expanded) identifier identifier

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 , cilt.235, sa.14, ss.2017-2032, 2021 (SCI-Expanded) identifier identifier

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

Asadi D., Farsadi T., KAYRAN A.
AIAA JOURNAL , cilt.59, sa.4, ss.1422-1440, 2021 (SCI-Expanded) identifier identifier

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

Farsadi T., KAYRAN A.
WIND AND STRUCTURES , cilt.32, sa.3, ss.267-281, 2021 (SCI-Expanded) Sürdürülebilir Kalkınma identifier identifier

Classical flutter analysis of composite wind turbine blades including compressibility

Farsadi T., KAYRAN A.
WIND ENERGY , cilt.24, sa.1, ss.69-91, 2021 (SCI-Expanded) Sürdürülebilir Kalkınma identifier identifier

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

Farsadi T., Rahmanian M., KAYRAN A.
JOURNAL OF FLUIDS AND STRUCTURES , cilt.92, 2020 (SCI-Expanded) identifier identifier

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 , cilt.141, 2019 (SCI-Expanded) identifier identifier

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

Farsadi T., Rahmanian M., KAYRAN A.
JOURNAL OF FLUIDS AND STRUCTURES , cilt.83, ss.259-292, 2018 (SCI-Expanded) identifier identifier

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 , cilt.140, 2018 (SCI-Expanded) identifier identifier

Aircraft vulnerability assessment against fragmentation warhead

Konokman H. E., KAYRAN A., KAYA M.
AEROSPACE SCIENCE AND TECHNOLOGY , cilt.67, ss.215-227, 2017 (SCI-Expanded) identifier identifier

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 , cilt.51, ss.2347-2361, 2017 (SCI-Expanded) identifier identifier

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 , cilt.19, sa.2, ss.139-166, 2017 (SCI-Expanded) identifier identifier

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 , cilt.37, sa.5, ss.494-507, 2014 (SCI-Expanded) identifier identifier

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

Gunel M., KAYRAN A.
JOURNAL OF SANDWICH STRUCTURES & MATERIALS , cilt.15, sa.3, ss.309-339, 2013 (SCI-Expanded) identifier identifier

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 , cilt.78, sa.6, 2011 (SCI-Expanded) identifier identifier

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

Konokman H. E., Coruh M. M., KAYRAN A.
ACTA MECHANICA , cilt.220, ss.61-85, 2011 (SCI-Expanded) identifier identifier

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

KAYRAN A., Yavuzbalkan E.
AIAA JOURNAL , cilt.48, sa.4, ss.749-762, 2010 (SCI-Expanded) identifier identifier

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 , cilt.11, sa.5, ss.385-408, 2009 (SCI-Expanded) identifier identifier

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 , cilt.319, ss.260-281, 2009 (SCI-Expanded) identifier identifier

Flight flutter testing and aeroelastic stability of aircraft

Kayran A.
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY , cilt.79, sa.2, ss.150-162, 2007 (SCI-Expanded) identifier identifier

Flight flutter testing and aeroelastic stability of aircraft

Kayran A.
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY , cilt.79, sa.5, ss.494-506, 2007 (SCI-Expanded) identifier identifier

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

Kayran A.
JOURNAL OF AIRCRAFT , cilt.43, sa.5, ss.1596-1599, 2006 (SCI-Expanded) identifier identifier

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

Kayran A.
Journal Of Aircraft , cilt.43, sa.5, ss.1596-1599, 2006 (SCI-Expanded)

Flutter qualification of transport aircraft with store suspension

Kayran A.
AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY , cilt.76, sa.1, ss.19-28, 2004 (SCI-Expanded) identifier identifier

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

Kayran A., Anlas G.
JOURNAL OF VIBRATION AND CONTROL , cilt.5, sa.3, ss.355-372, 1999 (SCI-Expanded) identifier identifier

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 , cilt.209, sa.1, ss.43-51, 1995 (SCI-Expanded) identifier identifier

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 , cilt.31, sa.24, ss.3457-3473, 1994 (SCI-Expanded) identifier identifier

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 , cilt.116, sa.1, ss.16-25, 1994 (SCI-Expanded) identifier identifier

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 , cilt.112, sa.4, ss.429-439, 1990 (SCI-Expanded) identifier identifier

TORSIONAL VIBRATIONS OF LAYERED COMPOSITE PARABOLOIDAL SHELLS

KAYRAN A., VINSON J.
JOURNAL OF SOUND AND VIBRATION , cilt.141, sa.2, ss.231-244, 1990 (SCI-Expanded) identifier identifier

FREE-VIBRATION ANALYSIS OF LAMINATED COMPOSITE TRUNCATED CIRCULAR CONICAL SHELLS

KAYRAN A., VINSON J.
AIAA JOURNAL , cilt.28, sa.7, ss.1259-1269, 1990 (SCI-Expanded) identifier identifier
Diğer Dergilerde Yayınlanan Makaleler

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

Demirel G., Kayran A.
Procedia Structural Integrity , cilt.21, ss.101-111, 2019 (Düzenli olarak gerçekleştirilen hakemli kongrenin bildiri kitabı) Creative Commons License

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 , cilt.21, ss.154-165, 2019 (Hakemli Dergi) Creative Commons License

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 , cilt.1037, sa.42015, ss.1-10, 2018 (Hakemli Dergi) Creative Commons License

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 , cilt.524, sa.12040, ss.1-10, 2014 (Hakemli Dergi) Creative Commons License

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 , cilt.555, sa.12059, ss.1-12, 2014 (Hakemli Dergi) Creative Commons License

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 , cilt.524, sa.12051, ss.1-11, 2014 (Hakemli Dergi) Creative Commons License

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 , cilt.524, sa.12040, 2014 (Hakemli Dergi)

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 , cilt.5, sa.3, ss.214-226, 2014 (ESCI) identifier identifier

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) identifier

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

KAYRAN A., Yavuzbalkan E.
ICCM International Conferences on Composite Materials , 2007 (Scopus) identifier
Hakemli Kongre / Sempozyum Bildiri Kitaplarında Yer Alan Yayınlar

Topology-Lattice Optimization of an Extendable Wing

KAYRAN A., Aksoy B.
10th World Congress on Mechanical, Chemical, and Material Engineering, MCM 2024, Barcelona, İspanya, 22 - 24 Ağustos 2024 identifier

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, Amerika Birleşik Devletleri, 29 Temmuz - 02 Ağustos 2024 identifier

Katman Azaltma Bölgelerinde katman Ayrılması Başlangıcının Geciktirilmesinde Kalınlık Boyunca Basınç Gerilmesinin Uygulanması

Ergin F., Kayran A.
International Workshop on Plasticity, Damage and Fracture of Engineering Materials, İstanbul, Türkiye, 4 - 06 Ekim 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, Türkiye, 13 - 15 Eylül 2023, ss.1-18

Yüksek Konik Laminatlarda Katman Ayrılmasının İncelenmesi

Ergin F., Kayran A.
Eccomass COMPOSITES 2023, Palermo, İtalya, 12 - 14 Eylül 2023

Değişen Kademeli Mesafelerin Konik Laminatların Yük Taşıma Kapasitesine Etkisinin İncelenmesi

Ergin F., Kayran A.
Wind Energy Science Conference, Glasgow, İngiltere, 23 - 26 Mayıs 2023

Improving the Load Carrying Capacity of Highly Tapered Laminates

ERGİN F., KAYRAN A.
ASME International Mechanical Engineering Congress and Exposition (IMECE), Louisiana, Amerika Birleşik Devletleri, 29 Ekim - 02 Kasım 2023 Sürdürülebilir Kalkınma identifier identifier

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, Amerika Birleşik Devletleri, 29 Ekim - 02 Kasım 2023 Sürdürülebilir Kalkınma identifier identifier

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, Türkiye, 15 - 18 Eylül 2022, ss.1-7

YÜKSEK DERECEDE KONİK LAMİNATLARIN YÜK TAŞIMA KAPSİTELERİNİN İNCELENMESİ

Ergin F., Kayran A.
Ulusal Havacılık ve Uzay Konferansı, İzmir, Türkiye, 14 - 16 Eylül 2022, ss.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, Amerika Birleşik Devletleri, 27 Haziran - 01 Temmuz 2022 identifier

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

Ekren M., KAYRAN A.
11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 08 Eylül 2021, ss.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, Türkiye, 08 Eylül 2021, ss.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, Türkiye, 08 Eylül 2021, ss.1-19

NURBS BASED OPTIMIZATION OF VARIABLE STIFNESS COMPOSITE STRUCTURES

ÇİMEN K., KAYRAN A.
11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Türkiye, 08 Eylül 2021, ss.1-16

Static and Dynamic Aeroelastic Analysis of a Very Light Aircraft

Demirer H. G., Kayran A.
Ankara International Aerospace Conference, Ankara, Türkiye, 8 - 10 Eylül 2021, sa.2021057, ss.1-14 Creative Commons License

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, Yunanistan, 23 - 25 Haziran 2021, sa.115, ss.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 Kasım 2019 identifier

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 Kasım 2019 identifier

Multibody Simulation of Helicopter Rotor with Structural Flexibility

Turan B. İ., KAYRAN A.
8th Asian/Australian Rotorcraf t Forum, 30 Ekim - 02 Kasım 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, Türkiye, 18 - 20 Eylül 2019, sa.2019046, ss.1-15 Creative Commons License

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, Türkiye, 18 - 20 Eylül 2019, ss.1-10 Creative Commons License

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 Ocak 2019 identifier

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, Türkiye, 22 - 23 Ağustos 2019, cilt.21, ss.101-111 identifier identifier

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, Türkiye, 22 - 23 Ağustos 2019, cilt.21, ss.154-165 identifier identifier

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, Türkiye, 22 - 23 Ağustos 2019, ss.101-111 Creative Commons License

ENERGY ABSORPTION MECHANISMS AND CRASH ANALYSIS OF HELICOPTER SEATS

Öztürk G., KAYRAN A.
International Mechanical Engineering Congress and Exposition IMECE2018, Amerika Birleşik Devletleri, 9 - 15 Kasım 2018 identifier

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, Amerika Birleşik Devletleri, 9 - 15 Kasım 2018 identifier

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, Amerika Birleşik Devletleri, 9 - 15 Kasım 2018 identifier

KANAT SUPERSONİK FLUTTER HIZININ İKİ BOYUTLU KANAT AERODİNAMİĞİ İLE TAHMİNİ

Okumuş B., Kayran A.
VII. ULUSAL HAVACILIK VE UZAY KONFERANSI, Samsun, Türkiye, 12 - 14 Eylül 2018, sa.20181040, ss.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, İsviçre, 19 - 22 Ağustos 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, İtalya, 20 - 22 Haziran 2018, cilt.1037 identifier identifier

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, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

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, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

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, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

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, Amerika Birleşik Devletleri, 8 - 12 Ocak 2018 identifier

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, Amerika Birleşik Devletleri, 3 - 09 Kasım 2017, ss.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, Japonya, 3 - 09 Kasım 2017 identifier identifier

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, Japonya, 3 - 09 Kasım 2017 identifier identifier

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, Japonya, 3 - 09 Kasım 2017 identifier identifier

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, Almanya, 16 - 20 Ekim 2017

Energy Absoption Mechanisms and Crash Analysis of Helicopter Seats

ÖZTÜRK G., KAYRAN A.
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Türkiye, 20 - 22 Eylül 2017

Investigation of the Effect of Boundary Conditions on the Buckling Coefficients of Stiffned Flat Panels

AYDIN E., KAYRAN A.
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Türkiye, 20 - 22 Eylül 2017

Performance Study of Wind Turbines with Bend-Twist Coupled Blades at Underrated Wind Speeds

ATALAY O., FARSADİ T., KAYRAN A.
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Türkiye, 20 - 22 Eylül 2017

Nonlinear Static Aeroelastic Behaviour of Composite Missile Fin with Interlaminar Damage

ÖZKAYA Ö., KAYRAN A.
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Türkiye, 20 - 22 Eylül 2017

The Effect of Modal Damping on Random Vibration Metal Fatigue Analysis

DEMİREL İ. G., KAYRAN A.
9thANKARA INTERNATIONAL AEROSPACE CONFERENCE, Türkiye, 20 - 22 Eylül 2017

Comparison of 2D and 3D Homogenization Processes for Micromechanics Analysis of Unidirectional Composites

ATASOY M., KAYRAN A.
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Türkiye, 20 - 22 Eylül 2017

Design Optimization of Variable Stiffness Composite Laminates Using Surrogate Models for Compliance and Buckling Load

İNCİ H., KAYRAN A.
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Türkiye, 20 - 22 Eylül 2017

Multibody Simulation of Helicopter Rotor with Flexible Blade

ÖZTURAN B. İ., KAYRAN A.
9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Türkiye, 20 - 22 Eylül 2017

Implementation of the Submodelling Technique on the Dovetail Attachments”

Akay A. A., Çöker D., Kayran A., Gürses E.
9th Ankara International Aerospace Conference, Ankara, Türkiye, 20 - 22 Eylül 2017

Effect of Fibre Orientation of Bend-Twist Coupled Blades on the Structural Performance of the Wind Turbine System

ŞENER Ö., FARSADİ T., KAYRAN A.
AIAA SciTech Forum 35th Wind Energy Symposium, Amerika Birleşik Devletleri, 9 - 13 Ocak 2017

Effect of Fiber Orientation of Bend-Twist Coupled Blades on the Structural Performance of the Wind Turbine System

Şener Ö., Farsadı T., Kayran A.
35th Wind Energy Symposium, Texas, Amerika Birleşik Devletleri, 9 - 13 Ocak 2017 identifier

High strain rate material characterization of Al 7075-T651 by modified Taylor impact test and velocity interferometry

Kesemen L., Kayran A.
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017, Texas, Amerika Birleşik Devletleri, 9 - 13 Ocak 2017 identifier

Stick model development of aircraft structures for dynamic analysis

Hayirli U., Kayran A.
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017, Texas, Amerika Birleşik Devletleri, 9 - 13 Ocak 2017 identifier

HELİKOPTER PALLERİNİN ÇOKLU KÜTLELİ BENZETİM ARACI VE İKİ BOYUTLU PANEL TABANLI AKIŞ ÇÖZÜCÜSÜ İLE ETKİLEŞİMLİ ANALİZİ

Soğancı S., KAYRAN A., TUNCER İ. H.
6. Ulusal Havacılık ve Uzay Konferansı, Kocaeli, Türkiye, 28 - 30 Eylül 2016

Eksenel Kesme ve Moment Yükü Altındaki Flanşlar İçin Yapay Sinir Ağına Dayalı Cıvatalı Flanş Tasarım Aracı Geliştirilmesi

Şanlı V., Akay A. A., Yıldırım A., Gürses E., Çöker D., Kayran A.
VI. Ulusal Havacılık ve Uzay Konferansı (UHUK), Kocaeli, Türkiye, 28 - 30 Eylül 2016

Structural Optimization of Composite Helicopter Rotor Blades

IŞIK A. A., KAYRAN A.
American Society for Composites, 31st Technical Conference and ASTM Committee D30 Meeting, 19 - 22 Eylül 2016 identifier

Comparative Study of Finite Element Analysis and Geometrically Exact Beam Analysis of a Composite Helicopter Blade

ATAÇ M. N., KAYRAN A.
American Helicopter Society AHS 72nd Annual Forum, 17 - 19 Mayıs 2016 identifier

Classical Aeroelastic Stability Analysis of Large Composite Wind Turbine Blades

FARSADİ T., KAYRAN A.
AIAA Science and Technology Forum and Exposition 2016, 4 - 08 Ocak 2016 identifier

Aeroelastic Stability Evaluation of Bend Twist Coupled Composite Wind Turbine Blades Designed for Load Alleviation in Wind Turbine Systems

FARSADİ T., KAYRAN A.
AIAA Science and Technology Forum and Exposition 2016, 4 Ocak - 08 Nisan 2016 identifier

Post Buckling Load Redistribution of Stiffened Panels in Aircraft Wingbox Structures

MERT M., KAYRAN A.
AIAA Science and Technology Forum and Exposition 2016, 4 - 08 Ocak 2016 identifier

Three dimensional delamination analysis in composite open hole tensile specimens with cohesive zone method

Bartan Kumbasar B., Acar B., Kayran A.
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier

Structural dynamics analysis and passive control of wind turbine vibrations with tuned mass damper (TMD) technique

Farsadi T., Kayran A.
57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016, California, Amerika Birleşik Devletleri, 4 - 08 Ocak 2016 identifier

DEVELOPMENT OF BOLTED FLANGE DESIGN TOOL BASED ON FINITE ELEMENT ANALYSIS AND ARTIFICIAL NEURAL NETWORK

Yildirim A., Kayran A., Gulasik H., Çöker D., Gürses E., Kayran A.
ASME International Mechanical Engineering Congress and Exposition (IMECE2015), Texas, Amerika Birleşik Devletleri, 13 - 19 Kasım 2015 identifier identifier

IMECE2015 51021 DEVELOPMENT OF BOLTED FLANGE DESIGN TOOL BASED ON FINITE ELEMENT ANALYSIS AND ARTIFICIAL NEURAL NETWORK

yıldırım a., hasan g., AKAY A. A., GÜRSES E., ÇÖKER D., KAYRAN A.
IMECE2015 - ASME 2015 International Mechanical Engineering Congress & Exposition, Houston, 13 - 19 Kasım 2015

Reduction of fatigue damage equivalent loads In the wind turbine system through the use bending twisting coupling induced in composite wind turbine blades

Şener Ö., Farsadi T., Gözcü O., KAYRAN A.
EERA JP-Wind/IRPWIND konferansı, Amsterdam, Hollanda, 28 - 29 Eylül 2015

PARAMETRIC STUDY FOR THE STUDY OF THE EFFECT OF CONTACT PARAMETERS FOR PLASTIC ANALYSIS OF BOLTED FLANGE CONNECTIONS

Yilmaz S. E., Kayran A., Gürses E., Çöker D.
8th Ankara International Aerospace Conference, Ankara, Türkiye, 10 - 12 Eylül 2015

PARAMETERS CORRELATION STUDY TO INVESTIGATE THE EFFECTS OF GEOMETRIC VARIABLES ON THE SAFETY OF BOLTED FLANGE CONNECTIONS

Yildirim A., Akay A. A., Gulasik H., Çöker D., Gürses E., Kayran A.
8th Ankarar International Aerospace Conference, Ankara, Türkiye, 10 - 12 Eylül 2015

MODELING OF A CIRCULAR DOUBLE FLANGE JOINT INCLUDING CONTACT AND FRICTION EFFECTS

Akay A. A., Gulasik H., Yildirim A., Çöker D., Kayran A., Gürses E.
8th Ankara International Aerospcae Conference, Ankara, Türkiye, 10 - 12 Eylül 2015

Modeling of Circular Double Flange Joint Including Contact and Friction Effects

AKAY A. A., Gülaşık H., Yıldırım A., ÇÖKER D., KAYRAN A., GÜRSES E.
8th Ankara International Aerospace Conference-AIAC, Ankara, Türkiye, 10 - 12 Eylül 2015

Utilizing Bending Twisting Coupling in Composite Wind Turbine Blades in Achieving Reduction in Fatigue Loads

Şener Ö., Farsadi T., Gözcü O., KAYRAN A.
8th Ankara International Aerospace Conference-AIAC, Ankara, Türkiye, 10 - 12 Eylül 2015

Investigation of Effects of Bird Strike on Wing Leading Edge By Using Explicit Finite Element Method

Dede O., KAYRAN A.
8th Ankara International Aerospace Conference-AIAC, Ankara, Türkiye, 10 - 12 Eylül 2015

FLUID STRUCTURE INTERACTION BASED ON PANEL METHOD AND GEOMETRICALLY NONLINEAR STRUCTURAL ANALYSIS

Sedat Ö., KAYRAN A., TUNCER İ. H.
Ankara International Aerospace COnference, 10 - 12 Eylül 2015

Parametric Study of Delamination Analysis in Composites with Cohesive Zone Method

Bartan B., KAYRAN A., Acar B.
8th Ankara International Aerospace Conference-AIAC, Ankara, Türkiye, 10 - 12 Eylül 2015

Reduction of Fatigue Damage Equivalent Loads in the Wind Turbine System Through the Use of Off Axis Plies in the Spar Caps of Composite Wind Turbine Blades

Gözcü O., Farsadi T., Şener Ö., KAYRAN A.
20th International Conference on Composite Materials, Kopenhag, Danimarka, 19 - 24 Temmuz 2015

Design of Experiments Study for Determination for the Study of the Effect of Contact Parameters in Bolted Flange Connections

Yılmaz S. E., Özcihan T., Kayran A., Gürses E., Çöker D.
International Conference on Advances in Mechanical Engineering (ICAME 2015), İstanbul, Türkiye, 13 - 15 Mayıs 2015

Maximizing Buckling Load Factors of Fiber Placed Composite Cylindrical Shells by Particle Swarm Optimization

Güldü S., Kayran A.
AIAA Science and Technology Forum and Exposition, AIAA SciTech 2015, 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015 identifier

Assessment of the Effect of Hybrid GFRP CFRP Usage in Wind Turbine Blades on the Reduction of Fatigue Damage Equivalent Loads in the Wind Turbine System

Gözcü O., Farsadi T., Şener Ö., KAYRAN A.
AIAA Science and Technology Forum and Exposition, AIAA SciTech 2015, 33rd Wind Energy Symposium, Kissimmee, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015

Assessment of the effect of hybrid GFRP-CFRP usage in wind turbine blades on the reduction of fatigue damage equivalent loads in the wind turbine system

Gözcü M. O., Farsadi T., ŞENER Ö., KAYRAN A.
33rd Wind Energy Symposium 2015, Florida, Amerika Birleşik Devletleri, 5 - 09 Ocak 2015 identifier

Reduction of fatigue damage equivalent loads in the wind turbine system through the use of off-axis plies in the spar caps of composite wind turbine blades

Ozan Gözcü M., Farsadi T., ŞENER Ö., KAYRAN A.
20th International Conference on Composite Materials, ICCM 2015, Copenhagen, Danimarka, 19 - 24 Temmuz 2015, cilt.2015-July identifier

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

Sargin H., Kayran A.
5th Science of Making Torque from Wind Conference, Copenhagen, Danimarka, 18 - 20 Haziran 2014, cilt.524 identifier identifier

Aeroservoelastic Modelling and Analysis of a Missile Control Surface with a Nonlinear Electromechanical Actuator

Mehmet Ozan N., Kayran A.
AIAA Atmospheric Flight Mechanics Conference, AIAA Aviation and Aeronautics Forum and Exposition, Georgia, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014, ss.1-31

Propulsion System Model of a Mini UAV System

Yanik S. N., Ozyetis E., Ozcan G., Alemdaroglu N., KAYRAN A., Kiran E.
International Conference on Unmanned Aircraft Systems (ICUAS), Florida, Amerika Birleşik Devletleri, 27 - 30 Mayıs 2014, ss.1073-1080 identifier identifier

Analysis of Aircraft Survivability Against Fragmenting Warhead Threat

Konokman H. E., KAYRAN A., KAYA M.
55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, National Harbor, Maryland, Amerika Birleşik Devletleri, 13 - 17 Ocak 2014

Investigation of the effect of off-axis spar cap plies on damage equivalent loads in wind turbines with superelement blade definition

GÖZCÜ M. O., OLGUN M. N., KAYRAN A.
AIAA SciTech 32nd ASME Wind Energy Symposium, Amerika Birleşik Devletleri, 13 - 17 Ocak 2014 identifier

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

Gozcu M. O., KAYRAN A.
5th Science of Making Torque from Wind Conference, Copenhagen, Danimarka, 18 - 20 Haziran 2014, cilt.524 identifier identifier

Aeroservoelastic modeling and analysis of a missile control surface with a nonlinear electromechanical actuator

Nalci M. O., KAYRAN A.
AIAA AVIATION 2014 -AIAA Atmospheric Flight Mechanics Conference 2014, Atlanta, GA, Amerika Birleşik Devletleri, 16 - 20 Haziran 2014 identifier

Static and dynamic analysis of shear deformable composite shells of revolution by semi-analytical approach

Kayran A.
10th Jubilee Conference on Shell Structures - Theory and Applications (SSTA), Gdansk, Polonya, 16 - 18 Ekim 2013, ss.301-304 identifier identifier

Two stage damage tolerance evaluation of an aircraft fuselage panel with a circumferential crack and a broken stringer

Burak Sayar M., KAYRAN A.
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Boston, MA, Amerika Birleşik Devletleri, 8 - 11 Nisan 2013 identifier

Two stage damage tolerance evaluation of an aircraft fuselage panel with a circumferential crack and a broken stringer

Burak Sayar M., KAYRAN A.
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Boston, MA, Amerika Birleşik Devletleri, 8 - 11 Nisan 2013 identifier

Fatigue life evaluation of an aircraft fuselage panel with a circumferential crack and a broken stringer

Sayar M. B., KAYRAN A.
3rd International Conference of Engineering Against Failure, ICEAF 2013, Kos, Yunanistan, 26 - 28 Haziran 2013, ss.177-186 identifier

Linear and non-linear progressive failure analysis of composite aerospace structures under combined loading

Günel M., KAYRAN A.
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, HI, Amerika Birleşik Devletleri, 23 - 26 Nisan 2012, sa.1860 identifier identifier

Investigation of the effect of geodesic and semi-geodesic winding on the vibration characteristics of variable stiffness filament wound shells of revolution

KAYRAN A., Yavuzbalkan E., Ibrahimoǧlu S.
53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012, Honolulu, HI, Amerika Birleşik Devletleri, 23 - 26 Nisan 2012 identifier identifier

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

KAYRAN A., Ibrahimoglu C. S.
4th Scientific Conference on Science of Making Torque from Wind, Oldenburg, Almanya, 9 - 11 Ekim 2012, cilt.555 Creative Commons License identifier identifier

On the Design and Aeroelastic Stability Analysis of Twin Wing-Tail Boom Configuration Unmanned Air Vehicle

ÖZÖZTÜRK S., KAYRAN A., ALEMDAROĞLU H. N., SEBER G.
52th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Amerika Birleşik Devletleri, 4 - 07 Nisan 2011 identifier

Non-linear progressive failure analysis of composite aerospace structures

Günel M., KAYRAN A.
18th International Conference on Composites Materials, ICCM 2011, Jeju, Güney Kore, 21 - 26 Ağustos 2011 identifier

A numerical integration based approach to the analysis of anisotropic shells of revolution subjected to non-axisymmetric loading

Oygür S., KAYRAN A.
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Palm Springs, CA, Amerika Birleşik Devletleri, 4 - 07 Mayıs 2009 identifier

FREE VIBRATION CHARACTERISTICS OF COMPOSITE SHELLS OF REVOLUTION WITH VARIABLE STIFFNESS COEFFICIENTS

KAYRAN A.
9th Biennial Conference on Engineering Systems Design and Analysis, Haifa, İsrail, 7 - 09 Temmuz 2008, ss.603-616 identifier

Lagrangian hydrocode formulation for large deformation problems and methods to prevent volumetric locking of triangular elements

KONOKMAN H. E., KAYRAN A., ÖZYÖRÜK Y.
AIAC'2007 Ankara International Aerospace Conference, Ankara, Turkey, 10 - 13 Eylül 2007

Numerical integration based vibration analysis of anisotropic branched shells of revolution with ring stiffeners

KAYRAN A., Yavuzbalkan E.
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Waikiki, HI, Amerika Birleşik Devletleri, 23 - 26 Nisan 2007, cilt.5, ss.4940-4961 identifier

Aeroelastic stability of a transport aircraft with wing mounted store suspension- Part II: Flight test

KAYRAN A.
Proceedings of the 7th Biennial Conference on Engineering Systems Design and Analysis - 2004, Manchester, İngiltere, 19 - 22 Temmuz 2004, cilt.2, ss.191-201 identifier

Aeroelastic stability of a transport aircraft with wing mounted store suspension- Part I: Analysis

KAYRAN A.
Proceedings of the 7th Biennial Conference on Engineering Systems Design and Analysis - 2004, Manchester, İngiltere, 19 - 22 Temmuz 2004, cilt.2, ss.179-189 identifier

Hava Taşıtlarına Uygulanan Güçlendirilmiş Silindirik Bir Dış Deponun Yapısal Analizi

TAŞ C., YAMAN Y., KAYRAN A.
11. Ulusal Makina Teorisi Sempozyumu, Ankara, Türkiye, 8 - 10 Eylül 2003

Method of failure prediction in laminated composites subjected to low-velocity impact

Erarslanoglu G., Ardic E., KAYRAN A., Bolcan C.
Proceedings of the 2nd Biennial European Joint Conference on Engineering Systems Design and Analysis. Part 1 (of 8), London, Kanada, 4 - 07 Temmuz 1994, cilt.64, ss.111-118 identifier
Metrikler

Yayın

149

Atıf (WoS)

251

H-İndeks (WoS)

9

Atıf (Scopus)

427

H-İndeks (Scopus)

11

Atıf (Scholar)

396

H-İndeks (Scholar)

12

Atıf (TrDizin)

1

H-İndeks (TrDizin)

1

Atıf (Diğer Toplam)

9

Proje

9

Tez Danışmanlığı

70

Açık Erişim

63
BM Sürdürülebilir Kalkınma Amaçları