Publications & Works

Published journal articles indexed by SCI, SSCI, and AHCI

Articles Published in Other Journals

Refereed Congress / Symposium Publications in Proceedings

Improving the Load Carrying Capacity of Highly Tapered Laminates

ASME International Mechanical Engineering Congress & Exposition 2023, Louisiana, United States Of America, 29 October - 02 November 2023

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

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

Numerical Investigation of Delamination in Highly Tapered Laminates

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

INVESTIGATION OF LOAD CARRYING CAPACITIES OF HIGHLY TAPERED LAMINATES

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

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

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

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

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

NURBS BASED OPTIMIZATION OF VARIABLE STIFNESS COMPOSITE STRUCTURES

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

Static and Dynamic Aeroelastic Analysis of a Very Light Aircraft

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

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

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

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

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

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

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

Multibody Simulation of Helicopter Rotor with Structural Flexibility

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

Implementation of Dirlik s damage model for the vibration fatigue analysis

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

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

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

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

ENERGY ABSORPTION MECHANISMS AND CRASH ANALYSIS OF HELICOPTER SEATS

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

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

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

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

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

KANAT SUPERSONİK FLUTTER HIZININ İKİ BOYUTLU KANAT AERODİNAMİĞİ İLE TAHMİNİ

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

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

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

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

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

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

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

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

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

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

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

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

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

EXPERIMENTAL STUDY AND FINITE ELEMENT ANALYSIS OF DOVETAIL ATTACHMENTS

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

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

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

Nonlinear Static Aeroelastic Behaviour of Composite Missile Fin with Interlaminar Damage

9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Turkey, 20 - 22 September 2017

Multibody Simulation of Helicopter Rotor with Flexible Blade

9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Turkey, 20 - 22 September 2017

The Effect of Modal Damping on Random Vibration Metal Fatigue Analysis

9thANKARA INTERNATIONAL AEROSPACE CONFERENCE, Turkey, 20 - 22 September 2017

Energy Absoption Mechanisms and Crash Analysis of Helicopter Seats

9th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Turkey, 20 - 22 September 2017

Implementation of the Submodelling Technique on the Dovetail Attachments”

9th Ankara International Aerospace Conference, Ankara, Turkey, 20 - 22 September 2017

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

58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017, Texas, United States Of America, 9 - 13 January 2017 identifier

Stick model development of aircraft structures for dynamic analysis

58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017, Texas, United States Of America, 9 - 13 January 2017 identifier

Structural Optimization of Composite Helicopter Rotor Blades

American Society for Composites, 31st Technical Conference and ASTM Committee D30 Meeting, 19 - 22 September 2016 identifier

Classical Aeroelastic Stability Analysis of Large Composite Wind Turbine Blades

AIAA Science and Technology Forum and Exposition 2016, 4 - 08 January 2016 identifier

Post Buckling Load Redistribution of Stiffened Panels in Aircraft Wingbox Structures

AIAA Science and Technology Forum and Exposition 2016, 4 - 08 January 2016 identifier

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

57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016, California, United States Of America, 4 - 08 January 2016 identifier

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

57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2016, California, United States Of America, 4 - 08 January 2016 identifier

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

ASME International Mechanical Engineering Congress and Exposition (IMECE2015), Texas, United States Of America, 13 - 19 November 2015 identifier identifier

Parametric Study of Delamination Analysis in Composites with Cohesive Zone Method

8th Ankara International Aerospace Conference-AIAC, Ankara, Turkey, 10 - 12 September 2015

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

8th Ankara International Aerospace Conference-AIAC, Ankara, Turkey, 10 - 12 September 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

AIAA Science and Technology Forum and Exposition, AIAA SciTech 2015, 33rd Wind Energy Symposium, Kissimmee, United States Of America, 5 - 09 January 2015

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

AIAA Science and Technology Forum and Exposition, AIAA SciTech 2015, 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Florida, United States Of America, 5 - 09 January 2015 identifier

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

5th Science of Making Torque from Wind Conference, Copenhagen, Denmark, 18 - 20 June 2014, vol.524 identifier identifier

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

AIAA Atmospheric Flight Mechanics Conference, AIAA Aviation and Aeronautics Forum and Exposition, Georgia, United States Of America, 16 - 20 June 2014, pp.1-31

Propulsion System Model of a Mini UAV System

International Conference on Unmanned Aircraft Systems (ICUAS), Florida, United States Of America, 27 - 30 May 2014, pp.1073-1080 identifier identifier

Analysis of Aircraft Survivability Against Fragmenting Warhead Threat

55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, National Harbor, Maryland, United States Of America, 13 - 17 January 2014

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

5th Science of Making Torque from Wind Conference, Copenhagen, Denmark, 18 - 20 June 2014, vol.524 identifier identifier

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

AIAA AVIATION 2014 -AIAA Atmospheric Flight Mechanics Conference 2014, Atlanta, GA, United States Of America, 16 - 20 June 2014 identifier

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

10th Jubilee Conference on Shell Structures - Theory and Applications (SSTA), Gdansk, Poland, 16 - 18 October 2013, pp.301-304 identifier identifier

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

54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Boston, MA, United States Of America, 8 - 11 April 2013 identifier

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

54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Boston, MA, United States Of America, 8 - 11 April 2013 identifier

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

3rd International Conference of Engineering Against Failure, ICEAF 2013, Kos, Greece, 26 - 28 June 2013, pp.177-186 identifier

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

53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Honolulu, HI, United States Of America, 23 - 26 April 2012, no.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

53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012, Honolulu, HI, United States Of America, 23 - 26 April 2012 identifier identifier

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

4th Scientific Conference on Science of Making Torque from Wind, Oldenburg, Germany, 9 - 11 October 2012, vol.555 Creative Commons License identifier identifier

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

52th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, United States Of America, 4 - 07 April 2011 identifier

Non-linear progressive failure analysis of composite aerospace structures

18th International Conference on Composites Materials, ICCM 2011, Jeju, South Korea, 21 - 26 August 2011 identifier

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

50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Palm Springs, CA, United States Of America, 4 - 07 May 2009 identifier

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

9th Biennial Conference on Engineering Systems Design and Analysis, Haifa, Israel, 7 - 09 July 2008, pp.603-616 identifier

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

48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Waikiki, HI, United States Of America, 23 - 26 April 2007, vol.5, pp.4940-4961 identifier

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

Proceedings of the 7th Biennial Conference on Engineering Systems Design and Analysis - 2004, Manchester, England, 19 - 22 July 2004, vol.2, pp.191-201 identifier

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

Proceedings of the 7th Biennial Conference on Engineering Systems Design and Analysis - 2004, Manchester, England, 19 - 22 July 2004, vol.2, pp.179-189 identifier

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

Proceedings of the 2nd Biennial European Joint Conference on Engineering Systems Design and Analysis. Part 1 (of 8), London, Canada, 4 - 07 July 1994, vol.64, pp.111-118 identifier

Metrics

Publication

142

Citation (WoS)

179

H-Index (WoS)

7

Citation (Scopus)

378

H-Index (Scopus)

11

Project

8

Thesis Advisory

65

Open Access

62
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