Publications & Works

Published journal articles indexed by SCI, SSCI, and AHCI

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

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

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

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

Aircraft vulnerability assessment against fragmentation warhead

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

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

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

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

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

Flight flutter testing and aeroelastic stability of aircraft

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

Flight flutter testing and aeroelastic stability of aircraft

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

Flutter qualification of transport aircraft with store suspension

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

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

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

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

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

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

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

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

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

TORSIONAL VIBRATIONS OF LAYERED COMPOSITE PARABOLOIDAL SHELLS

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

Articles Published in Other Journals

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

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

Refereed Congress / Symposium Publications in Proceedings

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

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

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

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

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

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

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

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

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

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

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

The Effect of Modal Damping on Random Vibration Metal Fatigue Analysis

9thANKARA 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

Nonlinear Static Aeroelastic Behaviour of Composite Missile Fin with Interlaminar Damage

9th ANKARA 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

Post Buckling Load Redistribution of Stiffened Panels in Aircraft Wingbox Structures

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

Classical Aeroelastic Stability Analysis of Large Composite Wind Turbine Blades

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

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

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

Parametric Study of Delamination Analysis in Composites with Cohesive Zone 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

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

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

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

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

AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Hawaii, United States Of America, 23 - 26 April 2012, no.1860, pp.1-30

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

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