Publications & Works

Journal articles indexed in SCI, SSCI, and AHCI
Papers Presented at Peer-Reviewed Scientific Conferences

EXTENSION OF THE MULTALL OPEN SOURCE THROUGHFLOW CODE FOR THE IMPROVED OFF – DESIGN CALCULATIONS

69th ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition, GT 2024, London, England, 24 - 28 June 2024, vol.12C identifier

Assessment and Extension of the WrayAgarwal Turbulence Model for Shock WaveBoundary Layer Interactions

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

EXTENSION OF THE MULTALL OPEN SOURCE THROUGHFLOW CODE FOR THE IMPROVED ENDWALL LOSS SIMULATION

ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition, GT 2023, Massachusetts, United States Of America, 26 - 30 June 2023, vol.13A identifier

The Influence of the Computational Mesh on the Prediction of Vortex Interactions about a Generic Missile Airframe

American Institute of Aeronautics and Astronautics SCITECH 2022 forum, San diego, United States Of America, 03 January 2022 identifier

An Automated Modeling And Meshing Tool For Helicopter Rotor Design

American Institute of Aeronautics and Astronautics SCITECH 2022 forum, San diego, United States Of America, 03 January 2022, (Full Text) identifier

Nonlinear Vibrations of Rotor-Bearing Systems Supported by Squeeze Film Dampers Due to Unbalance Excitation

American Society of Mechanical Engineers IMECE 2021, Florida, United States Of America, 01 November 2021 identifier

A HELICOPTER ROTOR MODELLING AND MESHING SYSTEM

11th Ankara International Aerospace Conference, Ankara, Turkey, 08 September 2021, (Full Text)

IMPLEMENTATION AND VERIFICATION OF K-KL TURBULENCE MODEL

11th Ankara International Aerospace Conference, Ankara, Turkey, 08 September 2021

Automatic Mesh Generator Integrated Missile Design Tool Development

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 18 - 20 September 2019, pp.1-12

PERFORMANCE COMPARISON OF SU2 REAL GAS MODELS AND TESTING FOR A COLD GAS THRUSTER

10th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 18 - 20 September 2019, pp.1-21

Unsteady Solutıon of 2D Converging-Dıverging Nozzle Using Lınearized Harmonic Method

18th International Conference on Machine Design and Production (UMTIK 2018), Eskişehir, Turkey, 3 - 06 July 2018, pp.74

A Cartesian Based Mesh Generator with Body Fitted Boundary Layers

18th International Conference on Machine Design and Production (UMTIK 2018), Eskişehir, Turkey, 3 - 06 July 2018, pp.72

Implementation of SU2 Solver with Cell-Based Data Structure for 3D RANS Equations

American Institute of Aeronautics and Astronautics 2018 Fluid Dynamics Conference, Georgia, United States Of America, 25 June - 29 November 2018, pp.1-15

A modeling and simulation tool for safe store separation envelope generation using monte carlo simulations

AIAA Modeling and Simulation Technologies Conference, 2018, Florida, United States Of America, 8 - 12 January 2018, (Full Text) identifier

Analysis of Hinge Moment and Drag Coefficients of a Grid Fin in Comparison with a Planar Fin

Ankara Int. Aerospace Conf. (AIAC), Ankara, Turkey, 10 - 12 September 2015, pp.1-8, (Summary Text)

Design And Optimisation Of High Speed Projectile Nose For Maximum Effectiveness And Stability

7. Ankara International Aerospace Conference, Ankara, Turkey, 11 - 13 September 2013, pp.1-8, (Full Text)

Static Aeroelastic calculations for a wing under large deformations

30th AIAA Applied Aerodynamics Conference 2012, New Orleans, LA, United States Of America, 25 - 28 June 2012, pp.245-253, (Full Text) identifier

Fluid-structure interaction model for hydroplaning simulations

2006 SAE World Congress, Detroit, MI, United States Of America, 3 - 06 April 2006 identifier

Numerical simulation of groundwater contamination

8th International Conference on Hydraulic Engineering Software (Hydrosoft 2000), Lisbon, Portugal, 12 - 14 June 2000, vol.7, pp.315-323 identifier identifier
Books

Chapter 9 ‒ PREDICTIONS OF VORTEX INTERACTIONS FOR LK6E2 – PART II

in: Vortex Interaction Effects Relevant to Military Air Vehicle Performance Vol 1 (NATO-STO Technical Report TR-AVT-316), , Editor, NATO-AVT, pp.357-382, 2023

Chapter 7- THE INFLUENCE OF MODELLING IN PREDICTIONS OF VORTEX INTERACTIONS

in: Vortex Interaction Effects Relevant to Military Air Vehicle Performance Vol 1 (NATO-STO Technical Report TR-AVT-316) , , Editor, NATO-AVT, pp.247-302, 2023

Chapter 12 − Fluent Computational Effort and Results

in: Joint Exercise in Aeroelastic Predictions, Guido DIETZ,Jennifer HEEG, Editor, NATO SCIENCE AND TECHNOLOGY ORGANIZATION, Brussels, pp.211-224, 2019
Metrics

Publication

41

Citation (WoS)

79

H-Index (WoS)

3

Citation (Scopus)

154

H-Index (Scopus)

5

Citation (Scholar)

252

H-Index (Scholar)

6

Citation (TrDizin)

1

H-Index (TrDizin)

1

Citation (Sum Other)

1

Project

3

Thesis Advisory

23

Open Access

8
UN Sustainable Development Goals