Asst. Prof. ÖZGÜR UĞRAŞ BARAN

Articles 16

1. A local correlation-based algebraic transition model in k-ω SST formulation

Okumu B., BARAN Ö. U., Baş O.

AEROSPACE SCIENCE AND TECHNOLOGY , vol.168, 2026 (SCI-Expanded, Scopus)

2. Mapping two-dimensional airfoil pressure distributions over a fighter wing via deep learning

Gomec F. S., BARAN Ö. U., ALEMDAR H.

Aerospace Science and Technology , vol.167, 2025 (SCI-Expanded, Scopus)

3. Optimized FDA Blood Pump: A Case Study in System-Level Customized Ventricular Assist Device Designs

Yıldırım C., Uçak K., Madayen A., Gölcez T., Ertürk H., BARAN Ö. U., et al.

Annals of Biomedical Engineering , vol.53, no.11, pp.2828-2844, 2025 (SCI-Expanded, Scopus)

4. A sensitivity study on the starting simulations of turbojet engines

Gullu E., Aran G., Erk M., BARAN Ö. U.

AERONAUTICAL JOURNAL , vol.128, no.1329, pp.2545-2560, 2024 (SCI-Expanded, Scopus)

5. Assessment of Effect of Flux Scheme and Turbulence Model on Blade-to-blade Calculations

Bilgiç M., BARAN Ö. U., Aksel M.

Journal of Applied Fluid Mechanics , vol.17, no.7, pp.1444-1456, 2024 (SCI-Expanded, Scopus)

6. Numerical investigation of trailing edge losses in transonic ORC turbines

Bilgiç M., Yasa T., Baran Ö. U., Aksel M. H.

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY , vol.237, no.5, pp.929-938, 2023 (SCI-Expanded, Scopus)

7. Towards Accurate Vortex Separation Simulations with RANS Using Improved k-kL Turbulence Model

Dikbaş E., BARAN Ö. U.

Aerospace , vol.10, no.4, 2023 (SCI-Expanded, Scopus)

8. Development of an automated missile design and analysis tool integrated with structured mesh generator Tam düzenli ağ üreteciyle entegre edilmiş otomatik mühimmat tasarım ve analiz yazılımı geliştirilmesi

Köseömür O. Z., BARAN Ö. U.

Journal of the Faculty of Engineering and Architecture of Gazi University , vol.38, no.4, pp.1995-2008, 2023 (SCI-Expanded, Scopus, TRDizin)

9. ASSESSMENT AND COMPARISON OF THE GAMMA AND BC TRANSITION MODELS FOR EXTERNAL FLOWS GAMMA VE BC GEÇİŞ MODELLERİNİN DIŞ AKIŞLAR İÇİN DEĞERLENDİRİLMESİ VE KARŞILAŞTIRILMASI

Karabay S., BARAN Ö. U.

Isi Bilimi Ve Teknigi Dergisi/ Journal of Thermal Science and Technology , vol.43, no.2, pp.135-157, 2023 (SCI-Expanded, Scopus, TRDizin)

10. IMPLEMENTATION, VERIFICATION AND ASSESSMENT OF VORTEX CAPTURING CAPABILITIES OF k-kL TURBULENCE MODEL

Baran Ö. U.

JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY , vol.42, no.1, pp.113-122, 2022 (SCI-Expanded, Scopus, TRDizin)

11. A deep learning approach for the transonic flow field predictions around airfoils

DURU C., ALEMDAR H., BARAN Ö. U.

Computers and Fluids , vol.236, 2022 (SCI-Expanded, Scopus)

12. CNNFOIL: convolutional encoder decoder modeling for pressure fields around airfoils

DURU C., ALEMDAR H., BARAN Ö. U.

Neural Computing and Applications , vol.33, no.12, pp.6835-6849, 2021 (SCI-Expanded, Scopus)

13. SU2 REAL GAS MODELS’ PERFORMANCE PREDICTIONS ON A COLD GAS THRUSTER

Baran Ö. U., Aksel M. H., Ak M. A.

JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY , vol.41, no.1, pp.77-88, 2021 (SCI-Expanded, Scopus)

14. DEVELOPMENT OF AN AUTOMATIC DESIGN AND ANALYSIS TOOL FOR AXIAL FLOW COMPRESSORS

Kundes N. A., AKSEL M. H., BARAN Ö. U.

ISI BILIMI VE TEKNIGI DERGISI-JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY , vol.39, no.2, pp.179-190, 2019 (SCI-Expanded, Scopus, TRDizin)

15. Simplified Numerical Approach for the Prediction of Aerodynamic Forces on Grid Fins

DIKBAS E., Baran O. U., SERT C.

JOURNAL OF SPACECRAFT AND ROCKETS , vol.55, no.4, pp.887-898, 2018 (SCI-Expanded, Scopus)

16. Experimental and numerical analysis of transient liquid slug motion in a voided line

Bozkus Z., BARAN Ö. U., GER M.

JOURNAL OF PRESSURE VESSEL TECHNOLOGY-TRANSACTIONS OF THE ASME , vol.126, no.2, pp.241-249, 2004 (SCI-Expanded, Scopus)

Papers Presented at Peer-Reviewed Scientific Conferences 23

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

Bilgiç M., BARAN Ö. U., Aksel M. H.

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

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

Akça S. C., Dikbaş E., BARAN Ö. U.

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

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

Bilgiç M., BARAN Ö. U., AKSEL M. H.

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

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

Dikbaş E., Schnepf C., Tormalm M., Anderson M., Shaw S., DeSpirito J., et al.

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

5. An Automated Modeling And Meshing Tool For Helicopter Rotor Design

Uzun H. E., Yutük K., BARAN Ö. U., Madayen A.

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

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

Sevencan F., Ciğeroğlu E., Baran Ö. U.

American Society of Mechanical Engineers IMECE 2021, Florida, United States Of America, 01 November 2021, (Full Text)

7. The Effect of Loss Functions on the Deep Learning Modeling for the Flow Field Predictions Around Airfoils

Doğan A., Duru C., Alemdar H., Baran Ö. U.

11th ANKARA INTERNATIONAL AEROSPACE CONFERENCE, Ankara, Turkey, 8 - 10 September 2021, pp.1-9, (Full Text)

8. DEVELOPMENT OF LINEARIZED EULER SOLVERS ON FREQUENCY DOMAIN FOR OSCILLATING AIRFOILS

ARDIÇ A. T., SAYGIN A., BARAN Ö. U., CİĞEROĞLU E.

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

9. A HELICOPTER ROTOR MODELLING AND MESHING SYSTEM

Uzun H. E., Yutük K., BARAN Ö. U., AKSEL M. H.

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

10. IMPLEMENTATION AND VERIFICATION OF K-KL TURBULENCE MODEL

Dikbaş E., BARAN Ö. U.

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

11. Automatic Mesh Generator Integrated Missile Design Tool Development

Köseömür O. Z., Baran Ö. U.

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

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

Özden A., Baran Ö. U., Aksel M. H.

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

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

Karshenass A., Baran Ö. U., Aksel M. H.

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

14. A Cartesian Based Mesh Generator with Body Fitted Boundary Layers

Özkan M., Baran Ö. U., Aksel M. H.

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

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

Saatloo M. M., Baran Ö. U., Aksel M. H.

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