Özgür Uğraş Baran

E-mail
ubaran@metu.edu.tr
Department
Department of Mechanical Engineering
Scopus Author ID
Web of Science Researcher ID
CNNFOIL: convolutional encoder decoder modeling for pressure fields around airfoils
Duru, Cihat; Alemdar, Hande; Baran, Özgür Uğraş (Springer Science and Business Media LLC, 2020-01-01)
In this study, we propose an encoder–decoder convolutional neural network-based approach for estimating the pressure field around an airfoil. The developed tool is one of the early steps of a machine-learning-based aerodyn...
Automatic Mesh Generator Integrated Missile Design Tool Development
Köseömür, Oğuz Ziya; Baran, Özgür Uğraş (2019-09-20)
In this study, a software that is utilized after the pre-design phase of the missile design is presented. This software consists of computational domain modeller and multi-block structured mesh generator. Geometrical desig...
PERFORMANCE COMPARISON OF SU2 REAL GAS MODELS AND TESTING FOR A COLD GAS THRUSTER
Özden, Aysu; Baran, Özgür Uğraş; Aksel, Mehmet Hâluk (null; 2019-09-19)
Cold gas propulsion systems are mainly used for attitude controlof satellites.It is possible to obtainvery low pressure and temperature at the exit section of the nozzledue to propulsion system’s nature. Investigation of s...
Aeroelastik Tahminler için müşterek çalışma
Atik, Hediye; Baran, Özgür Uğraş; Tüzün, Aydın (2019-03-01)
Aeroelasticity studies consist of the interaction and energy transfer between the elastic structure of an aircraft and the aerodynamic loads acting on it during the flight. Aeroelastic effects have a major influence on the...
DEVELOPMENT OF AN AUTOMATIC DESIGN AND ANALYSIS TOOL FOR AXIAL FLOW COMPRESSORS
Kundes, Necmettin Anil; Aksel, Mehmet Haluk; Baran, Özgür Uğraş (2019-01-01)
This paper presents a new design and analysis tool that is developed to be employed during the design process of axial flow compressors. The tool chain implemented by this design tool consists of five parts: a mean-line de...
A Cartesian Based Mesh Generator with Body Fitted Boundary Layers
Özkan, Merve; Baran, Özgür Uğraş; Aksel, Mehmet Haluk (2018-07-03)
Unsteady Solutıon of 2D Converging-Dıverging Nozzle Using Lınearized Harmonic Method
Karshenass, Aras; Baran, Özgür Uğraş; Aksel, Mehmet Haluk (2018-07-03)
Simplified Numerical Approach for the Prediction of Aerodynamic Forces on Grid Fins
DIKBAS, Erdem; Baran, Özgür Uğraş; Sert, Cüneyt (2018-07-01)
Grid fins are unconventional control devices used for aerodynamic control of various types of missiles. Low hinge moment requirement and superior packaging potential make grid fins attractive alternatives to conventional p...
Implementation of SU2 Solver with Cell-Based Data Structure for 3D RANS Equations
Saatloo, Mahtab Mansoor; Baran, Özgür Uğraş; Aksel, Mehmet Haluk (2018-06-25)
A modeling and simulation tool for safe store separation envelope generation using monte carlo simulations
Unal, Kenan; Baran, Özgür Uğraş (2018-01-01)
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.When an air released store is developed or undergoes substantial updates, integration to aircraft is realized through a certificatio...
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