Movies



Posters
- Control of Three-Dimensional Surface Separation on a Non-Slender Delta Wing Using Passive and Active Techniques PDF
- Characterization of Flow Structure and Wall Shear Stress in Patient Specific AAA Phantom Using PIV PDF
- Effect of Bleeding on Aerodynamics of Non-Slender Delta Wing in Ground Effect PDF
- Effect of Ground on Flow Structure of Non-Slender Delta and Reverse Delta Wings PDF
- Control of Flow Structure Over a Non-Slender Delta Wing Using Passive Bleeding PDF
- Effect of Thickness-to-Chord Ratio on Aerodynamics of Non-Slender Delta Wing PDF
- Control of Flow Structure Over a Non-Slender Delta Wing Using Periodic Blowing PDF
- Flow Structure on 35° Swept Delta Wing: Reynolds Number Dependence and Flow Control PNG
- Effect of Passive Bleeding on Flow Structure Over a Non-Slender Delta Wing PNG
- Flow Characterization of Full, Partial, and Inclined Ground Effect PNG
- Effect of Thickness-to-Chord Ratio on Flow Structure of a Low Swept Delta Wing PDF
Awards
PhD Thesis of the Year Award
Middle East Technical University, Institute of Natural and Applied Sciences
Göktuğ Koçak — “Effect of Ground on Flow Structure of Non-slender Delta and Reverse Delta Wings”, PhD Thesis, 2024.
Best Oral Presentation
9th International Conference on Mechanical and Aerospace Engineering (ICMAE)
Kayacan Kestel — “Effectiveness of Passive Bleeding as a Flow Control Method for The Flow Structure on Low to Moderate Swept Delta Wings”, 2018.
PhD Thesis of the Year Award
Prof. Dr. Mustafa N. Parlar Foundation
Alper Çelik — “Development and Implementation of Novel Flow Control Techniques for Nonslender Delta Wings”, 2017.
M.Sc. Thesis of the Year Award
Middle East Technical University, Institute of Natural and Applied Sciences
Cenk Çetin — “Control of Flow Structure on Low Swept Delta Wing Using Unsteady Leading Edge Blowing”, 2016.
Best Oral Presentation
8th International Conference on Mechanical and Aerospace Engineering (ICMAE)
Göktuğ Koçak — “Flow Characterization of Full, Partial and Inclined Ground Effect”, 2017.