| Design of a high pressure turbine nozzle guide vane with effective film cooling system on leading edge F Kiyici, T Aksu, S Uslu 54th AIAA Aerospace Sciences Meeting, 0654, 2016 | 3 | 2016 |
| Large-eddy simulation of a full annular RQL combustion chamber & fuel distribution effects on the combustor exit temperature profile OC Kocaman, T Aksu, S Uslu 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 4786, 2016 | 2 | 2016 |
| Experimental Validation Of An Air Intake Performance MT Akpolat, E Arısoy, C Çıtak, Ö Harputlu, T Aksu Ankara International Aerospace Conference, 2019 | 1 | 2019 |
| Large-eddy simulation of a dual-mode scramjet combustor using non-adiabatic flamelet modeling T Aksu, S Uslu 55th AIAA Aerospace Sciences Meeting, 0559, 2017 | 1 | 2017 |
| Mixed Compression Air-Intake Design for High-Speed Transportation C Çıtak, T Aksu, Ö Harputlu, GW Weber Modeling, Dynamics, Optimization and Bioeconomics IV: DGS VI JOLATE, Madrid …, 2021 | | 2021 |
| Farklı türbülans, yanma modelleri ve reaksiyon mekanizmalarının, süpersonik yanma üzerine etkisinin hesaplamalı akışkanlar dinamiği ile incelenmesi T Aksu Fen Bilimleri Enstitüsü, 2018 | | 2018 |
| STUDY ON SHOCK WAVE-BOUNDARY LAYER INTERACTION ON A MIXED COMPRESSION AIR INTAKE E Arısoy, MT Akpolat, T Aksu, C Çıtak, Ö Harputlu | | |
| EFFECT OF BLEED SYSTEM ON AIR INTAKE PERFORMANCE Ö Harputlu, T Aksu, MT Akpolat, E Arısoy, C Çıtak | | |
| INLET GEOMETRY EFFECT ON COMBUSTION IN A DUCTED ROCKET COMBUSTOR T Aksu, C Çıtak, Ö Harputlu, MT Akpolat, E Arısoy | | |
