| Issue Date | Title | Author(s) |
1 | 2016 | Aerodynamic heating prediction tool for a supersonic vehicle for conceptual design phase | Şimşek B.; Kuran, B.; Ak, M. A.; Uslu, S. |
2 | 2016 | Design of a high pressure turbine nozzle guide vane with effective film cooling system on leading edge | Kıyıcı, F.; Aksu, T.; Uslu, S. |
3 | 2018 | Development of a pressure based, unstructured, GPU accelerated CFD solver for compressible reacting flows at all MACH numbers | Özkan, B.; Uslu, S. |
4 | Jun-2020 | Effect of free-play and initial conditions on aeroelastic behavior of a missile canard in supersonic flow | Özçatalbaş, Mustafa; Acar, B.; Uslu, Sıtkı |
5 | 2016 | Effect of radiation on gas turbine combustor liner temperature with conjugate heat transfer (CHT) methodology | Saygın, Y.; Kocaman, O. C.; Uslu, S. |
6 | 2014 | Exit temperature profile measurement and CFD comparisons on small scale turbojet combustor with air blast atomizer configuration | Çatori, C.; Topal, A.; Uslu, S. ; Tuncer, O.; Çağan, L.; Özkan, S. A.; Çelik, E. |
7 | 2018 | Investigation of Aeroelastic Stability on AGARD 445.6 Wing at Transonic Regime | Özçatalbaş, Mustafa; Acar, B.; Uslu, Sıtkı |
8 | 2015 | Investigation of the effect of co/counter configurations of a double swirler airblast atomizer in an annular turbojet combustor with computational fluid dynamics | Bolat, Hasan Başar; Uslu, S. |
9 | Aug-2020 | Investigation of the effects of lobe number and configuration on mixing performance in lobed mixer | İper, B.; Ergin, Ç. C.; Cenik, B.; Süer, T. U.; Uslu, Sıtkı |
10 | 2017 | Large-Eddy simulation of a Dual-Mode Scramjet combustor using non-adiabatic Flamelet Modeling | Aksu, T.; Uslu S. |
11 | 2016 | Large-eddy simulation of a full annular RQL combustion chamber: Fuel distribution effects on the combustor exit temperature profile | Kocaman, Ozan Can; Aksu, T.; Uslu S. |
12 | 2014 | Unsteady RANS for simulation of high swirling non-premixed methane-air flame | Solmaz, M. B.; Uslu, S. ; Uzol, O. |
13 | 2015 | URANS and les CFD simulations of swirl stabilized non-premixed TECFLAM combustor | Solmaz, M. B.; Uslu, S. |