| Issue Date | Title | Author(s) |
1 | 2016 | Control Loss Recovery Autopilot Design for Fixed-Wing Aircraft | Akyürek, Şeyma; Kürkçü, Burak; Kaynak, Ünver ; Kasnakoğlu, Coşku |
2 | 2018 | A correlation-based algebraic transition model | Çakmakcıoğlu, Samet Caka; Baş, Onur; Kaynak, Ünver |
3 | 2016 | Design of a flight stabilizer system and automatic control using HIL test platform | Akyürek, Şeyma; Özden, G. S.; Atlas, E.; Kasnakoğlu, Coşku ; Kaynak, Ünver |
4 | 2009 | Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number | Genç, M. Serdar; Kaynak, Ünver ; Lock, G. D. |
5 | 2014 | A Mach-uniform preconditioner for incompressible and subsonic flows | Baş, Onur; Tuncer, İsmail H.; Kaynak, Ünver |
6 | 2017 | A Novel Alternating Cell Directions Implicit Method for the Solution of Incompressible Navier Stokes Equations on Unstructured Grids | Baş, Onur; Çete, A. R.; Mengi, S.; Tuncer, İsmail H.; Kaynak, Ünver |
7 | 2011 | Performance of transition model for predicting low Re aerofoil flows without/with single and simultaneous blowing and suction | Genç, M. Serdar; Kaynak, Ünver ; Yapıcı, Hüseyin |
8 | 2012 | Supersonic boundary-layer transition prediction under the effect of compressibility using a correlation-based model | Kaynak, Ünver |
9 | 2008 | A unifying grid approach for solving potential flows applicable to structured and unstructured grid configurations | Cete, A. Ruhsen; Yükselen, M. Adil; Kaynak, Ünver |
10 | 2011 | Unsteady compressible flow simulation around low-aspect-ratio rectangular flat wings | Durmuş, G.; Kavsaoğlu, M. S.; Kaynak, Ünver |