Performance of transition model for predicting low Re aerofoil flows without/with single and simultaneous blowing and suction MS Genç, Ü Kaynak, H Yapici European Journal of Mechanics-B/Fluids 30 (2), 218-235, 2011 | 146 | 2011 |
Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds number MS Genç, Ü Kaynak, GD Lock Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2009 | 112 | 2009 |
A correlation-based algebraic transition model SC Cakmakcioglu, O Bas, U Kaynak Proceedings of the Institution of Mechanical Engineers, Part C: Journal of …, 2018 | 66 | 2018 |
An experimental and computational study of low Re number transitional flows over an aerofoil with leading edge slat M Genc, G Lock, U Kaynak The 26th Congress of ICAS and 8th AIAA ATIO, 8877, 2008 | 49 | 2008 |
A revised one-equation transitional model for external aerodynamics SC Cakmakcioglu, O Bas, R Mura, U Kaynak AIAA aviation 2020 forum, 2706, 2020 | 47 | 2020 |
Control of laminar separation bubble over a NACA2415 aerofoil at low re transitional flow using blowing/suction MS Genc, Ü Kaynak International Conference on Aerospace Sciences and aviation technology 13 …, 2009 | 44 | 2009 |
Effect of turbulence modeling on dynamic stall of a NACA0012 airfoil M Dindar, U Kaynak 30th Aerospace Sciences Meeting and Exhibit, 27, 1992 | 37 | 1992 |
Advances in the computation of transonic separated flows over finite wings Ü Kaynak, J Flores Computers & fluids 17 (2), 313-332, 1989 | 30 | 1989 |
Control of flow separation and transition point over an aerofoil at low Re number using simultaneous blowing and suction M Genç, Ü Kaynak 19th AIAA Computational Fluid Dynamics, 3672, 2009 | 29 | 2009 |
A novel intermittency distribution based transition model for low-re number airfoils O Bas, SC Cakmakcioglu, U Kaynak 31st AIAA applied aerodynamics conference, 2531, 2013 | 24 | 2013 |
Transonic wing flows using an Euler/Navier-Stokes zonal approach TL Holst, U Kaynak, KL Gundy, SD Thomas, J Flores, NM Chaderjian Journal of aircraft 24 (1), 17-24, 1987 | 24 | 1987 |
Design of a flight stabilizer system for a small fixed wing unmanned aerial vehicle using system identification H Korkmaz, OB Ertin, C Kasnakoğlu IFAC Proceedings Volumes 46 (25), 145-149, 2013 | 23 | 2013 |
Design of a flight stabilizer for fixed-wing aircrafts using H∞loop shaping method S Akyurek, GS Ozden, B Kurkcu, U Kaynak, C Kasnakoglu 2015 9th International Conference on Electrical and Electronics Engineering …, 2015 | 21 | 2015 |
Supersonic boundary-layer transition prediction under the effect of compressibility using a correlation-based model Ü Kaynak Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2012 | 21 | 2012 |
Altitude control for small fixed-wing aircraft using H∞ loop-shaping method S Akyurek, U Kaynak, C Kasnakoglu IFAC-PapersOnLine 49 (9), 111-116, 2016 | 19 | 2016 |
Hardware-in-the-loop test platform design for UAV applications E Atlas, MI Erdoğan, OB Ertin, A Güçlü, YE Saygi, Ü Kaynak, ... Applied Mechanics and Materials 789, 681-687, 2015 | 19 | 2015 |
Design study of a short-range airborne UAV radar for human monitoring SZ Gürbüz, Ü Kaynak, B Özkan, OC Kocaman, F Kıyıcı, B Tekeli 2014 48th Asilomar Conference on Signals, Systems and Computers, 568-572, 2014 | 19 | 2014 |
Transition modeling for low to high speed boundary layer flows with CFD applications OB Unver Kaynak, SC Cakmakcioglu, IH Tuncer Boundary Layer Flows: Theory, Applications and Numerical Methods, 101, 2020 | 15 | 2020 |
Transonic Navier-Stokes wing solution using a zonal approach. Part 1: Solution methodology and code validation J Flores, K Gundy AGARD Symposium on Applications of Computational Fluid Dynamics in Aeronautics, 1986 | 15 | 1986 |
Computational aspects of zonal algorithms for solving the compressible Navier-Stokes equations in three dimensions TL Holst, SD Thomas, U Kaynak, KL Gundy, J Flores, NM Chaderjian | 15 | 1985 |