Takip et
Prof.Dr. Ünver Kaynak
Prof.Dr. Ünver Kaynak
etu.edu.tr üzerinde doğrulanmış e-posta adresine sahip - Ana Sayfa
Başlık
Alıntı yapanlar
Alıntı yapanlar
Yıl
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
1312011
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
1002009
A correlation-based algebraic transition model
SC Cakmakcioglu, O Bas, U Kaynak
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of …, 2018
582018
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
422009
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
422008
Effect of turbulence modeling on dynamic stall of a NACA0012 airfoil
M Dindar, U Kaynak
30th Aerospace Sciences Meeting and Exhibit, 27, 1992
371992
A revised one-equation transitional model for external aerodynamics
SC Cakmakcioglu, O Bas, R Mura, U Kaynak
AIAA Aviation 2020 Forum, 2706, 2020
312020
Advances in the computation of transonic separated flows over finite wings
Ü Kaynak, J Flores
Computers & fluids 17 (2), 313-332, 1989
311989
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
261987
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
222013
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
212013
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
212009
Design of a flight stabilizer for fixed-wing aircrafts using Hloop shaping method
S Akyurek, GS Ozden, B Kurkcu, U Kaynak, C Kasnakoglu
2015 9th International Conference on Electrical and Electronics Engineering …, 2015
202015
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
192016
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
182015
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
182014
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
182012
Numerical simulation of transonic separated flows over low-aspect-ratio wings
U Kaynak, TL Holst, BJ Cantwell, RL Sorenson
Journal of Aircraft 24 (8), 531-539, 1987
171987
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
161985
Computation of transonic separated wing flows using an Euler/Navier-Stokes zonal approach
U Kaynak, TL Holst, BJ Cantwell
151986
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