02.7. Department of Mechanical Engineering

Bibliometrics Email Alert

Card

Organization name
02.7. Department of Mechanical Engineering
Director
Parent OrgUnit
City
Ankara
Country
Turkey

OrgUnit's Researchers publications
(Dept/Workgroup Publication)

Refined By:
Fulltext:  No Fulltext
Author:  Kaynak, Ünver

Results 1-20 of 28 (Search time: 0.002 seconds).

Issue DateTitleAuthor(s)
12016Aerodynamic analysis of flow characteristics over rotors using CFD methodsÖktem, Onur; Başaran, E.; Kaynak, Ünver 
22016Altitude Control for Small Fixed-Wing Aircraft Using H-infinity Loop-Shaping MethodAkyürek, Şeyma; Kaynak, Ünver ; Kasnakoğlu, Coşku 
32010Automatic recovery and autonomous navigation of disabled aircraft after control surface actuator jamKasnakoğlu, Coşku ; Kaynak, Ünver 
42008Boundary-layer transition under the effect of compressibility for the correlation Based Transition ModelKaynak, Ünver ; Gürdamar, E.
52009Control of flow separation and transition point over an aerofoil at low Re number using simultaneous blowing and suctionGenç, M. Serdar; Kaynak, Ünver 
62018A correlation-based algebraic transition modelÇakmakcıoğlu, Samet Caka; Baş, Onur; Kaynak, Ünver 
72015Design of a Flight Stabilizer for Fixed-Wing Aircrafts Using H-infinity Loop Shaping MethodAkyürek, Şeyma; Ozden, Gizem Sezin; Kürkcü, Burak; Kaynak, Ünver ; Kasnakoğlu, Coşku 
82016Design of a flight stabilizer system and automatic control using HIL test platformAkyürek, Şeyma; Özden, G. S.; Atlas, E.; Kasnakoğlu, Coşku ; Kaynak, Ünver 
92014Design Study of a Short-Range Airborne UAV Radar for Human MonitoringGürbüz, Sevgi Zübeyde; Kaynak, Ünver ; Özkan, Bertan; Kocaman, Ozan Can; Kıyıcı, Firat; Tekeli, Burkam
102008An experimental and computational study of low Re number transitional flows over an aerofoil with leading edge slatGenç, M. Serdar; Lock, G.; Kaynak, Ünver 
112009Flow over an aerofoil without and with a leading-edge slat at a transitional Reynolds numberGenç, M. Serdar; Kaynak, Ünver ; Lock, G. D.
122013Hardware-in-the-loop test platform for a small fixed wing unmanned aerial vehicle embedded controllerErtin O. B.; Korkmaz H.; Kaynak, Ünver ; Kasnakoğlu, Coşku 
13Jan-2018Heading hold autopilot design for fixed wing aircraftAkyürek, Şeyma; Kasnakoğlu, Coşku ; Kaynak, Ünver 
142014A Mach-uniform preconditioner for incompressible and subsonic flowsBaş, Onur; Tuncer, İsmail H.; Kaynak, Ünver 
152006A new approximate factorization method suitable for structured and unstructured gridsÇete, R.; Kaynak, Ünver 
162017A Novel Alternating Cell Directions Implicit Method for the Solution of Incompressible Navier Stokes Equations on Unstructured GridsBaş, Onur; Çete, A. R.; Mengi, S.; Tuncer, İsmail H.; Kaynak, Ünver 
172016Numerical investigation of winglets used to improve the flying performance of unmanned aerial vehicleKaynak, Ünver ; Çoban, A. B.
18Jan-2019Output Feedback Sliding Mode Control of a Fixed-Wing UAV Under Rudder LossGüneş, U.; Sel, Artun; Kasnakoğlu, Coşku ; Kaynak, Ünver 
192011Performance of transition model for predicting low Re aerofoil flows without/with single and simultaneous blowing and suctionGenç, M. Serdar; Kaynak, Ünver ; Yapıcı, Hüseyin
202017Rudder Loss Recovery Autopilot System for a Small Fixed-Wing AircraftAkyürek, Şeyma; Güneş, Uygar; Elbir, Övunç; Kasnakoğlu, Coşku ; Kaynak, Ünver