02.7. Department of Mechanical Engineering

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

OrgUnit's Researchers publications
(Dept/Workgroup Publication)

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Author:  Kaynak, Ünver
Type:  Conference Object

Results 1-17 of 17 (Search time: 0.007 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 
62015Design of a Flight Stabilizer for Fixed-Wing Aircrafts Using H-infinity Loop Shaping MethodAkyürek, Şeyma; Ozden, Gizem Sezin; Kürkcü, Burak; Kaynak, Ünver ; Kasnakoğlu, Coşku 
72014Design Study of a Short-Range Airborne UAV Radar for Human MonitoringGürbüz, Sevgi Zübeyde; Kaynak, Ünver ; Özkan, Bertan; Kocaman, Ozan Can; Kıyıcı, Firat; Tekeli, Burkam
82008An experimental and computational study of low Re number transitional flows over an aerofoil with leading edge slatGenç, M. Serdar; Lock, G.; Kaynak, Ünver 
92013Hardware-in-the-loop test platform for a small fixed wing unmanned aerial vehicle embedded controllerErtin O. B.; Korkmaz H.; Kaynak, Ünver ; Kasnakoğlu, Coşku 
10Jan-2018Heading hold autopilot design for fixed wing aircraftAkyürek, Şeyma; Kasnakoğlu, Coşku ; Kaynak, Ünver 
112006A new approximate factorization method suitable for structured and unstructured gridsÇete, R.; Kaynak, Ünver 
122016Numerical investigation of winglets used to improve the flying performance of unmanned aerial vehicleKaynak, Ünver ; Çoban, A. B.
13Jan-2019Output Feedback Sliding Mode Control of a Fixed-Wing UAV Under Rudder LossGüneş, U.; Sel, Artun; Kasnakoğlu, Coşku ; Kaynak, Ünver 
142017Rudder Loss Recovery Autopilot System for a Small Fixed-Wing AircraftAkyürek, Şeyma; Güneş, Uygar; Elbir, Övunç; Kasnakoğlu, Coşku ; Kaynak, Ünver 
152009Technology Management in Turkish Defense IndustryGümüş, Bülent; Demir, Verda; Kaynak, Ünver 
162012Transition at low-re numbers for UAV type airfoils at high subsonic mach numbersÇakmakçıoğlu, Samet Çaka; Kaynak, Ünver ; Genç, M. S.
172009Unsteady navier stokes solutions of low aspect ratio rectangular flat wings in compressible FlowDurmuş, G.; Kavsaoğlu, M. Ş.; Kaynak, Ünver