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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Fulltext:  No Fulltext
Author:  Kaynak, Ünver
Date Issued:  [2010 TO 2020]

Results 1-20 of 20 (Search time: 0.006 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 
42018A correlation-based algebraic transition modelÇakmakcıoğlu, Samet Caka; Baş, Onur; Kaynak, Ünver 
52015Design of a Flight Stabilizer for Fixed-Wing Aircrafts Using H-infinity Loop Shaping MethodAkyürek, Şeyma; Ozden, Gizem Sezin; Kürkcü, Burak; Kaynak, Ünver ; Kasnakoğlu, Coşku 
62016Design of a flight stabilizer system and automatic control using HIL test platformAkyürek, Şeyma; Özden, G. S.; Atlas, E.; Kasnakoğlu, Coşku ; Kaynak, Ünver 
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
82013Hardware-in-the-loop test platform for a small fixed wing unmanned aerial vehicle embedded controllerErtin O. B.; Korkmaz H.; Kaynak, Ünver ; Kasnakoğlu, Coşku 
9Jan-2018Heading hold autopilot design for fixed wing aircraftAkyürek, Şeyma; Kasnakoğlu, Coşku ; Kaynak, Ünver 
102014A Mach-uniform preconditioner for incompressible and subsonic flowsBaş, Onur; Tuncer, İsmail H.; Kaynak, Ünver 
112017A 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 
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 
142011Performance of transition model for predicting low Re aerofoil flows without/with single and simultaneous blowing and suctionGenç, M. Serdar; Kaynak, Ünver ; Yapıcı, Hüseyin
152017Rudder Loss Recovery Autopilot System for a Small Fixed-Wing AircraftAkyürek, Şeyma; Güneş, Uygar; Elbir, Övunç; Kasnakoğlu, Coşku ; Kaynak, Ünver 
162020Sabit Kanatlı İnsansız Hava Araçları için AcilDurumlara Dayanaklı Uçuş Kontrol SistemiGeliştirilmesiKasnakoğlu, Coşku ; Kaynak, Ünver 
172017Sabit Kanatlı İnsansız Hava Araçları İçin Yüzey Kaybını Dengeleyici Otopilot TasarımıKasnakoğlu, Coşku ; Kaynak, Ünver 
182012Supersonic boundary-layer transition prediction under the effect of compressibility using a correlation-based modelKaynak, Ünver 
192012Transition at low-re numbers for UAV type airfoils at high subsonic mach numbersÇakmakçıoğlu, Samet Çaka; Kaynak, Ünver ; Genç, M. S.
202011Unsteady compressible flow simulation around low-aspect-ratio rectangular flat wingsDurmuş, G.; Kavsaoğlu, M. S.; Kaynak, Ünver