Kurum Yazarı "Kavsaoğlu, Mehmet Şerif" Scopus İndeksli Yayınlar Koleksiyonu İçin Listeleme
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Design and flight test study of a VTOL UAV
Öznalbant, Zafer; Kavsaoğlu, Mehmet Şerif (American Institute of Aeronautics and Astronautics Inc, AIAA, 2015)The aim of this paper is to present the ongoing studies about design and fight testing of a fixed wing UAV which is able to take-off and land vertically. The UAV concept discussed in this study has three propeller engines. ... -
Design, flight mechanics and flight demonstration of a tiltable propeller VTOL UAV
Öznalbant, Zafer; Kavsaoğlu, Mehmet Şerif; Cavcar, Mustafa (American Institute of Aeronautics and Astronautics Inc, AIAA, 2016)This paper presents the design, flight mechanics and flight demonstration studies of a novel tiltable propeller VTOL UAV. The aircraft, discussed in this study, consists of a forward-swept fixed wing, two pairs of counter ... -
Flight control and flight experiments of a tilt-propeller VTOL UAV
Öznalbant, Zafer; Kavsaoğlu, Mehmet Şerif (SAGE Publications LTD, 2018)The purpose of this work is to present a study on the stability and control of an unmanned, fixed wing, vertical take-off and landing aerial vehicle. This airplane is driven by a fixed-pitch tilt-propeller system with the ... -
Marching distance functions for smooth control of hyperbolic grids
Durmuş, Gökhan; Kavsaoğlu, Mehmet Şerif (Amer Inst Aeronaut Astronaut, 2000)… -
Numerical Solution of the Flow Field Around a Prolate Spheroid
Yüca, E.; Kavsaoğlu, Mehmet Şerif (Institute of Electrical and Electronics Engineers Inc., 2018)The flow field around a 6:1 prolate spheroid is numerically solved. The freestream velocity is 45 m/s. The angle between the principal axis of the prolate spheroid and the free flow direction is 30 degrees. Reynolds number ... -
Open and closed loop control of a transport aircraft after component failure
Daşkiran, O.; Kavsaoğlu, Mehmet Şerif (2011)Aircraft dynamics are severely affected by the damages and failures of components. If corrective commands are not supplied immediately, force and moment imbalances lead into catastrophic consequences. In this study, flight ... -
Parallel solution of low aspect ratio rectangular flat wings in compressible flow
Two block parallel Navier Stokes solutions of an aspect ratio 1.0 flat plate with sharp edges are obtained at different Mach numbers and angles of attack. Reynolds numbers are of the order of 200,000-300,000. The flow field ... -
Unsteady compressible flow simulation around low-aspect-ratio rectangular flat wings
Durmuş, Gökhan; Kavsaoğlu, Mehmet Şerif; Kaynak, Ünver (Professional Engineering Publishing LTD, 2011)Unsteady compressible flow solutions around a sharp-edged rectangular flat wing of an aspect ratio of 1.0 are obtained using a parallel Reynolds-averaged Navier-Stokes algorithm. The simulated cases are obtained for Mach ... -
Unsteady navier stokes solutions of low aspect ratio rectangular flat wings in compressible Flow
[No abstract available]