Dilek Funda Kurtuluş

E-mail

kurtulus@metu.edu.tr

Department

Department of Aerospace Engineering

ORCID

0000-0002-0678-9474

Scopus Author ID

15837320400

Web of Science Researcher ID

Y-7801-2019

Design and Analysis of a Small-Scale Solar Powered UAV ANILIR, BERKAN; Afzal, Aftab; Said Al Abri, Omar Khalifa; Khamis Al Dhafari, Luqman Sulaiman; Khan, Abid Ali; Kurtuluş, Dilek Funda (2023-12-16)
Experimental study on efficient propulsion system for multicopter UAV design applications Goli, Srikanth; Kurtuluş, Dilek Funda; Alhems, Luai M.; Memon, Azhar M.; Imran, Imil Hamda (2023-12-01) The usage of multicopter unmanned aerial vehicles (UAVs) has increased for various military and civilian purposes. The choice of propulsion system of such a vehicle is crucial to fulfill the intended mission requirements. ...
Estimating the pressure force around swimming plankton using micro particle image velocimetry Ergin, Fahrettin Gokhan; Gunaydinoglu, Erkan; Kurtuluş, Dilek Funda; Wadhwa, Navish (2023-12-01) Obtaining pressure force for freely swimming microorganisms is a challenging yet important problem. Here, we report the swimming kinematics and dynamics of the zooplankton Acartia tonsa nauplius investigated using Micro Pa...
Design and Analysis of a Small-Scale Solar Powered UAV Anılır, Berkan; Afzal, Aftab; Al Abri, Omar Khalifa Said; Al Dhafari, Luqman Sulaiman Khamis; Khan, Abid Ali; Kurtuluş, Dilek Funda (2023-10-05)
Future of Unmanned Power Aerial Vehicles Kurtuluş, Dilek Funda (2023-10-03)
A Bio-Inspired Control Approach for 3D Flapping-Flight Çalış, Özgün; ARIKAN, KUTLUK BİLGE; Kurtuluş, Dilek Funda (2023-10-03)
NUMERICAL INVESTIGATION OF SINUSOIDALLY PLUNGING NACA0012 AIRFOIL AT RE=1000 Anılır, Berkan; Kurtuluş, Dilek Funda; Platzer, Max (2023-09-13)
Aerodynamics of Close-coupled Stationary/Flapping Tandem NACA 0012 Airfoils Anilir, Berkan; Kurtuluş, Dilek Funda; Platzer, Max (2023-06-12) Two-dimensional numerical simulations of low-speed flow past close-coupled tandem NACA0012 airfoils are presented. A sinusoidally plunging airfoil is placed at 0.1c downstream of a stationary airfoil to investigate how the...
Extended Sliding Mode Control Scheme for a VTOL UAV with Time-Varying Disturbances Imran, Imil H.; Memom, Azhar M.; Kurtuluş, Dilek Funda; Goli, Srikanth; Alhems, Luai M. (2023-06-12) The control problem of VTOL UAV is studied in this paper. To manage the complexity of the control problem, the system dynamics are decomposed into two subsystems, i.e. translational dynamics and rotational or attitude dyna...
Unsteady aerodynamic performance of SD7062 airfoil at high Reynolds number Anilir, Berkan; Kurtuluş, Dilek Funda (2023-01-01) Aerodynamic performance of SD7062 airfoil in two-dimensional unsteady flows at high Reynolds number (Re approximate to 5 x 10(6)) has been investigated numerically for a wide range of angles of attack. The k-omega SST turb...

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