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Dilek Funda Kurtuluş

Department of Aerospace Engineering
Scopus Author ID
Pressure-velocity coupling algorithm-based pressure reconstruction from PIV for laminar flows
Gunaydinoglu, Erkan; Kurtuluş, Dilek Funda (Springer Science and Business Media LLC, 2020-01-01)
In this study, we propose a method to reconstruct pressure fields from planar particle image velocimetry measurements for laminar flows by employing semi-implicit method for pressure-linked equations algorithm to solve gov...
Unsteady aerodynamics of a pitching NACA 0012 airfoil at low Reynolds number
Kurtuluş, Dilek Funda (SAGE Publications, 2019-11-01)
The present paper aims to investigate numerically small amplitude oscillation of NACA 0012 airfoil at Re = 1000. The airfoil is sinusoidally pitching around the quarter chord point with 1 degrees pitch amplitude about a me...
Aerodynamic Loads of Small-Amplitude Pitching NACA 0012 Airfoil at Reynolds Number of 1000
Kurtuluş, Dilek Funda (2018-08-01)
Experimental and Numerical Results of a Flapping Wing Four Bar Mechanism
ŞENOL, münire gülay; ARIKAN, KUTLUK BİLGE; Kurtuluş, Dilek Funda (2017-01-13)
Winglet design and analysis for low-altitude solar-powered UAV
Gölcük, Ali Ihsan; Kurtuluş, Dilek Funda (2017-01-01)
Effect of glottic geometry on breathing: three-dimensional unsteady numerical simulation of respiration in a case with congenital glottic web
Gokcan, M. Kursat; Gunaydinoglu, Erkan; Kurtuluş, Dilek Funda (2016-10-01)
Glottic obstruction is a major cause of dyspnea. Without understanding the normal function of the glottis in breathing, treating dyspnea does not restore normal physiology. Therefore, we designed a computational fluid dyna...
Attitude and Altitude Stabilization of Fixed Wing VTOL Unmanned Air Vehicle
Güçlü, Anıl; Kurtuluş, Dilek Funda; Arıkan, Kutluk Bilge (2016-06-17)
On the wake pattern of symmetric airfoils for different incidence angles at Re=1000
Kurtuluş, Dilek Funda (SAGE Publications, 2016-06-01)
In the current study, numerical simulations are performed in order to investigate effects of incidence angle and airfoil thickness on alternating vortex pattern of symmetric airfoils at Re = 1000. This alternating vortex p...
Development of a Design Methodology Against Fast Cook-Off Threat for Insensitive Munitions
ŞAHİN, Hakan; NARİN, Bekir; Kurtuluş, Dilek Funda (Wiley, 2016-06-01)
This work provides a design methodology for a typical energetic system to get Type V insensitive munition (IM) response against fast cook-off threat. Experimental and numerical results for a generic test item filled with P...
On the Unsteady Behavior of the Flow Around NACA 0012 Airfoil with Steady External Conditions at Re=1000
Kurtuluş, Dilek Funda (2015-09-01)
Even for the stationary airfoils, due to the boundary and shear layer interactions of upper and lower surface of the airfoils, alternating vortex patterns form and the flow becomes time dependent. In the current study, the...