On the formation of three-dimensional separated flows over wings under tip effects
We perform direct numerical simulations of flows over unswept finite-aspect-ratio NACA
0015 wings at), the tip effects retard the near-tip shedding process, which desynchronizes …
0015 wings at), the tip effects retard the near-tip shedding process, which desynchronizes …
Two-and three-dimensional wake transitions of a NACA0012 airfoil
Flow transitions are an important fluid-dynamic phenomena for many reasons, including the
direct effect on the aerodynamic forces acting on the body. In the present study, two …
direct effect on the aerodynamic forces acting on the body. In the present study, two …
Vortex flow aerodynamics behind a symmetric airfoil at low angles of attack and Reynolds numbers
DF Kurtulus - International Journal of Micro Air Vehicles, 2021 - journals.sagepub.com
The low Reynolds number aerodynamics is important to investigate for micro air vehicle
applications. The current paper covers numerical simulations to present the downstream …
applications. The current paper covers numerical simulations to present the downstream …
Wing sweep effects on laminar separated flows
We reveal the effects of sweep on the wake dynamics around NACA 0015 wings at high
angles of attack using direct numerical simulations and resolvent analysis. The influence of …
angles of attack using direct numerical simulations and resolvent analysis. The influence of …
Linear modal instabilities around post-stall swept finite wings at low Reynolds numbers
Linear modal instabilities around post-stall swept finite wings at low Reynolds numbers Page 1
J. Fluid Mech. (2022), vol. 944, A6, doi:10.1017/jfm.2022.420 Linear modal instabilities around …
J. Fluid Mech. (2022), vol. 944, A6, doi:10.1017/jfm.2022.420 Linear modal instabilities around …
Bifurcations and chaos transition of the flow over an airfoil at low Reynolds number varying the angle of attack
The study of an airfoil at low Reynolds number regime was found to be a typical problem
where the inception of bifurcations leads the flow evolution from a stationary or periodic …
where the inception of bifurcations leads the flow evolution from a stationary or periodic …
Laminar post-stall wakes of tapered swept wings
While tapered swept wings are widely used, the influence of taper on their post-stall wake
characteristics remains largely unexplored. To address this issue, we conduct an extensive …
characteristics remains largely unexplored. To address this issue, we conduct an extensive …
Unsteady aerodynamics of a pitching NACA 0012 airfoil at low Reynolds number
DF Kurtulus - International Journal of Micro Air Vehicles, 2019 - journals.sagepub.com
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° …
airfoil at Re= 1000. The airfoil is sinusoidally pitching around the quarter chord point with 1° …
Lift characteristics of an airfoil at low Reynolds numbers for Newtonian and shear-thinning Carreau fluids
In the present study, we have numerically investigated Carreau and Newtonian fluid flow
over a stationary National Advisory Committee for Aeronautics 0012 airfoil using a sharp …
over a stationary National Advisory Committee for Aeronautics 0012 airfoil using a sharp …
Intermittency patterns in the chaotic transition of the planar flow past a circular cylinder
The present paper investigates the planar flow past a circular cylinder for Reynolds numbers
between 1000 and 10 000. The flow is studied as a dynamical system, so the present …
between 1000 and 10 000. The flow is studied as a dynamical system, so the present …