The two-dimensional characteristics of airfoil NACA 0018 have been measured for Reynolds numbers between 0.15×10⁶ and 1.0×10⁶ to establish the lift, drag and moment curves that serve as input to ...

Abstract: 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 behaviour ...

Aircraft morphing, especially in the case of the variable camber airfoil, has potential from the viewpoints of both fundamental aerodynamics and flight application. In the field of aerodynamics, the ...

Turbulent drag reduction downstream of largeeddy breakup (LEBU) devices is analyzed from the viewpoint of low-Reynolds number airfoil aerodynamics. It is argued that the variability of results between ...