This paper presents an experimental investigation of a propeller operating at low Reynolds
numbers and provides insights into the role of aerodynamic flow features on both propeller …

We use resolvent analysis to design active control techniques for separated flows over a
NACA 0012 airfoil. Spanwise-periodic flows over the airfoil at a chord-based Reynolds …

The spatio-temporal dynamics of separation bubbles induced to form in a fully developed
turbulent boundary layer (with Reynolds number based on momentum thickness of the …

In this study, the flowfields around NACA0012 and NACA0002 airfoils at Reynolds number
of 23,000 and the aerodynamic characteristics of these flowfields were analyzed using …

A comparative study of two airfoils at low Reynolds numbers using the transitional unsteady
Reynolds-averaged Navier–Stokes shear-stress transport γ-R e θ model and the ANSYS …

A comparative assessment of the prediction capability of transitional turbulence models was
carried out in the chord Reynolds number range R ec= 2. 3× 1 0 4− 2× 1 0 5 with the NACA …

THE flow properties in the low-Reynolds-number range, which are applicable to small-sized
aerovehicles, wind turbines, propellers, and human-powered aerovehicles, have generally …

This paper investigates the flow field around a NACA (National Advisory Committee for
Aeronautics) 0012 airfoil undergoing pure pitching motion using continuous wavelet …

The effect of shark skin on the boundary-layer separation process under dynamic conditions
(maneuvers) has been studied experimentally. We use a foil covered with biomimetic shark …

Measurements on a wall-mounted NACA 0012 airfoil with an aspect ratio (AR) of 0.5
operating in the low Reynolds number (274,000, based on chord) regime were performed …