Vorticity transport is analysed within the leading-edge vortex generated on a rectangular flat
plate of aspect ratio 4 undergoing a starting rotation motion in a quiescent fluid. Two …

A numerical study is conducted to examine the vortex structure and aerodynamic loading on
a revolving wing in quiescent flow. A high-fidelity, implicit large eddy simulation technique is …

This paper provides a systematic and critical review of dynamic experimental rigs used for
insect wing aerodynamics research. The goal is to facilitate meaningful comparison of data …

We investigate experimentally the effect of aspect ratio () on the time-varying, three-
dimensional flow structure of flat-plate wings rotating from rest at 45° angle of attack. Plates …

The three-dimensional structure of the leading-edge vortex on a rotating wing is addressed
using a technique of particle image velocimetry. Organized patterns of chordwise-oriented …

The sequence of events constituting the formation of a leading-edge vortex (LEV) has been
investigated for a periodically plunging nominally two-dimensional flat plate and a similarly …

A numerical study is conducted to examine the vortex structure and aerodynamic loading
about a revolving wing in quiescent flow. The high-fidelity, implicit large eddy simulation …

The interaction between leading-edge-vortex and tip-vortex development on a low-aspect-
ratio plate has been investigated and compared to a nominally two-dimensional rectangular …

Plenoptic particle image velocimetry and surface pressure measurements were used to
analyse the early development of leading-edge vortices (LEVs) created by a flat-plate wing …

THE flow produced by a bio-inspired flapping wing is unsteady, three-dimensional, and
dominated by separated flow and strong vortices. To better understand which structures in …