Abstract

Leading-edge vortex burst on a rotating flat plate wing was investigated experimentally using stereoscopic particle image velocimetry. Vortex burst was found to occur near the point of maximum lift production and was characterized by a concentration of opposite-sign vorticity entrainment and axial flow stagnation within the vortex core.

Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call