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Timothy Lee
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1. Dynamic-stall flow control
2. Wingtip vortex measurement and its control
3. Rotorcraft blade-vortex interaction and its control
4. Flow over oscillating circular cylinder
Typical spatial-temporal evolution of the streamwise iso-vorticity contours
of a tip vortex generated by a NACA 0015 wing oscillated with α(t) =
0o + 6osinωt at κ = 0.1, x/c = 2 and Re = 1.7 x
105.
Solid line denotes the instantaneous location of the wing trailing edge.
Attmov [.pdf] Click here to play the PDF
Typical spatial-temporal evolution of the phase-averaged streamwise iso-vorticity contours of a tip vortex generated by a NACA 0015 wing oscillated with α(t) = 18o + 6osinωt at κ = 0.1 and x/c = 2.
DeepStall [.pdf] Click here to play the PDF