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SUMMARY:MechE Colloquium : Instability and breakdown phenomena in vortical
  flows
DTSTART:20260428T120000
DTEND:20260428T130000
DTSTAMP:20260416T115438Z
UID:a5a224a7ce6937c1ac2921ddb28d2cef84f50468b1e4eb82c9a168fe
CATEGORIES:Conferences - Seminars
DESCRIPTION:Prof. Thomas Leweke\, IRPHE\, CNRS\, Marseille\, France\nSumma
 ry\nVortical structures generated by fixed or rotating lifting surfaces pl
 ay a central role in many aerodynamic and hydrodynamic flows. Their stabil
 ity and eventual breakdown influence wake dynamics\, mixing processes\, an
 d overall flow performance. This seminar presents two recent studies explo
 ring vortex stability and vortex breakdown.\nPart I – Short-wave instabi
 lity of a helical vortex\nThe first part of the seminar discusses the shor
 t-wave instability of a helical vortex generated by a rotating blade. Comb
 ining experimental dye visualisations\, numerical simulations\, and theore
 tical analysis\, the study identifies displacement perturbations whose wav
 elengths are small relative to the helix radius and pitch but may remain l
 arge compared with the vortex core size. Stability analysis based on exper
 imentally measured vortex profiles reveals broad bands of unstable wavenum
 bers for several vortex bending modes. These results differ from predictio
 ns of existing theories for short-wave vortex instability. Similar instabi
 lity modes are also observed in arrays of straight vortices\, indicating t
 hat the phenomenon is not related to vortex curvature. A theoretical exami
 nation of the dispersion relation of Kelvin modes for the measured vortex 
 profiles uncovers a previously unidentified family of modes associated wit
 h the specific vorticity distribution. Their non-resonant interaction thro
 ugh the strain field provides a plausible explanation for the experimental
 ly observed instability features.\nPart II – Two-phase wing-tip vortex b
 reakdown\nThe second part presents the discovery of a new flow feature obs
 erved in the wake of a rectangular wing in water: the breakdown of the win
 g-tip vortex triggered by the injection of air into the vortex core downst
 ream of the wing. Experiments show that\, for certain combinations of Reyn
 olds number and angle of attack\, a stationary air bubble becomes trapped 
 within the vortex core at a finite distance behind the wing and can persis
 t for several minutes even after the air injection is stopped. Under diffe
 rent conditions\, the bubble may drift upstream or downstream\, or it may 
 disintegrate immediately. Measurements of bubble properties and vortex cha
 racteristics reveal that the breakdown behaviour depends primarily on the 
 vortex circulation and on the axial flow component within the core. The fo
 rmation of a stable breakdown bubble occurs only when a velocity excess re
 lative to the free stream is present.\nThe two studies highlight new mecha
 nisms governing the stability and transformation of vortical flows\, offer
 ing insight into the dynamics of vortex instabilities and vortex-core modi
 fications in fluid systems.\n\n\nBiography\nThomas Leweke graduated from R
 WTH Aachen University in Germany in 1990 with a “Diplom” (Master) in P
 hysics. He completed his PhD in 1994 at the Université de Provence in Mar
 seille\, on the experimental study and modelling of bluff-body wakes. Afte
 r a post-doctoral stay at Cornell University on vortex instabilities\, he 
 joined the IRPHE institute in Marseille in 1996 as a CNRS Researcher and b
 ecame a Senior Researcher in 2007. His research focusses on the experiment
 al study of fundamental aspects of fluid mechanics\, especially in vortex 
 dynamics and fluid-structure interactions\, with relevance to applications
 . He was the co-organiser of a conference series on Bluff-Boddy Wakes and 
 Vortex-Induced Vibrations (BBVIV)\, and an associate editor for the Journa
 l of Fluids and Structures and the Journal of Visualization
LOCATION:MED 0 1418 https://plan.epfl.ch/?room==MED%200%201418 https://epf
 l.zoom.us/j/61360740951
STATUS:CONFIRMED
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