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SUMMARY:MechE Colloquium : Instability and breakdown phenomena in vortical
  flows
DTSTART:20260428T120000
DTEND:20260428T130000
DTSTAMP:20260403T211741Z
UID:ff62217a38b88efe7a1f600fde93a0de2bb357559b36c1e937ffc4de
CATEGORIES:Conferences - Seminars
DESCRIPTION:Prof. Thomas Leweke\, IRPHE-CNRS\, Marseille\, France\nSummary
 \nVortical structures generated by fixed or rotating lifting surfaces play
  a central role in many aerodynamic and hydrodynamic flows. Their stabilit
 y and eventual breakdown influence wake dynamics\, mixing processes\, and 
 overall flow performance. This seminar presents two recent studies explori
 ng vortex stability and vortex breakdown.\nPart I – Short-wave instabili
 ty of a helical vortex\nThe first part of the seminar discusses the short-
 wave instability of a helical vortex generated by a rotating blade. Combin
 ing experimental dye visualisations\, numerical simulations\, and theoreti
 cal analysis\, the study identifies displacement perturbations whose wavel
 engths are small relative to the helix radius and pitch but may remain lar
 ge compared with the vortex core size. Stability analysis based on experim
 entally measured vortex profiles reveals broad bands of unstable wavenumbe
 rs for several vortex bending modes. These results differ from predictions
  of existing theories for short-wave vortex instability. Similar instabili
 ty modes are also observed in arrays of straight vortices\, indicating tha
 t the phenomenon is not related to vortex curvature. A theoretical examina
 tion of the dispersion relation of Kelvin modes for the measured vortex pr
 ofiles uncovers a previously unidentified family of modes associated with 
 the specific vorticity distribution. Their non-resonant interaction throug
 h the strain field provides a plausible explanation for the experimentally
  observed instability features.\nPart II – Two-phase wing-tip vortex bre
 akdown\nThe second part presents the discovery of a new flow feature obser
 ved in the wake of a rectangular wing in water: the breakdown of the wing-
 tip vortex triggered by the injection of air into the vortex core downstre
 am of the wing. Experiments show that\, for certain combinations of Reynol
 ds number and angle of attack\, a stationary air bubble becomes trapped wi
 thin the vortex core at a finite distance behind the wing and can persist 
 for several minutes even after the air injection is stopped. Under differe
 nt conditions\, the bubble may drift upstream or downstream\, or it may di
 sintegrate immediately. Measurements of bubble properties and vortex chara
 cteristics reveal that the breakdown behaviour depends primarily on the vo
 rtex circulation and on the axial flow component within the core. The form
 ation of a stable breakdown bubble occurs only when a velocity excess rela
 tive to the free stream is present.\nThe two studies highlight new mechani
 sms governing the stability and transformation of vortical flows\, offerin
 g insight into the dynamics of vortex instabilities and vortex-core modifi
 cations in fluid systems.\n\n\nBiography\nThomas Leweke graduated from RWT
 H Aachen University in Germany in 1990 with a “Diplom” (Master) in Phy
 sics. He completed his PhD in 1994 at the Université de Provence in Marse
 ille\, on the experimental study and modelling of bluff-body wakes. After 
 a post-doctoral stay at Cornell University on vortex instabilities\, he jo
 ined the IRPHE institute in Marseille in 1996 as a CNRS Researcher and bec
 ame a Senior Researcher in 2007. His research focusses on the experimental
  study of fundamental aspects of fluid mechanics\, especially in vortex dy
 namics and fluid-structure interactions\, with relevance to applications. 
 He was the co-organiser of a conference series on Bluff-Boddy Wakes and Vo
 rtex-Induced Vibrations (BBVIV)\, and an associate editor for the Journal 
 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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