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UID:0-1530@aerospace.technion.ac.il

DTSTART;TZID=Asia/Jerusalem:20260209T133000

DTEND;TZID=Asia/Jerusalem:20260209T143000

DTSTAMP:20260104T144955Z

URL:https://aerospace.technion.ac.il/events/seminar-slot-2026-02-09/

SUMMARY:Physically Consistent Outflow Boundary Conditions for Global Stabil
 ity Analysis of Bluff Body Wakes
DESCRIPTION:Lecturer:Amit Sigawi\n Faculty:The Stephen B. Klein Faculty of 
 Aerospace Engineering\n Institute:Technion – Israel Institute of Technol
 ogy\n Location:Classroom 165\, ground floor\, Library\, Aerospace Eng.\n Z
 oom: https://technion.zoom.us/j/93549691766\n Abstract: Global linear stab
 ility analysis of bluff body wakes must be carried out on truncated comput
 ational domains\, even though the physical problem is unbounded. Because t
 he global eigenfunctions are not known a priori\, the outlet location and 
 the outflow boundary condition are often selected heuristically and valida
 ted a posteriori by inspecting the computed eigenspectrum and eigenfunctio
 ns. In practice\, standard outflow treatments can create a localized non-p
 hysical region near the outlet\, which is then identified in post-processi
 ng and excluded from physical interpretation. To mitigate these outlet eff
 ects\, the downstream boundary is often moved farther away by extending th
 e computational domain\, increasing the computational cost.\n\n&nbsp\;\n\n
 &nbsp\;\n\nThis seminar presents a matrix-forming BiGlobal stability frame
 work based on finite-difference discretization and assesses how the outflo
 w boundary condition influences the predicted eigenspectrum and eigenmodes
 . Common outlet closures (Dirichlet\, Neumann\, and extrapolation-type) ar
 e compared with a physically consistent Robin boundary condition that inco
 rporates local linear stability theory information at the outlet. For stea
 dy\, incompressible\, low Reynolds number (of order of 100) wakes of cylin
 ders and airfoils at high angles of attack\, the proposed Robin condition 
 eliminates outlet-induced artifacts and yields robust convergence\, even w
 hen the computational domain is severely truncated. Our findings pave the 
 way for efficient and accurate computations of global eigenfunctions in mo
 re complex flows.\n\n&nbsp\;\n\n&nbsp\;\n\n&nbsp\;\n\n&nbsp\;\n Details: \
 n 
CATEGORIES:Seminars,סמינרים
LOCATION:Classroom 165\, ground floor\, Library\, Aerospace Eng.

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DTSTART:20251026T010000

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