Title of article :
An efficient and general numerical method to compute steady uniform vortices
Author/Authors :
Luzzatto-Fegiz، نويسنده , , Paolo and Williamson، نويسنده , , Charles H.K.، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2011
Pages :
17
From page :
6495
To page :
6511
Abstract :
Steady uniform vortices are widely used to represent high Reynolds number flows, yet their efficient computation still presents some challenges. Existing Newton iteration methods become inefficient as the vortices develop fine-scale features; in addition, these methods cannot, in general, find solutions with specified Casimir invariants. On the other hand, available relaxation approaches are computationally inexpensive, but can fail to converge to a solution. In this paper, we overcome these limitations by introducing a new discretization, based on an inverse-velocity map, which radically increases the efficiency of Newton iteration methods. In addition, we introduce a procedure to prescribe Casimirs and remove the degeneracies in the steady vorticity equation, thus ensuring convergence for general vortex configurations. We illustrate our methodology by considering several unbounded flows involving one or two vortices. Our method enables the computation, for the first time, of steady vortices that do not exhibit any geometric symmetry. In addition, we discover that, as the limiting vortex state for each flow is approached, each family of solutions traces a clockwise spiral in a bifurcation plot consisting of a velocity-impulse diagram. By the recently introduced “IVI diagram” stability approach [Phys. Rev. Lett. 104 (2010) 044504], each turn of this spiral is associated with a loss of stability for the steady flows. Such spiral structure is suggested to be a universal feature of steady, uniform-vorticity flows.
Keywords :
Steady vortex flows , Contour dynamics , Vortex stability
Journal title :
Journal of Computational Physics
Serial Year :
2011
Journal title :
Journal of Computational Physics
Record number :
1483598
Link To Document :
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