2011
DOI: 10.1063/1.3589842
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Edge states in a boundary layer

Abstract: is an open access repository that collects the work of Arts et Métiers ParisTech researchers and makes it freely available over the web where possible.This is an author-deposited version published in: http://sam.ensam.eu Handle

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Cited by 48 publications
(42 citation statements)
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“…The situation for the Blasius boundary layer is a step up in complexity, both conceptually and technically: the spatial development implies that the control parameters vary along a trajectory, and the flow is not confined in the wall-normal direction. A recent calculation in a narrow periodic domain demonstrates the applicability of edge tracking in a spatially developing flow [16]. The introduction of a fixed length scale is, however, incompatible with the localization and the spatial spreading of the disturbance which follows from the spatial expansion of the flow.…”
mentioning
confidence: 99%
“…The situation for the Blasius boundary layer is a step up in complexity, both conceptually and technically: the spatial development implies that the control parameters vary along a trajectory, and the flow is not confined in the wall-normal direction. A recent calculation in a narrow periodic domain demonstrates the applicability of edge tracking in a spatially developing flow [16]. The introduction of a fixed length scale is, however, incompatible with the localization and the spatial spreading of the disturbance which follows from the spatial expansion of the flow.…”
mentioning
confidence: 99%
“…This type of turbulent band was also reported in the direct numerical simulation by Tsukahara et al 13 In spite of mathematical difficulties, nonlinear analyses of disturbance in the shear flows around the marginal Re were vigorously performed for the last few decades. Recently, a new concept, "edge state" was proposed [14][15][16][17][18][19] and successfully described behavior of the nonlinear disturbances in the transitional pipe flow. [20][21][22] When considering the marginal Re, one can examine the largest vortical scale of turbulent disturbances in the wall unit.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, following the theoretical work of Waleffe (1997), the maximum values of the streamwise and wall-normal components of the velocity are chosen as state variables. Figure 6 provides the trajectories in this reduced phase space (Cherubini et al 2011b) of nonlinear optimal perturbations with different initial energy (the ones also used in figure 3, top frame). The origin (corresponding to zero disturbance velocity with respect to the laminar Blasius solution) is the laminar attractor; the turbulent attractor is localized on the top right, for values of the perturbation velocity components around u ≈ 0.7, v ≈ 0.3; the relative attractor on the edge is the looping trajectory represented by the black thick line and is localized around u ≈ 0.25, v ≈ 0.045 (cf also the inset in the figure).…”
Section: Resultsmentioning
confidence: 99%