2010
DOI: 10.1017/s0022112009993946
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Structural sensitivity of the secondary instability in the wake of a circular cylinder

Abstract: The sensitivity of the three-dimensional secondary instability of a circular-cylinder wake to a structural perturbation of the associated linear equations is investigated. In particular, for a given flow condition, the region of maximum coupling between the velocity components is localized by using the most unstable Floquet mode and its adjoint mode. The variation of this region in time is also found by considering a structural perturbation which is impulsively applied in time at a given phase of the vor… Show more

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Cited by 54 publications
(62 citation statements)
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“…In figure 7(a,c,e), the solid and dashed lines denote positive and negative spanwise vorticity of the corresponding base flow, respectively, whereas temporal accumulation of the streamwise vorticity contours on the line x = 2.5 is shown in figure 7(b,d,f ). It is seen in figure 7 and the strong localization of the core of modes A and B in the near wake (Giannetti, Camarri & Luchini 2010). The present Floquet stability analysis does not reveal any other instability mode, confirming the affirmation of Marques et al (2004).…”
Section: Secondary Instability 341 Floquet Stability Analysissupporting
confidence: 82%
“…In figure 7(a,c,e), the solid and dashed lines denote positive and negative spanwise vorticity of the corresponding base flow, respectively, whereas temporal accumulation of the streamwise vorticity contours on the line x = 2.5 is shown in figure 7(b,d,f ). It is seen in figure 7 and the strong localization of the core of modes A and B in the near wake (Giannetti, Camarri & Luchini 2010). The present Floquet stability analysis does not reveal any other instability mode, confirming the affirmation of Marques et al (2004).…”
Section: Secondary Instability 341 Floquet Stability Analysissupporting
confidence: 82%
“…Consistent with this mode A mechanism is a recent study by [19] which investigates the spatial origins of the mode A and mode B instabilities by determining the locations in the flow where a perturbation force-velocity feedback is maximized. This study corroborates the Floquet analysis done on successively reduced domains by [20] and shows that the mode A instability is formed in a relatively small region very close to the back of the cylinder (within 1.5D of the rear stagnation point).…”
Section: Mode a Stabilization Mechanismmentioning
confidence: 92%
“…Following on from a series of papers characterising the structural stability of stationary and rotating cylinder wakes (Giannetti & Luchini 2007;Giannetti, Camarri & Luchini 2010;Pralits, Brandt & Giannetti 2010), Pralits et al (2013) investigated the nature of the instability causing the transition from two-to three-dimensional steady flow for a rotating cylinder at the high rotation rate of α = 5 at Re = 100. Middle column: structure of the adjoint mode for matching rotation rates, again depicted as coloured contours of spanwise perturbation vorticity.…”
Section: Structural Stability Of Mode Ementioning
confidence: 99%