2009
DOI: 10.1007/978-3-642-02225-8_48
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Hairpin Structures in a Turbulent Boundary Layer under Stalled-Airfoil-Type Flow Conditions

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Cited by 4 publications
(3 citation statements)
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“…They also compute the maximum azimuthal velocity given by the Gaussian model by obtaining the circulation from the surface integral of the out-of-plane component of vorticity inside the vortex section. Maciel and Shafiei Mayam (2010) do not rely on any theoretical vortex model to study the properties of spanwise and hairpin-like vortices in spanwise-wall normal planes of an adverse-pressuregradient boundary layer. They use directly the vortex detection function k ci , with thresholds applied, to compute the vortex characteristics.…”
Section: Introductionmentioning
confidence: 99%
“…They also compute the maximum azimuthal velocity given by the Gaussian model by obtaining the circulation from the surface integral of the out-of-plane component of vorticity inside the vortex section. Maciel and Shafiei Mayam (2010) do not rely on any theoretical vortex model to study the properties of spanwise and hairpin-like vortices in spanwise-wall normal planes of an adverse-pressuregradient boundary layer. They use directly the vortex detection function k ci , with thresholds applied, to compute the vortex characteristics.…”
Section: Introductionmentioning
confidence: 99%
“…The and proposed by many investigators for the identification of vortices [43][44][45][46][47][48][49][50][51]. In this study, the ci λ method [47] is used to extract the vortices.…”
Section: Turbulence Structuresmentioning
confidence: 99%
“…Hence, a precise vortex extraction method is required to reveal the vortical structures. Various tools and algorithms have been proposed and used by many investigators to identify vortices[43][44][45][46][47][48][49][50][51]. The ci  method[51] is used to extract vortices in the present study.…”
mentioning
confidence: 99%