The nonlinear dynamics of singularities in boundary layer flow separation

The phenomenon of laminar-turbulent transition in wall-bounded shear flows is not yet completely understood. We focus on the high Reynolds number asymptotic description of transition in separated boundary layers, which may be depicted through a succession of singular perturbation problems. Each significant change of the dominant balance between nonlinear (inertia), pressure and friction forces results in the breakdown of the current asymptotic flow stage through a finite-time (point) blow-up event, and initiates the subsequent (regularisation) stage in close proximity around the singularity. We consider two scenarios, that respectively serve the purpose to study the influence of time-dependence and three-dimensionality on the incipient transition process. We begin with the classical planar boundary layer stage and numerically study its unsteady suction-induced breakdown within a laminar channel flow. A suitable combination of finite differences and Chebyshev collocation, enables us to compare the emerging reversed flow area with its asymptotic representation of the Van Dommelen–Shen finite-time singularity structure. In the main part of the thesis, we switch to the quasi-steady limit of a laminar separation bubble, within a planar marginally separated boundary layer. We impose weak three-dimensional and time-dependent disturbances, that eventually cause a (repeated) bursting of the bubble and the creation of turbulence in its wake, a process which may happen commonly on the leading-edge suction-side of an airfoil during flight. Here, the initial evolution and amplification of the generated flow disturbances are related to blow-up solutions of a forced Fisher-KPP equation. This reaction-diffusion equation even allows an extension beyond the blow-up time, where the solution consists of two moving singularities that repel each other in spanwise direction. Using matched asymptotic expansions, we closely resolve their creation and initial motion in a succession of asymptotic sublayers and ultimately unveil their hidden self-similar structure to be a singular travelling wave with a time-dependent speed. The locations of the singularities are closely connected to the positions of large vorticity inside the boundary layer flow, enabling us a first glimpse of the creation of three-dimensional coherent vortical structures (lambda or hairpin vortices) in a new asymptotic stage of the laminar-turbulent transition process.

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Publication Details

Journal
reposiTUm (TU Wien)
Published
2024-09-01
DOI
https://doi.org/10.34726/hss.2024.119281
Primary Topic
Biomedical and Chemical Research
Type
article
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article

The nonlinear dynamics of singularities in boundary layer flow separation

reposiTUm (TU Wien)
Biomedical and Chemical Research
article

The nonlinear dynamics of singularities in boundary layer flow separation

article en

Abstract

The phenomenon of laminar-turbulent transition in wall-bounded shear flows is not yet completely understood. We focus on the high Reynolds number asymptotic description of transition in separated boundary layers, which may be depicted through a succession of singular perturbation problems. Each significant change of the dominant balance between nonlinear (inertia), pressure and friction forces results in the breakdown of the current asymptotic flow stage through a finite-time (point) blow-up event, and initiates the subsequent (regularisation) stage in close proximity around the singularity. We consider two scenarios, that respectively serve the purpose to study the influence of time-dependence and three-dimensionality on the incipient transition process. We begin with the classical planar boundary layer stage and numerically study its unsteady suction-induced breakdown within a laminar channel flow. A suitable combination of finite differences and Chebyshev collocation, enables us to compare the emerging reversed flow area with its asymptotic representation of the Van Dommelen–Shen finite-time singularity structure. In the main part of the thesis, we switch to the quasi-steady limit of a laminar separation bubble, within a planar marginally separated boundary layer. We impose weak three-dimensional and time-dependent disturbances, that eventually cause a (repeated) bursting of the bubble and the creation of turbulence in its wake, a process which may happen commonly on the leading-edge suction-side of an airfoil during flight. Here, the initial evolution and amplification of the generated flow disturbances are related to blow-up solutions of a forced Fisher-KPP equation. This reaction-diffusion equation even allows an extension beyond the blow-up time, where the solution consists of two moving singularities that repel each other in spanwise direction. Using matched asymptotic expansions, we closely resolve their creation and initial motion in a succession of asymptotic sublayers and ultimately unveil their hidden self-similar structure to be a singular travelling wave with a time-dependent speed. The locations of the singularities are closely connected to the positions of large vorticity inside the boundary layer flow, enabling us a first glimpse of the creation of three-dimensional coherent vortical structures (lambda or hairpin vortices) in a new asymptotic stage of the laminar-turbulent transition process.

reposiTUm (TU Wien)
TU Wien (AT)
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