Abstract

The method of matched asymptotic expansions is applied to the investigation of transitional separation bubbles. The problem-specific Reynolds number is assumed to be large and acts as the primary perturbation parameter. Four subsequent stages can be identified as playing key roles in the characterization of the incipient laminar–turbulent transition process: due to the action of an adverse pressure gradient, a classical laminar boundary layer is forced to separate marginally (I). Taking into account viscous–inviscid interaction then enables the description of localized, predominantly steady, reverse flow regions (II). However, certain conditions (e.g. imposed perturbations) may lead to a finite-time breakdown of the underlying reduced set of equations. The ensuing consideration of even shorter spatio-temporal scales results in the flow being governed by another triple-deck interaction. This model is capable of both resolving the finite-time singularity and reproducing the spike formation (III) that, as known from experimental observations and direct numerical simulations, sets in prior to vortex shedding at the rear of the bubble. Usually, the triple-deck stage again terminates in the form of a finite-time blow-up. The study of this event gives rise to a noninteracting Euler–Prandtl stage (IV) associated with unsteady separation, where the vortex wind-up and shedding process takes place. The focus of the present paper lies on the triple-deck stage III and is twofold: firstly, a comprehensive numerical investigation based on a Chebyshev collocation method is presented. Secondly, a composite asymptotic model for the regularization of the ill-posed Cauchy problem is developed.

Highlights

  • The present paper is concerned with the investigation of the early stages of laminar–turbulent transition induced by localized boundary layer separation

  • The present paper essentially is a revision of the fundamental work of Elliott and Smith [29]

  • A spectral collocation method based on Chebyshev polynomials has been developed for treating the second—shorter—interactive stage of marginally separated flows

Read more

Summary

Introduction

The present paper is concerned with the investigation of the early stages of laminar–turbulent transition induced by localized boundary layer separation. The mentioned structures, of size comparable with the laminar boundary layer thickness, convey the early stage of the turbulent part of the flow and persist a certain distance downstream of the mean reattachment point until they disintegrate into small-scale vortices (the ‘cloudy’ pattern at the top right of Fig. 1) characteristic of the developing turbulence This laminar–turbulent transition scenario generated by a locally detached shear layer is not yet fully understood, but it is commonly accepted that the repetitive bursting of a LSB, i.e. the (largely) periodic vortex shedding at its rear has to play a key role insofar as it precedes and initiates rather than follows full transition, see e.g. As shown below in more detail, the successive passage of these distinct

16 Page 4 of 32
From classical to interaction boundary layer theory
16 Page 6 of 32
16 Page 8 of 32
Numerical treatment of the triple-deck stage
16 Page 10 of 32
16 Page 12 of 32
16 Page 14 of 32
Numerical results
16 Page 16 of 32
Finite-time blow-up
16 Page 18 of 32
16 Page 20 of 32
Composite asymptotic model
16 Page 22 of 32
Numerical evidence of regularization
Outlook
16 Page 26 of 32
Concluding remarks
Lower deck LD
Main deck MD
Affine transformations and fundamental triple-deck formulation
Findings
16 Page 32 of 32
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call