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Numerical studies of the transition in a flat-plate boundary layer under the influence of free-stream turbulence
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics, Turbulence. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. (FLOW)ORCID iD: 0000-0001-6465-1193
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics, Turbulence. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. (FLOW)ORCID iD: 0000-0001-9627-5903
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics, Turbulence. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. (FLOW)ORCID iD: 0000-0002-5913-5431
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics, Turbulence. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. (FLOW)ORCID iD: 0000-0001-7864-3071
(English)Manuscript (preprint) (Other academic)
Abstract [en]

Free-stream turbulence (FST) and its effect on boundary-layer transition is a complex multiscale problem. Under action of FST, elongated streamwise streaky structures are generated inside the boundary layer, and their amplitude and wavelength are crucial for the transition onset. While turbulence intensity is strongly correlated with the transitional Reynolds number, characteristic length scales of the FST are often considered to have a slight impact on the transition location. Conversely, a recent experiment by Fransson & Shahinfar (2020) shows significant effects of FST scales. They found that, for low values of turbulence intensity, an increase in length scale advances transition, which agrees with literature. However, for high turbulence intensities, an increase in length scale postpones transition. Here, we aim at physically understanding and verifying the results of Fransson & Shahinfar (2020) by performing a series of high-fidelity simulations. These results provide understanding why the FST integral length scale affects the transition location differently depending on intensity. Knowing this relation is crucial for the development of transition models, which are commonly used in turbomachinery and aeronautics. A correct transition point is essential as all boundary layer properties, including friction and heat-transfer coefficients, drastically change from laminar to turbulent, and thus fundamentally affects the complete flow.

National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-307388OAI: oai:DiVA.org:kth-307388DiVA, id: diva2:1631297
Note

QC 20220125

Available from: 2022-01-24 Created: 2022-01-24 Last updated: 2025-02-09Bibliographically approved
In thesis
1. Direct Numerical Simulation of Boundary-layer Transition with Free-stream Turbulence
Open this publication in new window or tab >>Direct Numerical Simulation of Boundary-layer Transition with Free-stream Turbulence
2022 (English)Doctoral thesis, comprehensive summary (Other academic)
Abstract [en]

This thesis considers the generation and influence of free-stream turbulence toboundary layer transition on both flat and curved bodies in the flow. Variousflow configurations such as flow around the flat plate with a sharp leading edgeand low-pressure turbine blades are considered. This study aims at contributingto a better understanding of stability characteristics and different transitionmechanisms in such flows, which are of great interest for fundamental andindustrial applications.In the first part of the thesis, we study the effects of the free-streamturbulence characteristic length scales and intensity on the transition in anincompressible flat-plate boundary layer through direct numerical simulations(DNS). Computations are performed using the spectral element code Nek5000.The numerical setup corresponds to the experimental investigations by Fransson & Shahinfar (2020). Numerically generated homogeneous isotropic turbulenceupstream of the leading edge is designed to reproduce the characteristics of thegrid-generated turbulence in the wind tunnel experiments. Various combinationsof integral length scales are simulated. To ensure the quality of the data, classicalturbulence statistics and integral quantities are carefully evaluated, showingclose agreement with the corresponding experimental data.In the second part, we study both the effect of the free-stream turbulencelevel and the effect of the wake on the low-pressure turbine blades. Thehomogeneous and isotropic free-stream turbulence is prescribed at the inlet asa superposition of Fourier modes with a random phase shift. In the secondstage of the study, cylinders moving in front of the leading edge of the turbineare included to model the effect of the wake coming from the upstream blade.That is done using the tool NekNek which simultaneously runs two differentsimulations that communicate with each other at each time-step through aspecific boundary condition.We also analysed laminar/turbulent regions in the boundary layer flow forboth cases mentioned earlier. To achieve this, we proposed a topology-basedmethod based on extracting the extrema of the flow data. The goal was topropose a method to reduce the subjective choices to a minimum and provideefficient results regardless of the chosen flow case.

Place, publisher, year, edition, pages
Stockholm: KTH Royal Institute of Technology, 2022. p. 61
Series
TRITA-SCI-FOU ; 2021:56
National Category
Fluid Mechanics
Research subject
Engineering Mechanics
Identifiers
urn:nbn:se:kth:diva-307394 (URN)978-91-8040-106-7 (ISBN)
Public defence
2022-02-11, D3, Lindstedtsvägen 5, Stockholm, 14:00 (English)
Opponent
Supervisors
Note

QC 20220510

Available from: 2022-01-24 Created: 2022-01-24 Last updated: 2025-02-09Bibliographically approved

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Durovic, KristinaSchlatter, PhilippHanifi, ArdeshirHenningson, Dan S.

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