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Free-Stream Turbulence-Induced Boundary-Layer Transition in Low-Pressure Turbines
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW.ORCID iD: 0000-0001-6465-1193
KTH, School of Engineering Sciences (SCI), Engineering Mechanics.ORCID iD: 0000-0002-6612-604x
Univ Studi Genova, DIME, I-16145 Genoa, Italy..
Univ Studi Genova, DIME, I-16145 Genoa, Italy..
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2021 (English)In: Journal of turbomachinery, ISSN 0889-504X, E-ISSN 1528-8900, Vol. 143, no 8, article id 081015Article in journal (Refereed) Published
Abstract [en]

The aerodynamic efficiency of turbomachinery blades is profoundly affected by the occurrence of laminar-turbulent transition in the boundary layer since skin friction and losses rise for the turbulent state. Depending on the free-stream turbulence level, we can identify different paths toward a turbulent state. The present study uses direct numerical simulation as the primary tool to investigate the flow behavior of the low-pressure turbine blade. In the simulations, the flow past only one blade is computed, with periodic boundary conditions in the cross-flow directions to account for the cascade. Isotropic homogeneous free-stream turbulence is prescribed at the inlet. The free-stream turbulence is prescribed as a super-position of Fourier modes with a random phase shift. Two levels of the free-stream turbulence intensity were simulated (Tu = 0.19% and 5.2%), with the integral length scale being 0.167c, at the leading edge. We observed that in the case of low free-stream turbulence on the suction side, the Kelvin-Helmholz instability dominated the transition process and full-span vortices were shed from the separation bubble. Transition on the suction side proceeded more rapidly in the high-turbulence case, where streaks broke down into turbulent spots and caused bypass transition. On the pressure side, we have identified the appearance of longitudinal vortical structures, where increasing the turbulence level gives rise to more longitudinal structures. We note that these vortical structures are not produced by Gortler instability.

Place, publisher, year, edition, pages
ASME International , 2021. Vol. 143, no 8, article id 081015
Keywords [en]
boundary layer development, computational fluid dynamics (CFD)
National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-299481DOI: 10.1115/1.4050450ISI: 000675351400013Scopus ID: 2-s2.0-85107326838OAI: oai:DiVA.org:kth-299481DiVA, id: diva2:1584804
Note

QC 20210813

Available from: 2021-08-13 Created: 2021-08-13 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)
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Note

QC 20220510

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

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Durovic, KristinaDe Vincentiis, LucaHenningson, Dan S.Hanifi, Ardeshir

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