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On the receptivity of low-pressure turbine blades
DIME—Università di Genova, Via Montallegro 1, 16145 Genoa, Italy.ORCID iD: 0000-0001-6347-0817
DIME—Università di Genova, Via Montallegro 1, 16145 Genoa, Italy.ORCID iD: 0000-0002-1701-9045
DICCA—Università di Genova, Via Montallegro 1, 16145 Genoa, Italy.ORCID iD: 0000-0001-7285-7482
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
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(English)Manuscript (preprint) (Other academic)
Abstract [en]

In the present work, the laminar-turbulent transition of the flow evolving arounda low-pressure turbine blade has been investigated. Direct numerical simulationshave been carried out for two different free-stream turbulence intensity (FSTI)levels to investigate the role of free-stream oscillations on the evolution of theblade boundary layer. Emphasis is posed on identifying the mechanisms drivingthe formation and breakup of coherent structures in the high FSTI case andhow these processes are affected by the leading-edge receptivity and/or bythe continuous forcing in the blade passage. Proper orthogonal decomposition(POD) has been adopted to provide a clear statistical representation of theshape of the structures. Extended POD projections provided temporal andspanwise correlations that allowed us to identify dominant temporal structuresand spanwise wavelengths in the transition process.The extended POD analysis shows that the structures on the pressure sideare not related to what happens at the leading edge. The results on the suctionside show that the modes defining the leading edge and the passage basescorrelate with coherent structures responsible for the transition. The mostenergetic mode of the passage basis is strongly related to the most amplifiedwavelength in the boundary layer and breakup events leading to transition.Modes with a smaller spanwise wavelength belong to the band predicted byoptimal disturbance theory, they amplify with a smaller gain in the rear suctionside, and they show the highest degree of correlation between the passage regionand the rear suction side.

National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-307390OAI: oai:DiVA.org:kth-307390DiVA, id: diva2:1631307
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, KristinaDe Vincentiis, LucaHenningson, Dan S.Hanifi, Ardeshir

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Lengani, DavideSimoni, DanielePralits,, Jan O.Durovic, KristinaDe Vincentiis, LucaHenningson, Dan S.Hanifi, Ardeshir
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