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Effects of upstream wakes on the boundary layer over a low-pressure turbine blade
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: 0000-0002-6612-604x
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
DIME—Università di Genova, Via Montallegro 1, 16145 Genoa, Italy..ORCID iD: 0000-0002-1701-9045
DIME—Università di Genova, Via Montallegro 1, 16145 Genoa, Italy..ORCID iD: 0000-0001-6347-0817
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(English)Manuscript (preprint) (Other academic)
Abstract [en]

In the present work the evolution of the boundary layer over a low-pressureturbine blade is studied by means of direct numerical simulations. The set-upof the simulations follows the experiments by Lengani et al. (2017), aimingto investigate the unsteady flow field induced by the rotor-stator interaction.The free-stream flow is characterized by high level of free-stream turbulenceand periodically impinging wakes. As in the experiments, the wakes are shedby moving bars modeling the rotor blades and placed upstream of the turbineblades. To include the presence of the wake without employing an ad-hoc model,we simulate both the moving bars and the stationary blades in their respectiveframes of reference and the coupling of the two domains is done throughappropriate boundary conditions. The presence of the wake mainly affects thedevelopment of the boundary layer on the suction side of the blade. In particular,the flow separation in the rear part of the blade is suppressed. Moreover, thepresence of the wake introduces alternating regions in the streamwise direction ofhigh- and low-velocity fluctuations inside the boundary layer. These fluctuationsare responsible for significant variations of the shear stress. The analysis of thevelocity fields allows the characterization of the streaky structures forced inthe boundary layer by turbulence carried by upstream wakes. The breakdownevents are observed once positive streamwise velocity fluctuations reach theend of the blade. Both the fluctuations induced by the migration of the wakein the blade passage and the presence of the streaks contribute to high valuesof the disturbance velocity inside the boundary layer with respect to a steadyinflow case. The amplification of the boundary layer disturbances associatedwith different spanwise wavenumbers has been computed. It was found thatthe migration of the wake in the blade passage stands for the most part of theperturbations with zero spanwise wavenumber. The non-zero wavenumbers arefound to be amplified in the rear part of the blade at the boundary betweenthe low and high speed regions associated with the wakes.

National Category
Fluid Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-307389OAI: oai:DiVA.org:kth-307389DiVA, id: diva2:1631302
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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De Vincentiis, LucaDurovic, KristinaHenningson, Dan S.Hanifi, Ardeshir

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De Vincentiis, LucaDurovic, KristinaSimoni, DanieleLengani, DavidePralits, Jan O.Henningson, Dan S.Hanifi, Ardeshir
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