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Faculté des Sciences appliquées
Faculté des Sciences appliquées
MASTER THESIS
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Master thesis and internship[BR]- Master's thesis : Assessment of secondary loss models for throughflow solver[BR]- Integration Internship

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Jolis, Martin ULiège
Promotor(s) : Hillewaert, Koen ULiège ; Terrapon, Vincent ULiège
Date of defense : 27-Jun-2022/28-Jun-2022 • Permalink : http://hdl.handle.net/2268.2/14557
Details
Title : Master thesis and internship[BR]- Master's thesis : Assessment of secondary loss models for throughflow solver[BR]- Integration Internship
Translated title : [fr] Evaluation de modèles des pertes secondaires pour un solveur méridien
Author : Jolis, Martin ULiège
Date of defense  : 27-Jun-2022/28-Jun-2022
Advisor(s) : Hillewaert, Koen ULiège
Terrapon, Vincent ULiège
Committee's member(s) : Budo, Arnaud ULiège
Bilocq, Amaury ULiège
Language : English
Number of pages : 107
Keywords : [en] computational fluid dynamics
[en] meridional plane
[en] 3D blades
[en] axial compressor
[en] Adamczyk's cascade
[en] deviation angle
[en] profile loss
[en] RANS
[en] throughflow model
[en] secondary flows
Discipline(s) : Engineering, computing & technology > Aerospace & aeronautics engineering
Institution(s) : Université de Liège, Liège, Belgique
Degree: Master en ingénieur civil en aérospatiale, à finalité spécialisée en "aerospace engineering"
Faculty: Master thesis of the Faculté des Sciences appliquées

Abstract

[en] This master thesis describes the assessment of secondary flows model for a viscous throughflow solver in the scope of two test cases. They are the classic axial compressor stage CME2 and a multi-stage axial low-pressure compressor with highly loaded blades developed by Safran Aero Boosters.

The review of the literature for secondary flow models has shown that geometrical and flow parameters are of great importance in the formulation of these correlations.

By the comparison with three-dimensional RANS simulations, the assessment of the reliability of different types of correlations for design and off-design conditions, various boundary layer thicknesses and blade geometries has shown that the distributions for the total pressure loss coefficient and deviation angle from Roberts are providing the most promising results.

However, the implementation of Roberts’ correlations in theirs current forms in the throughflow model has not shown a substantial improvement in terms of the prediction of performance maps for the two test cases.

Even tough secondary flows physics are still hardly predictable, such models can be completed by additional terms and coefficients for improving preliminary design applications. Some suggestions are discussed at the end of this thesis.


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Author

  • Jolis, Martin ULiège Université de Liège > Master ingé. civ. aérospat., à fin.

Promotor(s)

Committee's member(s)

  • Budo, Arnaud ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Modélisation et contrôle des écoulements turbulents
    ORBi View his publications on ORBi
  • Bilocq, Amaury ULiège Université de Liège - ULiège > Département d'aérospatiale et mécanique > Design of Turbomachines
    ORBi View his publications on ORBi
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