Investigation of the primary design parameters of a splitter vane integrated to a low pressure compressor stator
Magein, Christophe
Promotor(s) :
Terrapon, Vincent
Date of defense : 6-Sep-2018/7-Sep-2018 • Permalink : http://hdl.handle.net/2268.2/5291
Details
Title : | Investigation of the primary design parameters of a splitter vane integrated to a low pressure compressor stator |
Author : | Magein, Christophe ![]() |
Date of defense : | 6-Sep-2018/7-Sep-2018 |
Advisor(s) : | Terrapon, Vincent ![]() |
Committee's member(s) : | Ponthot, Jean-Philippe ![]() AYOUB, Gilles Dimitriadis, Grigorios ![]() |
Language : | English |
Keywords : | [en] Booster [en] splitter vane [en] low pressure compressor [en] stall [en] stator |
Discipline(s) : | Engineering, computing & technology > Aerospace & aeronautics engineering |
Research unit : | Safran Aero Boosters |
Target public : | Professionals of domain |
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 studies the influence of a splitter vane in a low pressure compressor stator. The analysis is based on CFD simulations conducted in the scope of an internship at Safran Aero Boosters. The goal of this work is to evaluate the aeronautical interest of the technology in the specific study case. More specifically, in a preliminary design phase, it is to determine the relevant geometric parameters and the associated trends. Six parameters are investigated by means of manual geometric iterations.
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