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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.

Booster --- splitter vane --- low pressure compressor --- stall --- stator --- Ingénierie, informatique & technologie > Ingénierie aérospatiale