Modeling and design of aerodynamic technologies for low pressure compressor stators

(2023)

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LeBussy_30421600_2023.pdf
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Abstract
Tandem blades are usefull when there is an high turning angle of the flow. However, when the tandem blades are placed in front of a strut, it induces a static pressure distortion which can degrade the aerodynamic performance. The impact of the tandem blades rotations (also called Tilting) on the compressor performance and operability is investigated in this thesis.