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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.

Citations

le Bussy, G. (2023). Modeling and design of aerodynamic technologies for low pressure compressor stators. https://dial-mem.test.bib.ucl.ac.be/handle/2078.2/32817