Experimental Aerodynamic and Aeroelastic Investigation of a Highly-Loaded 1.5-Stage Transonic Compressor with Tandem Stator

This paper experimentally investigates a highly-loaded 1.5-stage transonic axial compressor, which comprises a variable inlet guide vane, a BLISK rotor, and a variable stator in tandem arrangement. A detailed comparison between the newly designed compressor stage and a reference stage with a convent...

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Autors principals:	Jonas Foret, Daniel Franke, Fabian Klausmann, Alexandra Schneider, Heinz-Peter Schiffer, Bernd Becker, Hauke Müller
Format:	Artigo
Idioma:	Inglês
Publicat:	MDPI AG 2021-06-01
Col·lecció:	International Journal of Turbomachinery, Propulsion and Power
Matèries:	transonic axial compressor experimental aerodynamics aeroelasticity tandem stator
Accés en línia:	https://www.mdpi.com/2504-186X/6/3/21
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