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Experimental Aerodynamic and Aeroelastic Investigation of a Transonic Compressor Rotor with Reduced Blade Count

This study investigates the aerodynamic and aeroelastic characteristics of a transonic axial compressor, focusing on blade count reduced rotor behavior. The analysis is based on experiments, conducted at the Transonic Compressor Darmstadt test rig at Technical University of Darmstadt and compulsory...

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Principais autores: Daniel Franke, Daniel Möller, Maximilian Jüngst, Heinz-Peter Schiffer, Thomas Giersch, Bernd Becker
Formato: Artigo
Idioma:Inglês
Publicado: MDPI AG 2021-06-01
Series:International Journal of Turbomachinery, Propulsion and Power
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Acceso en liña:https://www.mdpi.com/2504-186X/6/2/19
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