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

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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Bibliographic Details
Main Authors: Daniel Franke, Daniel Möller, Maximilian Jüngst, Heinz-Peter Schiffer, Thomas Giersch, Bernd Becker
Format: Article
Language:English
Published: MDPI AG 2021-06-01
Series:International Journal of Turbomachinery, Propulsion and Power
Subjects:
transonic
axial compressor
experimental
aeroelasticity
NSV
BLISK
Online Access:https://www.mdpi.com/2504-186X/6/2/19

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