Flutter Measurement of a Linear Turbine Blade Cascade with an Angular Position Deviation of One Blade

Experimental flutter testing of high-aspect ratio rotor blades is a mainstay of turbomachinery research. However, rotor blades are never identical, and geometrical errors between actual and nominal geometries exist due to limited machining precision or assembly imperfection. The paper presents the i...

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Bibliographic Details
Main Authors: Eret Petr, Tsymbalyuk Volodymyr, Eckert Markus
Format: Article
Language:English
Published: Sciendo 2023-11-01
Series:Journal of Mechanical Engineering
Subjects:
Online Access:https://doi.org/10.2478/scjme-2023-0019