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Vibration Tests of a Turbine Blade with Internal Damping Manufactured using Additive Technology Cover

Vibration Tests of a Turbine Blade with Internal Damping Manufactured using Additive Technology

Fatigue of Aircraft Structures
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By: ,  ,  ,  ,   and    
Open Access
|Jun 2026
Authors

Authors

Sławomir Cieślak

Slawomir.Cieslak@ilot.lukasiewicz.gov.pl

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

Grzegorz Moneta

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

Michał Szmidt

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

Wiesław Krzymień

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

Andrzej Leski

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland
Faculty of Mechanical Engineering, Military University of Technology, Warsaw, Poland

Michał Fedasz

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland
DOI: https://doi.org/10.2478/fas-2025-0006 | Journal eISSN: 2300-7591
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Language: English
Submitted on: Dec 31, 2024
Accepted on: Feb 3, 2026
Published on: Jun 6, 2026
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
vibration,
damping,
fatigue,
turbine,
blade,
vibrometer,
Additive Manufacturing (AM),
Selective Laser Melting (SLM)
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2026 Sławomir Cieślak, Grzegorz Moneta, Michał Szmidt, Wiesław Krzymień, Andrzej Leski, Michał Fedasz, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution 4.0 License.

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