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A New Approach to Modelling and Testing the Fatigue Strength of Helicopter Rotor Blades during Repair Process Cover

A New Approach to Modelling and Testing the Fatigue Strength of Helicopter Rotor Blades during Repair Process

Fatigue of Aircraft Structures
Volume 2019 (2019): Issue 11 (December 2019)
By: Michał Sałaciński,  Rafał Kowalski,  Michał Szmidt and  Sławomir Augustyn  
Open Access
|Jul 2020
Authors

Authors

Michał Sałaciński

michal.salacinski@itwl.pl

Air Force Institute of Technology, Warsaw, Poland

Rafał Kowalski

Dęblin, Poland

Michał Szmidt

Łukasiewicz Research Network ‒ Institute of Aviation, Warsaw, Poland

Sławomir Augustyn

Military University of Technology, Warsaw, Poland
DOI: https://doi.org/10.2478/fas-2019-0006 | Journal eISSN: 2300-7591
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Language: English
Page range: 56 - 67
Published on: Jul 15, 2020
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
rotor blade,
helicopter,
fatigue test,
repairs,
bonding,
composites
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2020 Michał Sałaciński, Rafał Kowalski, Michał Szmidt, Sławomir Augustyn, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Volume 2019 (2019): Issue 11 (December 2019)
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