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Crack Propagation Tests for Load Sequences Developed Using Different Flight Parameters of a Trainer Aircraft Cover

Crack Propagation Tests for Load Sequences Developed Using Different Flight Parameters of a Trainer Aircraft

Fatigue of Aircraft Structures
Volume 2023 (2023): Issue 15 (December 2023)
By: Piotr Reymer,  Kamil Kowalczyk,  Marta Baran,  Dominik Nowakowski,  Michał Dziendzikowski and  Andrzej Leski  
Open Access
|Oct 2024

Authors

Piotr Reymer

piotr.reymer@itwl.pl

Air Force Institute of Technology, Warsaw, Poland
Military University of Technology, Warsaw, Poland

Kamil Kowalczyk

kamil.kowalczyk@itwl.pl

Air Force Institute of Technology, Warsaw, Poland

Marta Baran

marta.baran@itwl.pl

Air Force Institute of Technology, Warsaw, Poland

Dominik Nowakowski

dominik.nowakowski@itwl.pl

Air Force Institute of Technology, Warsaw, Poland

Michał Dziendzikowski

michal.dziendzikowski@itwl.pl

Air Force Institute of Technology, Warsaw, Poland

Andrzej Leski

andrzej.leski@ilot.lukasiewicz.gov.pl

Military University of Technology, Warsaw, Poland
Lukasiewicz Research Network – Institute of Aviation, Warsaw, Poland
DOI: https://doi.org/10.2478/fas-2023-0010 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738
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Language: English
Page range: 155 - 165
Published on: Oct 28, 2024
Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
In partnership with: Paradigm Publishing Services
Publication frequency: 1 issue per year
Keywords:
fatigue crack propagation,
flight parameters,
load sequence
Related subjects:
Engineering,
Introductions and overviews,
Engineering, other

© 2024 Piotr Reymer, Kamil Kowalczyk, Marta Baran, Dominik Nowakowski, Michał Dziendzikowski, Andrzej Leski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

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