Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading Cover

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Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading

Fatigue of Aircraft Structures

By: Grzegorz Socha , Piotr Dąbrowski and Jakub Kaczkowski

Open Access

|Dec 2025

Authors

Grzegorz Socha

grzegorz.socha@ilot.lukasiewicz.gov.pl

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

Piotr Dąbrowski

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

Jakub Kaczkowski

Łukasiewicz Research Network – Institute of Aviation, Warsaw, Poland

DOI: https://doi.org/10.2478/fas-2025-0003 | Journal eISSN: 2300-7591 | Journal ISSN: 2081-7738

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Language: English

Published on: Dec 26, 2025

Published by: ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION

In partnership with: Paradigm Publishing Services

Publication frequency: 1 issue per year

Keywords:

Carbon Fiber Reinforced Polymer (CFRP) composites,

Tubular specimens,

Combined axial and pressure loading,

Experimental investigation,

Failure criterion,

Multiaxial stress state,

Mechanical behavior

Related subjects:

Introductions and overviews,

Engineering, other

© 2025 Grzegorz Socha, Piotr Dąbrowski, Jakub Kaczkowski, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.