METHODS FOR STUDYING FATIGUE CRACK NUCLEATION AND PROPAGATION IN ALUMINUM ALLOYS EXPOSED TO SURFACTANTS

Authors

DOI:

https://doi.org/10.18372/0370-2197.2(107).20133

Keywords:

fatigue damage, fatigue crack nucleation, fatigue crack propagation, surfactants, corrosion preventive compounds, surface deformation relief

Abstract

The issue described in the paper arises from the growing number of substances interacting with aircraft metallic components. This paper examines newly developed and recommended methods for studying the nucleation and propagation of fatigue cracks in aluminum alloys exposed to surfactants, with a particular focus on corrosion preventive compounds. While many of these compounds exhibit excellent functional properties, their potential side effects have been studied insufficiently and remain unclear, thus targeted experimental investigations are required. Given that the fatigue life of metal components comprises two distinct stages, fatigue crack nucleation and crack propagation, separate analyses are essential to assess the applicability of specific surfactants.

The first stage of the fatigue for many metals is associated with formation of so called surface deformation relief, which constituents are extrusions, intrusions, persistent slip bands. The dislocation nature of these substructures presumes the possibility of their sensitivity to the surfactants. Among the metal exhibiting surface deformation relief there are alclad alloys having layer of the pure aluminium, particular alclad alloys 2024T3, 7075T6 widely used in the aircraft manufacturing, for example for the skin of the fuselage. The intensity of the surface relief evolves with the number of loading cycles, thus providing the information regarding the consumption of the duration of the nucleation stage.

To study the first stage of the fatigue, i.e. fatigue crack nucleation, computer-aided optical analysis of surface deformation relief is proposed as the primary method. The method was tested and proved by numerous tests of aluminium alloys specimens and aircraft structural components. For examining fatigue crack behavior in contact with surfactants, linear fracture mechanics techniques are considered reliable and indispensable. Details of both procedures are described.

Author Biographies

Mykhailo Karuskevich, State University "Kyiv Aviation Institute"

Doctor of Technical Sciences, Professor, Professor of the Department of Aircraft Design at the State University "Kyiv Aviation Institute", Kyiv, Ukraine, +38(050)2284505

Olena Korchuk, State University "Kyiv Aviation Institute"

PhD in Technical Sciences, Senior Research Fellow, Head of the Department of Philological and Natural Sciences at the State University "Kyiv Aviation Institute", Kyiv, Ukraine, , +38(098)0041943;

Oleh Karuskevich, State University "Kyiv Aviation Institute"

PhD in Technical Sciences, Doctoral Candidate at the State University "Kyiv Aviation Institute", Kyiv, Ukraine;

Vladyslav Korchuk, State University "Kyiv Aviation Institute"

Postgraduate Student at the State University "Kyiv Aviation Institute", Kyiv, Ukraine; +38(095)1203334

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Published

2025-06-17

How to Cite

Karuskevich, M., Korchuk, O., Karuskevich, O., & Korchuk, V. (2025). METHODS FOR STUDYING FATIGUE CRACK NUCLEATION AND PROPAGATION IN ALUMINUM ALLOYS EXPOSED TO SURFACTANTS. Problems of Friction and Wear, (2(107), 11–18. https://doi.org/10.18372/0370-2197.2(107).20133

Issue

Section

Проблеми тертя та зношування