Energetic and Fractographic Investigation of Crack Growth Under Variable Amplitude Loading

Abstract This study investigates fatigue crack propagation in aluminum alloy 2024-T351 under constantamplitude loading (CAL) and variable-amplitude loading (VAL), with a focus on energy parameters. The hysteretic energy dissipated at each load level (or per block) exhibits trends comparable to those observed under CAL conditions. At high propagation rates, both the dissipated hysteretic energy and the crack growth rate vary linearly, consistent with a propagation mechanism characterized by the formation of striations in each cycle. At lower propagation rates, the relationship between crack growth rate and dissipated energy per block follows a power-law form. The analysis is extended through quantitative microfractographic observations using scanning electron microscopy, which reveal the spatial distribution of key fractographic features and the mechanisms governing crack propagation. Based on these findings, an energy-based model is proposed that allows the replacement of load spectra with an equivalent constant-amplitude loading.

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Publication Details

Journal
Fatigue of Aircraft Structures
Published
2025-11-14
DOI
https://doi.org/10.2478/fas-2025-0002
Primary Topic
Fatigue and fracture mechanics
Type
article
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article

Energetic and Fractographic Investigation of Crack Growth Under Variable Amplitude Loading

Mustapha Benachour, Soumia Benguediab, M. Benguediab, Tayeb Kebir et al.
Fatigue of Aircraft Structures
Fatigue and fracture mechanics
article

Energetic and Fractographic Investigation of Crack Growth Under Variable Amplitude Loading

Mustapha Benachour, Soumia Benguediab, M. Benguediab, Tayeb Kebir, Abdelkader Lahcene, Hichem Mebarki
article en

Abstract

Abstract This study investigates fatigue crack propagation in aluminum alloy 2024-T351 under constantamplitude loading (CAL) and variable-amplitude loading (VAL), with a focus on energy parameters. The hysteretic energy dissipated at each load level (or per block) exhibits trends comparable to those observed under CAL conditions. At high propagation rates, both the dissipated hysteretic energy and the crack growth rate vary linearly, consistent with a propagation mechanism characterized by the formation of striations in each cycle. At lower propagation rates, the relationship between crack growth rate and dissipated energy per block follows a power-law form. The analysis is extended through quantitative microfractographic observations using scanning electron microscopy, which reveal the spatial distribution of key fractographic features and the mechanisms governing crack propagation. Based on these findings, an energy-based model is proposed that allows the replacement of load spectra with an equivalent constant-amplitude loading.

Fatigue of Aircraft Structures
University Frères Mentouri Constantine 1 (DZ), Northwest African American Museum (US), University of Abou Bekr Belkaïd (DZ), Université Djilali de Sidi Bel Abbès (DZ), Dynamic Systems (United States) (US), Université de Saida Dr.Moulay Tahar (DZ), University of Blida (DZ)
Openalex Percentile: Top 59%
Fatigue and fracture mechanics
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Energetic and Fractographic Investigation of Crack Growth Under Variable Amplitude Loading — Mustapha Benachour, Soumia Benguediab, et al. · Fatigue of Aircraft Structures (2025) | TGRS Research Map | TGRS