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Fatigue life estimation of notched components under multiaxial non-proportional loading with variable amplitudes.

Calculation concepts for determining component fatigue life under non-proportional variable amplitudes loading were investigated.

The fatigue life of notched components until technical crack initiation can be described using the local strain concept. For fatigue life estimation under locally non-proportional loadings, the concept of critical planes has proven effective. In this approach, fatigue life in different planes is examined through the material element at the notch root. The plane with the lowest fatigue life is considered the critical plane.

The presented algorithm consists of two parts: a notch simulation to determine local multiaxial, elasto-plastic stresses and a subsequent damage assessment using the critical plane method.

In this work, the…

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Calculation concepts for determining component fatigue life under non-proportional variable amplitudes loading were investigated.

The presented algorithm consists of two parts: a notch simulation to determine local multiaxial, elasto-plastic stresses and a subsequent damage assessment using the critical plane method.

In this work, the Fatemi/Socie parameter (shear-based), the Smith/Watson/Topper parameter (normal strain-based), and a parameter based on short crack fracture mechanics were investigated for accuracy. The accuracy assessment is based on a comprehensive dataset, including test results of notched specimens subjected to both proportional and non-proportional variable amplitude loading.

Artikelnummer: VAL5-2024-035

Titel: Fatigue life estimation of notched components under multiaxial non-proportional loading with variable amplitudes.
Autor(en): J. Kraft, M. Vormwald
DOI: 10.48447/VAL5-2024-035
Veranstaltung: VAL5 - Fifth International Conference on Material and Component Performance under Variable Amplitude Loading
Jahr der Veröffentlichung: 2024
Publikationsart: Tagungsmanuskript (PDF)
Sprache: Englisch
Stichwörter: multiaxial fatigue,critical plane,notches

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1

Englisch

25,00 €

Nur online erhältlich

Autor(en): B. Möller, M. Scurria, T. Korschinsky

Application of Incremental Step Tests for Screening and Deriving Cyclic Properties of Metal Structures Using the Example of Additively Manufactured AlSi10Mg

Publikationsart: Tagungsmanuskript (PDF)

Englisch

25,00 €

Nur online erhältlich

Autor(en): A. Niesłony, M. Böhm, M. Sgamma, A. Chiocca, F. Bucchi, F. Frendo

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A Comparative Analysis: Time vs. Frequency Domain Definitions of the Fatemi-Socie Criterion

Publikationsart: Tagungsmanuskript (PDF)

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1

Englisch

25,00 €

Nur online erhältlich

Autor(en): D. Fräulin, A. Trapp, M. Hinz, P. Wolfsteiner

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1

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Publikationsart: Tagungsmanuskript (PDF)

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1

Englisch

25,00 €

Nur online erhältlich

Autor(en): G. Curti, T. Dengler, M. Palmieri, A. Trapp, P. Wolfsteiner, F. Cianetti, K. Schneider

Modal driven load tailoring for efficient vibration fatigue assessment on non-stationary processes: A versatile approach exploiting the Fatigue Damage Spectrum

Publikationsart: Tagungsmanuskript (PDF)

Englisch

25,00 €

Nur online erhältlich

Autor(en): D. Benasciutti

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1

Englisch

25,00 €

Nur online erhältlich

Autor(en): L. Solazzi, A. Mazzoni, N. Danzi, M. Cima

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1

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Publikationsart: Tagungsmanuskript (PDF)

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1

Englisch

25,00 €

Nur online erhältlich

Autor(en): A. Visentin, A. Campagnolo, V. Babini, G. Meneghetti

Fatigue strength assessment of tube-to-flange welded steel joints with reinforcement ribs under variable amplitude loadings according to the Peak Stress Method

Publikationsart: Tagungsmanuskript (PDF)

Englisch

25,00 €

Nur online erhältlich

Autor(en): J. D. Mattos, M. A. Arbelo

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Comparative Study of Crack Growth Retardation Models for an Integral Stiffened Panel Subjected to Overload.

Publikationsart: Tagungsmanuskript (PDF)

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1

Englisch

25,00 €

Nur online erhältlich