Prediction of Fatigue Cracks Using Gamma Function

• Autorzy: Moussouni Abdelfetah , Benachour Mustapha , Benachour Nadjia

Identyfikatory

DOI

10.2478/fas-2022-0004

• Języki publikacji: EN

Abstrakty

EN

In the present study it has been endeavored to estimate the fatigue crack propagation in V-notch Charpy specimens of 2024 T351 Al-alloy. For this purpose, a new application of fatigue crack growth (FCG) is developed based on the “Gamma function.” Experimental fatigue tests are conducted for stress ratios from 0.1 to 0.5 under constant amplitude loading. The empiric model depends principally on physical parameters and materials’ properties in non-dimensional form. Deviation percentage, prediction ratio, and band error are used for validation of the performance of the fatigue life. The results determined from Gamma application are in good agreement with experimental FCG rates and those obtained from using Paris law.

Słowa kluczowe

EN

fatigue crack growth; stress ratio; fatigue; 2024 T351 Al-alloy; Gamma function

• Wydawca: Wydawnictwa Naukowe Sieci Badawczej Łukasiewicz - Instytutu Lotnictwa
• Czasopismo: Fatigue of Aircraft Structures
• Rocznik: 2022
• Tom: Iss. 14
• Strony: 29--46
• Opis fizyczny: Bibliogr. 34 poz., rys., tab., wykr., wzory

Twórcy

autor

Moussouni Abdelfetah

• Faculty of Technology and Science, University of Tlemcen, BP 230 - 13000 ChetouaneTlemcen, Algeria

• https://orcid.org/0000-0001-5404-5106

autor

Benachour Mustapha

• Faculty of Technology and Science, University of Tlemcen, BP 230 - 13000 ChetouaneTlemcen, Algeria

• https://orcid.org/0000-0002-8415-241X

autor

Benachour Nadjia

• Faculty of Technology and Science, University of Tlemcen, BP 230 - 13000 ChetouaneTlemcen, Algeria

• https://orcid.org/0000-0001-9938-9201

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