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Pregled bibliografske jedinice broj: 1280317

Notch-Stress S–N Curves for Welded Aluminum-Alloy Components Subjected to Bending


Matić, Tomislav; Vulić, Nenad; Kustura, Dražen; Peko, Ivan
Notch-Stress S–N Curves for Welded Aluminum-Alloy Components Subjected to Bending // Metals, 13 (2023), 6; 1133, 15 doi:10.3390/met13061133 (međunarodna recenzija, članak, znanstveni)


CROSBI ID: 1280317 Za ispravke kontaktirajte CROSBI podršku putem web obrasca

Naslov
Notch-Stress S–N Curves for Welded Aluminum-Alloy Components Subjected to Bending

Autori
Matić, Tomislav ; Vulić, Nenad ; Kustura, Dražen ; Peko, Ivan

Izvornik
Metals (2075-4701) 13 (2023), 6; 1133, 15

Vrsta, podvrsta i kategorija rada
Radovi u časopisima, članak, znanstveni

Ključne riječi
fatigue strength, finite element analysis, notch-stress approach, welded components

Sažetak
Fatigue analysis of aluminum-alloy welded joints based on the linear elastic notch-stress approach is presented in this paper. The International Institute of Welding proposes two variants of the approach, one for thick joints, i.e., joints with a plate thickness of 5 mm or more, with a reference radius rref = 1 mm, using the FAT71 notch-stress design curve, and one for thin joints, i.e., joints with a plate thickness of less than 5 mm, with a reference radius rref = 0.05 mm, using the FAT180 notch-stress design curve. In this work, the feasibility of the proposed S–N curves, obtained mainly by fatigue tests on axially loaded joints, was investigated for 4 mm thick joints subjected to bending. The fatigue analysis was performed for two types of joints: a joint with longitudinal fillet-welded attachment and a joint with round sheet fillet- welded attachment. It was shown that a more accurate estimation of the fatigue life of 4 mm thick aluminum joints loaded in bending can be obtained using the FAT71 notch-stress design curve.

Izvorni jezik
Engleski

Znanstvena područja
Strojarstvo



POVEZANOST RADA


Ustanove:
Prirodoslovno-matematički fakultet, Split,
Pomorski fakultet, Split

Profili:

Avatar Url Ivan Peko (autor)

Avatar Url Dražen Kustura (autor)

Avatar Url Nenad Vulić (autor)

Avatar Url Tomislav Matić (autor)

Poveznice na cjeloviti tekst rada:

doi www.mdpi.com www.mdpi.com

Citiraj ovu publikaciju:

Matić, Tomislav; Vulić, Nenad; Kustura, Dražen; Peko, Ivan
Notch-Stress S–N Curves for Welded Aluminum-Alloy Components Subjected to Bending // Metals, 13 (2023), 6; 1133, 15 doi:10.3390/met13061133 (međunarodna recenzija, članak, znanstveni)
Matić, T., Vulić, N., Kustura, D. & Peko, I. (2023) Notch-Stress S–N Curves for Welded Aluminum-Alloy Components Subjected to Bending. Metals, 13 (6), 1133, 15 doi:10.3390/met13061133.
@article{article, author = {Mati\'{c}, Tomislav and Vuli\'{c}, Nenad and Kustura, Dra\v{z}en and Peko, Ivan}, year = {2023}, pages = {15}, DOI = {10.3390/met13061133}, chapter = {1133}, keywords = {fatigue strength, finite element analysis, notch-stress approach, welded components}, journal = {Metals}, doi = {10.3390/met13061133}, volume = {13}, number = {6}, issn = {2075-4701}, title = {Notch-Stress S–N Curves for Welded Aluminum-Alloy Components Subjected to Bending}, keyword = {fatigue strength, finite element analysis, notch-stress approach, welded components}, chapternumber = {1133} }
@article{article, author = {Mati\'{c}, Tomislav and Vuli\'{c}, Nenad and Kustura, Dra\v{z}en and Peko, Ivan}, year = {2023}, pages = {15}, DOI = {10.3390/met13061133}, chapter = {1133}, keywords = {fatigue strength, finite element analysis, notch-stress approach, welded components}, journal = {Metals}, doi = {10.3390/met13061133}, volume = {13}, number = {6}, issn = {2075-4701}, title = {Notch-Stress S–N Curves for Welded Aluminum-Alloy Components Subjected to Bending}, keyword = {fatigue strength, finite element analysis, notch-stress approach, welded components}, chapternumber = {1133} }

Časopis indeksira:


  • Current Contents Connect (CCC)
  • Web of Science Core Collection (WoSCC)
    • Science Citation Index Expanded (SCI-EXP)
    • SCI-EXP, SSCI i/ili A&HCI
  • Scopus


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