Repository logo
 
Publication

Effects of Shot-Peening and Stress Ratio on the Fatigue Crack Propagation of AL 7475-T7351 Specimens

dc.contributor.authorFerreira, Natália
dc.contributor.authorAntunes, Pedro
dc.contributor.authorFerreira, José
dc.contributor.authorCosta, José D. M.
dc.contributor.authorCapela, Carlos
dc.date.accessioned2025-06-30T12:59:03Z
dc.date.available2025-06-30T12:59:03Z
dc.date.issued2018-03-05
dc.description.abstractShot peening is an attractive technique for fatigue enhanced performance of metallic components, because it increases fatigue crack initiation life prevention and retards early crack growth. Engineering design based on fatigue crack propagation predictions applying the principles of fracture mechanics is commonly used in aluminum structures for aerospace engineering. The main purpose of present work was to analyze the effect of shot peening on the fatigue crack propagation of the 7475 aluminum alloy, under both constant amplitude loading and periodical overload blocks. The tests were performed on 4 and 8 mm thickness specimens with stress ratios of 0.05 and 0.4. The analysis of the shot-peened surface showed a small increase of the micro-hardness values due to the plastic deformations imposed by shot peening. The surface peening beneficial effect on fatigue crack growth is very limited; its main effect is more noticeable near the threshold. The specimen’s thickness only has marginal influence on the crack propagation, in opposite to the stress ratio. Periodic overload blocks of 300 cycles promotes a reduction of the fatigue crack growth rate for both intervals of 7500 and 15,000 cycles.eng
dc.description.sponsorshipThis research is sponsored by FEDER funds through the program COMPETE—Programa Operacional Factores de Competitividade—and by national funds through FCT—Fundação para a Ciência e a Tecnologia—under the project PEst-C/EME/UI0285/2013. The authors would also like to acknowledge OGMA-Indústria Aeronáutica de Portugal, Alverca, Portugal, and Dra Ana Guimarães and Eng. João Miranda for the collaboration in the shot-peening processing.
dc.identifier.citationFerreira, N., Antunes, P. V., Ferreira, J. A. M., D. M. Costa, J., & Capela, C. (2018). Effects of Shot-Peening and Stress Ratio on the Fatigue Crack Propagation of AL 7475-T7351 Specimens. Applied Sciences, 8(3), 375. https://doi.org/10.3390/app8030375
dc.identifier.doi10.3390/app8030375
dc.identifier.issn2076-3417
dc.identifier.urihttp://hdl.handle.net/10400.8/13463
dc.language.isoeng
dc.peerreviewedyes
dc.publisherMDPI AG
dc.relation.hasversionhttps://www.mdpi.com/2076-3417/8/3/375
dc.relation.ispartofApplied Sciences
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectaeronautical aluminum alloys
dc.subjectfatigue crack propagation
dc.subjectoverloads
dc.subjectshot peening
dc.subjectParis law
dc.titleEffects of Shot-Peening and Stress Ratio on the Fatigue Crack Propagation of AL 7475-T7351 Specimenseng
dc.typejournal article
dspace.entity.typePublication
oaire.citation.issue3
oaire.citation.titleApplied sciences
oaire.citation.volume8
oaire.versionhttp://purl.org/coar/version/c_970fb48d4fbd8a85
person.familyNameCapela
person.givenNameCarlos
person.identifier.ciencia-id9B1E-6857-3D6B
person.identifier.orcid0000-0003-3334-4945
person.identifier.ridG-6395-2016
person.identifier.scopus-author-id7801358401
relation.isAuthorOfPublication9b079aa3-b79b-4395-b081-1f23d6a17514
relation.isAuthorOfPublication.latestForDiscovery9b079aa3-b79b-4395-b081-1f23d6a17514

Files

Original bundle
Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
applsci-08-00375.pdf
Size:
5.24 MB
Format:
Adobe Portable Document Format
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.32 KB
Format:
Item-specific license agreed upon to submission
Description: