A formula for the crack opening level under random loading in 2024-T351 aluminum alloy

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 518
  • Download : 79
Based on the fatigue crack growth results of the previous work for 2024-T351 aluminum alloy, the crack closure behavior under random loading was analyzed, and the correlation between the crack opening ratio and the stress ratio under random loading was discussed. The crack opening ratio under random loading can be expressed as a function of the stress ratio for the largest load cycle in a random load history. The correlation obtained is found to provide good predictions for crack growth under random loading.
Publisher
KOREAN SOC MECHANICAL ENGINEERS
Issue Date
2014-02
Language
English
Article Type
Article
Keywords

SHORT FATIGUE CRACKS; STRIP-YIELD MODEL; VARIABLE-AMPLITUDE; GROWTH-BEHAVIOR; CLOSURE; CONSTANT

Citation

JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, v.28, no.2, pp.521 - 525

ISSN
1738-494X
DOI
10.1007/s12206-013-1119-2
URI
http://hdl.handle.net/10203/188798
Appears in Collection
ME-Journal Papers(저널논문)
Files in This Item

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0