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Crack initiation and early propagation plane orientation of 2A12-T4 aluminum alloy under tension-torsion fatigue loading including mean tensile stress

Structurae cannot make the full text of this publication available at this time. The full text can be accessed through the publisher via the DOI: 10.3221/igf-esis.35.50.
  • About this
    data sheet
  • Reference-ID
    10458267
  • Published on:
    24/10/2020
  • Last updated on:
    24/10/2020
 
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