Approach to Critical Crack Opening Displacement Modeling of Damage in Metal Sheets after Composite Patch Bonded Repair

  • Michał Sałacinski, Andrzej Leski, Michał Stefaniuk
  • Fatigue of Aircraft Structures, January 2016, De Gruyter
  • DOI: 10.1515/fas-2016-0009

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http://dx.doi.org/10.1515/fas-2016-0009