Damage identification in composite panels using guided waves

R. Loendersloot, M. Moix-Bonet

Research output: Contribution to conferencePaperAcademicpeer-review

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Abstract

A methodology for the identification of barely visible impact damage using guided waves on a typical aircraft composite structure is implemented. Delaminations and debondings have been introduced in two stiffened panels by means of impact loads.
Original languageEnglish
Pages1-14
Publication statusPublished - 7 Sep 2015
Event5th CEAS Air & Space Conference 2015: Challenges in European Aerospace - Delft, Netherlands
Duration: 7 Sep 201511 Sep 2015
Conference number: 5

Conference

Conference5th CEAS Air & Space Conference 2015
CountryNetherlands
CityDelft
Period7/09/1511/09/15

Keywords

  • IR-97412
  • METIS-308627

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