Documents

The fatigue life of composite stiffened panels with indentation damage was investigated experimentally using single stringer compression specimens. Indentation damage was induced on one of the two flanges of the stringer. The experiments were conducted using advanced instrumentation, including digital image correlation, passive thermography, and in-situ ultrasonic scanning. Specimens with initial indentation damage lengths of 37 mm to 56 mm were tested in fatigue and the effects of cyclic load amplitude and damage size were studied. A means of comparison of the damage propagation rates and collapse loads based on a stress intensity measure and the Paris law is proposed.
Original languageEnglish
Title of host publicationProceedings of the 17th European Conference on Composite Materials
Subtitle of host publicationMunich, Germany 2016
Place of PublicationReston
Number of pages9
Publication statusPublished - 2016
Event17th European Conference on Composite Materials - Munich, Germany
Duration: 26 Jun 201630 Jun 2016
Conference number: 17
http://www.eccm17.org/

Publication series

Name
PublisherAIAA

Conference

Conference17th European Conference on Composite Materials
Abbreviated titleECCM 2016
CountryGermany
CityMunich
Period26/06/1630/06/16
Internet address

    Research areas

  • fatigue, postbuckling, damage tolerance, indentation damage, delamination

ID: 10411317