On the prediction of bolted single-lap composite joints Articles uri icon

publication date

  • May 2012

start page

  • 2110

end page

  • 2117

issue

  • 6

volume

  • 94

international standard serial number (ISSN)

  • 0263-8223

electronic international standard serial number (EISSN)

  • 1879-1085

abstract

keywords

  • composite joint; finite element modelling; bolted joint; aeronautical structures