Corrosion pillowing in aircraft fuselage lap joints

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/1.18589
AuthorSearch for: 1; Search for: 1; Search for: 1
Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
Conference46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 13th AIAA/ ASME/AHS Adaptive Structures Conference, 7th AIAA Non-Deterministic Approaches Forum, 6th AIAA Gossamer Spacecraft Forum, and 1st AIAA Multidisciplinary Design Optimization Specialist Conference, April 18-21, 2005, Austin, Texas
Subjectcorrosion pillowing; fracture surfaces; lap joints; semi-elliptical cracks; aircraft; computer simulation; corrosion resistance; cracks; finite element method; fracture; stress analysis; fuselages
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LanguageEnglish
Peer reviewedYes
NPARC number21275955
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Record identifier721bd37e-9324-476a-b481-b4b4485d6c0f
Record created2015-08-21
Record modified2020-04-07
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