Design of the composite spar-wingskin joint

Volume: 13, Issue: 1, Pages: 47 - 53
Published: Jan 1, 1982
Abstract
null null A variety of composite spar-wingskin joint concepts have been investigated to optimize out-of-plane strength while still providing low weight and ease of fabrication. The spar-wingskin configuration consists of a thin spar which overlaps and is co-cured perpendicular to a thick wingskin. Investigation parameters were the joint geometry in the immediate vicinity of the base of the spar, and the spar-to-spar spacing. It was found that by...
Paper Details
Title
Design of the composite spar-wingskin joint
Published Date
Jan 1, 1982
Journal
Volume
13
Issue
1
Pages
47 - 53
Citation AnalysisPro
  • Scinapse’s Top 10 Citation Journals & Affiliations graph reveals the quality and authenticity of citations received by a paper.
  • Discover whether citations have been inflated due to self-citations, or if citations include institutional bias.