Design of the composite spar-wingskin joint
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
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Notes
History