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Adhesive bonded aircraft structures

Publisher
Elsevier Science
Year
1955
Tongue
English
Weight
221 KB
Volume
259
Category
Article
ISSN
0016-0032

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Ab6traet--The problem of a cracked metallic layer bonded to a composite (orthotropic) layer is analyzed. The analysis takes into consideration the nonlinear behavior of the adhesive. The structure is considered to be under generalized plane-stress loading, and the adhesive layer is treated as a nonl