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- W765401241 abstract "The results of an analytical study of the nonlinear response of stiffened fuselage shells with long cracks are presented. The shells are modeled with a hierarchical modeling strategy that accounts for global and local response phenomena accurately. Results are presented for internal pressure and mechanical bending loads. The effects of crack location and orientation on shell response are described. The effects of mechanical fasteners on the response of a lap joint and the effects of elastic and elastic-plastic material properties on the buckling response of tension-loaded flat panels with cracks are also addressed." @default.
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- W765401241 date "1994-09-01" @default.
- W765401241 modified "2023-09-27" @default.
- W765401241 title "Nonlinear analysis of damaged stiffened fuselage shells subjected to combined loads" @default.
- W765401241 hasPublicationYear "1994" @default.
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