Multi-level experimental and numerical analysis of composite stiffener debonding. Part 1: Non-specific specimen level

Volume: 90, Issue: 4, Pages: 381 - 391
Published: Oct 1, 2009
Abstract
null null A multi-level analysis of skin/stiffener debonding is used for the fuselage design of future aircraft during postbuckling. The specimens composed of a laminate (the skin) to which an over-thickness (the flange) had been added were subjected to four-point bending, which led to interface failure between the flange and the skin. These tests were performed with several configurations and parameters, such as the orientation of the plies...
Paper Details
Title
Multi-level experimental and numerical analysis of composite stiffener debonding. Part 1: Non-specific specimen level
Published Date
Oct 1, 2009
Volume
90
Issue
4
Pages
381 - 391
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