Progressive Damage Analyses of Skin/Stringer DebondingThe debonding of skin/stringer constructions is analyzed using a step-by-step simulation of material degradation based on strain softening decohesion elements and a ply degradation procedure. Decohesion elements with mixed-mode capability are placed at the interface between the skin and the flange to simulate the initiation and propagation of the delamination. In addition, the initiation and accumulation of fiber failure and matrix damage is modeled using Hashin-type failure criteria and their corresponding material degradation schedules. The debonding predictions using simplified three-dimensional models correlate well with test results.
Document ID
20040086002
Acquisition Source
Langley Research Center
Document Type
Other
Authors
Daville, Carlos G. (NASA Langley Research Center Hampton, VA, United States)