Simplified procedure for damage-oriented evaluation of a stiffened panel with skin-stringer de-bonding in preliminary design stage
- Aeronautics and Aerospace Open Access Journal
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Giacomo Frulla
Abstract
In aeronautical design activities it is necessary to have reasonable indications on the characteristic dimensions of typical defects that may occur in structures under load in order to indicate their correct hazard/risk level as a function of size and to allocate time/importance of any necessary corrective action.
Keywords
damage-oriented evaluation, preliminary design of stiffened panels, skin-stringer de-bonding effect on global performance