The purpose of this work is the numerical investigation of the stringer termination debonding in composite stiffened panels, subjected to a traction load. A parametric analysis has been carried out, considering the influence of the plies' number and of the stringer width on the delamination initiation load as well as on the skin-stringer complete separation load.
Numerical investigation of the stringer termination debonding in composite stiffened panels
Sellitto, A.;RICCIO, Aniello
2016
Abstract
The purpose of this work is the numerical investigation of the stringer termination debonding in composite stiffened panels, subjected to a traction load. A parametric analysis has been carried out, considering the influence of the plies' number and of the stringer width on the delamination initiation load as well as on the skin-stringer complete separation load.File in questo prodotto:
Non ci sono file associati a questo prodotto.
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.