In this work, a Ritz formulation for the analysis of damage initiation and evolution in composite plates under progressive loading is presented. The proposed model assumes a first order shear deformation theory and considers geometric non-linearities through the von Karman assumptions. The damage is modelled through Continuum Damage Mechanics. A set of results is presented to show the potential of the method and highlight some issues to be addressed by suitable developments of the method.

Campagna D., Milazzo A., Oliveri V., Benedetti I. (2023). On modelling damage in composite laminates using the Ritz method and continuum damage mechanics. In Aerospace Science and Engineering (pp. 233-238) [10.21741/9781644902677-34].

On modelling damage in composite laminates using the Ritz method and continuum damage mechanics

Campagna D.
;
Milazzo A.;Benedetti I.
2023-01-01

Abstract

In this work, a Ritz formulation for the analysis of damage initiation and evolution in composite plates under progressive loading is presented. The proposed model assumes a first order shear deformation theory and considers geometric non-linearities through the von Karman assumptions. The damage is modelled through Continuum Damage Mechanics. A set of results is presented to show the potential of the method and highlight some issues to be addressed by suitable developments of the method.
2023
Settore ING-IND/04 - Costruzioni E Strutture Aerospaziali
9781644902677
Campagna D., Milazzo A., Oliveri V., Benedetti I. (2023). On modelling damage in composite laminates using the Ritz method and continuum damage mechanics. In Aerospace Science and Engineering (pp. 233-238) [10.21741/9781644902677-34].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/10447/621426
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