A semi-analytical model for shear buckling analysis of stiffened composite panel with debonding defect

Author:

da Silva Douglas ConradoORCID,Donadon Maurício VicenteORCID,Arbelo Mariano Andrés

Funder

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior

Conselho Nacional de Desenvolvimento Científico e Tecnológico

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference32 articles.

1. Mechanics of Composite Materials;Jones,1998

2. Conventional and advanced composites in aerospace industry: Technologies revisited;Toozandehjani;Am. J. Aerosp. Eng.,2018

3. Aircraft Structures for Engineering Students;Megson,2007

4. Assembly of semi-analytical models to address linear buckling and vibration of stiffened composite panels with debonding defect;Castro;Compos. Struct.,2017

5. The analysis of skin-to-stiffener debonding in composite aerospace structures;Yap;Compos. Struct.,2002

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