Failure analysis in secondary bonded T-stiffened composite panels subject to cyclic and quasi-static compression loading

Author:

Cândido Geraldo Maurício,de Cássia Mendonça Sales RitaORCID,Arbelo Mariano AndrésORCID,Donadon Maurício VicenteORCID

Funder

Fundação de Amparo à Pesquisa do Estado de São Paulo

Coordenação de Aperfeiçoamento de Pessoal de Nível Superior

Conselho Nacional de Desenvolvimento Científico e Tecnológico

Publisher

Elsevier BV

Subject

Polymers and Plastics,General Chemical Engineering,Biomaterials

Reference20 articles.

1. Fiber-reinforced polymer composites: manufacturing, properties, and applications;Rajak;Polymer,2019

2. A composite cost model for the aeronautical industry: methodology and case study;Hagnell;Compos. Part B,2015

3. Structural evaluation of aircraft stiffened panel;Pravallika;Int J Sci Res,2016

4. Experimental investigation of the aircraft stiffened panel structure under pressure loads;Vishwanath Vashisht;Intern. J. Innov. Eng. Technol.,2016

5. Experimental and numerical studies on the buckling and post-buckling behavior of single blade-stiffened CFRP panels;Kolanu;Compos Struct,2018

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