Investigations of fml profile buckling and post-buckling behaviour under axial compression

Author:

Banat D.,Kolakowski Z.,Mania R.J.

Funder

Ministry of Science and Higher Education of Poland - National Science Centre

Publisher

Elsevier BV

Subject

Mechanical Engineering,Building and Construction,Civil and Structural Engineering

Reference37 articles.

1. Development of fibre metal laminates for advanced aerospace structures;Vogelesang;J. Mater. Process. Technol.,2000

2. The mechanical behavior of GLARE laminates for aircraft structures;Wu;JOM,2005

3. Mechanics of Composite Materials;Jones;Mech. Compos. Mater.,1999

4. Influence of Fibre Arrangement on the Buckling Load of Composite Plates - Analytical Solution;Czapski;Fibres Text. East. Eur.,2015

5. Inspection methods for quality control of fibre metal laminates (FML) in aerospace components;Dragan;Compos. Theory Pract.,2012

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