Composite material selection for aircraft structures based on experimental and numerical evaluation of mechanical properties

Author:

Kastratović G.,Grbović A.,Sedmak A.,Božić Ž.,Sedmak S.

Publisher

Elsevier BV

Subject

General Engineering,Energy Engineering and Power Technology

Reference14 articles.

1. ASTM D7264/D7264M-15, Standard Test Method for Flexural Properties of Polymer Matrix Composite Materials, ASTM International, West Conshohocken, PA, 2015, www.astm.org

2. Multiscale fatigue crack growth modelling for welded stiffened panels;Božić;Fatigue and Fracture of Engineering Materials and Structures,2014

3. The effect of residual stresses on fatigue crack propagation in welded stiffened panels;Božić;Engineering Failure Analysis,2018

4. Castanie, B., Bouvet, C., and Ginot, M. 2020. Review of composite sandwich structure in aeronautic applications, Composites Part C: Open Access 1, 100004.

5. Stress intensity factors numerical calculations for two penny shaped cracks in the elastic solid;Đukić;Engineering Failure Analysis,2020

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