Enhancing buckling performance of perforated composite laminates by manipulating fiber direction using a genetic algorithm

Author:

Cho Hee Keun,Rowlands Robert E.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Reference33 articles.

1. H. A. Qablan, H. Katkhuda and H. Dwairi, Assessment of the buckling behavior of square composite plates with circular cutout subjected to in-plnae shear, Jordan J. of Civil Engineering, 3 (2) (2009) 184–195.

2. T. Ungwattanapanit and H. Baier, Strength-stability optimization of hybrid-stiffness laminated plates with cut-outs subjected to multiple loads, Royal Aeronautical Society 3rd Aircraft Structural Design Conference, Delft, Netherlands (2012).

3. R. Spallino and G. Thierauf, Thermal buckling optimization of composite laminates by evolution strategies, Computers & Structures, 78 (5) (2000) 691–697.

4. M. W. Hyer and R. F. Charette, The use of curvilinear fiber format in composite structure design, 30th AIAA SDM Conference, Paper No. 89-1404, Mobile, AL (1989).

5. A. Teter and S. Samborski, Buckling of thin-walled plates made of curvilinear fibre reinforced composite under uniaxial compression, Computer Methods in Mechanics Conference, Poznan, Poland (2013).

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