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HomeKey Engineering MaterialsKey Engineering Materials Vols. 334-335The Effects of a Cutout and Stacking Sequences on...

The Effects of a Cutout and Stacking Sequences on the Buckling Behaviour of Composite Panels

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Advances in Composite Materials and Structures

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Periodical:

Key Engineering Materials (Volumes 334-335)

Pages:

521-524

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.334-335.521

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Online since:

March 2007

Authors:

Faruk Elaldi

Keywords:

Composite, Cutout, Damage Tolerance, Stacking Sequence, Stiffness

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© 2007 Trans Tech Publications Ltd. All Rights Reserved

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[2] S. W. Tsai, In-Plane Stiffness of Symmetric Laminates, Composites Design, 4 th Edt., 7-1, Think Composites, Ohio. (1987).

[3] G. Stöffler, Determination of Torsion Strength and Shear Module of a Multi-Layer Composite, Journal of Composite Materials, 14, (1980), p.95.

DOI: 10.1177/002199838001400202

[4] M. Knight, Three-Dimensional Elastic Module of Graphite/Epoxy Composites, Journal of Composite Materials, 16, (1982), p.153.

DOI: 10.1177/002199838201600206

[5] C. T. Sun, and L. Sihan, Three-Dimensional Effective Elastic Constants for Thick Laminates, Journal of Composite Materials, 22, (1988), pp.629-639.

DOI: 10.1177/002199838802200703

[6] H.J. Chen, and S. W. Tsai, Three-Dimensional Effective Module of Symmetric Laminates, Journal of Composite Materials, 30, (1996), p.906. Effect of Layup and Cutout 0 100 200 300 400 500 600 1 Stress at Max. Load [MPa]

,0,0] - With Cutout

,0,0] - Without Cutout

,45,0] - With Cutout

,45,0] - Without Cutout

[45] ,45,45] - With Cutout

[45] ,45,45] - Without Cutout Figure 6: Comparing the stresses, effect of lay-up and cutout