Stress analysis and strength prediction of composite laminates with two interacting holes

Author:

Özaslan E.,Güler M.A.,Yetgin A.,Acar B.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference34 articles.

1. Özaslan, E., Acar, B., Yetgin, A., 2018a. Design and validation of a filament wound composite rocket motor case. In: ASME 2018 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, pp. V03AT03A007–V03AT03A007.

2. Prediction of size effects in notched laminates using continuum damage mechanics;Camanho;Compos Sci Technol,2007

3. Experimental and numerical investigation of the tension and compression strength of un-notched and notched quasi-isotropic laminates;Wang;Compos Struct,2004

4. Size effects in unnotched tensile strength of unidirectional and quasi-isotropic carbon/epoxy composites;Wisnom;Compos Struct,2008

5. A finite fracture mechanics model for the prediction of the open-hole strength of composite laminates;Camanho;Compos Part A: Appl Sci Manuf,2012

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