Predicting notched tensile strength of full-scale composite structures from small coupons using fracture mechanics

Author:

Xu Xiaodong,Takeda Shin-ichiORCID,Aoki Yuichiro,Hallett Stephen R.,Wisnom Michael R.

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference23 articles.

1. Tension fracture of laminates for transport fuselage Part II: large notches;Walker,1995

2. Aoki Y, Takeda S, Shoji H, Sugimoto S, Iwahori Y. Evaluation on discrete source damages of CFRP stiffened panels. In 28th international congress of the aeronautical sciences. Brisbane; 2012.

3. Xu X, Takeda S, Hallett SR, Wisnom MR. On the application of fracture mechanics to a full-scale stiffened composite panel test. In Hallett SR, Remmers JJC, editors. V ECCOMAS thematic conference on the mechanical response of composites – COMPOSITES 2015. Bristol; 2015.

4. Assessment of damage containment features of a full-scale PRSEUS fuselage panel;Bergan;Compos Struct,2014

5. Bergan AC, Dávila CG, Leone FA, Awerbuch J, Tan T-M. An analysis methodology to predict damage propagation in notched composite fuselage structures. SAMPE 2015 Baltimore, MD, USA; 2015.

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