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Table 1.

Nomenclature.

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Table 1 Expand

Fig 1.

(a) Representative flexural load-displacement curve; (b) schematic of three-point loading test (ASTM D7264).

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Fig 1 Expand

Fig 2.

(a) Tensile test set-up with a representative load-displacement curve; (b) schematic of standard tensile test method for composite materials (ASTM D3039).

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Fig 2 Expand

Fig 3.

(a) A representative load-displacement curve obtained from mode II fracture mechanics testing; (b) schematic of end notch flexure specimen.

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Fig 3 Expand

Fig 4.

Methodology chart illustrating steps of data preparation and model training.

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Fig 4 Expand

Table 2.

Mean and standard deviation values of glass transition temperature and mechanical properties nine different types of CFRP composites.

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Table 2 Expand

Table 3.

Summary of the RMSE and R2 from ridge regression, support vector regression, and random forest based on LOOCV without including the Type as an independent variable. Note: only independent variables were normalized. Asterisks correspond to the highest obtained values with respect to the three models.

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Table 3 Expand

Fig 5.

Prediction of flexural strength using ridge regression.

(a) Predicted versus actual values; (b) Feature premutation.

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Fig 5 Expand

Fig 6.

Prediction of flexural modulus using ridge regression.

(a) Predicted versus actual values; (b) Feature premutation.

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Fig 6 Expand

Fig 7.

Prediction of mode II energy-release rate using the random forest model without including the Type variable.

(a) Predicted versus actual values; (b) Feature premutation.

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Fig 7 Expand

Table 4.

Summary of the RMSE and R2 from ridge regression, SVM, and RF based on LOOCV with including the Type as independent variable. Note: only independent variables were normalized. Arrows are used to indicated changes in the values compared with results obtained in Table 3.

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Table 4 Expand

Fig 8.

Prediction of mode II Energy Release Rate using ridge regression with including the type.

(a) Predicted versus actual values; (b) Feature premutation.

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Fig 8 Expand