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Hence, the flexural strengths of the specimens were calculated using linear elastic approach.
In addition, the shear strengths of the squat specimens were calculated using two different models.
The shear capacities of the tested specimens were calculated using the strut and tie models (STM) and non-linear finite element analysis (NLFEA).
Variations in mechanical properties such as the tensile strength, the inter-laminar shear strength and the impact strength of various specimens were calculated using a computer-assisted universal testing machine and an Izod Impact testing machine.
Small crack growth rates and fatigue lives of naturally occurring small cracks in shot peened and unpeened specimens were calculated using small crack theory and a crack closure model.
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The spring-back of the specimens was calculated using a numerical procedure based on the pure bending theory.
The energy release rate in delamination of angle-ply laminated double cantilever composite beam specimens was calculated using the compliance equation, and interlaminar cohesive strengths were obtained.
Furthermore, with respect to ACI 318 (Eq. (5)), when the maximum flexural crack spacing in all specimens is calculated using the larger value of ( d_{1}^ ) and ( d_{2}^ ), those calculated values are more conservative than those calculated using only ( d_{2}^ ), as shown in Fig. 17e.
The tensile strength of the specimens was calculated using Rocco's empirical equation (Eq. 1), where B and D are the specimen dimensions, P is the load and β = b/D (5%%) which is the relative width of the bearing strips.
The volume of the nine standardized re-resection margin specimens was calculated using the formula of the volume of a cuboid, rather than the formula of the volume of an ellipsoid, since each standardized re-resection margin specimen generally better approximated that of a cuboid rather than that of an ellipsoid.
The relation between the specimen curvature and the strain energy due to the residual stress was theoretically investigated and the mode II energy release rate for each specimen was calculated using measured specimen curvature.
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