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Inter-story drift of the specimens was calculated with data from laboratory apparatus and verified with test results.
The spring-back of the specimens was calculated using a numerical procedure based on the pure bending theory.
The first cracking load for the different test specimens was calculated by applying similar method as that used for reinforced concrete section.
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.
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.
To determine the stress intensity factor, KIc, critical crack tip opening displacement CTODc, the Two Parameter Method was used and the fracture energy, Gf of the specimens was calculated to evaluate the fracture properties of FRPC.
Similar(45)
Structural performance indicators of concrete specimens were calculated.
The bending lengths of the specimens were calculated based on ASTM D 1388-96 (2002).
Damage indices of test specimens were calculated based on strength, ductility and energy dissipation characteristics.
The residual stresses in pristine DLC specimens were calculated with Stoney equation.
Strength, stiffness, ductility and energy dissipation capacities of specimens are calculated and compared.
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com