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Bolt location affects the damage modes, ultimate load and structure stiffness of the joint, and longer lap length has a tendency to promote ultimate load and structure stiffness.
The ultimate load and ductility decreased substantially with increasing notch depth.
Significant decreases of both ultimate load and stiffness were also observed.
The ultimate load and the effective anchor length were also obtained.
Furthermore, ultimate load and slip displacement behavior between the same surfaces were examined.
Advantages of the numerical analysis are the prediction of the ultimate load and the understanding of failure mechanisms.
In addition, grouting and opening on the failure mode, lateral ultimate load, and stiffness of specimens are presented.
The collapse load is known variously as the failure load, the ultimate load, and the limit load.
The main goal was to assess the effect of these parameters on the ultimate load and failure type.
There is a significant increase in the deflection at ultimate load and the deflection at failure as the reinforcing index increases in a linear manner.
Addition of fibres in hybrid form improved many of the engineering properties such as the first crack load, ultimate load and ductility factor of the composite.
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