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Table 5 Ductility ratio of all specimens.
Results indicated that the in-plane shear properties (shear strength τxy and shear modulus Gxy) oFailurerectional fiber comodeste can be cofsiderally improved by incorporation of random glaspecimensand forming hybrid composites.
The load and deflection of all specimens were instrumented.
Figure 9 indicates loads of all specimens at initial cracking, yield and ultimate.
The load-rebar strain relationships of all specimens are presented in Fig. 11.
The failure pattern of all specimens was shear failure as shown in Figure 4 a-d).
The initial crack of all specimens occurred at the bottom of the beams below loading point.
The surface hardness of all specimens is found to increase and the wear resistance thereby improves.
14C dates of all specimens range from AD 1006 to 1891 (Table 2).
Moment vertical displacement curves of all specimens have obvious elastic, elastic plastic and plastic stages.
The maximum blocking temperature of all specimens distributes around 550 °C.
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