Page 9 - Open-Access-Dec-2019
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                                                                                        TECHNICAL PAPER

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                                                                shows strong dependency to the mass loss of steel bar
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                                                                and decreases with the increasing mass loss of steel. This
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                                                                residual flexural load capacity of the reinforced prism specimens.


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                i                                              Figure 7 shows the typical failure mode of the R/FRCs and R/
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    (4%               (4%                                       ECC prism specimens subject to four-point bending before and

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                                                                after accelerated corrosion. The failure modes are categorized

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                    (4%                 (4%                               into shear failure, bond failure, and bending failure as shown in





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      iviV̈œ˜ ­““®              iviV̈œ˜ ­““®                Table 4. As can be seen, shear failure was the dominant failure

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  œ>` ­Ž ®       œ>` ­Ž ®         (b)                           2-d accelerated corrosion as major shear cracks were observed
                                                                mode for all pristine R/FRC prism specimens before and after


                                                                as shown in Figures 7a, 7b, 7d, 7e, 7g and 7h. With the increase
 (4%        (4%            (4%                                  of accelerated corrosion duration to 4 d, the failure mode

     (4%        (4%            (4%                              changed from shear failure to bond failure in R/FRC specimens.
 (4%       (4%             (4%                                  This phenomenon was attributed to the failure of bonding

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                                                                              of steel bar. For example, a visible wider longitudinal crack was



  œ>` ­Ž ®       œ>` ­Ž ®       iviV̈œ˜ ­““®   œ>` ­Ž ®       iviV̈œ˜ ­““®  found in R/FRC 1 and R/FRC 2 specimens after 4-d accelerated
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                                                                corrosion as shown in Figures 7c and 7f. The increase of fibre
                                                                dosage delays the change of failure mode in R/FRC specimens,
                                                                and bond failure was not observed in R/FRC 3 specimen (Figure
                                                                7i). R/ECC showed a consistent bending failure before and after

                                                                accelerated corrosion (Figures 7j, 7k and 7l) owning to the high
                                                                ductility and damage tolerance of the ECC cover. In a sense, the

                                                                strong confinement effect of ECC on steel bar can compromise
  iviV̈œ˜ ­““®   iviV̈œ˜ ­““®   iviV̈œ˜ ­““®              the sharp deterioration of bonding between corroded steel
                                  (c)                           and ECC in comparison with FRCs. Multiple micro-cracks were
                                                                observed at the tension side (bottom surface) of the specimen,
          Figure 5: Load-deflection curves of reinforced prisms (a) before, and (b)   and the crack width was limited to be less than 150 mm in R/
                  after 2-d and (c) after 4-d accelerated corrosion.  ECC specimens.
                                                                         The IndIan ConCreTe Journal | deCember 2019  15
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