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Flexural Behaviour of Precast, Prestressed Ribbed RPC Bottom Panels
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This study introduces a new type of precast, prestressed reactive powder concrete (RPC) bottom panel for a
large-span composite slab. The bottom panels, which have one or two inverted ribs with openings, act as formwork during
the construction stage. The paper experimentally investigated the crack characteristics, deflection, and normal section
bearing capacity of four precast, prestressed ribbed RPC bottom panels under flexural load. The results indicated that the
RPC ultimate strain under non-uniform compression is 5500x106 and the plastic influence coefficient of the section
modulus is linear with the longitudinal reinforcement ratio. The tensile stress of RPC at the cracked section should be
considered while calculating the flexural stiffness; the equation used to determine the nominal tensile stress of RPC as a
major variable for calculating the crack width at the bottom of panels was proposed. The bottom panels generally exhibit
an over-reinforced failure mode behaviour without the composite layer; the calculation method of the normal section bearing
capacity of this mode was established.
Bentham Science Publishers Ltd.
Title: Flexural Behaviour of Precast, Prestressed Ribbed RPC Bottom Panels
Description:
This study introduces a new type of precast, prestressed reactive powder concrete (RPC) bottom panel for a
large-span composite slab.
The bottom panels, which have one or two inverted ribs with openings, act as formwork during
the construction stage.
The paper experimentally investigated the crack characteristics, deflection, and normal section
bearing capacity of four precast, prestressed ribbed RPC bottom panels under flexural load.
The results indicated that the
RPC ultimate strain under non-uniform compression is 5500x106 and the plastic influence coefficient of the section
modulus is linear with the longitudinal reinforcement ratio.
The tensile stress of RPC at the cracked section should be
considered while calculating the flexural stiffness; the equation used to determine the nominal tensile stress of RPC as a
major variable for calculating the crack width at the bottom of panels was proposed.
The bottom panels generally exhibit
an over-reinforced failure mode behaviour without the composite layer; the calculation method of the normal section bearing
capacity of this mode was established.
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