Fiber reinforced polymer(FRP) have unique advantages like high strength to weight ratio, excellent corrosion resistance, improving deformability and cost effectiveness. These advantages have gained wide acceptance in civil engineering applications. FRP tendons for prestressing applications are emerging as one of the most promising technologies in the civil engineering industry. However, the behavior of such members under the influence of elevated temperatures is still unknown. The knowledge and application of this could lead to a cost effective and practical considerations in fire safety design. Therefore, this study examines the deflection behavior of the carbon fiber reinforced polymer(CFRP) prestressed concrete beam at elevated temperatures. In this article, an analytical model is developed which integrates the temperature dependent changes of effective modulus of FRP in predicting the deflection behavior of CFRP prestressed concrete beams within the range of practical temperatures. This model is compared with a finite element mode (FEM) of a simply supported concrete beam prestressed with CFRP subjected to practical elevated temperatures. In addition, comparison is also made with an indirect reference to the real behavior of the material. The results of the model correlated reasonably with the finite element model and the real behavior. Finally, a practical application is provided.
. [J]. Frontiers of Structural and Civil Engineering, 2019, 13(1): 81-91.
Mohammed FARUQI, Mohammed Sheroz KHAN. Deflection behavior of a prestressed concrete beam reinforced with carbon fibers at elevated temperatures. Front. Struct. Civ. Eng., 2019, 13(1): 81-91.
= Young’s modulus of prestressed FRP composite at elevated temperatures
= Concrete stresses at top surface
= Concrete stresses at bottom surface
= Compressive strength of concrete
= Stress in the prestressed system
= Modulus of rupture
I= Moment of inertia
= Cracking moment of inertia
= Effective moment of inertia
= Gross moment of inertia
= Support conditions of the system
L= Span of the beam
l= Original length
M= Moment
= Mid-span moment due to dead load
= Applied moment
= Cracking moment
= Mid-span moment due to live load
P= Prestress force
= Effective prestress force
= Initial prestress force
r= Strength reduction factor due to elevated temperature
= Radius of gyration
= Reaction at support
= Reaction at support
= Section modulus at top fiber
= Section modulus at bottom fiber
= Temperature at which the deflecton is calculated
= Volume fraction of fiber
= Volume fraction of matrix
w= Uniformly distributed superimposed load
= Live load acting on the beam
= Dead load acting on the beam
W= Self weight of the beam
x= Distance of NA from top surface
= Distance from center of gravity of beam to extreme fibers
= CFRP expansion per degree temperature of variation
= Coefficient of thermal expansion of fiber
= Coefficient of thermal expansion of matrix
= Coefficient of thermal expansion of frp composite in longitudinal direction
= Deflection from ANSY
= Deflection due to elevated temperature
= Modular ratio
= Stress
= Strain
= Strain in concrete due to shrinkage
= Shrinkage curvature due to elevated temperatures
= Deflection constant
= Poisson’s ratio
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