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Structural Concrete - Hassoun

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780 Chapter 19 Introduction to Prestressed <strong>Concrete</strong><br />

SUMMARY<br />

Section 19.1<br />

The main objective of prestressing is to offset or counteract all or most of the tensile stresses in a<br />

structural member produced by external loadings, thus giving some advantages over a reinforced<br />

concrete member. A concrete member may be pretensioned or posttensioned. Nonprestressed reinforcement<br />

may also be added to the concrete member to increase its ultimate strength.<br />

Section 19.2<br />

1. The allowable stresses in concrete at transfer are<br />

Maximum compressive stress = 0.6 f ′ ci<br />

Maximum compressive stress at end of simply supported beam = 0.7 f ′ ci<br />

√<br />

Maximum tensile stress = 3 f ′ ci<br />

√<br />

Maximum tensile stress at end of simply supported beam = 6<br />

The allowable stresses after all losses are 0.45 f ′ c for compression and 6 f ′ c for tension.<br />

2. The allowable stress in a pretensioned tendon at transfer is the smaller of 0.74 f pu or 0.82<br />

f py . The maximum stress due to the tendon jacking force must not exceed 0.85 f pu or 0.94<br />

f py ; and the maximum stress in a posttensioned tendon after the tendon is anchored is<br />

0.70 f pu .<br />

Section 19.3<br />

The sources of prestress loss are the elastic shortening, shrinkage, and creep of concrete; relaxation<br />

of steel tendons; and friction. An approximate lump-sum loss is 35 ksi for pretensioned members<br />

and 25 ksi for posttensioned members (friction is not included).<br />

Loss due to elastic shortening = nF i<br />

A c<br />

(Eq. 19.1)<br />

Loss due to shrinkage = ε sh E s (Eq. 19.6)<br />

Loss due to creep = C c (ε c E s ) (Eq. 19.7)<br />

Loss due to relaxation of steel varies between 2.5 and 12%. Loss due to friction in posttensioned<br />

members stems from the curvature and wobbling of the tendon.<br />

{<br />

P<br />

P px = pj e −(kl px+μ p α px )<br />

(Eq.19.10)<br />

P pj (1 + Kl px + μ p α px ) −1<br />

(Eq.19.11)<br />

Section 19.4<br />

Elastic stresses in a flexural member due to loaded and unloaded conditions are given by Eqs.<br />

19.13 through 19.16. The limiting values of the eccentricity, e, are given by Eqs. 19.20, 19.22,<br />

19.24, and 19.26. The minimum and maximum values of F i are given by Eqs. 19.31 and Eqs.<br />

19.32, respectively.<br />

f ′ ci

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