24.02.2017 Views

Structural Concrete - Hassoun

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

19.4 Analysis of Flexural Members 747<br />

e = K b = Lower kern<br />

e′ = K t = Upper kern<br />

Figure 19.5<br />

Kern points: (a) lower,(b) upper, and (c) central.<br />

compressive stress at the extreme bottom fibers. The stress at the top fibers is<br />

σ t =− F i<br />

A + (F ie)y t<br />

= 0<br />

I<br />

e = K b = lower Kern =<br />

I<br />

(19.17)<br />

Ay t<br />

Similarly, if the prestressing force is applied at an eccentricity e ′ above the centroid such that<br />

the stress at the bottom fibers is equal to 0, that prestressing force is considered acting at the upper<br />

Kern point (Fig. 19.5). In this case the eccentricity e ′ is denoted by K t , and the stress distribution<br />

is triangular, with maximum compressive stress at the extreme top fibers. The stress at the bottom<br />

fibers is<br />

σ b =− F i<br />

A + (F ie ′ )y b<br />

= 0<br />

I<br />

e ′ = K t = upper Kern =<br />

I<br />

(19.18)<br />

Ay b<br />

The Kern limits of a rectangular section are shown in Fig. 19.5.<br />

19.4.3 Limiting Values of Eccentricity<br />

The four stress equations, Eqs. 19.13 through 19.16, can be written as a function of the eccentricity<br />

e for the various loading conditions. For example, Eq. 19.13 can be rewritten as follows:<br />

(f i e)y t<br />

I<br />

σ ti =− F i<br />

A + (F ie)y t<br />

− M Dy t<br />

I I<br />

≤ f ti + F i<br />

A + M Dy t<br />

I<br />

I<br />

(<br />

Fi<br />

F i y t A + M )<br />

Dy t<br />

+ f<br />

I ti<br />

e ≤<br />

≤ f ti<br />

(19.19)

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!