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Structural Concrete - Hassoun

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658 Chapter 17 Design of Two-Way Slabs<br />

and y 2 = 15 in.<br />

(<br />

C =<br />

1 − 0.63 × 12<br />

22<br />

= 9528 in. 4<br />

β t = E cb C<br />

2E cs I s<br />

= 9528<br />

2 × 6860 = 0.69<br />

) ( )<br />

12 3 (<br />

× 22<br />

+ 1 − 0.63 × 7<br />

3<br />

15<br />

) ( )<br />

7 3 × 15<br />

3<br />

a. Distribute the interior negative moment, M ni : Referring to Table 17.5 and by interpolation, the<br />

percentage of moment assigned to the column strip (for l 2 /l 1 = 0.83 and α f1 l 2 /l 1 > 1.0 is 80%).<br />

Column strip = 0.8 × 254.8 =−203.8K⋅ ft<br />

Middle strip = 0.2 × 254.8 =−51.0K⋅ ft<br />

Because α f1<br />

l 2 ∕l 1 > 1.0, 85% of the moment in the column strip is assigned to the beam. Therefore,<br />

Beam = 0.85 × 203.8 =−173.3K⋅ ft<br />

Column strip = 0.15 × 203.18 =−30.6K⋅ ft<br />

Middle strip =−51.0K⋅ ft<br />

b. Distribute the positive moment, M p : Referring to Table 17.5 and by interpolation, the percentage<br />

of moment assigned to the column strip is 80% (85% of this value is assigned to the beam).<br />

Therefore,<br />

Beam =(0.85)(0.8 × 207.5) =+141.1K⋅ ft<br />

Column strip =(0.15)(0.8 × 207.5) =24.9K⋅ ft<br />

Middle strip = 0.2 × 207.5 =+41.5K⋅ ft<br />

c. Distribute the exterior negative moment, M ne : Referring to Table 17.5 and by interpolation,<br />

the percentage of moment assigned to the column strip (for l 2 /l 1 = 0.83, α f1 l 2 /l 1 > 1.0, and<br />

β t = 0.69) is 94%, and 85% of the moment is assigned to the beam. Therefore,<br />

Beam =(0.85)(0.94 × 58.2) =−46.5K⋅ ft<br />

Column strip =(0.15)(0.94 × 58.2) =−8.2K⋅ ft<br />

Middle strip = 0.06 × 58.2 =−3.5K⋅ ft<br />

17.9 DESIGN MOMENTS IN COLUMNS<br />

When the analysis of the equivalent frames is carried out by the direct design method, the moments<br />

in columns due to the unbalanced loads on adjacent panels are obtained from the following equation,<br />

which is specified by the ACI Code, Section 8.10.7.2:<br />

M u = 0.07[(q Du + 0.5q Lu )l 2 l 2 n − q ′ Du l′ 2 (l′ n) 2 ]<br />

(17.22a)<br />

If the modified stiffness method using K ec and α ec is used, then the moment M u is computed as<br />

follows:<br />

M u = 0.08[(q Du + 0.5q Lu )l 2 l 2 n − q ′ Du l′ 2 (l′ n) 2 ]<br />

1 + 1∕α ec<br />

(17.22b)

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