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Building Design and Construction Handbook - Merritt - Ventech!

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5.94 SECTION FIVE<br />

joints by the actual unbalanced moments at those joints divided by 1000, <strong>and</strong> summing<br />

(see also Art. 5.11.9 <strong>and</strong> Table 5.6).<br />

5.11.9 Procedure for Sidesway<br />

Computations of moments due to sidesway, or drift, in rigid frames is conveniently<br />

executed by the following method:<br />

1. Apply forces to the structure to prevent sidesway while the fixed-end moments<br />

due to loads are distributed.<br />

2. Compute the moments due to these forces.<br />

3. Combine the moments obtained in Steps 1 <strong>and</strong> 2 to eliminate the effect of the<br />

forces that prevented sidesway.<br />

Suppose the rigid frame in Fig. 5.77<br />

is subjected to a 2000-lb horizontal load<br />

acting to the right at the level of beam<br />

BC. The first step is to compute the moment-influence<br />

factors (Table 5.6) by<br />

applying moments of �1000 at joints B<br />

<strong>and</strong> C, assuming sidesway prevented.<br />

Since there are no intermediate loads<br />

on the beams <strong>and</strong> columns, the only<br />

fixed-end moments that need be considered<br />

are those in the columns resulting<br />

from lateral deflection of the frame<br />

caused by the horizontal load. This deflection,<br />

however is not known initially.<br />

FIGURE 5.77 Rigid frame.<br />

So assume an arbitrary deflection, which<br />

produces a fixed-end moment of<br />

�1000M at the top of column CD. M is an unknown constant to be determined<br />

from the fact that the sum of the shears in the deflected columns must be equal to<br />

the 2000-lb load. The same deflection also produces a moment of �1000M at the<br />

bottom of CD [see Eq. (5.126)].<br />

From the geometry of the structure, furthermore, note that the deflection of B<br />

relative to A is equal to the deflection of C relative to D. Then, according to Eq.<br />

(5.126) the fixed-end moments in the columns are proportional to the stiffnesses of<br />

TABLE 5.6 Moment-Influence Factors<br />

for Fig. 5.77<br />

Member �1000 at B �1000 at C<br />

AB<br />

BA<br />

BC<br />

CB<br />

CD<br />

DC<br />

351<br />

702<br />

298<br />

70<br />

�70<br />

�35<br />

�105<br />

�210<br />

210<br />

579<br />

421<br />

210

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