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Building Design and Construction Handbook - Merritt - Ventech!

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STRUCTURAL THEORY 5.105<br />

Wall A: 6.6 � 0.7 � 7.3 kips<br />

Wall B: 4.4 � 0.1 � 4.5 kips<br />

Wall C: kips<br />

5.12.3 Deflections of Bents or Shear Walls<br />

When parallel bents or shear walls are connected by rigid diaphragms (Art. 5.12.1)<br />

<strong>and</strong> horizontal loads are distributed to the vertical resisting elements in proportion<br />

to their relative rigidities, the relative rigidity of the framing depends on the combined<br />

horizontal deflections due to shear <strong>and</strong> flexure. For the dimensions of lateralforce-resisting<br />

framing used in many high-rise buildings, however, deflections due<br />

to flexure greatly exceed those due to shear. In such cases, only flexural rigidity<br />

need be considered in determination of relative rigidity of the bents <strong>and</strong> shear walls<br />

(Art. 5.12.5).<br />

Horizontal deflections can be determined by treating the bents <strong>and</strong> shear walls<br />

as cantilevers. Deflections of braced bents can be calculated by the dummy-unitload<br />

method (Art. 5.10.4) or a matrix method (Art. 5.13.3). Deflections of rigid<br />

frames can be obtained by summing the drifts of the stories, as determined by<br />

moment distribution (Art. 5.11.9) or a matrix method. And deflections of shear<br />

walls can be computed from formulas given in Art. 5.5.15, the dummy-unit-load<br />

method, or a matrix method.<br />

For a shear wall with a solid, rectangular cross section, the flexural deflection<br />

at the top under uniform loading is given by the formula for a cantilever in Fig.<br />

5.39:<br />

4 wH<br />

�c � (5.142)<br />

8EI<br />

where w � uniform lateral load<br />

H � height of the wall<br />

E � modulus of elasticity of the wall material<br />

I � moment of inertia of wall cross section � tL3 /12<br />

t � wall thickness<br />

L � length of wall<br />

The cantilever shear deflection under uniform loading may be computed from<br />

2 0.6wH<br />

�v � (5.143)<br />

EA<br />

where Ev � modulus of rigidity of wall cross section<br />

� E/2(1 � �)<br />

� � Poisson’s ratio for the wall material (0.25 for concrete <strong>and</strong> masonry)<br />

A � cross-sectional area of the wall � tL<br />

The total deflection then is<br />

3<br />

1.5wH H H<br />

�c � �v � �� � � �<br />

(5.144)<br />

Et L L<br />

For a cantilever wall subjected to a concentrated load P at the top, the flexural<br />

deflection at the top is<br />

v

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