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Building Design and Construction Handbook - Merritt - Ventech!

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7.76 SECTION SEVEN<br />

7.22 WEB OR FLANGE LOAD-BEARING<br />

STIFFENERS<br />

Members subject to large concentrated loads within their length or large end reactions<br />

should be proportioned so that the forces on the web or flange cannot cause<br />

local failure or the webs or flanges should be stiffened to carry the concentrated<br />

loads. Both ASD <strong>and</strong> LRFD procedures include design criteria.<br />

7.22.1 ASD for Load-Bearing Stiffeners<br />

Webs of rolled beams <strong>and</strong> plate girders should be so proportioned that the compressive<br />

stress, ksi, at the web toe of the fillets does not exceed<br />

F � 0.66F (7.45)<br />

a y<br />

where F y � specified minimum yield stress, ksi.<br />

Web failure probably would be in the form of buckling caused by concentrated<br />

loading, either at an interior load or at the supports. The capacity of the web to<br />

transmit the forces safely should be checked.<br />

FIGURE 7.35 Web crippling in a simple<br />

beam. The critical web section is assumed to<br />

occur at the fillet.<br />

Load Distribution. Loads are resisted<br />

not only by the part of the web directly<br />

under them but also by the parts immediately<br />

adjacent. A 45� distribution<br />

usually is assumed, as indicated in Fig.<br />

7.35 for two common conditions. The<br />

distance k is determined by the point<br />

where the fillet of the flange joins the<br />

web; it is tabulated in the beam tables<br />

of the AISC ‘‘Manual of Steel <strong>Construction</strong>.’’<br />

F a is applicable to the horizontal<br />

web strip of length b � k at the end<br />

support or b � 2k under an interior load.<br />

Bearing stiffeners are required when F a<br />

is exceeded.<br />

Bearing atop Webs. The sum of the compression stresses resulting from loads<br />

bearing directly on or through a flange on the compression edge of a plate-girder<br />

web should not exceed the following:<br />

When the flange is restrained against rotation, the allowable compressive stress,<br />

ksi, is<br />

� �<br />

4 10,000<br />

Fa � 5.5 � (7.46)<br />

2 2<br />

(a/h) (h/t)<br />

When the flange is not restrained against rotation,<br />

� �<br />

4 10,000<br />

Fa � 2 � (7.47)<br />

2 2<br />

(a/h) (h/t)

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