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Building Design and Construction Handbook - Merritt - Ventech!

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STRUCTURAL STEEL CONSTRUCTION 7.81<br />

r b � corresponding radius of gyration, in<br />

K � effective-length factor in the plane of bending<br />

C m � reduction factor determined from the following conditions:<br />

1. For compression members in frames subject to joint translation (sidesway),<br />

C m � 0.85.<br />

2. For restrained compression members in frames braced against joint translation<br />

<strong>and</strong> not subject to transverse loading between their supports in the plane of bending,<br />

C m � 0.6 � 0.4M 1/M 2, but not less than 0.4. M 1/M 2 is the ratio of the smaller to<br />

larger moments at the ends of that portion of the member unbraced in the plane of<br />

bending under consideration. M 1/M 2 is positive when the member is bent in reverse<br />

curvature, <strong>and</strong> negative when it is bent in single curvature.<br />

3. For compression members in frames braced against joint translation in the<br />

plane of loading <strong>and</strong> subjected to transverse loading between their supports, the<br />

value of C m may be determined by rational analysis. Instead, however, C m may be<br />

taken as 0.85 for members whose ends are restrained, <strong>and</strong> 1.0 for ends unrestrained.<br />

In wind <strong>and</strong> seismic design may be increased one-third. The resultant section,<br />

F� e<br />

however, should not be less than that required for dead <strong>and</strong> live loads alone without<br />

the increase in allowable stress.<br />

Additional information, including illustrations of the foregoing three conditions<br />

for determining the value of C m, is given in the AISC ‘‘Commentary’’ on the AISC<br />

ASD ‘‘Specification for Structural Steel for <strong>Building</strong>s.’’<br />

7.24.2 LRFD for Compression <strong>and</strong> Bending<br />

Members subject to both axial compression <strong>and</strong> bending stresses should be proportioned<br />

to satisfy Eq. (7.58) or (7.59), whichever is applicable.<br />

For (P u/� cP n) � 0.2,<br />

For (P u/� cP n) � 0.2,<br />

� �<br />

P 8 M M<br />

u ux uy<br />

� � � 1.0 (7.58)<br />

� P 9 � M � M<br />

c n b nx b ny<br />

� �<br />

P M M<br />

u ux uy<br />

� � � 1.0 (7.59)<br />

2� P � M � M<br />

c n b nx b ny<br />

where P u � required compressive strength, kips, calculated for the factored axial<br />

loads<br />

M u � required flexural strength, kip-in calculated for primary bending <strong>and</strong><br />

P-� effects<br />

� cP n � design compressive strength (Art. 7.19.3)<br />

� bM n � design flexural strength (Art. 7.20.2)<br />

M u may be determined for the factored loads from a second-order elastic analysis.<br />

The AISC LRFD specification, however, permits M u to be determined from<br />

Eq. (7.60) with the variables in this equation determined from a first-order analysis.<br />

M � BM � BM (7.60)<br />

u 1 nt 2 lt

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