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Steel Joist Manual

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SPECIFICATIONS FOR VULCRAFT SUPER LONGSPAN STEEL JOISTS SLH-SERIES<br />

203.4 MEMBERS<br />

(a) Chords<br />

The bottom chord shall be designed as an axially loaded<br />

tension member.<br />

The radius of gyration of the top chord about its vertical<br />

axis shall not be less than l/170 where l is the spacing in<br />

inches (millimeters) between lines of bridging as specified<br />

in Section 204.5(d)<br />

The top chord shall be considered as stayed laterally by<br />

the floor slab or roof deck provided the requirements of<br />

Section 204.9(e) of this specification are met.<br />

The top chord shall be designed as a continuous member<br />

subject to combined axial and bending stresses and shall<br />

be so proportioned that<br />

For LRFD:<br />

at the panel point:<br />

f au + f bu ≤ 0.9F y (203.4-1)<br />

at the mid panel: for ≥ 0.2,<br />

φ c F cr<br />

f au<br />

P u<br />

f bu<br />

f au +<br />

8<br />

φ c F cr 9<br />

( )<br />

f au<br />

2φ c F cr<br />

+<br />

1–<br />

f au<br />

for < 0.2,<br />

φ c F cr<br />

1–<br />

≤ 1.0 (203.4-2)<br />

≤ 1.0 (203.4-3)<br />

= P u /A = Required compressive stress, ksi (MPa)<br />

= Required axial strength using LRFD load combinations,<br />

kips (N)<br />

= M u /S = Required bending stress at the location<br />

under consideration, ksi (MPa)<br />

M u = Required flexural strength using LRFD load<br />

combinations, kip-in. (N-mm)<br />

S = Elastic Section Modulus, in. 3 (mm 3 )<br />

F cr = Nominal axial compressive stress in ksi (MPa)<br />

based on l/r as defined in Section 203.2(b)<br />

C m = 1 - 0.3 f au /φF' e for end panels<br />

C m = 1 - 0.4 f au /φF' e for interior panels<br />

F y = Specified minimum yield strength, ksi (MPa)<br />

F' e = π<br />

( 2 E<br />

) , ksi (MPa)<br />

2<br />

Kl<br />

r x<br />

Where l is the panel length,in inches (millimeters),<br />

as defined in Section 203.2(b) and r x is the radius<br />

of gyration about the axis of bending.<br />

Q = Form factor defined in Section 203.2(b)<br />

A = Area of the top chord, in. 2 , (mm 2 )<br />

For ASD:<br />

at the panel point:<br />

f a + f b ≤ 0.6F y (203.4-4)<br />

at the mid panel: for ≥ 0.2,<br />

f a<br />

( )<br />

+ 8<br />

F 1.67f a 9<br />

a<br />

F' e<br />

f a<br />

F a<br />

f au<br />

( ) C<br />

( m f b<br />

f a<br />

)<br />

+ 1.67f<br />

C m f a<br />

bu<br />

2F a<br />

Qφ b F y<br />

( )<br />

f au<br />

φ c F' e<br />

C m f ( ) bu<br />

f au<br />

φ c F' e<br />

Qφ b F y<br />

f a<br />

f a<br />

F a<br />

C m f b<br />

1– QF b<br />

for < 0.2,<br />

1– QF<br />

F' b<br />

e<br />

≤ 1.0 (203.4-5)<br />

≤ 1.0 (203.4-6)<br />

= P/A = Required compressive stress, ksi (MPa)<br />

P = Required axial strength using ASD load<br />

combinations, kips (N)<br />

f b = M/S = Required bending stress at the location under<br />

consideration, ksi (MPa)<br />

M = Required flexural strength using ASD load<br />

combinations, kip-in. (N-mm)<br />

S = Elastic Section Modulus, in. 3 (mm 3 )<br />

F a = Allowable axial compressive stress, based on l/r<br />

as defined in Section 203.2(b), ksi (MPa)<br />

F b = Allowable bending stress; 0.6F y , ksi (MPa)<br />

C m = 1 - 0.50 f a /F' e for end panels<br />

C m = 1 - 0.67 f a /F' e for interior panels<br />

(b) Web<br />

The vertical shears to be used in the design of the web<br />

members shall be determined from full uniform loading,<br />

but such vertical shears shall be not less than 25 percent<br />

of the end reaction.<br />

Interior vertical web members used in modified Warren<br />

type web systems shall be designed to resist the gravity<br />

loads supported by the member plus an additional axial<br />

load of 1 1 ⁄2 percent of the top chord axial force.<br />

84

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