ASD/LRFD Manual - American Wood Council
ASD/LRFD Manual - American Wood Council
ASD/LRFD Manual - American Wood Council
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<strong>ASD</strong>/<strong>LRFD</strong> MANUAL FOR ENGINEERED <strong>Wood</strong> Construction<br />
145<br />
M16.2 Design Procedures for Exposed <strong>Wood</strong> Members<br />
For members stressed in one principle direction, simplifications<br />
can be made which allow the tabulation of load<br />
factor tables for fire design. These load factor tables can<br />
be used to determine the structural design load ratio, R s , at<br />
which the member has sufficient capacity for a given fire<br />
endurance time. This section provides the rational used to<br />
develop the load ratio tables provided later in this section<br />
(Tables M16.2-1 through M16.2-10). For more complex<br />
calculations where stress interactions must be considered,<br />
use the provisions of AF&PA’s Technical Report 10 with<br />
the appropriate NDS provisions.<br />
Bending Members (Tables M16.2-1<br />
through M16.2-2)<br />
Load ratio tables were developed for standard reference<br />
conditions where: C D = 1.0; C M = 1.0; C t = 1.0; C L-f<br />
= 1.0<br />
The calculation of C L-s and C L-f require the designer<br />
to consider both the change in bending section relative<br />
to bending strength and the change in buckling stiffness<br />
relative to buckling strength. While these relationships can<br />
be directly calculated using NDS provisions, they can not<br />
be easily tabulated. However, for most beams exposed on<br />
three sides, the beams are braced on the protected side.<br />
For long span beams exposed on four sides, the beam<br />
failure is influenced by buckling due to lateral instability.<br />
When buckling is considered, the following equations<br />
should be used:<br />
Structural: D+L R s F b S s C L-s C D C M C t<br />
Structural (buckling): D+L R s E min I yy-s / < e C M C t<br />
Fire:<br />
D+L 2.85 F b S f C L-f<br />
Fire (buckling):<br />
D+L 2.03 E min I yy-f / < e<br />
where:<br />
where:<br />
D = Design dead load<br />
D = Design dead load<br />
L = Design live load<br />
L = Design live load<br />
R s = Design load ratio<br />
R s = Design load ratio (buckling)<br />
F b = Tabulated bending design value<br />
S s = Section modulus using full crosssection<br />
dimensions<br />
S f = Section modulus using cross-section<br />
dimensions reduced from fire exposure<br />
C L-s = Beam stability factor using full crosssection<br />
dimensions<br />
C L-f = Beam stability factor using crosssection<br />
dimensions reduced from fire<br />
exposure<br />
C D = Load duration factor<br />
C M = Wet service factor<br />
C t = Temperature factor<br />
E min = Reference modulus of elasticity for<br />
beam stability calculations<br />
I yy-s = Lateral moment of inertia using full<br />
cross-section dimensions<br />
I yy-f = Lateral moment of inertia using<br />
cross-section dimensions reduced from<br />
fire exposure<br />
R s =<br />
C M = Wet service factor<br />
C t = Temperature factor<br />
2.03 I<br />
yy- f<br />
I C C<br />
yy-s M t<br />
(M16.2-2)<br />
M16: FIRE DESIGN<br />
Solve for R s :<br />
R s =<br />
2.85 S f C L- f<br />
S C C C C<br />
s L-s D M t<br />
(M16.2-1)<br />
16<br />
<strong>American</strong> Forest & paper association