Adjustment Factors

ADJUSTMENT FACTORS FOR DESIGN VALUES

Design values obtained by the methods described earlier should be multiplied by adjustment factors based on conditions of use, geometry, and stability. The adjustments are cumulative, unless specifically indicated in the following:
The adjusted design value Fb‘ for extreme-fiber bending is given by

Fb‘=FbCDCMCtCLCFCVCfuCrCcCf

where
Fb= design value for extreme-fiber bending
CD= load-duration factor
CM =wet-service factor
CCt =temperature factor

CL =beam stability factor

CF =size factor—applicable only to visually graded, sawn lumber and round timber flexural members

Cv =volume factor—applicable only to glued- laminated beams

Cfu= flat-use factor—applicable only to dimension- lumber beams 2 to 4 in (50.8 to 101.6 mm) thick and glued-laminated beams

Cr= repetitive-member factor—applicable only to dimension-lumber beams 2 to 4 in (50.8 to101.6 mm) thick

Cc =curvature factor—applicable only to curved portions of glued-laminated beams

Cf =form factor

For glued-laminated beams, use eitherCL or Cc (whichever is smaller), not both.
The adjusted design value for tension Ft‘ is given by

Ft‘= FtCDCMCtCF

where
Ft is the design value for tension.

For shear, the adjusted design value Fv‘ is computed from

Fv‘=FvCDCMCtCH

where
Fv is the design value for shear and CH is the shear stress factor ?1—permitted for Fvparallel to the grain for sawn lumber members.

For compression perpendicular to the grain, the adjusted

design value Fc1‘is obtained from

Fc1‘= Fc1CDCtCb

where
Fc1is the design value for compression perpendicular to the grain and Cb is the bearing area factor.

For compression parallel to the grain, the adjusted design

value isFc

given by

Fc‘= FcCDCMCtCFCp

where
Fc is the design value for compression parallel to grain and Cp is the column stability factor.

For end grain in bearing parallel to the grain, the adjusted design value, Fg‘ is computed from

Fg‘= FgCDCt

where
Fg is the design value for end grain in bearing parallel to the grain.
The adjusted design value for modulus of elasticity, E’ is obtained from

E’= ECMCTC..

where E= design value for modulus of elasticity

CT= buckling stiffness factor—applicable only to sawn-lumber truss compression chords 2*4 in(50.8*101.6 mm) or smaller, when subject to combined bending and axial compression and plywood sheathing 3 /8 in (9.5 mm) or more thick is nailed to the narrow face

C..= other appropriate adjustment factors

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