AISCAISC 360-22
Appendix 8 Approximate analysis

8.2approximate inelastic moment redistribution

PDF page 354 · AISC 360-22

The required flexural strength of indeterminate beams composed of compact sections, as defined in Section B4.1, carrying gravity loads only, and satisfying the unbraced length requirements provided in this section, is permitted to be taken as nine-tenths of the negative moments at the points of support, produced by the gravity loading and determined by an elastic analysis satisfying the requirements of Chapter C, provided that the maximum positive moment is increased by one-tenth of the average negative moment determined by an elastic analysis. This moment redistribution is not permitted for moments in members with FyF_{y} exceeding 65 ksi (450 MPa), for moments produced by loading on cantilevers, for design using partially restrained (PR) moment connections, or for design by inelastic analysis using the provisions of Appendix 1.3. This moment redistribution is permitted for design according to Section B3.1 (LRFD) and for design according to Section B3.2 (ASD). The required axial strength shall not exceed 0.15ϕcFyAg0.15 \phi_{c} F_{y} A_{g} for LRFD or 0.15FyAg/Ωc0.15 F_{y} A_{g} / \Omega_{c} for ASD, where ϕc\phi_{c} and Ωc\Omega_{c} are determined from Section E1, Ag=A_{g}= gross area of member, in. 2{ }^{2} (mm2)\left(\mathrm{mm}^{2}\right), and Fy=F_{y}= specified minimum yield stress, ksi (MPa).

The laterally unbraced length, LbL_{b}, of the compression flange adjacent to the redistributed end moment locations shall not exceed LmL_{m} determined as follows.

  • (a) For doubly symmetric and singly symmetric I-shaped beams with IycI_{y c} of the compression flange equal to or larger than IytI_{y t} of the tension flange loaded in the plane of the web
Lm=[0.12+0.076(M1M2)](EFy)ryL_{m}=\left[0.12+0.076\left(\frac{M_{1}}{M_{2}}\right)\right]\left(\frac{E}{F_{y}}\right) r_{y}

(A-8-9)

  • (b) For solid rectangular bars and for rectangular HSS and symmetric box beams bent about their major axis
Lm=[0.17+0.10(M1M2)](EFy)ry0.10(EFy)ryL_{m}=\left[0.17+0.10\left(\frac{M_{1}}{M_{2}}\right)\right]\left(\frac{E}{F_{y}}\right)_{r_{y}} \geq 0.10\left(\frac{E}{F_{y}}\right)_{r_{y}}

(A-8-10)

where

Fy=F_{y}= specified minimum yield stress of the compression flange, ksi (MPa)

M1=M_{1}= smaller moment at end of unbraced length, kip-in. (N-mm)

M2=M_{2}= larger moment at end of unbraced length, kip-in. (N-mm)

(

ry= radius of gyration about y-axis, in. (mm) (M1/M2) is positive when moments cause re \begin{aligned} r_{y} & =\text { radius of gyration about } y \text {-axis, in. (mm) } \\ \left(M_{1} / M_{2}\right) & \text { is positive when moments cause re }\end{aligned}

(M1/M2)\left(M_{1} / M_{2}\right) is positive when moments cause reverse curvature and negative for single curvature

There is no limit on LbL_{b} for members with round or square cross sections or for any beam bent about its minor axis.

COMMENTARY on the Specification for Structural Steel Buildings

August 1, 2022

(The Commentary is not a part of ANSI/AISC 360-22, Specification for Structural Steel Buildings, but is included for informational purposes only.)

INTRODUCTION

The Specification is intended to be complete for normal design usage.

The Commentary furnishes background information and references for the benefit of the design professional seeking further understanding of the basis, derivations, and limits of the Specification.

The Specification and Commentary are intended for use by design professionals with demonstrated engineering competence.

COMMENTARY SYMBOLS

The Commentary uses the following symbols in addition to the symbols defined in the Specification. The section number in the right-hand column refers to the Commentary sec- tion where the symbol is first used.

SymbolDefinitionSection
ArArea of properly developed slab reinforcement parallel to the steel beam and within the effective width of the slab, in.2 (mm2) I3.2b
BOverall width of rectangular HSS, in. (mm)I3
CCompression force in the concrete slab, kips (N)I3.2a
CfCompression force in concrete slab for fully composite beam;
smaller of FyAs and 0.85f'Ac, kips (N)
I3.2
DHeat perimeter, in. (mm)App. 4.2.2
FyReported yield stress, ksi (MPa)App. 5.2.2
FyrSpecified minimum yield stress of the slab reinforcement, ksi (MPa) I3.2b
FysStatic yield stress, ksi (MPa)App. 5.2.2
HOverall height of rectangular HSS, in. (mm)I3
HHeight of anchor, in. (mm)I8.2
ILBLower-bound moment of inertia, in.4 (mm4)I3.2
InegEffective moment of inertia for negative moment, in.4 (mm4)I3.2
IpMoment of inertia of the steel faceplates, in.4 (mm4)I1.6b
IposEffective moment of inertia for positive moment, in.4 (mm4)I3.2
IsMoment of inertia for the structural steel section, in.4 (mm4)I3.2
ItrMoment of inertia for fully composite uncracked transformed section, in.4 (mm4) I3.2
IwMoment of inertia for the major principal axis, in.4 (mm4)Table C-F10.1
Iy TopMoment of inertia of the top flange about an axis through the web, in.4 (mm4) F1
KsSecant stiffness, kip-in. (N-mm)B3.4
LUnbraced member length of steel encasement, in. (mm)I2.2a
LcLength of anchor, in. (mm)I8.2b
MCDesign flexural strength at point C", determined in accordance with Section 13, kip-in. (N-mm) I5
MCAllowable flexural strength at point C", determined in accordance with Section 13, kip-in. (N-mm) I5
MCLMoment at the middle of the unbraced length, kip-in. (N-mm)F1
MsMoment at service loads, kip-in. (N-mm)B3.4
MTTorsional moment, kip-in. (N-mm)G3
Ma1Sum of the moments due to the nominal lateral loads and the moments due to the nominal gravity loads on the windward side of the connection, kip-in. (N-mm) J10.6
Ma1GMoment due to the nominal gravity loads on the windward side of the connection, kip-in. (N-mm) J10.6
SymbolDefinitionSection
Ma1LMoment due to the nominal lateral loads on the windward side of the connection, kip-in. (N-mm)J10.6
Ma2Difference between the moments due to the nominal lateral loads and the moments due to the nominal gravity loads on the leeward side of the connection, kip-in. (N-mm)J10.6
Ma2GMoment due to the nominal gravity loads on the leeward side of the connection, kip-in. (N-mm)J10.6
Ma2LMoment due to the nominal lateral loads on the leeward side of the connection, kip-in. (N-mm)J10.6
MoMoment at end of unbraced length that gives the largest compressive stress in the bottom flange, kip-in. (N-mm)F1
MoMaximum first-order moment within the member due to the transverse loading, kip-in. (N-mm)App. 8
Mu1Sum of the moments due to the factored lateral loads and the moments due to the factored gravity loads on the windward side of the connection, kip-in. (N-mm)J10.6
Mu1GMoment due to the factored gravity loads on the windward side of the connection, kip-in. (N-mm)J10.6
Mu1LMoment due to the factored lateral loads on the windward side of the connection, kip-in. (N-mm)J10.6
Mu2Difference between the moments due to the factored lateral loads and the moments due to the factored gravity loads on the leeward side of the connection, kip-in. (N-mm)J10.6
Mu2GMoment due to the factored gravity loads on the leeward side of the connection, kip-in. (N-mm)J10.6
Mu2LMoment due to the factored lateral loads on the leeward side of the connection, kip-in. (N-mm)J10.6
M1Moment at other end of unbraced length, kip-in. (N-mm)F1
NNumber of cycles to failureApp. 3.3
PADesign axial compressive strength at point A″ in Figure C-15.3, determined in accordance with Section I2, kips (N)I5
PAAllowable compressive strength at point A″ in Figure C-15.3, determined in accordance with Section I2, kips (N)I5
PcDesign axial compressive strength at point C″, kips (N)I5
PcAllowable axial compressive strength at point C″, kips (N)I5
PbrRequired brace strength, kips (N)App. 6.1
PnNominal axial tensile strength, kips (N)I6.2
PrRequired external tensile force applied to the composite member, kips (N)I6.2
PyTensile strength of steel section, kips (N)I3.2a
PycCompressive strength of steel section, kips (N)I3.2b
mMean value of the load effect Q̅B3.1
QyFirst moment of the area of one component about the y-axis, in.³ (mm³)E6.1
RRadius of fillet between the flange and web of channel anchor, in. (mm)I8.2b
RcapMinimum rotation capacityApp. 1.3.1
SymbolDefinitionSection
RmMean value of the resistance RB3.1
SBStefan-Boltzmann constantApp. 4.2.2
SrStress rangeApp. 3.3
SsSection modulus for the structural steel section, referred to the tension flange, in.³ (mm³)I3.2
StrSection modulus for the fully composite uncracked transformed section, referred to the tension flange of the steel section, in.³ (mm³)I3.2
TFTemperature of the fire, °F (°C)App. 4.2.2
TsTemperature of the steel, °F (°C)App. 4.2.2
VQCoefficient of variation of the load effect QB3.1
VRCoefficient of variation of the resistance RB3.1
VbComponent of the shear force parallel to the angle leg with width b and thickness t, kips (N)G3
V'Required longitudinal shear force to be transferred to the steel section or longitudinal reinforcement, kips (N)I6.2
WWeight (mass) per unit length, lb/ft (kg/m)App. 4.2.2
aHeat transfer coefficient, Btu/(ft²-s-°F) (W/m²-°C)App. 4.2.2
aBracing offset measured from the shear center in x-direction, in. (mm)E4
acConvective heat transfer coefficientApp. 4.2.2
acrNeutral axis location for force equilibrium, slender section, in. (mm)13.4
apNeutral axis location for force equilibrium, compact section, in. (mm)13.4
arRadiative heat transfer coefficientApp. 4.2.2
ayNeutral axis location for force equilibrium, noncompact section, in. (mm)13.4
bBracing offset measured from the shear center in y-direction, in. (mm)E4
bShorter overall outside width of rectangular cross section, in. (mm)I2.2a
bEffective width of concrete slab, in. (mm)I3.2a
bcShorter inner width of rectangular cross section, in. (mm)I2.2a
csSpecific heat of the steel, Btu/lb-°F (J/kg-°C)App. 4.2.2
dm1, dm2Distance between flange forces in the moment connection, in. (mm)J10.6
d1Distance from the centroid of the compression force in the concrete slab to the top of the steel section, in. (mm)I3.2a
d1Distance from the centroid of the longitudinal slab reinforcement to the top of the steel section, in. (mm)I3.2b
d2Distance from the centroid of the compression force in the steel section to the top of the steel section, in. (mm)I3.2a
d2Distance from the centroid of the tension force in the steel section to the top of the steel section, in. (mm)I3.2b
d3Distance from the resultant steel tension force for full section tension yield to the top of the steel, in. (mm)I3.2
d3Distance from Py to the top of the steel section, in. (mm)I3.2a
fCritical stress when slender element is not considered, ksi (MPa)E7.1
fvShear stress in angle, ksi (MPa)G3
hLonger overall outside width of rectangular cross section, in. (mm)I2.2a
hcShorter inner width of rectangular cross section, in. (mm)I2.2a
SymbolDefinitionSection
kPlate buckling coefficient characteristic of the type of plate edge-restraintE7.1
pHydrostatic pressure, ksi (MPa)I2.2a
q″Net heat flux incident on the steel member, Btu/s-ft-in. (J/s-m²)App.4.2.2
stTie bar spacing, in.4 (mm4)I1.6b
tThickness of wall, in. (mm)I2.2a
tfThickness of channel anchor flange, in. (mm)I8.2b
twThickness of channel anchor web, in. (mm)I8.2b
zoCoordinate along the z-axis of the shear center with respect to the centroid, in. (mm)Table C-F10.1
ΩBSafety factor for bearing on concreteI6.3a
αpRatio of the flexural stiffness of the steel plate to the flexural stiffness of the tie barI1.6b
βReliability indexB3.1
βBrace stiffness, kip/in. (N/mm)App. 6.1
βactActual bracing stiffness provided, kip/in. (N/mm)App. 6.1
δoMaximum deflection due to transverse loading, in. (mm)App. 8
εFEmissivity of the fire and view coefficientApp. 4.2.2
θSRotation at service loads, radB3.4
vPoisson's ratioE7.1
φBResistance factor for bearing on concreteI6.3a
ωEmpirical adjustment factorE4

COMMENTARY GLOSSARY

The Commentary uses the following terms in addition to the terms defined in the Glossary of the Specification.

  • Alignment chart. Nomograph for determining the effective length factor, K, for some types of columns.

Biaxial bending. Simultaneous bending of a member about two perpendicular axes.

Brittle fracture. Abrupt cleavage with little or no prior ductile deformation.

  • Column curve. Curve expressing the relationship between axial column strength and slenderness ratio.

  • Critical load. Load at which a perfectly straight member under compression may either assume a deflected position or may remain undeflected, or a beam under flexure may either deflect and twist out-of-plane or remain in its in-plane deflected position, as determined by a theoretical stability analysis.

  • Drift damage index. Parameter used to measure the potential damage caused by interstory drift.

  • Effective moment of inertia. Moment of inertia of the cross section of a member that remains elastic when partial plastification of the cross section takes place, usually under the combination of residual stress and applied stress; also, the moment of inertia based on effective widths of elements that buckle locally; also, the moment of inertia used in the design of partially composite members.

  • Effective stiffness. Stiffness of a member computed using the effective moment of inertia of its cross section.

  • Fatigue threshold. Stress range at which fatigue cracking will not initiate regardless of the number of cycles of loading.

  • First-order plastic analysis. Structural analysis based on the assumption of rigid-plastic behavior—in other words, that equilibrium is satisfied throughout the structure and the stress is at or below the yield stress—and in which equilibrium conditions are formulated on the undeformed structure.

  • Flexible connection. Connection permitting a portion, but not all, of the simple beam rotation of a member end.

  • Inelastic action. Material deformation that does not disappear on removal of the force that produced it.

  • Interstory drift. Lateral deflection of a floor relative to the lateral deflection of the floor immediately below, divided by the distance between floors, (δnδn1)/h\left(\delta_{n}-\delta_{n-1}\right) / h.

  • Permanent load. Load in which variations over time are rare or of small magnitude. All other loads are variable loads.

  • Plastic plateau. Portion of the stress-strain curve for uniaxial tension or compression in which the stress remains essentially constant during a period of substantially increased strain.

  • Primary member. For ponding analysis, beam or girder that supports the concentrated reactions from the secondary members framing into it.

  • Residual stress. Stress that remains in an unloaded member after it has been formed into a finished product. (Examples of such stresses include, but are not limited to, those induced by cold bending, cooling after rolling, or welding.)

  • Rigid frame. Structure in which connections maintain the angular relationship between beam and column members under load.

  • Secondary member. For ponding analysis, beam or joist that directly supports the distributed ponding loads on the roof of the structure.

  • Sidesway. Lateral movement of a structure under the action of lateral loads, unsymmetrical vertical loads, or unsymmetrical properties of the structure.

  • Sidesway buckling. Buckling mode of a multistory frame precipitated by the relative lateral displacements of joints leading to failure by sidesway of the frame.

  • Shape factor. Ratio of the plastic moment to the yield moment, Mp/MyM_{p} / M_{y}, also given by Z/SZ / S.

  • St. Venant torsion. Portion of the torsion in a member that induces only shear stresses in the member.

  • Strain hardening. Phenomenon wherein ductile steel, after undergoing considerable deformation at or just above yield point, exhibits the capacity to resist substantially higher loading than that which caused initial yielding.

  • Stub-column. A short compression test specimen utilizing the complete cross section, suf- ficiently long to provide a valid measure of the stress-strain relationship as averaged over the cross section, but short enough so that it will not buckle as a column in the elastic or plastic range.

  • Total building drift. Lateral frame deflection at the top of the most occupied floor divided by the height of the building to that level, Δ/H\Delta / H.

  • Undercut. Notch resulting from the melting and removal of base metal at the edge of a weld. Variable load. Load with substantial variation over time.

  • Warping torsion. Portion of the total resistance to torsion that is provided by resistance to warping of the cross section.

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