Combined N+M Utilization — LRFD
—
Slenderness KL/r (AISC 360-22 §E1)
KL/r in-plane (x-x)
—
KL/r out-of-plane (y-y)
—
Limit
≤ 200
Governing axis
—
Section Classification (AISC 360-22 Table B4.1a)
Flange λ = bf/2tf
—
Flange class
—
Web λ = (d−2tf)/tw
—
Overall
—
In-Plane Buckling (AISC 360-22 §E3) — x-x axis
Fe (elastic critical)
—
Fcr (column stress)
—
φPn (design capacity)
—
Out-of-Plane Buckling (AISC 360-22 §E3) — y-y axis
Fe (elastic critical)
—
Fcr (column stress)
—
φPn (design capacity)
—
Torsional Buckling (AISC 360-22 §E4)
Fe_t (ksi)
—
Fcr_t (ksi)
—
φPn_t (kip)
—
Torsional governs?
—
Slender-Element Reduction (AISC 360-22 §E7)
Qs (flange)
—
Qa (web)
—
Q = Qs·Qa
—
Ae (in²)
—
Fcr_e (ksi)
—
φPn_e (kip)
—
Slender governs?
—
Fcr vs KL/r Column Curve (AISC 360-22 §E3)
Moment Magnifier (AISC 360-22 §C2.2)
Cm
—
δ = Cm/(1 − P/Pcr)
—
Effective Mu (LRFD)
—
φMn (LRFD)
—
Applied Loads (LRFD)
Pu (design axial)
—
Mu (design moment)
—
Combined N+M Interaction (AISC 360-22 Eq. H1-1a/b)
Pu/φPn
—
Mu/φMn
—
Combined check η
—
Governing check
—
W section column elevation (schematic)
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