Combined N+M Utilisation — 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, LRFD)
—
Out-of-Plane Buckling (AISC 360-22 §E3) — y-y axis
Fe (elastic critical)
—
Fcr (column stress)
—
φPn (design capacity, LRFD)
—
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
—
Util. ratio η
—
W14×90
L
Pu
Mu
K=1.0
W section column elevation (schematic)
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