Free Tool · EN 1993-1-1 §6.3.3 · Combined N+M · Eqs 6.61 + 6.62

Steel N+M Interaction Check

Combined axial compression + bi-axial bending per EN 1993-1-1 §6.3.3. Interaction equations 6.61 and 6.62 with k-factors from Annex A (alternative) or Annex B (general). Full step-by-step: χy, χz, χLT, Cm, all four k-factors.

Presets:
Section
Design Forces
ψ = Mmin/Mmax. Uniform moment: ψ=1. Triangular: ψ=0. Antisymmetric double-curvature: ψ=−1 (gives Cm=0.4, lowest amplification).
Buckling Lengths
LLT = distance between lateral restraints. If compression flange is continuously restrained, χLT = 1 (no LTB reduction).
Interaction Method
Annex B is simpler and conservative. Annex A is more accurate, preferred for critical members in DE/NL practice.
Interaction Results
Equation Detail

Eq 6.61

NEd / (χy·NRkM1)
kyy·My,Ed / (χLT·My,RkM1)
kyz·Mz,Ed / (Mz,RkM1)
Total Eq 6.61

Eq 6.62

NEd / (χz·NRkM1)
kzy·My,Ed / (χLT·My,RkM1)
kzz·Mz,Ed / (Mz,RkM1)
Total Eq 6.62
Flexural Buckling (§6.3.1)
Npl,Rd
Nb,Rd,y
λ̄y
Curvey
χy
Nb,Rd,z
λ̄z
Curvez
χz
Lateral-Torsional Buckling (§6.3.2)
Mcr
λ̄LT
χLT
Mb,Rd
Equivalent Moment Factors
Cmy (Annex B Table B.3)
Cmz
CmLT
Interaction Factors (Annex B)
kyy
kyz
kzy
kzz
Section Capacity
Mpl,Rd,y
Mpl,Rd,z
Wpl,y
Wpl,z
Section class
If member is NOT susceptible to torsional deformation, χLT = 1 can be assumed per §6.3.3(4) — increase LLT to simulate this.
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Methodology & Clause References

EN 1993-1-1:2005+A1:2014 §6.3.3 — Two interaction equations govern beam-column design:

Eq 6.61: NEd/(χy·NRk/γM1) + kyy·My,Ed/(χLT·My,Rk/γM1) + kyz·Mz,Ed/(Mz,Rk/γM1) ≤ 1

Eq 6.62: NEd/(χz·NRk/γM1) + kzy·My,Ed/(χLT·My,Rk/γM1) + kzz·Mz,Ed/(Mz,Rk/γM1) ≤ 1

χy, χz — Flexural buckling (§6.3.1): Ncr = π²·E·I/Lcr², λ̄ = √(A·fy/Ncr), χ from Eq 6.49. Buckling curves per Table 6.2 (rolled I: h/b>1.2, tf≤40mm → y=a, z=b).

χLT — LTB (§6.3.2.2): Mcr from Annex F (simplified fork BC), λ̄LT = √(Wpl·fy/Mcr). LTB curve: Table 6.4 (h/b≤2.0 → curve b, else curve c). Plateau λ̄LT,0 = 0.4, β = 0.75.

Cm — Equivalent moment factors (Annex B Table B.3): Cm = 0.6 + 0.4·ψ ≥ 0.4. CmLT = max(Cmy², 0.9).

Annex B (general): kyy, kzz from Table B.1. kyz = 0.6·kzz. kzy from Table B.2 using CmLT.

Annex A (alternative): Auxiliary C-factors Cyy, Czz from Table A.2. kyy = Cmy²·(1/μy)·Cyy/χy etc. More accurate for stocky members with high axial ratio.

Cross-verify χy, χz independently: /tools/steel-column-buckling (§6.3.1).

For LTB verification: /tools/lateral-torsional-buckling-en (§6.3.2).

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