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Beam-Column Interaction Calculator

Combined bending and axial compression check per EN 1993-1-1 §6.3.3 Equations 6.61 and 6.62. Computes χyz (flexural buckling §6.3.1), χLT (LTB §6.3.2), Annex B interaction factors kyy/kzy/kyz/kzz, and both interaction utilisations. HEA, HEB, HEM, IPE, UC, UB. S235–S460.

EN 1993-1-1 §6.3.3 Eqs 6.61 + 6.62
Eq. 6.61: NEd/(χy·NRkM1) + kyy·My,Ed/(χLT·My,RkM1) + kyz·Mz,Ed/(Mz,RkM1) ≤ 1
Eq. 6.62: NEd/(χz·NRkM1) + kzy·My,Ed/(χLT·My,RkM1) + kzz·Mz,Ed/(Mz,RkM1) ≤ 1
Member Parameters

EN: γM1 = 1.0 (recommended value, used by NL and BE)

L = K·L_member. K = 1.0 pin-pin, 0.5 fixed-fixed, 0.7 fixed-pin

Interaction Results
56.7%
Eq. 6.62   PASS ✓
η = 0.567  |  Eq. 6.61 = 0.466  |  Eq. 6.62 = 0.567
Flexural Buckling §6.3.1
λ̄_y / χ_y0.503 / 0.883
λ̄_z / χ_z0.861 / 0.624
N_b,Rd,y / N_b,Rd,z (kN)3321.7 / 2349.1
Curves y-y / z-z B / C
LTB §6.3.2
C1 / M_cr (kNm)1 / 1049.6
λ̄_LT / χ_LT0.597 / 0.891
M_b,Rd (kNm) / curve333.1 / A
Resistances
N_Rk (kN)3763
M_y,Rk / M_z,Rk (kNm)373.8 / 116.1
Annex B Interaction Factors
C_my / C_mz / C_mLT1 / 1 / 1
k_yy / k_zy1.041 / 0.984
k_yz / k_zz0.743 / 1.238
== FLEXURAL BUCKLING §6.3.1 ==
λ̄_y = 0.503   curve B   χ_y = 0.883
λ̄_z = 0.861   curve C   χ_z = 0.624
N_Rk = A·fy = 3763 kN

== LTB §6.3.2 ==
C1 = 1   M_cr = 1049.6 kNm
λ̄_LT = √(Wpl·fy / M_cr) = 0.597
curve LT = A   χ_LT = 0.891
M_b,Rd = χ_LT·Wpl·fy/γM1 = 333.1 kNm

== INTERACTION FACTORS (ANNEX B) ==
C_my = 1   C_mz = 1   C_mLT = 1
k_yy = 1.041   k_zy = 0.984
k_yz = 0.743   k_zz = 1.238

== EQUATIONS 6.61 & 6.62 ==
Eq. 6.61 = 400/3322.7
        + 1.041×80/333.1
        + 0.743×15/116.1
        = 0.466

Eq. 6.62 = 400/2348.1
        + 0.984×80/333.1
        + 1.238×15/116.1
        = 0.567

→ Governing: Eq. 6.62   η = 56.7%   PASS ✓
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Frequently Asked Questions

EN 1993-1-1 §6.3.3 provides two interaction equations (6.61 and 6.62) for members subject to combined bending and axial compression. Eq. 6.61 checks the member against y-y buckling with major-axis bending; Eq. 6.62 checks against z-z buckling with biaxial bending. Both must be satisfied simultaneously. The most common situation is Eq. 6.62 governing, because the z-z buckling reduction factor χ_z is typically lower and k_zz amplifies minor-axis moments.
Annex B (simplified method) provides conservative closed-form formulas for k_yy, k_zy, k_yz and k_zz based on slenderness and moment distribution factors C_my/C_mz/C_mLT. It is easier to apply and safe for typical members. Annex A (general method) gives more accurate — often less conservative — k-factors, requiring C_yy/C_zz/C_yz/C_zy auxiliary terms and plastic modulus ratios. Most national codes accept either; Annex B is the default used here.
The equivalent uniform moment factors C_my and C_mz account for the shape of the bending moment diagram along the member. For linear (end-moment) loading: C_m = 0.6 + 0.4ψ ≥ 0.4, where ψ = M₂/M₁ is the ratio of the smaller to larger moment. Uniform moment (ψ = 1) gives C_m = 1.0 (worst case). For parabolic UDL diagrams C_m ≈ 0.4 and for triangular (point load at midspan) C_m ≈ 0.6. Annex B Table B.3 gives the full table.
L_y and L_z are effective buckling lengths for flexural buckling about the major (y-y) and minor (z-z) axes, respectively. L_LT is the unrestrained length for lateral-torsional buckling. For most columns in a non-sway frame: L_y = L_z = L_LT = full height. For columns in a sway frame: L_y = L_z ≈ 2L. Bracing or intermediate restraints shorten L_z and L_LT independently.
Yes. γM1 divides all resistances (N_Rk, M_y,Rk, M_z,Rk) in the denominator of each term. For EN/NL/BE: γM1 = 1.0. For DE (DIN EN 1993-1-1/NA): γM1 = 1.1, which reduces all design resistances by ~9% and makes the check more conservative. Switch the National Annex dropdown to see the effect.