Eurocode 3 Verification

Benchmarking against SCI P364, Designers' Guide to EN 1993-1-1, EUR 22898 EN, and Worked Examples in EC3 & EC4.

Open Eurocode 3 Calculator

Verification Cases
126
reference comparisons
Avg Difference
0.43%
vs. reference
Check Types
7
verification categories
Section Types
6
section families

Methodology

The Eurocode 3 engine implements the requirements of EN 1993-1-1: General rules and rules for buildings. Verification is performed using high-quality benchmarks from Designers' Guide to EN 1993-1-1 Eurocode 3 (Gardner & Nethercot), SCI P364 (Steel Building Design: Worked Examples for Open Sections), Worked Examples in EC3 & EC4, and EUR 22898 EN (Commentary and Worked Examples to EN 1993-1-5).

  • Cross-section Resistance: Axial, bending, and shear benchmark cases are compared with Section 6.2 reference calculations.
  • Buckling Resistance: Flexural buckling (6.3.1) and Lateral-Torsional Buckling (6.3.2) benchmark cases are compared with analytical reference calculations.
  • Combined stability: Implements Annex B (Method 2) for interaction factors k_yy, k_yz, k_zy, k_zz across diverse loading scenarios.

Verification Results

Demand rows compare the engine to a published number. Capacity-policy rows are labelled as a split, not scored as a percent fail.

IDDescriptionSectionExpectedResultDiff %
EC3-01
406x178x54 UB flange class (pure bending)
Designers' Guide to EN 1993-1-1, Ex 5.1
406x178x54 UBClass 1Class 10.00%
EC3-02
406x178x54 UB web class (pure bending)
Designers' Guide to EN 1993-1-1, Ex 5.1
406x178x54 UBClass 1Class 10.00%
EC3-03
406x178x54 UB overall class (pure bending)
Designers' Guide to EN 1993-1-1, Ex 5.1
406x178x54 UBClass 1Class 10.00%
EC3-04
406x178x54 UB flange class (N=300kN)
Designers' Guide to EN 1993-1-1, Ex 5.1
406x178x54 UBClass 1Class 10.00%
EC3-05
406x178x54 UB web class (N=300kN)
Designers' Guide to EN 1993-1-1, Ex 5.1
406x178x54 UBClass 2Class 20.00%
EC3-06
406x178x54 UB overall class (N=300kN)
Designers' Guide to EN 1993-1-1, Ex 5.1
406x178x54 UBClass 2Class 20.00%
EC3-07
254x254x73 UC flange class (pure compression)
Designers' Guide to EN 1993-1-1, Ex 6.2
254x254x73 UCClass 2Class 20.00%
EC3-08
254x254x73 UC overall class
Designers' Guide to EN 1993-1-1, Ex 6.2
254x254x73 UCClass 2Class 20.00%
EC3-09
229x89 Channel flange class
Designers' Guide to EN 1993-1-1, Ex 6.4
229x89 ChannelClass 1Class 10.00%
EC3-10
229x89 Channel web class
Designers' Guide to EN 1993-1-1, Ex 6.4
229x89 ChannelClass 1Class 10.00%
EC3-11
229x89 Channel overall class
Designers' Guide to EN 1993-1-1, Ex 6.4
229x89 ChannelClass 1Class 10.00%
EC3-12
CHS 244.5x10 overall class
Designers' Guide to EN 1993-1-1, Ex 6.7
CHS 244.5x10Class 1Class 10.00%
EC3-13
RHS 200x100x16 flange class
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x16Class 1Class 10.00%
EC3-14
RHS 200x100x16 web class
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x16Class 1Class 10.00%
EC3-15
RHS 200x100x16 overall class
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x16Class 1Class 10.00%
EC3-17
229x89 Channel Vpl,Rd
Designers' Guide to EN 1993-1-1, Ex 6.4
229x89 Channel332 kN332.1 kN0.05%
EC3-18
UB 533x210x92 Mc,Rd
Designers' Guide to EN 1993-1-1 / SCI P364
UB 533x210x92649.0 kN·m649.0 kN·m0.00%
EC3-20
UB 406x178x74 rho factor (shear-bending)
Designers' Guide to EN 1993-1-1, Ex 6.5
UB 406x178x740.270.2741.50%
Rounding of the ρ factor intermediate value — textbook rounds to 2 significant figures mid-calculation, engine retains full precision.
EC3-21
UB 406x178x74 My,V,Rd (Aw per Eq 6.30)
Designers' Guide to EN 1993-1-1, Ex 6.5
UB 406x178x74386.8 kN·m386.8 kN·m0.00%
EC3-22
H 305x305x240 Cl.6.2.9 biaxial interaction ratio
Designers' Guide to EN 1993-1-1, Ex 6.10
H 305x305x2400.330.3392.77%
Textbook rounds reduced plastic moment MN,Rd and interaction terms to 2 significant figures. The engine retains full intermediate precision, leading to a slightly higher biaxial ratio.
EC3-23
UB 457x191x98 n ratio (N/Npl)
Designers' Guide to EN 1993-1-1, Ex 6.6
UB 457x191x980.4770.4770.08%
EC3-24
UB 457x191x98 a parameter
Designers' Guide to EN 1993-1-1, Ex 6.6
UB 457x191x980.3950.3950.10%
EC3-25
UB 457x191x98 MN,y,Rd
Designers' Guide to EN 1993-1-1, Ex 6.6
UB 457x191x98342.2 kN·m342.2 kN·m0.01%
EC3-26
CHS 244.5x10 radius of gyration i
Designers' Guide to EN 1993-1-1, Ex 6.7
CHS 244.5x1082.97 mm82.97 mm0.01%
EC3-27
CHS 244.5x10 λ_bar
Designers' Guide to EN 1993-1-1, Ex 6.7
CHS 244.5x100.560.5550.83%
EC3-28
CHS 244.5x10 χ (curve a)
Designers' Guide to EN 1993-1-1, Ex 6.7
CHS 244.5x100.910.9060.42%
EC3-29
CHS 244.5x10 Nb,Rd
Designers' Guide to EN 1993-1-1, Ex 6.7
CHS 244.5x101836.5 kN1836.5 kN0.00%
EC3-30
CHS 244.5x10 buckling ratio (NEd=1630 kN)
Designers' Guide to EN 1993-1-1, Ex 6.7
CHS 244.5x100.8880.8880.00%
EC3-31
H 305x305x240 iy
Designers' Guide to EN 1993-1-1, Ex 6.10
H 305x305x240144.86 mm144.85 mm0.01%
EC3-32
H 305x305x240 λ_bar_y
Designers' Guide to EN 1993-1-1, Ex 6.10
H 305x305x2400.230.2341.65%
Textbook rounds λ̄ to 2 decimal places. Engine retains full precision from section property calculations.
EC3-33
H 305x305x240 χ_y (curve b)
Designers' Guide to EN 1993-1-1, Ex 6.10
H 305x305x2400.990.9880.20%
EC3-34
H 305x305x240 iz
Designers' Guide to EN 1993-1-1, Ex 6.10
H 305x305x24081.46 mm81.47 mm0.01%
EC3-35
H 305x305x240 λ_bar_z
Designers' Guide to EN 1993-1-1, Ex 6.10
H 305x305x2400.590.5940.65%
EC3-36
H 305x305x240 χ_z (curve c)
Designers' Guide to EN 1993-1-1, Ex 6.10
H 305x305x2400.790.7890.12%
EC3-37
RHS 200x100x16 iy
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x1666.56 mm66.57 mm0.01%
EC3-38
RHS 200x100x16 λ_bar_y
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x161.421.4160.31%
EC3-39
RHS 200x100x16 χ_y (curve a)
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x160.410.4100.10%
EC3-40
RHS 200x100x16 iz
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x1637.17 mm37.17 mm0.01%
EC3-41
RHS 200x100x16 λ_bar_z
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x160.840.8450.59%
EC3-42
RHS 200x100x16 χ_z (curve a)
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x160.770.7690.12%
EC3-43
UC 203x203x46 λ_bar_y
Worked Examples in EC3 & EC4
UC 203x203x460.650.6530.46%
EC3-44
UC 203x203x46 χ_y (curve b)
Worked Examples in EC3 & EC4
UC 203x203x460.810.8100.05%
EC3-45
UC 203x203x46 λ_bar_z
Worked Examples in EC3 & EC4
UC 203x203x460.560.5610.24%
EC3-46
UC 203x203x46 χ_z (curve c)
Worked Examples in EC3 & EC4
UC 203x203x460.810.8080.24%
EC3-47
UB 762x267x173 Mcr Segment CD
Designers' Guide to EN 1993-1-1
UB 762x267x1734311 kN·m4311 kN·m0.01%
EC3-48
UB 762x267x173 λ_LT Segment CD
Designers' Guide to EN 1993-1-1
UB 762x267x1730.630.6290.13%
EC3-49
UB 762x267x173 χ_LT Segment CD (general)
Designers' Guide to EN 1993-1-1
UB 762x267x1730.820.8220.26%
EC3-50
UB 762x267x173 λ_LT Segment BC
Designers' Guide to EN 1993-1-1
UB 762x267x1730.550.5470.54%
EC3-51
UB 762x267x173 χ_LT Segment BC (general)
Designers' Guide to EN 1993-1-1
UB 762x267x1730.860.8630.32%
EC3-52
UB 762x267x173 Mb,Rd Segment BC
Designers' Guide to EN 1993-1-1
UB 762x267x1731469 kN·m1471 kN·m0.10%
EC3-53
UB 457x191x82 λ_LT
Designers' Guide to EN 1993-1-1
UB 457x191x820.640.6410.20%
EC3-54
UB 457x191x82 χ_LT (general)
Designers' Guide to EN 1993-1-1
UB 457x191x820.820.8160.51%
EC3-55
UB 457x191x82 Mb,Rd
Designers' Guide to EN 1993-1-1
UB 457x191x82411 kN·m411 kN·m0.06%
EC3-56
UC 203x203x46 Cl.6.3.3 ratio (Annex B)
Worked Examples in EC3 & EC4
UC 203x203x460.510.5031.37%
Interaction factors kyy, kzy computed with full precision vs textbook's 2 d.p. rounding of intermediate χ and λ̄ values.
EC3-57
H 305x305x240 Cl.6.3.3 ratio (Annex B)
Designers' Guide to EN 1993-1-1, Ex 6.10
H 305x305x2400.970.9670.34%
EC3-58
RHS 200x100x16 Cl.6.3.3 ratio (Annex B)
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x160.940.9470.73%
EC3-62
533x210x92 UKB shear area Av
SCI P364, Example 2
533x210x92 UKB5723.6 mm²5723.6 mm²0.00%
EC3-63
533x210x92 UKB Vpl,Rd
SCI P364, Example 2
533x210x92 UKB909 kN909 kN0.03%
EC3-64
533x210x92 UKB VEd/Vc,Rd
SCI P364, Example 2
533x210x92 UKB0.2970.2970.03%
EC3-66
533x210x92 UKB MEd/Mc,Rd
SCI P364, Example 2
533x210x92 UKB0.8310.8310.00%
EC3-70
457x191x67 Av
SCI P364, Example 3
457x191x67 UKB4093.57 mm²4093.57 mm²0.00%
EC3-71
457x191x67 Vpl,Rd
SCI P364, Example 3
457x191x67 UKB650 kN650 kN0.01%
EC3-72
457x191x67 Mc,Rd
SCI P364, Example 3
457x191x67 UKB404.25 kN·m404.25 kN·m0.00%
EC3-73
457x191x67 Mcr uniform
SCI P364, Example 3
457x191x67 UKB134.2 kN·m133.7 kN·m0.37%
EC3-74
457x191x67 Mcr with C1=2.65
SCI P364, Example 3
457x191x67 UKB355.7 kN·m354.2 kN·m0.42%
EC3-75
457x191x67 λ_LT
SCI P364, Example 3
457x191x67 UKB1.071.0680.19%
EC3-76
457x191x67 χ_LT base
SCI P364, Example 3
457x191x67 UKB0.600.5980.27%
EC3-77
457x191x67 f factor
SCI P364, Example 3
457x191x67 UKB0.830.8330.37%
EC3-78
457x191x67 χ_LT,mod
SCI P364, Example 3
457x191x67 UKB0.720.7180.24%
EC3-79
457x191x67 Mb,Rd
SCI P364, Example 3
457x191x67 UKB291 kN·m290.4 kN·m0.22%
EC3-80
457x191x67 MEd/Mb,Rd
SCI P364, Example 3
457x191x67 UKB0.890.8960.61%
EC3-81
305x305x97 UKC flange class
SCI P364, Example 5
305x305x97 UKCClass 3Class 30.00%
EC3-82
305x305x97 UKC web class
SCI P364, Example 5
305x305x97 UKCClass 1Class 10.00%
EC3-83
305x305x97 UKC overall class
SCI P364, Example 5
305x305x97 UKCClass 3Class 30.00%
EC3-84
305x305x97 Av
SCI P364, Example 5
305x305x97 UKC3517.38 mm²3517.38 mm²0.00%
EC3-85
305x305x97 Vpl,Rd
SCI P364, Example 5
305x305x97 UKC721 kN721 kN0.01%
EC3-86
305x305x97 Mc,Rd (elastic, Class 3)
SCI P364, Example 5
305x305x97 UKC514.75 kN·m514.75 kN·m0.00%
EC3-87
305x305x97 MEd/Mc,Rd
SCI P364, Example 5
305x305x97 UKC0.6410.6410.00%
EC3-88
305x305x97 Mcr uniform
SCI P364, Example 5
305x305x97 UKC460.5 kN·m461.4 kN·m0.20%
EC3-89
305x305x97 Mcr with C1=1.32
SCI P364, Example 5
305x305x97 UKC607.7 kN·m609.1 kN·m0.23%
EC3-90
305x305x97 λ_LT
SCI P364, Example 5
305x305x97 UKC0.920.9190.08%
EC3-91
305x305x97 χ_LT base
SCI P364, Example 5
305x305x97 UKC0.740.7491.15%
Engine uses continuous LTB curve formula; textbook rounds intermediate Φ_LT to 2 d.p.
EC3-92
305x305x97 χ_LT,mod
SCI P364, Example 5
305x305x97 UKC0.790.7991.14%
Cascading from EC3-91: textbook rounds Φ_LT to 2 d.p., propagating through to χ_LT,mod.
EC3-93
305x305x97 Mb,Rd
SCI P364, Example 5
305x305x97 UKC407 kN·m411 kN·m1.05%
Cascading from χ_LT,mod precision difference (EC3-91/92). Engine gives a slightly higher Mb,Rd.
EC3-94
305x305x97 MEd/Mb,Rd
SCI P364, Example 5
305x305x97 UKC0.810.8020.94%
EC3-95
356x368x129 UKC flange class
SCI P364, Example 9
356x368x129 UKCClass 3Class 30.00%
EC3-96
356x368x129 UKC overall class
SCI P364, Example 9
356x368x129 UKCClass 3Class 30.00%
EC3-97
356x368x129 Nc,Rd
SCI P364, Example 9
356x368x129 UKC5658 kN5658 kN0.00%
EC3-98
356x368x129 NEd/Nc,Rd
SCI P364, Example 9
356x368x129 UKC0.6190.6190.00%
EC3-99
356x368x129 λ_bar_z
SCI P364, Example 9
356x368x129 UKC0.820.8210.11%
EC3-100
356x368x129 χ_z
SCI P364, Example 9
356x368x129 UKC0.650.6490.15%
EC3-101
356x368x129 Nb,Rd
SCI P364, Example 9
356x368x129 UKC3678 kN3672 kN0.16%
EC3-102
356x368x129 buckling ratio
SCI P364, Example 9
356x368x129 UKC0.9520.9530.16%
EC3-103
305x305x97 λ_bar_y
SCI P364, Example 10
305x305x97 UKC0.5160.5160.05%
EC3-104
305x305x97 χ_y
SCI P364, Example 10
305x305x97 UKC0.870.8770.82%
EC3-105
305x305x97 Nb,y,Rd
SCI P364, Example 10
305x305x97 UKC2943 kN2967 kN0.82%
EC3-106
305x305x97 λ_bar_z
SCI P364, Example 10
305x305x97 UKC0.4490.4490.05%
EC3-107
305x305x97 χ_z
SCI P364, Example 10
305x305x97 UKC0.880.8711.00%
Engine uses continuous buckling curve c formula; textbook rounds intermediate Φ to 2 d.p.
EC3-108
457x191x82 Vpl,Rd
SCI P364, Example 4
457x191x82 UKB756 kN756 kN0.03%
EC3-109
457x191x82 χ_LT,mod (6.3.2.3 rolled)
SCI P364, Example 4
457x191x82 UKB0.920.8824.15%
Engine uses the NCCI SN003 closed-form Mcr formula (standard analytical method). The reference derives Mcr from a numerical lateral-torsional buckling model, which yields ~4% lower λ_LT for this section. The analytical result is conservative (safe side).
EC3-110
457x191x82 Mb,Rd
SCI P364, Example 4
457x191x82 UKB463 kN·m444 kN·m4.10%
Cascading from Mcr method difference above. Engine uses NCCI SN003 analytical Mcr; the reference uses a numerical lateral-torsional buckling model. Result is conservative (safe side).
EC3-111
203x203x46 χ_y
SCI P364, Example 11
203x203x46 UKC0.800.8101.20%
Textbook rounds intermediate Φ to 2 d.p. in buckling curve b; engine retains full precision.
EC3-112
203x203x46 χ_z
SCI P364, Example 11
203x203x46 UKC0.470.4720.49%
EC3-113
203x203x46 χ_LT
SCI P364, Example 11
203x203x46 UKC0.830.8461.93%
Engine’s SCI/NCCI C1 polynomial approximation overestimates C1 for this moment diagram, yielding a lower λ_LT (0.725 vs reference 0.76 from its numerical Mcr model) and higher χ_LT. The structural interaction ratio remains within 1.6% of the reference.
EC3-114
203x203x46 Cl.6.3.3 combined ratio
SCI P364, Example 11
203x203x46 UKC0.980.9961.59%
Combined cascading effect from χ_y (EC3-111) and χ_LT (EC3-113) C1 approximation differences.
EC3-115
457x191x67 χ_y (S355)
SCI P364, Example 12
457x191x67 UKB0.940.9460.66%
EC3-116
457x191x67 χ_z (S355)
SCI P364, Example 12
457x191x67 UKB0.620.6271.14%
Textbook rounds intermediate Φ to 2 d.p. in buckling curve b; engine retains full precision.
EC3-117
457x191x67 χ_LT (S355, Class 3)
SCI P364, Example 12
457x191x67 UKB0.880.8256.24%
Engine uses NCCI SN003 analytical Mcr with fork support (free warping) at each 3m segment. The reference uses a numerical model with warping continuity at the intermediate restraint, giving a higher Mcr. Lower χ_LT = lower capacity prediction = conservative (safe side).
EC3-118
457x191x67 Cl.6.3.3 combined ratio (Class 3)
SCI P364, Example 12
457x191x67 UKB0.880.9346.11%
Cascading from χ_LT difference above. Engine’s analytical Mcr (fork support) vs the reference numerical model with warping continuity propagates into the 6.3.3 interaction factors. Result is conservative (safe side).
EC3-119
EUR 22898 §16: Panel I plate slenderness (450×12, S355)
EUR 22898 EN, §16 (pp.182)
Plate panel 450×120.8110.8120.06%
EC3-120
EUR 22898 §16: Panel I reduction factor ρ
EUR 22898 EN, §16 (pp.182)
Plate panel 450×120.8990.8980.08%
EC3-121
EUR 22898 §16: Panel III plate slenderness (288×6, S355)
EUR 22898 EN, §16 (pp.182)
Plate panel 288×61.0381.0390.06%
EC3-122
EUR 22898 §16: Panel III reduction factor ρ
EUR 22898 EN, §16 (pp.182)
Plate panel 288×60.7590.7590.02%
EC3-123
EUR 22898 §15: Bottom flange plate slenderness (700×26, S420)
EUR 22898 EN, §15 (pp.174-178)
Plate panel 700×260.630.6340.58%
EC3-124
EUR 22898 §15: Stiffener plate slenderness (350×8, S420)
EUR 22898 EN, §15 (pp.174-178)
Plate panel 350×81.031.0300.03%
EC3-125
EUR 22898 §15: Stiffener reduction factor ρ
EUR 22898 EN, §15 (pp.174-178)
Plate panel 350×80.7630.7640.09%
EC3-126
EUR 22898 §15: Inclined web plate slenderness (391×8, S420)
EUR 22898 EN, §15 (pp.174-178)
Plate panel 391×81.151.1500.03%
EC3-127
EUR 22898 §15: Inclined web reduction factor ρ
EUR 22898 EN, §15 (pp.174-178)
Plate panel 391×80.7030.7030.01%
EC3-128
EUR 22898 §15: kσ for web ψ=−1.30 (Table 4.1)
EN 1993-1-5 Table 4.1 (kσ = 5.98(1−ψ)² for ψ < −1)
EN 1993-1-5 Table 4.131.6331.630.00%
EUR 22898 EN p.178 uses an approximate formula giving kσ=32.5; the correct Table 4.1 formula gives 31.63.
EC3-129
EUR 22898 §15: ρ web bending at λp=1.07, ψ=−1.30
EUR 22898 EN, §15 (p.178)
Plate panel (bending)0.8530.8530.01%
EC3-130
EUR 22898 Eq 4.1: ρ internal λp=2.0 ψ=1
EUR 22898 EN, Eq 4.1 (pp.46-47)
EN 1993-1-5 Eq 4.10.4450.4450.00%
EC3-131
EUR 22898 Eq 4.2: ρ outstand λp=1.5
EUR 22898 EN, Eq 4.2 (pp.46-47)
EN 1993-1-5 Eq 4.20.5830.5830.02%
EC3-132
EUR 22898 §15.2: Stiffener ρ at λp=0.857
EUR 22898 EN, §15.2 (p.177)
Plate panel (stiffener)0.8680.8670.08%
EC3-133
254x254x73 UC Compression Resistance Nc,Rd (S355)
Designers' Guide to EN 1993-1-1, Ex 6.2
254x254x73 UC3305 kN3305.1 kN0.00%
EC3-134
CHS 244.5x10 Section Compression Npl,Rd (S275)
Designers' Guide to EN 1993-1-1, Ex 6.7
CHS 244.5x102026.75 kN2025.9 kN0.04%
EC3-135
RHS 200x100x16 Bending Resistance Mc,Rd (S355, Class 1)
Designers' Guide to EN 1993-1-1, Ex 6.9
RHS 200x100x16174.3 kN·m174.3 kN·m0.00%

Disclaimer: This verification page is provided for informative purposes only and does not constitute a guarantee of accuracy for all possible configurations. While we use automated verification checks to help find defects, no software is entirely free of defects. Engineers must exercise independent professional judgement and verify results through their own checks before relying on any output for design or construction decisions. AutoCalcs accepts no liability for errors, omissions, or any consequences arising from the use of this software.