$$\frac{N_{Ed}}{N_{b,Rd}}+ k_{yy}\frac{M_{y,Ed}}{M_{b,Rd}}\leq 1.0$$
Reduction factor: $\chi = \frac{1}{\Phi + \sqrt{\Phi^2 - \bar{\lambda}^2}}$
Slenderness: $\bar{\lambda}= \sqrt{\frac{A f_y}{N_{cr}}}$
Real-time EN 1993-1-1 combined axial-bending check for steel beam-columns. Plot the design point on the P-M interaction envelope and get instant PASS/FAIL judgment.
The core of the check is the interaction formula, which ensures the combined stress from axial load and bending doesn't cause instability. The European standard EN 1993-1-1 uses this linear interaction check.
$$\frac{N_{Ed}}{N_{b,Rd}}+ k_{yy}\frac{M_{y,Ed}}{M_{b,Rd}}\leq 1.0$$$N_{Ed}, M_{y,Ed}$ = Design axial force and bending moment (your inputs in the simulator).
$N_{b,Rd}, M_{b,Rd}$ = Design buckling resistance for compression and lateral-torsional buckling for bending.
$k_{yy}$ = Interaction factor that depends on moment distribution and member slenderness.
The buckling resistance $N_{b,Rd}$ is reduced from the pure squash load by a factor $\chi$, which depends on the member's slenderness $\bar{\lambda}$. This captures how long, slender columns fail at much lower loads.
$$\chi = \frac{1}{\Phi + \sqrt{\Phi^2 - \bar{\lambda}^2}}\quad \text{with}\quad \bar{\lambda}= \sqrt{\frac{A f_y}{N_{cr}}}$$$\chi$ = Reduction factor (between 0 and 1).
$\bar{\lambda}$ = Non-dimensional slenderness.
$A f_y$ = Squash load (cross-section area × yield strength).
$N_{cr}$ = Elastic critical buckling load (Euler load). Try increasing the "Effective Length" in the simulator: watch $\bar{\lambda}$ increase and $\chi$ drop, shrinking the safe zone on the diagram.
Building Frame Columns: In multi-storey steel buildings, columns are rarely under pure axial load. They experience significant bending moments from floor beams, wind loads, and imperfect alignment. Engineers use P-M diagrams to verify every column, especially corner columns which have biaxial bending.
Crane Runway Girders: The vertical girder of an overhead crane is a classic beam-column. It carries the vertical weight of the crane and load (axial compression) while also resisting the horizontal thrust and eccentric loads from movement (bending). Failure is often a buckling instability.
Offshore Platform Legs: The legs of jacket-type offshore platforms are subjected to enormous axial loads from the platform weight and environmental forces, combined with large bending moments from waves and currents. The interaction check is critical for safety in these harsh environments.
Industrial Storage Racks: The uprights in pallet racking are slender beam-columns. They carry vertical pallet loads (axial force) and moments from the eccentricity of the loads and potential impacts from forklifts. Fast, accurate P-M checks allow for optimizing material use while ensuring safety against collapse.
When you start using this kind of tool, there are a few common pitfalls. The first is the assumption that strengthening the cross-section solves everything. It's true that increasing the flange width or web thickness of an H-section will improve its sectional properties. However, if the member length L remains long, the buckling resistance $N_{b,Rd}$ will hardly improve. For example, for a 5m long member, changing from an H-200x200 to an H-250x250 will increase the Euler buckling load proportionally to the moment of inertia, but if the slenderness ratio $\bar{\lambda}$ is still large, the buckling reduction factor $\chi$ won't increase as much as you might think. Effective buckling countermeasures require considering both "section strengthening" and "re-evaluating support conditions (effectively shortening the length)".
The second is misidentifying the "main player" between axial force and bending moment. Because the tool lets you adjust N and M independently, you might tend to think of their limit values separately. But in actual structures, for instance in a column with eccentric loading, axial force and bending moment are proportional. In your simulation, unless you evaluate by moving points on the graph along the expected path of the design load (e.g., a case where bending increases under constant axial force), your verification won't be realistic.
The third is forgetting to consider local buckling. This tool deals with member buckling (global buckling). However, parts composed of plate elements, like the flanges and web of an H-section, can experience "local buckling" where the plate itself buckles under high compressive stress. EN1993 prevents this through limits on width-to-thickness ratios. Even if the tool shows sufficient strength, if the section's width-to-thickness ratio exceeds the code limit, that section cannot be used. You must always check for both global and local buckling.
HEB 300 steel beam (S235, fy = 235 MPa, E = 210 GPa) with L = 4500 mm, N = 450 kN axial compression, My = 85 kN·m, Mz = 12 kN·m. Relative slenderness λ̄y ≈ 0.78 (Class b, α = 0.34). χy ≈ 0.82. Interaction check: (450/715) + 0.92×(85/330) + 0.65×(12/110) ≈ 0.629 + 0.235 + 0.071 = 0.935 < 1.0 → PASS. Design point plots safely within interaction envelope.