Second-Order Effects — Geometric Nonlinearity & Frame Stability
Second-order effects are the additional internal forces and displacements that result from structural loads acting through the deformed geometry of a structure. In a first-order analysis, equilibrium is written on the undeformed shape. In a second-order analysis, equilibrium includes the P-ÃÂàand P-ÃÂô contributions from axial loads acting through displacements.
First-order: M = M_applied (linear with load)
Second-order: M = M_applied + P*ÃÂà+ P*ÃÂô (nonlinear)
PRELIMINARY — NOT FOR CONSTRUCTION. All content is for educational and reference use only. Must be independently verified by a licensed Professional Engineer (PE) or Structural Engineer (SE) before use in any project.
P-ÃÂàand P-ÃÂô Contributions
Second-order effects decompose into two components:
| Effect | Cause | Impact |
|---|---|---|
| P-ÃÂÃÂ | Story gravity loads ÃÂÃÂ interstory drift | Amplifies story moments and drifts |
| P-ÃÂô | Member axial load ÃÂàmember curvature | Amplifies member internal moments |
Both reduce the effective stiffness of the structure. At the critical buckling load, the total stiffness matrix becomes singular — this is the limit point where second-order displacements grow without bound.
Geometric Stiffness Matrix
In finite element formulations, second-order effects are captured by the geometric stiffness matrix [Kg]:
[K_total] = [K_elastic] + [K_geometric]
where [Kg] = function(N, L) — depends on axial force, not material properties
For compressive axial loads, [Kg] is negative (softening). For tensile loads, [Kg] is positive (stiffening — the tension-stiffening effect used in cable structures). The eigenvalue problem det([K_elastic] + ÃÂû[Kg]) = 0 yields the elastic critical load factor ÃÂûcr.
Effective Length Method (ELM) vs Direct Analysis Method (DAM)
AISC 360 provides two methods for stability design, with the DAM being the preferred approach:
| Aspect | ELM | DAM |
|---|---|---|
| Analysis type | First-order | Rigorous second-order (P-ÃÂà+ P-ÃÂô) |
| K factors | From alignment charts | K = 1.0 for all columns |
| Stiffness reduction | None (implicit in K-factor calibration) | ÃÂÃÂb = 0.80 (bending); EI* = 0.80ÃÂÃÂb*EI |
| Notional loads | Not required | Ni = 0.002*Yi (min lateral load) |
| Accuracy | Approximate (system-dependent) | More accurate across frame types |
| AISC status | Permitted (Chapter C, Appendix 7) | Preferred (Chapter C) |
DAM Requirements
- Reduced stiffness: EI* = 0.80 * ÃÂÃÂb _ EI; EA_ = 0.80 * EA (ÃÂÃÂb = 1.0 when ÃÂñPr/Pns âÃÂä 0.50)
- Notional loads: Ni = 0.002 * Yi applied at each level in orthogonal directions
- Rigorous second-order analysis: Captures both P-ÃÂàand P-ÃÂô
- K = 1.0: Column effective length factor = 1.0 because frame stability is directly captured by the analysis
EN 1993-1-1 Approach
EN 1993-1-1 uses the elastic critical load factor ÃÂñcr:
ÃÂñcr = Fcr / FEd
ÃÂñcr âÃÂÃÂ¥ 10: First-order analysis sufficient
3 âÃÂä ÃÂñcr < 10: Second-order analysis required
ÃÂñcr < 3: Second-order analysis required; consider frame stiffness increase
For frames with ÃÂñcr âÃÂÃÂ¥ 3, second-order effects may be approximated by amplifying first-order results:
M_II = M_I * 1 / (1 - 1/ÃÂñcr)
This is the same 1/(1-ÃÂø) amplification used in AISC for P-ÃÂàeffects.
Frequently Asked Questions
When can I ignore second-order effects? Per AISC 360: when the ratio of second-order drift to first-order drift âÃÂä 1.10 (i.e., P-ÃÂàincreases drift by âÃÂä 10%). Per EN 1993-1-1: when ÃÂñcr âÃÂÃÂ¥ 10. In braced frames where sway is fully prevented, P-ÃÂàeffects on the frame are negligible, but member P-ÃÂô effects must still be checked via moment amplification (B1 in AISC).
Why does DAM use reduced stiffness? The 0.80 stiffness reduction accounts for inelastic softening before the member reaches its nominal capacity. Residual stresses cause partial yielding at stress levels below Fy, reducing the effective stiffness. The ÃÂÃÂb factor further accounts for the influence of axial load on flexural stiffness. Without these reductions, a second-order elastic analysis would over-predict stability.
What are notional loads? Notional loads are minimum lateral loads (Ni = 0.002*Yi) applied to account for geometric imperfections — primarily frame out-of-plumbness. The 0.002 factor corresponds to H/500 out-of-plumbness, which is the maximum permitted erection tolerance per AISC Code of Standard Practice. They ensure the analysis captures the destabilizing effect of unavoidable geometric imperfections.
International Code References
- AISC 360: Chapter C — Stability. DAM is preferred method. ELM permitted as alternative (Appendix 7). Second-order per Appendix 8.
- EN 1993-1-1: Clause 5.2.2 — global imperfections ÃÂà= ÃÂÃÂ0ÃÂñhÃÂñm. ÃÂñcr calculation per Clause 5.2.1(4)B.
- AS 4100: Section 4.7 — second-order elastic analysis. ÃÂôb for braced member moment amplification, ÃÂôs for sway amplification.
- CSA S16: Clause 8.3 — stability effects via geometric stiffness matrix or moment amplification (U1, U2 factors).
Educational reference only. Second-order analysis for tall buildings, irregular structures, or frames with high axial load may require full nonlinear geometric analysis with material nonlinearity (GMNIA). All designs must be independently verified by a licensed Professional Engineer.
Disclaimer: This content is for educational purposes only. Results must be verified by a licensed professional engineer. Steel Calculator provides preliminary design tools — NOT a substitute for professional engineering judgment.