P-Delta Effect Simulator Back
Structural Mechanics Simulator

P-Delta Effect Simulator — Second-Order Effects from Axial Loads

Real-time second-order analysis of a pin-pin column under combined axial load $P$ and central lateral point load $H$. Displays Euler buckling load $P_{cr}$, axial ratio $r = P/P_{cr}$, amplification factor $\psi = 1/(1-r)$, and amplified moment $M_2 = M_1\psi$, with deformed-shape and divergence visualizations.

Parameters
Column length L
m
Flexural rigidity EI
kN·m²
Axial load P
kN
Lateral load H
kN

Pin-pin support with a central lateral point load. First-order moment $M_1 = HL/4$, amplification $\psi = 1/(1-P/P_{cr})$, second-order moment $M_2 = M_1\psi$. Diverges (buckling) as $r \to 1$.

Results
Buckling load P_cr
Axial ratio r = P/P_cr
Amplification factor ψ
Amplified moment M₂
Deformed column (first vs second order)

Blue dots = pin supports / red arrow = central lateral point load H / orange arrows = axial load P / dashed cyan curve = first-order deflection (no axial) / thick yellow curve = P-Delta amplified second-order curve / white arrow = midspan deflection δ (exaggerated).

Amplification factor ψ = 1/(1−r)

x-axis = axial load ratio $r = P/P_{cr}$ in 0..1 / y-axis = amplification factor $\psi$ / blue line = hyperbola $\psi = 1/(1-r)$ / yellow dot = current (r, ψ) / orange dashed line = $\psi = 2$ (r = 0.5) / red dashed line = $r = 1$ asymptote (divergence at buckling).

Theory & Key Formulas

Euler buckling load for a pin-pin column:

$$P_{cr} = \frac{\pi^2 EI}{L^2}$$

Axial load ratio and P-Delta amplification factor:

$$r = \frac{P}{P_{cr}},\qquad \psi = \frac{1}{1-r}$$

First-order moment under a central lateral load $H$ and amplified second-order moment:

$$M_1 = \frac{H L}{4},\qquad M_2 = M_1\,\psi = \frac{H L/4}{1 - P/P_{cr}}$$

$E$ is Young's modulus, $I$ the second moment of area, $EI$ the flexural rigidity, $L$ the column length, $P$ the axial load, $H$ the lateral load. As $r \to 1$, $\psi \to \infty$, capturing the divergence near buckling.

What is the P-Delta Effect

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"P-Delta effect" sounds intimidating. What is it, and how is it different from ordinary beam bending?
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Roughly speaking, it is the extra bending moment $P\cdot\Delta$ that appears when an axial force $P$ acts on a lateral displacement $\Delta$. Stand a ruler upright, push down with your finger while nudging the middle sideways, and watch the deflection grow much faster than without the axial push. That growth is the essence of P-Delta. First-order analysis ignores it because it enforces equilibrium on the undeformed shape. At the default settings (L=4 m, P=100 kN, H=10 kN) the Results card shows the moment is already 8.8% larger than the first-order value.
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When I drag P higher, the amplification factor $\psi$ skyrockets and eventually goes to infinity. What is happening physically?
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That is exactly buckling. When $P = P_{cr}$ the denominator of $\psi = 1/(1-r)$ hits zero and the factor diverges. The column is on the verge of buckling under the axial load alone, so any tiny lateral disturbance is amplified without bound. At the default settings $P_{cr} \approx 1234$ kN, so as you push P toward 1200 kN $\psi$ shoots up — you can see it on the lower-right chart. In practice once $r > 0.6$ linear analysis is no longer trustworthy and a geometric nonlinear analysis (GNLA) is required.
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I have heard of P-delta and P-Delta. What is the difference, and which one is this tool?
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Lowercase P-delta is the local amplification of a single member's internal deflection, which is what this tool simulates. Uppercase P-Delta refers to the global story drift $\Delta$ of multi-story buildings multiplied by gravity loads, generating overturning moments important in seismic response and design under AISC and Eurocode 8. Both share the same physics — coupling between axial force and displacement — and both are often grouped under the same name. In finite element practice they are handled identically through the geometric stiffness matrix.
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When I push L all the way to 10 m, $P_{cr}$ drops below 200 kN and $\psi$ explodes. Is this why slender columns are dangerous?
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Exactly. Since $P_{cr} = \pi^2 EI/L^2$, the buckling load drops with the square of length. Going from L=4 m to 10 m cuts $P_{cr}$ to roughly 1/6.25 of its original value. With the same P = 100 kN, $r$ now exceeds 0.5 and $\psi$ more than doubles. Design codes use the slenderness ratio $\lambda = L/i$ (i is the radius of gyration); JIS, AISC and Eurocode all require second-order checks once $\lambda > 100$. Sliding L in this tool gives you a quick feel for that sensitivity.

Frequently Asked Questions

The formula $\psi = 1/(1-P/P_{cr})$ is the standard moment-amplification approximation adopted by AISC 360 and Eurocode 3. It is highly accurate for pin-pin columns with equal end moments or with a single lateral load. The exact solution comes from solving $EI\,y'' + P\,y = M(x)$ and involves $\sec(kL/2)$; for $P/P_{cr} < 0.5$ the two differ by only a few percent and the approximation is considered adequate. Once $P/P_{cr} > 0.7$ the error grows and a full geometric nonlinear finite-element analysis (GNLA) is necessary.
Boundary conditions are absorbed into the effective length $L_e = K \cdot L$, giving $P_{cr} = \pi^2 EI/(KL)^2$. Typical values are K = 1.0 for pin-pin, K = 0.5 for fixed-fixed, K = 0.7 for fixed-pin, and K = 2.0 for a cantilever (one end fixed, one end free). A fixed-fixed column of the same length therefore has four times the buckling load, while a cantilever has only one quarter. The tool covers the canonical pin-pin case; for other supports rescale the length by K.
Major codes use a stability index $\theta = P\Delta/(Vh)$ or the ratio $r = P/P_{cr}$ as the trigger. AISC 360 requires second-order analysis when the story amplification $B_2 > 1.4$; Eurocode 3 requires it when $\alpha_{cr} = F_{cr}/F_{Ed} < 10$ (elastic) or $< 15$ (plastic). The amplification $\psi > 1.4$ in this tool (i.e. r > 0.286) is therefore a rough trigger. Seismic design is stricter because additional drift is expected during earthquakes — second-order effects are typically considered from $\psi > 1.1$ onward.
This tool assumes elastic behavior, so plasticity is not modeled. Real steel columns lose effective stiffness as stresses approach yield, lowering the actual buckling load. The Engesser tangent-modulus theory and the Shanley reduced-modulus theory describe this inelastic regime, and AISC standardizes the inelastic buckling curve. Residual stresses from rolling or welding cause early yielding and can reduce $P_{cr}$ to 60 to 80% of the theoretical value. Design codes lump these effects into a buckling reduction factor $\chi$ (Eurocode 3 curves a, b, c, d).

Real-World Applications

Seismic design of tall buildings: In buildings over 30 stories the story drift $\Delta$ during an earthquake multiplied by the gravity load $P$ from upper floors (thousands of tonnes) produces overturning moments that cannot be ignored. Japan's Building Standard Law Enforcement Order, AISC 341 and Eurocode 8 all require P-Delta inclusion in second-order analysis once the stability index $\theta$ exceeds 0.10. This is one reason modern tall buildings undergo dynamic nonlinear time-history analysis.

Bridge piers and long-span bridges: Piers support vehicle and train dynamic loads plus self-weight while suffering long-term displacements from temperature, shrinkage and creep. Spans above 100 m often require piers above 50 m tall; since $P_{cr}$ falls with length squared the P-Delta effect dominates. The Honshu-Shikoku Bridges and the Akashi-Kaikyo Bridge use whole-bridge geometric nonlinear analysis as standard from the design stage.

Support structures for nuclear power equipment: Reactor vessels and steam generators sit high above their supports and concentrate hundreds to thousands of tonnes. Horizontal displacement during earthquakes pushes P-Delta moments up sharply. Seismic reviews under SRP (US NRC) and JEAG 4601 (Japan) require elastic-plastic response analyses that include second-order effects, and post-Fukushima the design basis earthquake levels were strengthened significantly.

Wind turbines and offshore structures: Onshore 100 m and offshore 200 m wind turbine towers carry self-weight, rotor torque, wind and wave loads with top displacements that may exceed 1 m. Since $P_{cr}$ drops with the square of tower height, modern towers operate well into slenderness ratios above 100, so geometric nonlinear design is mandatory. Setting L=10 m and EI=10000 kN.m^2 in this tool gives a feel for that slender regime.

Common Misconceptions and Pitfalls

The most common pitfall is assuming that "the axial load is small, so P-Delta can be ignored". With $r \approx 0.1$ the amplification is only 11% and seems negligible at preliminary design. But in seismic design an $r = 0.1$ at the moderate earthquake level can temporarily rise to $r = 0.5$ ($\psi = 2.0$) under a major earthquake, especially after plastic hinge formation reduces stiffness and so reduces the effective $P_{cr}$. Higher-than-design-level earthquakes demand pushover or time-history analyses that include P-Delta.

The next pitfall is believing that linear superposition still works. In first-order analysis the response to $1.0 P + 1.0 H$ equals the sum of responses to $1.0 P$ and $1.0 H$. In a P-Delta-corrected second-order analysis this is no longer true because $\psi = 1/(1-P/P_{cr})$ is nonlinear in P. Comparing P=50 kN, H=10 kN with P=100 kN, H=10 kN in this tool shows that $M_2$ does not scale by a simple ratio. Each load combination must be evaluated by its own second-order analysis.

The last pitfall is thinking that computing $P_{cr}$ is enough. The $P_{cr}$ used here is the theoretical Euler value; it ignores local buckling, lateral-torsional buckling, initial imperfections, residual stresses, and plasticity. For real steel columns the Eurocode 3 buckling curves (a-d) or the AISC 360 Q-factor reduce the design buckling load to 60 to 90% of the theoretical value. For H-sections and open sections where lateral-torsional buckling (LTB) governs, $P_{cr}$ alone is insufficient and specialized code formulas or FE linear buckling analysis (LBA) are required. Treat this tool as an introduction to the underlying physics, and combine code-based design with FE verification in practice.