Welding Residual Stress Back
Welding & Structural Analysis

Welding Residual Stress Simulator

Adjust heat input, joint type, thickness, material, and restraint to instantly compute residual stress distribution, angular distortion, and longitudinal shrinkage. PWHT stress-relief effects included.

Welding Parameters
Voltage V (V)
V
Current I (A)
A
Thermal efficiency η
Travel speed v (mm/s)
mm/s
Joint type
Plate thickness t (mm)
mm
Material
Preheat temp. T₀ (°C)
°C
Restraint condition
PWHT hold time (h)
h
Results
σ_res (MPa)
θ distortion (°)
δ_L shrinkage (mm)
PWHT relief (%)
Heat input Q (J/mm)
σ_res (MPa)
Distortion (°)
Shrinkage (mm)
Chart 1: Residual Stress Distribution σ_x(y) — Distance from Weld Centerline
Chart 2: Angular Distortion vs Heat Input (by plate thickness)
Theory & Key Formulas

Heat input: $Q = V \cdot I \cdot \eta / v$

Angular distortion: $\theta = C_1 Q / t^2$

Longitudinal shrinkage: $\delta_L = C_2 Q / (EA)$

Peak residual stress ≈ yield stress $f_y$ (fully restrained)

What is Welding Residual Stress?

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What exactly is "residual stress" in welding? Is it like the stress from the weight of the parts?
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Not at all. Basically, it's stress that's "locked in" the metal after welding, even with no external load. In practice, the intense, localized heat causes metal to expand and then contract unevenly as it cools. This tug-of-war between hot and cold zones creates permanent internal tension. Try moving the "Heat Input" slider up in the simulator—you'll see the predicted residual stress spike toward the material's yield strength.
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Wait, really? So if the stress is already so high, can the part just crack on its own?
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Exactly. A common case is "cold cracking" in high-strength steels, where residual stress combines with hydrogen from the weld and a brittle microstructure. That's why the simulator lets you change the "Material" and "Preheat Temp." For instance, preheating slows the cooling rate, reducing the stress and risk. Change the preheat from 20°C to 150°C and watch the stress prediction drop.
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What about the "distortion" and "shrinkage" it also calculates? Are those just different words for the same thing?
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Good question. They're related but different physical results. Distortion is the visible bending or twisting of the whole part (like a warped plate). Shrinkage is the actual shortening of the weld seam itself. For instance, in a long bridge girder, shrinkage can throw off the entire length tolerance. In the simulator, switch the "Joint Type" to a thick "T-joint" and see how the angular distortion changes dramatically with the same heat input.

Physical Model & Key Equations

The core driver of all welding effects is the heat input per unit length, which determines how much metal melts and subsequently contracts.

$$Q = \frac{V \cdot I \cdot \eta}{v}$$

Where $Q$ is the heat input (J/mm), $V$ is voltage (V), $I$ is current (A), $\eta$ is the arc thermal efficiency, and $v$ is the travel speed (mm/s). This is the primary parameter you control in the simulator. Higher $Q$ means more heat, leading to greater shrinkage and stress.

The resulting deformations are often empirically related to heat input and geometry. Angular distortion (bending) depends heavily on plate thickness, while longitudinal shrinkage depends on the cross-sectional area resisting the contraction force.

$$\theta = C_1 \frac{Q}{t^2}\quad \text{and}\quad \delta_L = C_2 \frac{Q}{E A}$$

Here, $\theta$ is the angular distortion (radians), $t$ is plate thickness (mm), $\delta_L$ is longitudinal shrinkage (mm), $E$ is Young's modulus, $A$ is the weld cross-section area, and $C_1, C_2$ are empirical constants. The simulator solves these instantly when you adjust thickness or joint type.

Real-World Applications

Shipbuilding & Offshore Structures: Massive welded panels are prone to buckling distortion (a type of angular distortion). Engineers use simulators like this to optimize welding sequence and heat input before production, saving millions in rework. Preheating thick high-strength steel joints is standard to prevent cracking.

Pipeline Construction: Longitudinal shrinkage in long pipeline welds can accumulate, causing the pipeline to shorten beyond allowable tolerances. The travel speed and heat input are carefully controlled based on calculations similar to this tool's output to ensure fit-up for the next pipe section.

Pressure Vessel Fabrication: High residual stress at welds can combine with internal pressure stress, leading to premature failure or reduced fatigue life. Post-Weld Heat Treatment (PWHT), which you can model with the "PWHT hold time" parameter, is often mandated to relax these stresses and ensure safe operation.

Automotive Frame Assembly: Distortion in chassis components from welding can misalign mounting points for engines or suspensions. CAE engineers use this physics to simulate welding during virtual prototyping, adjusting clamp positions (modeled by "Restraint Condition") to minimize warpage before building physical tools.

Common Misconceptions and Points to Note

First and foremost, keep in mind that this simulation is not an "all-knowing oracle." If you put in arbitrary input parameters, the output will be "garbage in, garbage out." For example, material property data. Many people use catalog values for room temperature data as-is, but in welding simulations, properties like Young's modulus and yield stress at 600°C or 800°C significantly influence the results. The room temperature Young's modulus for SUS304 is about 193 GPa, but at 800°C, it drops to less than half, around 90 GPa. If you get this data wrong, both the deformation and residual stress results will be way off the mark.

Next, errors in constraint condition settings. In reality, the workpiece is firmly fixed by jigs, but if you apply a fully fixed condition (constraining all degrees of freedom) in the simulation, it can sometimes calculate unnaturally high residual stresses. Conversely, if the constraints are too loose, the deformation may appear larger than in reality. For instance, for long butt joints, settings that imagine the actual jig—like constraining only certain directions to allow for thermal expansion-induced "snaking"—are essential.

Finally, don't overlook mesh dependency. Sharp temperature gradients occur around the weld bead, so if you don't use a fine mesh there, you won't accurately capture the temperature or stress fields. However, making the entire mesh too fine will cause computation time to explode. A standard practice is "graded mesh refinement"; for example, using a 1mm mesh near the weld line and a 5mm mesh farther away for a 20mm thick joint. If doubling the mesh density doesn't significantly change the results, you can be reasonably confident.

How to Use

  1. Enter welding parameters: voltage (18–32 V), current (150–350 A), and arc efficiency (0.75–0.85) for your process
  2. Set travel speed (100–600 mm/min) and select base material (mild steel, stainless 316L, aluminum 6061)
  3. Choose joint restraint condition (free, partially restrained, fully fixed) and specify section thickness
  4. Click Calculate to obtain residual stress (σ_res in MPa), angular distortion (θ in degrees), linear shrinkage (δ_L in mm), and post-weld heat treatment (PWHT) stress relief percentage

Worked Example

Butt joint in 8 mm mild steel plate using GMAW: voltage = 24 V, current = 280 A, efficiency = 0.80, travel speed = 200 mm/min. Heat input Q = (24 × 280 × 0.80) / 200 = 26.88 J/mm. With full restraint, residual stress σ_res ≈ 220 MPa (70% of yield), angular distortion θ ≈ 1.8°, linear shrinkage δ_L ≈ 0.65 mm. PWHT at 650 °C for 1 hour reduces σ_res by 45%, yielding 121 MPa.

Practical Notes

  1. Higher heat input (above 30 J/mm) increases HAZ softening in HSLA steels; prioritize speed over current for thick sections
  2. Aluminum exhibits 3× greater shrinkage than steel; use preheat to 150 °C and backstep sequences to manage distortion
  3. Fully constrained joints (box columns, pressure vessels) develop peak tensile stress at fusion line; stress relief is mandatory for fatigue-critical applications
  4. Measure actual distortion with dial indicators on test coupons; FEA predictions typically overestimate by 10–15% due to material nonlinearity