τw = F / (a · leff)
The force is carried across the throat area a·leff; a thinner or shorter weld raises stress proportionally.
The force is carried across the throat area a·leff; a thinner or shorter weld raises stress proportionally.
Select a target and calculate.
The force is carried across the throat area a·leff; a thinner or shorter weld raises stress proportionally.
10 kN across a = 5 mm and leff = 80 mm give τw = 25 MPa.
Simplified method per DIN EN 1993-1-8: resultant stress in the throat section, uniform along the weld length; notch effects and residual stress are excluded.
This calculator finds the nominal shear stress in a fillet weld from the transmitted force, the throat thickness a and the effective weld length leff, using the simplified method.
In the simplified method per DIN EN 1993-1-8, the entire force acting on the weld is treated as uniformly distributed over the throat area a·leff: τw = F/(a·leff). The actual stress distribution along the weld and across the oblique throat section is less uniform; the simplified method gives a conservative, easy-to-follow design value instead.
Picture the fillet weld as a thin, angled web carrying the entire load from one plate to the other. The thinner (smaller a) or shorter (smaller leff) that web is, the more force the same area must carry and the higher the stress — just like a thinner rope carrying the same load.
τw = F / (a · leff)
τw = F / (a · leff)F = τw · a · leffa = F / (τw · leff)| Symbol / input | Meaning |
|---|---|
| Weld shear stress τw | Nominal shear stress in the throat section. |
| Force F | Force transmitted across the weld. |
| Throat thickness a | Throat thickness of the inscribed triangle in the weld cross-section. |
| Effective weld length leff | Load-carrying weld length after deducting end craters. |
F is the force to be transmitted across the weld, a is the throat thickness (the height of the inscribed isosceles triangle in the weld cross-section), and leff is the effective weld length after deducting end craters at both ends.
Enter F, a and leff to get τw. For sizing, instead enter τw as the allowable value and two of the other three quantities to find the third (usually a).
F = 10 kN, a = 5 mm and leff = 80 mm give τw = 10,000 N / (5 mm · 80 mm) = 25 MPa.
τw = 25 MPa is the nominal, uniformly assumed shear stress in the throat section. Compare it against the weld's allowable stress, e.g. via the weld safety factor calculator.
F is usually given in N or kN, a and leff in mm, and the resulting stress in MPa (N/mm²).
For a symmetric 45° fillet weld with leg length s, the throat thickness is a = s·cos(45°) ≈ 0.7·s, because a is the height of the inscribed right triangle from the root point to the weld surface — the shortest path along which the weld can fail in the governing section. Mistakenly using the leg length instead of a overstates the weld's capacity by about 40%.
The formula is used for preliminary sizing of fillet welds on steel structures, machine frames, brackets and welded gusset connections.
The simplified method neglects the split into longitudinal and transverse shear stress in the oblique throat section, as well as notch effects and residual stress from welding. Highly loaded or fatigue-critical joints require the more detailed DIN EN 1993-1-8 method (items 30–33).
Common mistake: A common mistake is using the plate thickness t instead of the actual throat thickness a — for a symmetric 45° fillet weld, a is noticeably smaller than the leg length. End craters at the weld ends are also sometimes forgotten, overstating the effective length.
a is the throat thickness (height of the inscribed triangle); the leg length is the visible side length of the weld; at 45° a ≈ 0.7 · leg length.
Subtract twice the throat thickness a from the actual weld length l for end craters at both ends, unless the weld runs fully around a closed shape.
For preliminary sizing, yes; for a code-compliant DIN EN 1993-1-8 check, the more detailed directional method with an equivalent stress is usually required.
The formula treats the resultant force per unit length as pure shear in the throat section; combined tension and shear needs an equivalent stress from the more detailed method.
The resulting τw feeds directly into that calculator as the actual stress σ/τ, to determine the safety factor against the allowable stress.