Check shear stress for bolts in seconds today. Choose units, planes, and bolt counts easily. Download CSV or PDF for clear engineering reports anytime.
Bolt shear stress is computed from the total applied shear load divided by the effective resisting area.
If shank area is selected, the calculator uses A = πd²/4. Use custom area when the shear plane passes through threads or reduced sections.
These examples show typical inputs and resulting stresses. Values are illustrative.
| Total Load (N) | Bolts (n) | Planes (p) | Diameter (mm) | Area/Plane (mm²) | Shear Stress (MPa) |
|---|---|---|---|---|---|
| 12000 | 2 | 1 | 12 | 113.097 | 53.051 |
| 18000 | 3 | 2 | 10 | 78.540 | 38.197 |
| 25000 | 4 | 2 | 16 | 201.062 | 15.539 |
Shear stress is the tangential stress a bolt resists when plates try to slide. This calculator reports stress in MPa and psi. Remember: 1 MPa = 1 N/mm², so using millimeters keeps the math direct and clean for design checks.
The tool uses τ = V / (n × p × A). Here, V is total shear load, n is bolt count, p is shear planes per bolt, and A is shear area per plane. Increasing n or p reduces stress linearly.
In single shear, p = 1. In double shear, p = 2, which ideally halves the stress for the same bolt area. For example, with identical bolts and load, moving from 1 to 2 planes cuts τ by about 50% if load distribution is even.
Shank area uses A = πd²/4. A 12 mm shank gives about 113.10 mm². If the shear plane crosses threads, the effective area is smaller, raising stress. Use the custom area option when you know a reduced net area.
Real joints rarely share load perfectly. Eccentricity, clearance, and plate stiffness can bias load to a few bolts. A practical approach is to check a conservative case by reducing the effective bolt count or applying a distribution factor before entering V.
The calculator converts 1 lbf = 4.448 N, 1 in = 25.4 mm, and 1 in² = 645.16 mm². Stress converts as 1 MPa ≈ 145.038 psi. These constants help compare catalog data with metric-based joint geometry.
If you enter an allowable shear stress, the tool adds utilization and factor of safety. Utilization is τ/τallow. Values under 1.00 indicate the stress is below allowable. Factor of safety is the inverse, τallow/τ.
Suppose V = 12,000 N, n = 2, p = 1, d = 12 mm. Area per plane is about 113.10 mm², effective area is 226.19 mm², and τ ≈ 53.05 MPa. If allowable is 150 MPa, utilization is about 0.35 and safety factor is about 2.83.
Shear load is the total force trying to slide parts. Shear stress is that force divided by resisting area. Stress depends on bolt size, bolt count, and the number of shear planes.
Use custom area if the shear plane passes through threads, a reduced shank, or a drilled region. Enter the net area you trust from standards, drawings, or supplier data.
It halves stress only when both planes carry load evenly and the geometry is symmetric. If clearances or stiffness differences exist, one plane may attract more load.
MPa matches N/mm² and is common in metric design, while psi appears often in catalogs and legacy drawings. Showing both helps you compare results without manual conversions.
Yes, if the resisting element behaves like a round shank in shear and the load path is similar. Ensure the correct shear area and planes, and confirm any code-specific factors separately.
Use an allowable value from your design code or material specification. Many standards provide allowables based on bolt grade and safety factors. Avoid guessing when the application is critical.
Count the shear interfaces crossed by each bolt. A simple lap joint is usually 1 plane. A double-lap joint often has 2 planes. Complex stacks can have more, depending on the load path.
Important Note: All the Calculators listed in this site are for educational purpose only and we do not guarentee the accuracy of results. Please do consult with other sources as well.