σ = F / A
The same force creates higher stress in a smaller section.
The same force creates higher stress in a smaller section.
Select a target and calculate.
The same force creates higher stress in a smaller section.
10 kN / 100 mm² = 100 MPa.
Concentric, uniformly distributed load; notches and bending are excluded.
This calculator finds the missing quantity among normal stress σ, force F and cross-sectional area A from the other two. It explains why designing tension members, cables and bolts depends not on force alone but on the ratio of force to bearing cross-section for safety or failure.
The average normal stress in a cross-section under tension or compression is force relative to the bearing area: σ = F/A. It describes internal material loading, independent of the part's absolute size.
An elevator cable and a rigging chain for the same load can be sized very differently: a thinner cable experiences higher stress than a thicker one at the same load. That's why standards for passenger elevators mandate safety factors of about 8 to 10 times breaking load, while general lifting equipment is often designed to a minimum factor of 5.
σ = F / A
σ = F / AF = σ · AA = F / σ| Symbol / input | Meaning |
|---|---|
| Normal stress σ | Average stress normal to the section. |
| Axial force F | Tension or compression force through centroid. |
| Load-bearing area A | Net area normal to force; subtract holes. |
Enter two of the three quantities. Stress requires force and area, force requires stress and area, area requires force and stress. Use the actual bearing net area; holes or notches must be subtracted where applicable.
Select the target quantity and enter the two known values with units. Compare the result against the material's allowable stress (yield strength divided by a safety factor) afterward, not directly against tensile strength.
Given F = 10,000 N and A = 100 mm², substitution gives σ = 10,000 N / 100 mm² = 100 MPa.
A stress of 100 MPa means a force of 100 newtons acts on every square millimetre of the considered cross-section. Whether this is safe depends on the material: for structural steel with a yield strength of about 235-355 MPa, this stress sits well within the elastic range, while for many aluminium alloys it can already be close to yield.
The SI unit is the pascal (Pa = N/m²), but N/mm² (equal to MPa) is more practical in engineering, since 1 N/mm² = 1 MPa. Component tables often use N/mm² because it matches typical millimetre dimensions directly.
For passenger elevators, standards such as EN 81 and ASME A17.1 mandate safety factors of about 8:1 to 10:1 against the breaking load of the suspension means. General lifting and rigging equipment is often instead designed to a minimum safety factor of about 5:1. The required factor depends on the risk to people, load type (static or dynamic), and the applicable standard, and does not substitute for verification against the rules governing the specific application.
Stress calculations are used to design tension members, cables, chains, bolted joints, rigging equipment, and components under simple tension or compression.
The formula gives an area-averaged stress for a concentric, uniformly distributed load. Notches, holes, section changes or off-centre force application create local stress concentrations well above this calculated average, requiring a separate notch-factor or FEA analysis.
Common mistake: Do not compare calculated stress directly against tensile strength — compare it against the allowable stress (usually yield strength divided by a safety factor). Also, do not use the unweakened gross cross-section for notched or drilled sections, since actual stress at the notch can be considerably higher than the average.
It depends on the material: for structural steel with typical yield strengths of 235-355 MPa, this is well within the safe range; for weaker materials it may already be critical. What matters is comparison with allowable stress, not an absolute number.
To cover uncertainty in material, manufacturing, load assumptions and ageing. Depending on application and standard, typical factors range from about 1.5 (general mechanical engineering) to 10 (passenger elevators).
Because a local stress concentration (notch effect) occurs at the edge of the hole, well above the stress averaged over the net cross-section.