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Bolt Tensile Stress Area⚠ unverified

Mechanical / Fasteners · Compute the approximate tensile stress area of a bolt

Parameters

InputSymbolUnitDefaultDescription
ddm1.0Nominal bolt diameter
OutputSymbolUnitDescription
resultAtm**2Tensile stress area, in square metres (m**2)

The science & history

Understanding the Parameters

Derivation (Approaching a Proof)

Why not use the minor-diameter area? Because a bolt tested to failure breaks at a load higher than minor-area × strength but lower than nominal-area × strength. Empirically, the load correlates best with the area of a circle whose diameter is the average of the pitch and minor diameters:

$$A_t = \frac{\pi}{4}\left(\frac{d_p + d_r}{2}\right)^2.$$

From thread geometry (Unified/ISO 60° threads), the pitch and minor diameters relate to the major diameter $d$ and pitch $p$ (or threads-per-inch $n = 1/p$) by $d_p = d - 0.6495\,p$ and $d_r = d - 1.2269\,p$. Averaging:

$$\frac{d_p + d_r}{2} = d - 0.9382\,p \quad(\text{ISO metric}).$$

The Unified form uses the slightly different empirical constant $0.9743/n$:

$$A_t = \frac{\pi}{4}\left(d - \frac{0.9743}{n}\right)^2.$$

Setting $n = 6$ gives $0.9743/6 = 0.1624$, the registry's baked-in constant. So the formula is the standard tensile-stress-area relation with the pitch frozen at one coarse value — accurate only for that thread, and imperial in units.

Dimensional check. $[A_t] = (\text{length})^2$; consistent only if $d$ and the $0.1624$ offset share units (both inches). Mixing metres and the inch constant is invalid — see note.

History and Development

The tensile-stress-area concept was calibrated from bolt tension tests in the early-mid 20th century and codified in ASME B1.1 (Unified threads) and ISO 898-1 (metric). Tabulated $A_t$ values for every standard size fill Machinery's Handbook and Shigley; they are the basis of every bolt strength rating. The metric $0.9382\,p$ and Unified $0.9743/n$ forms are the standard closed expressions.

Related Concepts: Bolt Tensile Strength Area, Bolt Proof Load, Bolt Yield Torque, Bolt Thread Stiffness, Thread Stripping Strength

Notes: Prefer tabulated $A_t$ or the pitch-dependent form $\frac{\pi}{4}(d-0.9382p)^2$ (metric). This calculator hard-codes a coarse imperial thread ($n=6$) and is a duplicate of Bolt Tensile Strength Area — flagged for Track B registry cleanup.

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