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Equation 4 · Part 1 · Why Materials Fail: Fracture, Flaws and the Inspection Interval

Symbol sigma_max

σmax⁡=σ∞(1+2aρ).\sigma_{\max} = \sigma_\infty\left(1 + 2\sqrt{\frac{a}{\rho}}\right).
σmax⁡\sigma_{\max}

What this part means

sigmama_max is part of the quantity the equation computes from the expression on the right.

Its job in the formula

sigmama_max is part of the quantity the equation computes from the expression on the right.

The passage around this formula

The first half of the argument is purely elastic and predates Griffith. An elliptical hole in a stressed plate does not merely remove load-bearing material; it redistributes the stress that would have passed through that material into the region around the hole’s sharpest curvature. For an elliptical flaw of half-length a and tip radius of curvature ρ\rho in a plate under remote tension σ∞\sigma_\infty , the peak stress at the tip is approximately σmax⁡=σ∞(1+2aρ)\sigma_{\max} = \sigma_\infty\left(1 + 2\sqrt{\frac{a}{\rho}}\right). Three things follow. First, the concentration depends on the flaw’s aspect ratio, not on its absolute size — a long shallow scratch and a short sharp one can concentrate stress equally. Second, as the tip sharpens toward an…

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