Stress concentration

Stress concentrations occur when there are irregularities in the geometry or material of a structural component that cause an interruption to the flow of stress.

Geometric discontinuities cause an object to experience a localised increase in stress. Examples of shapes that cause stress concentrations are sharp internal corners, holes, and sudden changes in the cross-sectional area of the object as well as unintentional damage such as nicks, scratches and cracks. High local stresses can cause objects to fail more quickly, so engineers typically design the geometry to minimize stress concentrations.

Material discontinuities, such as inclusions in metals, may also concentrate the stress. Inclusions on the surface of a component may be broken from machining during manufacture leading to microcracks that grow in service from cyclic loading. Internally, the failure of the interfaces around inclusions during loading may lead to static failure by microvoid coalescence.

The stress concentration factor, ${\displaystyle K_{t}}$, is the ratio of the highest stress ${\displaystyle \sigma _{\max }}$ to a nominal stress ${\displaystyle \sigma _{\text{nom}}}$ of the gross cross-section and defined as[3]

${\displaystyle K_{t}={\frac {\sigma _{\max }}{\sigma _{\text{nom}}}}}$

Note that the dimensionless stress concentration factor is a function of the geometry shape and independent of its size.[4] These factors can be found in typical engineering reference materials.

Stress concentration around an elliptical hole in a plate in tension

E. Kirsch derived the equations for the elastic stress distribution around a hole. The maximum stress felt near a hole or notch occurs in the area of lowest radius of curvature. In an elliptical hole of length ${\displaystyle 2a}$ and width ${\displaystyle 2b}$, under a far-field stress ${\displaystyle \sigma _{0}}$, the stress at the ends of the major axes is given by Inglis' equation:[5]

${\displaystyle \sigma _{\max }=\sigma _{0}\left(1+2{\cfrac {a}{b}}\right)=\sigma \left(1+2{\sqrt {\cfrac {a}{\rho }}}\right)}$

where ${\displaystyle \rho }$ is the radius of curvature of the elliptical hole. For circular holes in an infinite plate where ${\displaystyle a=b}$, the stress concentration factor is ${\displaystyle K_{t}=3}$.

As the radius of curvature approaches zero, such as at the tip of a sharp crack, the maximum stress approaches infinity and a stress concentration factor cannot therefore be used for a crack. Instead, the stress intensity factor which defines the scaling of the stress field around a crack tip, is used.[2]

There are experimental methods for measuring stress concentration factors including photoelastic stress analysis, thermoelastic stress analysis,[6] brittle coatings or strain gauges.

During the design phase, there are multiple approaches to estimating stress concentration factors. Several catalogs of stress concentration factors have been published.[7] Perhaps most famous is Stress Concentration Design Factors by Peterson, first published in 1953.[8][9] Finite element methods are commonly used in design today.

Known as crack tip blunting, a counter-intuitive method of reducing one of the worst types of stress concentrations, a crack, is to drill a large hole at the end of the crack. The drilled hole, with its relatively large size, serves to increase the effective crack tip radius and thus reduce the stress concentration.[4]

Another method used to decrease the stress concentration is by adding a fillet to internal corners. This reduces the stress concentration and results in smoother flow of stress streamlines.

In a threaded component, the force flow line is bent as it passes from shank portion to threaded portion; as a result, stress concentration takes place. To reduce this, a small undercut is made between the shank and threaded portions.

The sharp corner at the brick has acted as a stress concentrator within the concrete causing it to crack

• The de Havilland Comet aircraft experienced a number of catastrophic failures that were eventually found to be due to fatigue cracks growing from the high stress concentration caused by the use of punched rivet holes around the automatic direction finder cutouts (sometimes referred to as windows). The square passenger windows were also found to have higher stress concentrations than expected and were redesigned.
• Brittle fractures at the corners of hatches in Liberty ships in cold and stressful conditions in winter storms in the Atlantic Ocean.

• A focus point of stress on the margins of an implant, where metal meets bone, of an implanted orthosis is very likely to be the point of failure.

• When Metal Lets Us Down