What is the purpose of a stress concentration factor?

AI Thread Summary
Stress concentration factors arise from inconsistencies in material shape under load, affecting crack propagation. Drilling a hole in a crack, known as "stop drilling," redistributes stress over a larger area, effectively blunting the crack tip and delaying further propagation. This method is commonly used in aircraft structures to manage crack growth. The mathematical principle indicates that as a crack sharpens, the stress concentration factor increases, thus making it beneficial to blunt the crack. Overall, this technique helps mitigate the risks associated with crack tips in materials under stress.
Cvan
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Hello, in a recent lecture on introductory engineering, our professor made reference to a stress concentration factor that pops up due to inconsistencies or changes in the shape of a material subject to a load.

The introduction he gave referenced a method of stopping cracks by drilling a hole in them, and this point didn't settle well with me. It seems counterintuitive--the only way I was able to reconcile with this idea is in--say a steel rectangular bar, that the hole's added area to the bar creates a larger surface for the crack to attempt to propagate along (the area I mean is (pi*diameter)(depth of material).

Is this an incorrect way of thinking about this situation? Or does it just mean that the stress concentration factor of a crack in a member under load is greater than one with a hole in it--and why?
 
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Without knowing the specifics, e.g. geometry, I think the professor is implying that drilling a hole effectively blunts the crack, and the local stress in the material is redistributed over a large surface rather in the vicinity of the crack tip, which is usually very sharp.
 
Astronuc said:
Without knowing the specifics, e.g. geometry, I think the professor is implying that drilling a hole effectively blunts the crack, and the local stress in the material is redistributed over a large surface rather in the vicinity of the crack tip, which is usually very sharp.
That is exactly the point being made. That is a very common method for stopping/delaying crack propagation in aircraft structures (when in areas allowed) and is known as "stop drilling". The tip of a crack is an extremely complex area. The drill spot opens up that geometry and spreads the loading out over a larger area as Astronuc pointed out. Fatigue in the crack tip zone still is a point of concern though.
 
ok here's the mathematical reply.

If you have an elliptical crack in an infinite plate, the Stress Concentration factor theory says that the stress at the vicinity of the crack is SCF = 1 + 2a/b. So, as the crack goes sharper (a/b increases), the SCF increases. The idea then is to reduce the SCF by making it blunt.
 
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