What is the purpose of a stress concentration factor?

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SUMMARY

The discussion centers on the purpose of the stress concentration factor (SCF) in materials under load, particularly in the context of crack propagation. It is established that drilling a hole at the tip of a crack, a technique known as "stop drilling," redistributes stress over a larger area, effectively blunting the crack and reducing the SCF. The mathematical relationship for an elliptical crack in an infinite plate is defined as SCF = 1 + 2a/b, where increasing the sharpness of the crack (a/b ratio) raises the SCF. This method is commonly employed in aircraft structures to delay crack propagation.

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  • Understanding of stress concentration factors in materials
  • Familiarity with crack propagation mechanics
  • Knowledge of stop drilling techniques in engineering
  • Basic grasp of mathematical relationships in material science
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  • Research the mathematical modeling of stress concentration factors in various geometries
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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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