Brittle crack growth in normally ductile materials

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SUMMARY

Brittle crack growth in normally ductile materials can be effectively mitigated by drilling holes at the ends of macroscopic cracks to reduce internal stresses, thereby arresting crack propagation. This method is routinely employed in aircraft maintenance to enhance service life and prevent catastrophic failures. An industrial example is documented in the NRC report (ML013400370), which includes a formula for stress concentration around an elliptical crack arresting hole. Adhering to established procedures is crucial to avoid introducing new issues during this repair process.

PREREQUISITES
  • Understanding of brittle fracture mechanics
  • Familiarity with ductile materials properties
  • Knowledge of stress concentration factors
  • Experience with aircraft maintenance protocols
NEXT STEPS
  • Research the NRC report ML013400370 for detailed case studies
  • Study stress concentration around elliptical holes in materials
  • Learn about crack arresting techniques in aerospace engineering
  • Explore guidelines for maintenance procedures in load-bearing structures
USEFUL FOR

Engineers, materials scientists, and maintenance professionals involved in structural integrity assessments and repair strategies for ductile materials in various applications, particularly in aerospace and heavy machinery.

C0rnNutts
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Hey guys,
I'm new here so please be easy on me if I break any "unwritten" rules.
I'm doing a design study on brittle crack growth in ductile materials. As I understand it, when a macroscopic crack is found in a load bearing plate, holes can be drilled at each end to reduce the internal stresses at the crack tips and therefor arrest the growth. My question is: Does anyone know of a specific instance where this method was used to prevent failure and increase service life? Alternatively, an instance where this method could have been used to prevent a failure but was not?
Thanks in advance!
 
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Does anyone know of a specific instance where this method was used to prevent failure and increase service life?
We hillbillies do it all the time on our shovels and tractor fenders.

An industrial example is mentioned around page six here:

http://pbadupws.nrc.gov/docs/ML0134/ML013400370.pdf

about page 22 is a formula for stress concentration around an elliptical crack arresting hole.
Surely a search engine will take you places.. just have to feed it the right keywords. Maybe that report will help you with vocabulary.
 
Last edited:
Drilling a hole to arrest a crack is almost routine in aircraft maintenance.
Usually the specifications allow for small failures, but larger ongoing breaks are taboo. Do note that there are procedures to ensure that this does not cause additional problems.
 

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