How to calculate Stress Intensity Factor?

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SUMMARY

This discussion focuses on calculating the Stress Intensity Factor (SIF) for a flat circular disc subjected to a central point load, with a crack present on the bottom surface. The key approach involves calculating the stress under the point load without the crack using resources like "Roark's Formulas for Stress and Strain." The SIF is determined using the formula Ki = (max stress without crack)(Y)(sqrt(C)), where Y is a geometric factor and C is the crack depth. For brittle materials such as glass, the critical stress intensity factor (Kic) is approximately 1 MPa(m^1/2), which is essential for assessing failure risk.

PREREQUISITES
  • Understanding of fracture mechanics principles.
  • Familiarity with stress analysis techniques for circular plates.
  • Knowledge of stress intensity factor calculations.
  • Experience with finite element analysis tools like ANSYS or Abaqus.
NEXT STEPS
  • Study "Roark's Formulas for Stress and Strain" for foundational stress analysis.
  • Learn about the derivation of stress equations for simply supported circular plates.
  • Explore the application of ANSYS or Abaqus for modeling crack behavior in materials.
  • Research the properties of brittle materials and their critical stress intensity factors.
USEFUL FOR

Graduate students in engineering, researchers in fracture mechanics, and professionals involved in material failure analysis will benefit from this discussion.

saurabh anand
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Hello everyone,
I am currently doing my masters research project on fracture mechanics. My problem is such that I have a flat circular disc(brittle) which is simply supported around its circumference. The top surface of the disc is subjected to a point load at its centre. the bottom surface has a crack of a given length and a depth of less that half the thickness of the plate ( part through crack). This crack passes through the centre of the plate. What kind of forces will the crack experience? and how can I calculate the stress intensity factor at any point on this crack. There has been a lot of work previously carried out for plates with remote tensile and bending loads on the edges of the plate. I am not sure which category my problem falls into because I am applying a local force at the centre. thanks in advance. Any help will be deeply appreciated.
 
Thank you for the information. I will look into it.
 
I am not very sure how to derive the mathematical equation for the stress field. But the way I would follow is to first look at and understand how the equations for simple supported circular plate with point load at the center are derived from first principles. What this will do is to give you a better perspective of the problem to be solved. I liked the book "Stresses in Plates and shells" by Ugural. You can perhaps look into that. Also Fracture Mechanics notes by Alan Zehnder from Cornell can be looked into. Then in the same problem without crack introduce a crack which is represented by zero traction boundary conditions.Try to solve for the stress function and solve with the s.s. plate with point load BC's.
Then may be you can solve the original problem using Ansys/Abaqus and look at the results.
 
If crack runs along major diameter then it will experience bending forces tending to hinge open the crack .

If crack is of trivial depth compared to plate dimensions then stresses can be approximated using analysis of a solid plate and then treating crack as a stress raiser .

If crack is of significant depth then an analytic solution is only possible if shape and size of crack can be described by a limited range of mathematical functions .

Apart from a few trivial cases solving the resulting equations is very difficult indeed .
 
Thankyou Koolraj09 the approach you suggested is exactly how I am going about it. thanks for the reference book. I will look into it.
 
Nidum thanks for the reply. the crack in my case is of trivial depth.
 
saurabh anand said:
Hello everyone,
I am currently doing my masters research project on fracture mechanics. My problem is such that I have a flat circular disc(brittle) which is simply supported around its circumference. The top surface of the disc is subjected to a point load at its centre. the bottom surface has a crack of a given length and a depth of less that half the thickness of the plate ( part through crack). This crack passes through the centre of the plate. What kind of forces will the crack experience? and how can I calculate the stress intensity factor at any point on this crack. There has been a lot of work previously carried out for plates with remote tensile and bending loads on the edges of the plate. I am not sure which category my problem falls into because I am applying a local force at the centre. thanks in advance. Any help will be deeply appreciated.
Here is what you need to do. Calculate the stress under point load with no crack- use a book like ROARK for this. The stress intensity is given as
stress = Ki/(y) (SQRT(C) where c is flaw depth and Y = 1.26, for penny crack. Thus Ki = (max stress without crack)(y)( sqrt(C)). If stress intensity is less than critical stress intensity factor, Kic. then it will not fail. Kic = inherent property of material which you need to know. For britle materials like glass Kic = about 1MPa (m^1/2). The stress is in Mpa and the flaw depth is in meters. Note that stress must be in tension for failure to occur.
Edit: I corrected the equations as now noted above.
 
Last edited:

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