Stress Intensity Calculation for Beam Cracks

In summary: So, in summary, the stress intensity factor for the maximum and minimum stresses is calculated, as well as the stress intensity difference. The fracture toughness is also calculated and compared to the stress intensity factor at the critical crack size to determine if the crack is critical.
  • #1
thephysicsman
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Homework Statement



[PLAIN]http://img232.imageshack.us/img232/8514/unbenannthz.png

In this system, a single-span beam is exposed to the following stresses:

[tex]\sigma_{max}= 255 Mpa[/tex] at [tex]F_{max} = 50 kN[/tex] and
[tex]\sigma_{min}= 102 MPa[/tex] at [tex]F_{min} = 20 kN[/tex]

The stress range is accordingly [tex]\Delta\sigma = 153 MPa[/tex]

A crack is detected during an inspection of the construction. This runs in the bottom flange of the support, and has a length of 2a = 5 mm. The flange has a thickness of 2t = 10 mm.

[PLAIN]http://img62.imageshack.us/img62/3403/unbenanntcc.png

[tex]f(\frac{a}{t})[/tex] = 1.186

a) Calculate the stress intensity K for the maximum and minimum stress!

b) Calculate stress intensity difference [tex]\Delta K[/tex]!

c) A fracture test of the steel of the beam is carried out. The test specimen has a [tex]a_{0}/W[/tex] ratio of 0.5335. The data record below was recorded during the test.

[PLAIN]http://img830.imageshack.us/img830/6829/unbenannthty.png

Determine the fracture toughness [tex]K_{IC}[/tex] using the following formula and check if the crack is critical!

[tex]f(\frac{a_{0}}{W})=2.97[/tex]

[tex]K_{IC}=\frac{F_{max}*S}{\sqrt{B*B_{N}}W^{1.5}}f(\frac{a_{0}}{W})[/tex]

[tex]a_0 = 13,87 mm[/tex], W = 26 mm, B = 13 mm, [tex]B_N = 10,4 mm[/tex], S = 104 mm!

Homework Equations



[tex]K_{component}=\sigma \sqrt{\pi a} f(\frac{a}{t})[/tex]

The Attempt at a Solution



a)

[tex]K_{component, max}=255 MPa \sqrt{\pi 0.0025 m} 1.186 = 26.80 Mpa \sqrt{m}[/tex]

[tex]K_{component, min}=102 MPa \sqrt{\pi 0.0025 m} 1.186 = 10.72 Mpa \sqrt{m}[/tex]b)

[tex]\Delta K = 26.80-10.72 = 16.08 Mpa \sqrt{m}[/tex]

c)

[tex]K_{IC}=\frac{50 000 N*0.104m}{\sqrt{0.013m*0.0104m}0.026^{1.5}}2.97=317 MPa\sqrt{m}[/tex]Is this correct, or is there something that I have not understood?
 
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  • #2


Your calculations for parts a and b are correct. For part c, your calculation for K_IC is correct, but you also need to consider the stress intensity factor at the critical crack size, which is given by K_c = K_IC / f(a_0/W). This value should be compared to the calculated K_component values to determine if the crack is critical.
 

1. What is stress intensity calculation for beam cracks?

Stress intensity calculation for beam cracks is a method used to determine the magnitude of stress at the tip of a crack in a beam. It takes into account the geometry of the beam, the loading conditions, and the material properties to calculate the stress at the crack tip.

2. Why is stress intensity calculation important for beam cracks?

Stress intensity calculation is important because it helps engineers and scientists understand the behavior of cracks in beams and predict when they may fail. It also allows for the determination of critical crack sizes, which can help prevent catastrophic failures.

3. How is stress intensity calculated for beam cracks?

Stress intensity is typically calculated using analytical methods, such as the stress intensity factor (SIF) equations, or numerical methods, such as finite element analysis (FEA). These methods take into account the dimensions of the beam, the applied load, and the material properties to determine the stress at the crack tip.

4. What factors affect stress intensity in beam cracks?

There are several factors that can affect stress intensity in beam cracks, including the geometry of the beam, the type and magnitude of the applied load, and the material properties. The size and shape of the crack also play a significant role in determining stress intensity.

5. How can stress intensity calculations for beam cracks be used in real-world applications?

Stress intensity calculations for beam cracks are used in a variety of real-world applications, including the design and maintenance of structures such as bridges, buildings, and aircraft. It can also be used in failure analysis and risk assessment to determine the likelihood of crack propagation and potential failure.

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