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Material fatigue and stress |
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| Jan4-04, 11:09 AM | #1 |
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Material fatigue and stress
Could you please explain what each of the following symbols stand for:
da/dN=A(^K)m I have worked out that da is the crack length i have worked out that dN is the number of cycles Are both of these correct? Thanks |
| Jan4-04, 04:24 PM | #2 |
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What you have is a simplified model of the rate of crack propagation:
[tex] \frac{da}{dN} = A\Delta K^m [/tex] 2*a is the crack length (not da), N is the number of cycles (not dN). ΔK is the stress intensity factor range: [tex] \Delta K = Y\sqrt{\pi a}(\sigma_{\rm max} - \sigma_{\rm min}) [/tex] (Y is a crack geometry factor). A and m are empirical constants (found by plotting log(da/dN) versus log(ΔK)). |
| Jan5-04, 03:36 AM | #3 |
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Thanx for the help.
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| Jan5-04, 07:07 AM | #4 |
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Material fatigue and stress
you said that Y is a crack geometry factor, how do you find the crack geometry factor??
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| Jan5-04, 04:52 PM | #5 |
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It depends on the shape/aspect ratio of the crack. Hopefully, there is a table or explanation in your textbook. Here's a page I found with a bunch of them that might help:
http://www.ems.psu.edu/~green/436-8C.pdf |
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