7. The fatigue crack growth data as shown in the table are obtained under the air environment of the laboratory under the R = -1, -200MPa cyclic load of a central crack aluminum. a/mm 2.23 2.25 2.28 2.35 2.41 2.49 2.62 2.96 3.58 4.59 5.08 5.56 N/10³ 80 105 110 115 125 130 135 140 145 147 147.4 147.5 (a) Draw a max - N curve da (b) Draw Ig()-1g (AK) curve, and divide three zones according to the dN fatigue crack growth rate. (c) The linear part in the figure is described by Paris formula, and the parameters C and m are determined. Please calculate the C and m

Elements Of Electromagnetics
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7. The fatigue crack growth data as shown in the table are obtained under the air
environment of the laboratory under the R = -1, -200MPa cyclic load of a
central crack aluminum.
a/mm 2.23 2.25 2.28 2.35 2.41 2.49 2.62 2.96 3.58 4.59 5.08 5.56
N/10³ 80 105 110 115 125 130 135 140 145 147 147.4 147.5
(a) Draw a
max
-
N curve
da
(b) Draw Ig()-1g (AK) curve, and divide three zones according to the
dN
fatigue crack growth rate.
(c) The linear part in the figure is described by Paris formula, and the parameters C
and m are determined. Please calculate the C and m
Transcribed Image Text:7. The fatigue crack growth data as shown in the table are obtained under the air environment of the laboratory under the R = -1, -200MPa cyclic load of a central crack aluminum. a/mm 2.23 2.25 2.28 2.35 2.41 2.49 2.62 2.96 3.58 4.59 5.08 5.56 N/10³ 80 105 110 115 125 130 135 140 145 147 147.4 147.5 (a) Draw a max - N curve da (b) Draw Ig()-1g (AK) curve, and divide three zones according to the dN fatigue crack growth rate. (c) The linear part in the figure is described by Paris formula, and the parameters C and m are determined. Please calculate the C and m
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