(b) A steel component in the form of a narrow long plate has a uniform rectangular cross section with 120 mm width and 20 mm thickness. During service the plate is subjected to a tensile axial load which varies between 90 kN to 420 kN. A routine inspection has revealed that a small edge crack has formed in the plate. The crack appears to be through thickness and the plane of the crack is perpendicular to the applied load. The depth of the crack was measured to be 1.3 mm. The stress intensity factor for the configuration is given by K, =1.95 o v n a MNm-3/2. a The plate material has a fracture toughness of 124.9 MNm-3/2 and the fatigue crack growth rate is represented by the Paris-Erdogan equation, da (m/cycle) = 1.24 x 10-11 (AK)2 .4 dN where AK is in MNm-3/2. During service the crack length must not exceed 50% of the critical crack length. Estimate the maximum number of load cycles that can be safely applied to the component.

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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(b) A steel component in the form of a narrow long plate has a uniform
rectangular cross section with 120 mm width and 20 mm thickness. During
service the plate is subjected to a tensile axial load which varies between 90
kN to 420 kN.
A routine inspection has revealed that a small edge crack has formed in the
plate. The crack appears to be through thickness and the plane of the crack is
perpendicular to the applied load. The depth of the crack was measured to be
1.3 mm. The stress intensity factor for the configuration is given by
Κ,-1.95σν πα MNm32
a
W
The plate material has a fracture toughness of 124.9 MNm-3/2 and the
fatigue crack growth rate is represented by the Paris-Erdogan equation,
da
(m/cycle) =
dN
= 1.24 x 10-11 (AK)2.4
where AK is in MNm-3/2.
During service the crack length must not exceed 50% of the critical
crack length. Estimate the maximum number of load cycles that can be
safely applied to the component.
Transcribed Image Text:(b) A steel component in the form of a narrow long plate has a uniform rectangular cross section with 120 mm width and 20 mm thickness. During service the plate is subjected to a tensile axial load which varies between 90 kN to 420 kN. A routine inspection has revealed that a small edge crack has formed in the plate. The crack appears to be through thickness and the plane of the crack is perpendicular to the applied load. The depth of the crack was measured to be 1.3 mm. The stress intensity factor for the configuration is given by Κ,-1.95σν πα MNm32 a W The plate material has a fracture toughness of 124.9 MNm-3/2 and the fatigue crack growth rate is represented by the Paris-Erdogan equation, da (m/cycle) = dN = 1.24 x 10-11 (AK)2.4 where AK is in MNm-3/2. During service the crack length must not exceed 50% of the critical crack length. Estimate the maximum number of load cycles that can be safely applied to the component.
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