Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN: 9780190698614
Author: Sadiku, Matthew N. O.
Publisher: Oxford University Press
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A strain gauge mounted at a potentially critical point in a steel part has recorded the stress history shown below during 20 seconds of typical use. Identical parts have been fatigue tested under constant amplitude loading with R = -1 to give an endurance limit of 60 ksi and a fatigue strength of 140 ksi at N = 1000 cycles. The steel used has an ultimate strength of 165 ksi. Estimate the fatigue life of the part under typical use.

How much will the fatigue life in problem 3 (above) be reduced if a mean stress of 10 ksi is added to the stress history given?

A strain gauge mounted at a potentially critical point in a steel part has recorded the stress history
shown below during 20 seconds of typical use. Identical parts have been fatigue tested under
constant amplitude loading with R = -1 to give an endurance limit of 60 ksi and a fatigue strength
of 140 ksi at N = 1000 cycles. The steel used has an ultimate strength of 165 ksi. Estimate the
fatigue life of the part under typical use.
stress (ksi)
120
100
80
60
40
20
0
-20
-40
-60
-80
-100
-120
How much will the fatigue life in problem 3 be reduced if a mean stress of 10 ksi is added to the
stress history given?
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Transcribed Image Text:A strain gauge mounted at a potentially critical point in a steel part has recorded the stress history shown below during 20 seconds of typical use. Identical parts have been fatigue tested under constant amplitude loading with R = -1 to give an endurance limit of 60 ksi and a fatigue strength of 140 ksi at N = 1000 cycles. The steel used has an ultimate strength of 165 ksi. Estimate the fatigue life of the part under typical use. stress (ksi) 120 100 80 60 40 20 0 -20 -40 -60 -80 -100 -120 How much will the fatigue life in problem 3 be reduced if a mean stress of 10 ksi is added to the stress history given?
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