Parametric Study on Fatigue Life Design of Shaft with Holes
2011 ◽
Vol 295-297
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pp. 2366-2369
Keyword(s):
The prevention of fatigue failure is an important consideration in the design of aeroengine shafts. In this paper, based on the elastic and elstic-plastic finite element analyses, for a series of small-scale hollow shafts with transverse holes, the maximum princple stress and von Mises stresss around the hole have been obtained. Hence, using McDiarmid and Von Mises criteria, the fatigue crack initiation site and life can be determined. The hoop stress, which is the driving force for the Mode I growth of short cracks initiated around the hole, has been characterised as well.
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2004 ◽
Vol 449-452
◽
pp. 561-564
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2008 ◽
Vol 74
(739)
◽
pp. 329-334
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Keyword(s):
2017 ◽
Vol 40
(11)
◽
pp. 1718-1730
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1989 ◽
Vol 111
(4)
◽
pp. 363-367
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2018 ◽
Vol 8
(4)
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Keyword(s):