2004
DOI: 10.1111/j.1460-2695.2004.00824.x
|View full text |Cite
|
Sign up to set email alerts
|

Initiation and propagation behaviour of fatigue cracks in hard‐shot peened Type 316L steel in high cycle fatigue

Abstract: A B S T R A C T Observations of fatigue crack growth behaviour were made during rotating-bend testing of hard-shot peened Type 316L steel. From the results of these observations, the crack that developed in the axial direction was observed and the mechanism of the fatigue crack properties was clarified as follows: (1) Small circumferential surface fatigue cracks were detected at 60% of the fatigue lifetime. These cracks propagated very slowly in both the circumferential and radial directions.(2) When a radial … Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
17
0

Year Published

2008
2008
2022
2022

Publication Types

Select...
5
4

Relationship

0
9

Authors

Journals

citations
Cited by 23 publications
(17 citation statements)
references
References 12 publications
(24 reference statements)
0
17
0
Order By: Relevance
“…7 (l). These specimens revealed only one half of the initial RS value, which clearly indicates a relaxation of the surface RS during cyclic loading, which also has been reported for shot-peened steels [19]. This important result will be discussed in detail along with the obtained fatigue data and also in respect to studies dealing with RS, which were cited in the introduction.…”
Section: Residual Stressesmentioning
confidence: 57%
“…7 (l). These specimens revealed only one half of the initial RS value, which clearly indicates a relaxation of the surface RS during cyclic loading, which also has been reported for shot-peened steels [19]. This important result will be discussed in detail along with the obtained fatigue data and also in respect to studies dealing with RS, which were cited in the introduction.…”
Section: Residual Stressesmentioning
confidence: 57%
“…The residual stresses in austenite and martensite phases reach maximum values of about À1230 and À1520 MPa, respectively, at the topmost surface layer, and decrease gradually with increasing depth. In comparison with values obtained by other conventional surface treatments such as shot peening and deep rolling [59], the residual stresses are rather high in the GNS surface layer. Nevertheless, they are still reasonable values while the nanostructured 316L austenitic sample exhibits a yield strength as high as $1450 MPa and it might be much higher in samples with nanostructured martensitic grains [38,39].…”
Section: Residual Stresses Distributionmentioning
confidence: 69%
“…Traditional fatigue design methods are based on this fatigue limit for cycles within 10 7 . However, gigacycle fatigue failures have been reported in many materials, especially for high strength materials, such as high-strength steels [2], case hardening steels [9,10], Ti alloys [11], Mg alloys [12,13] and so on. The fatigue limits for these materials may vanish and fatigue failure can still occur even in the gigacycle regime, which is known as very high cycle fatigue (VHCF) or gigacycle fatigue.…”
mentioning
confidence: 99%