𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Prediction on notched fatigue limits for crack initiation and propagation

✍ Scribed by Kewei Xu; Jiawen He


Publisher
Elsevier Science
Year
1992
Tongue
English
Weight
575 KB
Volume
41
Category
Article
ISSN
0013-7944

No coin nor oath required. For personal study only.

✦ Synopsis


Alldraet

-Thef&urepraxgses of micro or small cracks may behave differently as suggested by ~ntinu~ medium mechanics. A minimum fracture unit should exist for a real ~1~ material, for any part sruaher than this unit fracture mechanics caunot be applied. Based on this idea, the elastic stress and stress intensity factor range are expressed in terms of an equivalent fracture unit which is conducted with a through-thickness crack. Theoretical predictions on notched fatigue limits of crack initiation and crack propagation are derived and discus&. Good agreement between predicted values and experimental results has been achieved. equivalent fracture unit non-propagating crack length notch radius notch depth number of a+ wetGent in ur equation stress inundation factor stress intensity factor range threshold AK for a long crack effective threshold AK nominal net stress at a notch local stress m y direction at a notch average stress of up over a series of o* plain fatigue limit of uniaxial loading notched fatigue limit of uniaxial loading theoretical fatigue limit of crack initiation theoretical fatigue limit of crack propagation threshold AK for non-propagating cracks threshold AK for a* at the surface (n = 0)


πŸ“œ SIMILAR VOLUMES


Prediction on fatigue limit of notches w
✍ Xu Kewei; Hu Naisai; Zhou Huijiu πŸ“‚ Article πŸ“… 1995 πŸ› Elsevier Science 🌐 English βš– 293 KB

Theoretical estimation of fatigue limit of notches under axial push-pull loading was made with an emphasis on the formation of non-propagating crack. A critical notch radius and a critical stress concentration factor were determined so as to distinguish notch fatigue limits with crack initiation and

Assessment of concepts for Fatigue Crack
✍ Dr.-Ing. P. Heuler; Dr.-Ing. W. SchΓΌz πŸ“‚ Article πŸ“… 1986 πŸ› John Wiley and Sons 🌐 English βš– 787 KB

In the following, some of the concepts discussed before afie assessed with respect to their ability to predict fatigue lives under variable amplitude loading. Typical trends of results are outlined.

Effect of notch root radius on the initi
✍ M.B.P. Allery; G. Birkbeck πŸ“‚ Article πŸ“… 1972 πŸ› Elsevier Science 🌐 English βš– 407 KB

Under the conditions of constant nominal applied stress. increasing notch root radius causes an increase in the number of cycles to initiate a fatigue crack at a notch root. An explanation of the effect is given in terms of the effective stress concentration factor of the notch. Data are presented w

Four lectures on fatigue crack growth: I
✍ J. Schivje πŸ“‚ Article πŸ“… 1979 πŸ› Elsevier Science 🌐 English βš– 797 KB

Ab&act-Two prediction techniques are introduced, (1) cycle-by-cycle prediction and (2) prediction by correlation. Attention is paid to the problem of describing varhbk-amplitude loading in terms of load cycles. Aspects of fatigtue damage am reviewed with reference to in&action effects and weakoesses

Verification of Fatigue Life Prediction
✍ Prof. Dr. A. Buch πŸ“‚ Article πŸ“… 1981 πŸ› John Wiley and Sons 🌐 English βš– 894 KB

## Abstract Crack initiation life estimates obtained with the local strain approach (LSA) and with the conventional nominal stress approach (NSA) were compared with experimental results obtained with stress block loading programs and flight simulation gust random loading programs. Programs with and