Fatigue behaviour of a commercial aluminium alloy in sea water at different temperatures

1993 ◽  
Vol 45 (3) ◽  
pp. 297-307 ◽  
Author(s):  
Mohamed Ragab Bayoumi
Volume 3 ◽  
2004 ◽  
Author(s):  
L. Han ◽  
K. Young ◽  
R. Hewitt ◽  
A. Chrysanthou ◽  
J. M. O’Sullivan

Self-piercing riveting, as an alternative joining method to spot-welding, has attracted considerable interest from the automotive industry and has been widely used in aluminium intensive vehicles. One of the important factors that need to be considered is the effect of cyclic loading in service, leading to possible fatigue failure. The previous work reported in the public domain on the behaviour of self-piercing rivets has mainly focused on static tests. The work which is reported in this paper is concerned with the fatigue behaviour of single-rivet joints, joining two 2mm 5754 aluminium alloy sheets. The investigation also examined the effect of interfacial conditions on the fatigue behaviour. A number of fatigue failure mechanisms were observed based on rivet fracture, sheet fracture and combinations of these. The investigation has shown that they were dependent on the applied load and the sheet surface condition. Three-parameter Weibull analysis, using Reliasoft Weibull ++5.0 software, was conducted to analyse the experimental results. The analysis enabled the prediction of early-type failure (infant mortality failure) and wear-out failure patterns depending on the condition of the self-piercing riveted joints and the alloy sheet surface.


2006 ◽  
Vol 22 (4) ◽  
pp. 253-262 ◽  
Author(s):  
E. S. Puchi-Cabrera ◽  
R. Maccio ◽  
M. H. Staia

2019 ◽  
Vol 42 (9) ◽  
pp. 1980-1990 ◽  
Author(s):  
Enrico Salvati ◽  
Joris Everaerts ◽  
Koji Kageyama ◽  
Alexander M. Korsunsky

Author(s):  
T Vuherer ◽  
J Kramberger ◽  
D Milčić ◽  
M Milčić ◽  
S Glodež

1962 ◽  
Vol 66 (614) ◽  
pp. 128-129 ◽  
Author(s):  
C. T. Mackenzie ◽  
P.P Benham

A recent paper(1) gives details of an investigation on the low endurance fatigue behaviour of an aluminium-zinc-magnesium alloy (D.T.D. 683). It becomes apparent in subsequent discussion that information on another aluminium alloy to B.S. L65C would satisfy a wider practical interest than the former. Although the equipment used for the earlier work was engaged on another project, it was decided that the latter should be halted for a period to enable a brief programme on low endurance fatigue to be conducted on B.S. L65C material which had previously been kindly provided by the Aluminium Development Association.


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