The application of chemical state AES and SAM to the examination of spray-formed aluminium alloy fracture surfaces

1993 ◽  
Vol 20 (7) ◽  
pp. 589-594 ◽  
Author(s):  
M. A. Baker ◽  
P. Tsakiropoulos
Metals ◽  
2019 ◽  
Vol 9 (3) ◽  
pp. 324 ◽  
Author(s):  
Marcin Chybiński ◽  
Łukasz Polus ◽  
Maria Ratajczak ◽  
Piotr Sielicki

The present study focused on the behaviour of the AW-6060 aluminium alloy in peak temper condition T6 under a wide range of loads: tensile loading, projectile and explosion. The alloy is used as a structural component of civil engineering structures exposed to static or dynamic loads. Therefore, it was crucial to determine the material’s behaviour at low and intermediate rates of deformation. Despite the fact that the evaluation of the strain rate sensitivity of the AW-6060 aluminium alloy has already been discussed in literature, the authors of this paper wished to further investigate this topic. They conducted tensile tests and confirmed the thesis that the AW-6060 T6 aluminium alloy has low strain rate sensitivity at room temperature. In addition, the fracture surfaces subjected to different loading (tensile loading, projectile and explosion) were investigated and compared using a scanning electron microscope, because the authors of this paper were trying to develop a new methodology for predicting how samples had been loaded before failure occurred based on scanning electron microscopy (SEM) micrographs. Projectile and explosion tests were performed mainly for the SEM observation of the fracture surfaces. These tests were unconventional and they represent the originality of this research. It was found that the type of loading had an impact on the fracture surface.


2014 ◽  
Vol 891-892 ◽  
pp. 621-626 ◽  
Author(s):  
Fabien Billy ◽  
Gilbert Hénaff ◽  
Guillaume Benoit ◽  
Sjoerd van der Veen

This paper reports on investigations on the residual fatigue resistance of a 2024 aluminium alloy of an A320 aircraft at the end of life. The fatigue data (S-N and da/dN curves) are compared with data obtained on a pristine alloy using a similar procedure. The results are analysed on the basis of fracture surfaces observations and of AFGROW fatigue life computations.


1991 ◽  
pp. 651-659 ◽  
Author(s):  
Katsuyuki Funaki ◽  
Yukio Nanayama ◽  
Yoshiji Ichimaru ◽  
Yukio Hirose ◽  
Keisuke Tanaka

2016 ◽  
Vol 16 (5) ◽  
pp. 1199-1204 ◽  
Author(s):  
Denisa Závodská ◽  
Eva Tillová ◽  
Lenka Kuchariková ◽  
Mária Chalupová

Fractals ◽  
1993 ◽  
Vol 01 (04) ◽  
pp. 1059-1067 ◽  
Author(s):  
J. PLANÈS ◽  
E. BOUCHAUD ◽  
G. LAPASSET

Experimental measurements of the roughness exponent ζ of some fracture surfaces are reported. Whatever the fracture mode, for unbranched (aluminium alloy) or branched (Ni3Al) surfaces, ζ is found quite close to 0.8, in accordance with other experimental determinations, but not with theoretical predictions of standard 3-d models. The complete height distribution for the complex branched structures is shown to slowly decrease with increasing altitude. It implies a power-law behavior for the low order moments which is experimentally recovered. Exponents reveal different from that of gaussian distributions.


Author(s):  
K C H Ashley ◽  
R W Ditchfield ◽  
G A McD Downie

An aluminium alloy (L65) was fatigue tested in a longitudinal tension compression mode at a frequency of 20 kHz with a mean strain of 1.65.10-3. The specimens used were simple cylinderical rods of fully hardened, solution heat treated or fully annealed aluminium alloy. The effects of the variation in heat treatment on the nature of fracture were investigated by examining the fracture surfaces of these specimens in a Cambridge S4-10 scanning electron microscope.The fracture surfaces of the fully hardened alloy exhibited the characteristics of cleavage fracture (Stage I and Stage II cracking) in agreement with Forsyth's theories. Occasionally these specimens underwent an unusual mode of centre initiated failure for which the fatigue endurance was greater than that experienced following the surface initiation in similar specimens.


1986 ◽  
Vol 172 (3) ◽  
pp. 641-667 ◽  
Author(s):  
H.H. Madden ◽  
W.O. Wallace

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