Plastics. Determination of mode I plane-strain crack-arrest toughness

2014 ◽  
1980 ◽  
Vol 8 (1) ◽  
pp. 25 ◽  
Author(s):  
KC Lieb ◽  
RT Horstman ◽  
B Power ◽  
RL Meltzer ◽  
MB Vieth ◽  
...  

1975 ◽  
Vol 97 (4) ◽  
pp. 291-298 ◽  
Author(s):  
P. B. Crosley ◽  
E. J. Ripling

The data presently available on the plane strain crack arrest toughness (KIa) of steels are reviewed, using as a definition of KIa the stress intensity factor, K, a short time after a run-arrest segment of rapid crack extension. The data indicate that KIa, defined in this way, is a material property, i.e., it is independent of the manner in which it is measured. Calculations, available in the literature, on the dependence of dynamic K on a crack velocity are used to justify this invariance. It is also shown that KIa may be the minimum value of toughness, at a given temperrature, as a function of loading rate.


1988 ◽  
Vol 110 (2) ◽  
pp. 129-136 ◽  
Author(s):  
K. Kussmaul ◽  
R. Gillot

In order to determine the influence of the test temperature on the crack arrest toughness, investigations were carried out on pressure vessel steels of various strength and toughness up to the upper-shelf of the Charpy V-notch impact energy (CV-energy). The tests were conducted on the basis of the proposed ASTM test method for ferritic steels with modified wedge-loaded compact specimens. The thickness ranged from 0.75–6.69 in. (19–170 mm), the in-plane dimensions from 3.94–15.75 in. (100–400 mm). The comparison with the reference curves of the American and German guidelines showed significant discrepancies at high temperatures.


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