Influence of dynamic strain ageing on mixed mode I/III fracture toughness of Armco iron

2007 ◽  
Vol 443 (1-2) ◽  
pp. 132-141 ◽  
Author(s):  
M. Srinivas ◽  
S.V. Kamat ◽  
P. Rama Rao
1991 ◽  
Vol 25 (11) ◽  
pp. 2585-2588 ◽  
Author(s):  
M. Srinivas ◽  
G. Malakondaiah ◽  
K.Linga Murty ◽  
P.Rama Rao

1998 ◽  
Vol 46 (14) ◽  
pp. 4985-4992 ◽  
Author(s):  
S.V Kamat ◽  
M Srinivas ◽  
P Rama Rao

2016 ◽  
Vol 879 ◽  
pp. 306-311
Author(s):  
Guo Cai Chai ◽  
Mattias Calmunger ◽  
Sten Johansson ◽  
Johan Moverare ◽  
Joakim Odqvist

Influences of dynamic strain ageing and long term ageing on deformation, damage and fracture behaviors of Alloy 617 material have been studied. Dynamic strain ageing can occur in this alloy at temperature from 400 to 700°C, which leads to a strain hardening and also an increase in fracture strain due to plastic deformation caused by twinning. Long term ageing at 700°C for up to 20 000 hours can cause different precipitation such as γ ́, M6C (Mo-rich) and M23C6 (Cr-rich) carbides. These carbides are both inter-and intra-granular particles. The long term ageing reduces the fracture toughness of the material, but the alloy can still have rather high impact toughness and fracture toughness even with an ageing at 700°C for 20 000 hour. The mechanisms have been studied using electron backscatter detection and electron channeling contrast imaging. It shows that besides dislocation slip, twinning is another main deformation mechanism in these aged Alloy 617 materials. At the crack front, plenty of micro or nanotwins can be observed. The formation of these twins leads to a high ductility and toughness which is a new observation or a new concept for this type of material.


2001 ◽  
Vol 98 (5) ◽  
pp. 473-484 ◽  
Author(s):  
D. Wagner ◽  
J. C. Moreno ◽  
C. Prioul ◽  
J. M. Frund ◽  
B. Houssin

2002 ◽  
Vol 93 (2) ◽  
pp. 160-163 ◽  
Author(s):  
S.V. Kamat ◽  
M. Srinivas ◽  
P. Rama Rao

1993 ◽  
Vol 29 (11) ◽  
pp. 1379-1384 ◽  
Author(s):  
D. Delafosse ◽  
G. Lapasset ◽  
L.P. Kubin

Materials ◽  
2021 ◽  
Vol 14 (9) ◽  
pp. 2103
Author(s):  
Christophe Floreani ◽  
Colin Robert ◽  
Parvez Alam ◽  
Peter Davies ◽  
Conchúr M. Ó. Brádaigh

Powder epoxy composites have several advantages for the processing of large composite structures, including low exotherm, viscosity and material cost, as well as the ability to carry out separate melting and curing operations. This work studies the mode I and mixed-mode toughness, as well as the in-plane mechanical properties of unidirectional stitched glass and carbon fibre reinforced powder epoxy composites. The interlaminar fracture toughness is studied in pure mode I by performing Double Cantilever Beam tests and at 25% mode II, 50% mode II and 75% mode II by performing Mixed Mode Bending testing according to the ASTM D5528-13 test standard. The tensile and compressive properties are comparable to that of standard epoxy composites but both the mode I and mixed-mode toughness are shown to be significantly higher than that of other epoxy composites, even when comparing to toughened epoxies. The mixed-mode critical strain energy release rate as a function of the delamination mode ratio is also provided. This paper highlights the potential for powder epoxy composites in the manufacturing of structures where there is a risk of delamination.


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