Materials Science Forum
Vol. 554
Vol. 554
Materials Science Forum
Vol. 553
Vol. 553
Materials Science Forum
Vols. 551-552
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Materials Science Forum
Vol. 550
Vol. 550
Materials Science Forum
Vols. 546-549
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Materials Science Forum
Vols. 544-545
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Materials Science Forum
Vols. 539-543
Vols. 539-543
Materials Science Forum
Vols. 537-538
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Materials Science Forum
Vols. 534-536
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Materials Science Forum
Vols. 532-533
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Vols. 530-531
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Materials Science Forum
Vols. 527-529
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Materials Science Forum
Vol. 526
Vol. 526
Materials Science Forum Vols. 539-543
Paper Title Page
Abstract: It was previously reported that fatigue life of some alloys can be dramatically reduced if the
grain boundaries contain a high level of impurity segregation before fatigue tests. In this paper the
susceptibility of single phase brass samples (90Cu10Zn) to this form of damage is studied. After cold
drawing of as cast brass bars, fatigue samples were heat treated at 800°C during 30min to promote
recrystallization and impurity segregation at grain boundary. The samples were then tested under high
frequency bending fatigue test at 200°C. After cracking, fracture surfaces were studied using both
scanning electron microscopy (SEM) and electron probe microanalysis (EPMA). The SEM
micrographs showed that the fractures were mostly intergranular. Chemical composition of
intergranular cracks surface were analyzed using EPMA at low accelerating voltage. A high
concentration of sulfur was found on most of grain boundary facets. The internal stress in alloys after
fatigue was qualitatively estimated using electron backscattering diffraction in scanning electron
microscopy. A high level of local misorientation was found near most grain boundaries. The
mechanism of intergranular cracks formation during fatigue is discussed taking into account both the
segregation of sulfur at grain boundaries and accumulation of plastic strain at grain boundaries
2137
Abstract: As examples of the most typical methods to determine the shear strength of SiC/SiC
composite joints, the asymmetrical four point bending test of butt joined composite, the tensile test
of lap joined composite and the compressive test of double-notched composite joint were analyzed
by using finite element method with the interface element. From the calculation results, it was
found that the shear strength in the asymmetrical bending test was controlled by both the surface
energy and the shear strength at the interface regardless of their combination although the strength
in the tensile test or the compressive test was governed by the surface energy when the shear
strength was large. Also, it was revealed that the apparent shear strength of the composite joint
obtained experimentally might be affected by the combination of the surface energy and the shear
strength at the interface.
2143
Abstract: A new method for evaluating the hydrogen embrittlement (HE) susceptibility of ultra high
strength steel was studied in order to propose a new method for assessing the delayed fracture
property. The material used was 1400MPa tempered martensitic steel with the chemical composition
0.40C-0.24Si-0.81Mn-1.03Cr-0.16Mo(mass%). The local approach originally used for evaluating the
brittle fracture property was applied to HE susceptibility assessment after modifying the method to
include the effect of hydrogen content. Critical HE data used in the modified local approach was
obtained by a stepwise test in which alternating processes of stress increase and stress holding were
repeated until the specimen fractured. The specimen used in the stepwise test was 10 mm in diameter
and the stress concentration factor was 4.9. Assessment of HE susceptibility for specimens with other
dimensions entailed the use of a critical hydrogen content for failure, Hc, representing the maximum
hydrogen content among the unfractured specimens in the HE test with constant loading. Matters to
be noted for obtaining the material parameters are discussed.
2155
Abstract: Several prematurely failed jack bolts were analyzed to determine the root causes of
failure. Bolts were employed to ensure that die halves do not separate during casting of high
pressure die castings of light metals. Fractography of jack bolts revealed unusual morphology
consisting of both circumferential and longitudinal cracking. The basic fracture type was identified
as transgranular cleavage (brittle) fracture mode. SEM / EDS analysis of the fracture surface
revealed the presence of, to varying degrees, chemical species containing sulfur (S), oxygen (O)
and chlorine (Cl). Material composition, heat treatment, microstructure and hardnesses of the jack
bolts were found to be in agreement with the expected steel grade and properties. It was concluded
that the failure of the bolts was due to a combination of inappropriately chosen mechanical
properties of the bolts, operating stress, and the presence of corrosive environmental materials
leading to ideal conditions that promoted stress corrosion cracking failures. Suitable remedial
actions to alleviate the risk of SCC failure of the bolts are presented and discussed in the paper.
2162
Abstract: Static and dynamic ductile crack propagation tests were carried out using thin single edge
notched tension (SENT) specimens of carbon-manganese steel, each of which had a fatigue pre-crack
or a sharp V-notch as a crack initiator. The crack tip opening angle (CTOA) was measured using
digital images on the surface of the SENT specimens, and the critical values of CTOA for crack
propagation decreased with increasing crack length while initial crack growth was still small. After
the initial crack growth up to the distance of the specimen thickness, the critical CTOA remained
almost constant. These tendencies were common in static and dynamic crack propagation specimens
as well as fatigue pre-cracked and sharp V-notched specimens. There was no particular difference in
the static crack propagation characteristics of both fatigue pre-cracked and sharp V-notched
specimens. On average, it was observed that higher crack speeds affected the constant values of the
critical CTOA by slightly reducing them. The constant CTOA tends to decrease with an increasing
global constraint factor, and this suggests that the factor is insensitive to a crack starter, fatigue
pre-crack or a sharp V-notch, but relatively sensitive to crack speed.
2180
Abstract: This study pays attention to reveal the material properties that control resistance curve for
ductile crack growth (CTOD-R curve) on the basis of the mechanism for ductile crack growth, so
that the R-curve could be numerically predicted only from those properties.
The crack growth tests using 3-point bend specimens with fatigue pre-crack were conducted for
two steels that have different ductile crack growth resistance with almost the same CTOD level for
crack initiation, whereas both steels have the same “Mechanical properties” in terms of strength and
work hardenability. The observation of crack growth behaviors provided that different mechanisms
between ductile crack initiations from fatigue pre-crack and subsequent growth process could be
applied. It was found that two “Mechanical properties” associated with ductile damage of steel
could mainly influence CTOD-R curve; one is a resistance of ductile crack initiation estimated with
critical local strain for ductile cracking from the surface of notched specimen, and the other one is a
dependence of stress triaxiality on ductility obtained with circumferentially notched round-bar
specimens.
The damage model for numerically simulating the R-curve was proposed taking the two “ductile
properties” into account, where ductile crack initiation from crack-tip was in accordance with
critical local strain based criterion, and subsequent crack growth GTN
(Gurson-Tvergaard-Needleman) based triaxiality dependent damage criterion. The proposed
model accurately predicted the measured R-curve for the two steels used with the same “strength
properties” through ductile crack initiation to growth.
2186
Abstract: Measurements of the activation volume and mean slip distance were used in the dynamic
dislocation-defect analysis to reveal the dislocation-obstacle evolution with strain. Due to the large
effect of point defect mobility above 250 K on the strain rate sensitivity, fine-grained Al specimens
with the grain-boundaries sealed and unsealed as vacancy sinks were tested at 300 K as the
reference behaviour. The activation distance diagrams revealed that the artificially aged products in
AA6111 and naturally aged extruded AA6063 can be used to examine the effect of chopping-up of
particles on the ductility of the samples. Thus a means to examine strength-structure-ductility of
specific products have been devised.
2192