Key Engineering Materials
Vols. 373-374
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Vols. 368-372
Vols. 368-372
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Vol. 367
Vol. 367
Key Engineering Materials
Vols. 364-366
Vols. 364-366
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Vols. 361-363
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Vols. 359-360
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Key Engineering Materials
Vols. 353-358
Vols. 353-358
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Vol. 352
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Vol. 351
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Vol. 350
Vol. 350
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Vols. 348-349
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Vol. 347
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Key Engineering Materials
Vols. 345-346
Vols. 345-346
Key Engineering Materials Vols. 353-358
Paper Title Page
Abstract: Recently, applications of integrated large composite structures have been attempted to
many structures of vehicles. In order to improve the cost performance and reliability, it is necessary to
judge the structural integrity of composite structures. Fracture simulation techniques using FEM have
been developed for the purpose. Since a number of iterations of finite element analysis are required in
the fracture simulation, the simulation techniques consume many memory resources and much
calculation time. In this study, a personal computer cluster (PC cluster) and the domain
decomposition method were incorporated into a fracture simulation system. Calculations using a
Windows PC cluster were carried out to confirm the efficiency of the proposed simulation system. As
a result, it is concluded that adopting the domain decomposition method and the computer cluster is
remarkably efficient to reduce calculation time.
1382
Abstract: Temperature induced change, and stress induced change as well, in intrinsic timescale
were investigated by nonlinear creep tests on poly(methyl methacrylate). With four different
experimental temperatures, from 14 to 26 degrees centigrade, time-dependent axial elongations of
the specimen were measured at seven different stress levels, from 14 MPa to 30 MPa, and modeled
according to the concept of time-temperature-stress equivalence. The test duration was only 4000
seconds. The corresponding temperature shift factors, stress shift factors and temperature-stress
shift factors were obtained according to the time-temperature superposition principle (TTSP), the
time-stress superposition principle (TSSP) and the time-temperature-stress superposition principle
(TTSSP). The master creep compliance curve up to about two-year at a reference temperature 14
degrees centigrade and a reference stress 14 MPa was constructed by shifting the creep curves
horizontally along the logarithmic time axis using shift factors. It is shown that TTSSP provides an
effective accelerated test technique in the laboratory, the results obtained from a short-term creep
test of PMMA specimen at high temperature and stress level can be used to construct the master
creep compliance curve for prediction of the long-term mechanical properties at relatively lower
temperature and stress level.
1386
Abstract: An experimental study of microstructure and mechanical properties in the Al2O3
particulate reinforced 6061 Aluminum composites has been used to determine the effect of
extrusion and particle volume fraction (20, 26, 30, 40, 50, 60%Vf) in deformed metal matrix
composites. The microstructure of Al2O3 /6061Al composite before and after hot extrusion is
investigated by TEM and SEM. Results show that dislocation and subgrain generated after hot
extrusion as well as the particle distribution of composite become more uniform with extrusion ratio
of 10:1. The ultimate strength, yield strength and elongation of the composite also increase after hot
extrusion. Dispersion strengthening and subgrain boundary strengthening is discussed and also the
effect of precipitate introduced by heat treatment both after casting and after extrusion. The yield
stress (0.2% offset) of the composites has been calculated and predicted using a standard dislocation
hardening model. Whilst the correlation between this and the measured value of yield stress
obtained in previous experimental test is reasonable.
1390
Abstract: This study was performed to evaluate the effects of micropowders content on the
compressive strength of cement-based composite pastes. Granular ground blast slag (GGBS), grade
I fly ash (FAI), ultra fine fly ash (UFA) and silica fume (SF) were selected as the micropowders.
The compressive strength was tested after 3d, 7d and 28d curing. Results show that the paste
containing both UFA and SF has the highest packing density and corresponding excellent
compressive strength. The higher the packing density is, the better the compacting and filling effect
of micropowders will be, which contributes to developing higher compressive strength of
cement-based pastes.
1394
Abstract: The rheological parameters of cement pastes were investigated by varying the type and
content of micropowders and the ratio of water to binder. Compressible packing model was used to
calculate the packing density and to evaluate the influence of micropowders gradation on the
rheological properties of fresh cement pastes. Results indicate that the higher the packing density is,
the lower the yielding shear stress and plastic viscosity will be. When the ratio of water to binder is
less than 0.20, the cement paste with 15% UFA and 15% SF has highest packing density and lowest
yielding shear stress and plastic viscosity, which is beneficial to the workability of ultra-high
performance concrete.
1398
Abstract: SiCp/Cu composites were fabricated at 700 oC and under 40MPa for 10min in vacuum by
electric conduction sintering. The mechanical properties and microstructure of the composites were
studied. The porosity of the composites increases when the volume fraction of SiCp exceeds 35%.
The flexural strength of the composites decreases with increasing fraction of SiCp. The composites
with 10 vol.% SiCp exhibited ductile fracture behavior, while composites with the volume fraction
of SiCp in the range of 20–65% exhibited brittle fracture behavior. The composites with 35 vol.%
SiCp showed the highest hardness.
1402
Abstract: The tension-tension fatigue tests for SiC/SiC composites were performed under the
conditions that the maximum load Pmax was 80-90% to the fracture load of the tensile tests and the
stress ratio was Rσ = 0.5. The composites exhibited a width in stress-strain hysteresis loop under
one load cycling. In some cases the mean strain εmean gradually increase with increasing in number
of cycles. These variations would reflect the developments of the fatigue damage at the fiber/matrix
interface during the cyclic loading process. The pull-out lengths of the fibers for the fatigued- and
not fatigued-specimens were measured through the SEM observations after the tensile test. In all
materials, the average pull-out length of fibers in fatigued material was larger than in not fatigued
material because the cyclic loading affected on the fiber/matrix interfacial strength.
1406
Abstract: The solvent debinding processes of wax-based binders in powder injection molded
Ti(C,N)-based cermets were studied. Effects of debinding temperature, debinding time, sample
thickness, solvent types and solvent concentration on binder removal were investigated. Also, the
dimension change of samples during the solvent debinding process was studied. It can be found that
upwards of 70% paraffin waxes were removed and open pore channels were formed basically when
the samples were immersed in heptane for 6 h at 50 °C.
1410
Abstract: It is attractive to use multi-wall carbon nanotubes (MWNTs), which has a high modulus
and strength, to enhance the properties of metal matrix composites by hybrid strategy. In this paper,
novel aluminum borate whisker (ABOw) and MWNTs hybrid composites were prepared by squeeze
cast technique and the properties were investigated. The results show that hybrid preforms may be
made by co-deposition of ABOw and MWNTs in a solution by wet method. MWNTs separate the
ABOw from whisker-to-whisker contact and decrease the compressive deformation of the hybrid
preforms during squeeze cast processing. MWNTs distribute along mainly in the grains of
aluminum matrix, making the mechanical properties of the hybrid composites higher than singularly
reinforced composite.
1414
Abstract: Tensile strength is an important material property and usually can be determined
experimentally. The strain rate dependent behavior of T300 carbon/epoxy matrix composite was
characterized over a wide strain rate range (10×10-5 s-1to10×104s-1). The low to moderate strain rate
experiments were carried out on a MTS machine, while the high strain rate experiment was
conducted with a split Hopkinson tensile bar. A rate dependent model was introduced to simulate
the material response. Two kinds of stacking sequence of composite specimens [(45/-45)4]s and
[(0/45/90/-45)2]s were tested at different strain rates, and the results were used to determine
parameters of the model. The predictions of the model showed to agree fairly well with the
experimental results. The tensile strength and initial elastic modulus of the composites increase
when the strain rate increases.
1418