Advanced Materials Research
Vols. 53-54
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Vol. 51
Vol. 51
Advanced Materials Research
Vols. 47-50
Vols. 47-50
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Vols. 44-46
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Advanced Materials Research
Vol. 43
Vol. 43
Advanced Materials Research
Vols. 41-42
Vols. 41-42
Advanced Materials Research
Vols. 39-40
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Advanced Materials Research
Vol. 38
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Vols. 33-37
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Advanced Materials Research
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Vol. 31
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Advanced Materials Research
Vols. 29-30
Vols. 29-30
Advanced Materials Research Vols. 41-42
DOI:
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Paper Title Page
Abstract: A special test setup was designed and used in compression shear test of unidirectional
carbon fiber composites to study the effect of short fiber interleaves (SFIs) on the interlaminar shear
behavior. The comparative tests for two kinds of double-notched compression specimens, with and
without SFIs, were carried out to determine the interlaminar shear strength and modulus (ILSS and
ILSM) and to examine the failure characteristics. To determine ILSM of the specimens with SFIs an
inversion analysis method was proposed based on comparing compression displacement of
specimens with and without SFIs. The experimental results show that SFIs makes ILSS decreasing
due to lower interface strength, and the complex damage process of SFIs leads to a considerable
increase of interlaminar shear compliance.
335
Abstract: A micro-mechanical model and simulation for the damage behavior of short fiber
interleaves (SFIs) were developed based on Mori-Tanaka method and an equivalent approach to
interface debonding (Fitoussi etc 1990). The damage evolution and the stress-strain relation of SFIs
have been predicted in the cases of interlaminar shear, out-of and in-plane tension, respectively. The
simulation indicates that the damage always starts from the interface debonding of fibers
perpendicular to load and the matrix cracking in the direction parallel to fibers, and then rapidly
spreads to more fibers during loading. The strength and the ultimate strain in out-of-plane tension
are much lower than that in interlaminar shear and in-pane tension. The strength and failure
probability of interface bonding are the most considerable factors to affect the damage and failure of
SFIs. The comparison of the simulation with the interlaminar shear test shows a good agreement.
341
Abstract: Corrosion rates and anode polarization curves of RE-Ni-W-P-SiC-PTFE
composite coatings in various concentrations of sulfuric acid and hydrochloric acid
solutions have been studied. Results show that corrosion law of the RE-Ni-W-P-PTFE-SiC
composite coatings in various concentrations of sulfuric acid solutions is identical. The
corrosion rates of the composite coatings are increased with increasing sulfuric acid concentration
while the corrosion rates are decreased with increasing concentration of hydrochloric acid. Anode
polarization curves of RE-Ni-W-P-SiC-PTFE composite coatings in various concentrations
of sulfuric acid and hydrochloric acid solutions have showed that anode polarization
electric current density of the composites at 200°C or 500°C heat treatment was below that
at other heat treatment, it is clear that the composite coatings at 200°C or 500°C heat
treatment has better corrosion resistance.
349
Abstract: The flexural behaviour of 6-ply unidirectional hybrid fibre-reinforced polymer (FRP)
matrix composites containing a mixture of E-glass and S2-glass fibres was investigated. A high
performance epoxy system comprising of Kinetix® R240 epoxy resin (combined with Kinetix®
H160 epoxy hardener) was utilised for the composite matrix. Flexural testing was conducted in
accordance with Procedure A of the ASTM D790-03 test standard on a universal testing machine
equipped with a three-point bend test rig. In addition to varying the stacking configurations of the
composite prepregs, the influence of span-to-depth ratio on the flexural properties and failure
mechanisms was also studied. The failure mechanisms of the resulting fractured specimens were
characterised using optical microscopy and compared with those noted by the authors in previous
work.
357
Abstract: The blast-resistant of an aluminum foam sandwich structure under impact has been
investigated. Plastic deformation and load distributions in each of the sub-layers during and after
impact were calculated by the material point method with the consideration of strain rate effect on
deformation of the aluminum foam. The numerical results from the 3D material point method
modeling show that the blast-resistant capability of the aluminum foam sandwich structure is
excellent, and the energy absorbability of the structure would be underestimated if the strain rate
effect on the aluminum foam is ignored.
363
Abstract: Effects of the concentrations of solid particles in the bath and plating conditions on
chemical components and polarization curves of oxygen separating out were studied by use of
PARSTAT2263 electrochemistry testing instrument made by Research Center of Princeton and
EPMA-1600 electron probe X-ray diffraction. And the results show that kinetic parameters of
oxygen evolution of the obtained Al/Pb-WC-ZrO2 composite electrode materials are a=771mV,
b=140mV, i0=3.11×10-6A·cm-2, and oxygen overvoltage is η=1009mV. The contents of WC and
ZrO2 particles in the Al/Pb-WC-ZrO2 composite coating are 10.02wt% and 3.55wt% respectively
when plating conditions are as follows: WC:50g/L,ZrO2:40g/L, bath temperature: 20°C, electric
current density: 1.5A/dm2, plating time: 2h.
369
Abstract: With the increasing demands of energy efficiency and environment protection, composite
materials have become an important alternative for traditional materials. Composite materials offer
many advantages over traditional materials including: low density, high strength, high stiffness to
weight ratio, excellent durability, and design flexibility. Despite all these advantages, composite
materials have not been as widely used as expected because of the complexity and cost of the
manufacturing process. One of the main causes is associated with poor dimensional control. General
curved composite parts are often used as the structural components in the composite industry. Due
to the anisotropic material nature, process-induced dimensional variations make it difficult for tighttolerance
control and limit the use of composites.
This research aims to develop a practical approach for the design of general curved composite
parts and assembly. First, the closed-form solution for the process-induced dimensional variations,
which is commonly called spring-in, was derived. For a general curved composite part, a Structural
Tree Method (STM) was developed to divide the curve into a number of pieces and calculate the
dimensional variations sequentially. This method can be also applied to an assembly of composite
parts. The approach was validated through a case study. The method presented in this paper
provides a convenient and practical tool for the dimensional and tolerance analysis in the early
design stage of general curved composite parts and assembly, which is extremely useful for the
realization of affordable tight tolerance composites. It also provides the foundation of Integrated
Product/Process Development (IPPD) and Design for Manufacturing/Assembly (DFM/DFA) for
composites.
377
Abstract: Process and properties of pulse electrodeposited RE-Ni-W-P-SiC composite coatings
were studied. The results show that the deposited rate by pulse current is larger than that by direct
current; the deposited coatings by pulse current are better than that by direct current in corrosion
resistance and microhardness. And the corrosion resistance of the coatings with pulse current is
better than that of stainless steel (1Cr18Ni9Ti). The duty ratio and the pulse frequency in the
process of electrodeposition have a large influence on the deposition rate, the composition and the
properties of coatings. SEM measurement shows that the crystals with pulse current are smaller and
the surface is smoother than that by direct current. It is beneficial to make crystalline grain finer by
mixing rare earth.
385
Abstract: The safe operation of both thermal and nuclear power plant is increasingly dependent
upon structural integrity assessment of pressure vessels and piping. Furthermore, structural failures
most commonly occur at welds so the accurate design and remnant life assessment of welded plant
is critical. The residual stress distribution assumed in defect assessments often has a deciding
influence on the analysis outcome, and in the absence of accurate and reliable knowledge of the
weld residual stresses, the design codes and procedures use assumptions that yield very conservative
assessments that can severely limit the economic life of some plant. However, recent advances in
both the modeling and measurement of residual stresses in welded structures and components open
up the possibility of characterising weld residual stresses in operating plant using state-of–the–art
fully validated Finite Element simulations. This paper describes research undertaken to predict
residual stresses in stainless steel welds in order to provide validated reliable, accurate Structural
Integrity assessment of nuclear power plant components
391
Abstract: Structural health monitoring or damage detection has long been a research interest for its
great potential for life safety and economic benefits to the industrialized world. Structural vibration
behavior is an essential signature of the integrity of structures and hence has been used for damage
detection. Structural vibration impedance by way of piezoceramic patch excitation offers a local
damage detection technique. It has been known that temperature change has adverse effects on the
measured impedance result and can complicate the damage analysis. It is believed that one way of
temperature influence on vibration is through adding thermal prestress to the structure. Prestress
affects vibration in different ways on different structures and application problems. For the
impedance method, prestress comes not only from temperature change but also from other sources
such as wind, gravity and working load. This paper deals with prestress effects in the context of
local vibration behavior of structures. A theoretical analysis is given on how prestress affects the
vibration. Experimental impedance measurement results for piezoceramic patch excited vibration of
simple structures such as plates under prestress are presented.
401