Materials Science Forum
Vol. 589
Vol. 589
Materials Science Forum
Vols. 587-588
Vols. 587-588
Materials Science Forum
Vols. 584-586
Vols. 584-586
Materials Science Forum
Vol. 583
Vol. 583
Materials Science Forum
Vols. 580-582
Vols. 580-582
Materials Science Forum
Vol. 579
Vol. 579
Materials Science Forum
Vols. 575-578
Vols. 575-578
Materials Science Forum
Vols. 573-574
Vols. 573-574
Materials Science Forum
Vols. 571-572
Vols. 571-572
Materials Science Forum
Vol. 570
Vol. 570
Materials Science Forum
Vol. 569
Vol. 569
Materials Science Forum
Vols. 567-568
Vols. 567-568
Materials Science Forum
Vol. 566
Vol. 566
Materials Science Forum Vols. 575-578
Paper Title Page
Abstract: Mullite interlayer of the carbon fiber reinforced Si-C-N matrix composite (C/Si-C-N)
was fabricated by liquid precursor impregnation and pyrolysis (PIP). The mixture of aluminium secbutoxide
(A1OBu) and tetraethoxysilicate (TEOS) were used as starting materials. The monophase
polymer gel used as mullite precursor could be formed from the mixture in the semi-closed air. A
mullite interlayer with a thickness about 500nm is obtained at 850°C- 1200°C. The fiber/interlayer
bonds are tight. The carbon fibers are not damaged in the fabrication procedure.
881
Abstract: A coupled thermo-mechanical model is employed to analyze the thermo-mechanical
behavior of a widely used laminated composite subject to temperature decrease at service conditions.
Three sets of governing equations, i.e. heat transfer, thermo-mechanical deformation and damage
evolution are respectively described in the model. These equations are then assembled into a coupled
matrix equation using finite element formulation and then solved simultaneously at each time
interval. A numerical model of two layered composites with some preexisting equal-spacing cracks
along the interface in the lower layer is set up to investigate the thermal induced crack propagation
due to temperature decrease. Results are presented in the form of crack propagation process in stress
profiles and discussed. Numerical simulations show that the crack propagation behavior of the
composites is closely dependent on the physico-mechanical properties of two layers and preexisting
cracks. It is found that thermal induced cracks penetrate into the upper layer and grow in the upper
layer due to the low strength of the upper layer when the model is subject to uniform temperature
decrease.
886
Abstract: Basing on the experimental results of the hardenability investigations, which employed
Jominy method, the model of the neural networks was developed and fully verified experimentally.
The model makes it possible to obtain Jominy hardenability curves basing on the steel chemical
composition. The modified hardenability curves calculation method is presented in the paper,
initially developed by Tartaglia, Eldis, and Geissler, later extended by T. Inoue. The method makes
use of the similarity of the Jominy curve to the hyperbolic secant function. The empirical formulae
proposed by the authors make calculation of the hardenability curve possible basing on the chemical
composition of the steel. However, regression coefficients characteristic for the particular steel
grade must be known. Replacing some formulae by the neural network models is proposed in the
paper.
892
Abstract: Two mild steels with Nb-microalloying and Nb-free were smelted. After single-pass hot
compression of various processes conducted on a Gleeble-2000 thermomechanical simulator, the
effects of deformation conditions and Nb-microalloying on microstructural evolution kinetics,
including the volume fraction, grain size and grain number per unit area were investigated through
quantitative metallographic analysis. The experimental results show that, grain number per unit area
of DIF increases with decreasing deformation temperature or increasing deformation amount; the
grain size of DIF is not very sensitive to the deformation conditions; the volume fraction of DIF
increases due to the increased grain number per unit area. The microalloying element of Nb
dissolved in austenite inhibits the grain growth and reduces the volume fraction of DIF.
898
Abstract: Improved methods to estimate the kinetics of dynamic and static recrystallization are
proposed in this paper. The kinetics for dynamic and static recrystallization can be evaluated by
inverse analysis of the flow curves obtained using the single-hit and double-hit hot compression
tests carried out on Gleeble 3500. The dynamic and static recrystallization volume fractions can be
seen as functions of plastic strain and time, respectively. The mathematical formulations between
the recrystallization volume fractions and the dislocation density related to the flow stress are used
in incremental forms in the study. The methods are applied to the hot compression tests of plain
carbon steel and the kinetics of dynamic and static recrystallization are gained successfully for some
conditions at elevated temperature. The results are clarified by comparing them with those reported
in previous investigations. It is confirmed that the present methods can provide accurate kinetics for
dynamic and static recrystallization with shorter time for experiment and computation.
904
Abstract: Microstructures and toughness of simulated coarse grain heat-affected zone of hot
continuously rolled copper-bearing steel were investigated using physical simulation. The results
showed that brittlement is easy to happen in the region of CGHAZ with slower thermal cycles
(t8/5≥45s). Granular bainite transformed from austenite led to brittlement. The dimensions of
granular martensite and austenite (M-A) constituents are main factors influencing the impact
toughness. There is no visible effect on the toughness when the dimensions of M-A constituents are
less than 1μ m. However, the toughness decreases greatly once the dimensions exceed 1μ m.
Therefore, decreasing the dimensions of M-A constituents by controlling weld heat input will do
good to improve the impact toughness of copper-bearing steel.
910
Abstract: This paper presents our effort to reduce thermo-mechanical failures related IC packaging
reliability problems. These reliability problems are driven by the mismatch between the different
material properties. First of all, finite element analysis are adopted to investigate the influence of
encapsulation structures and material properties on the stress distribution in dielectric layers and
plastic strain distribution in die for a typical stacked package of IC microstructures. Results show
that thinner package body, lower thermal stress and smaller plastic strain can be realized in this
micro-structure with the different design geometry parameters and materials properties. Secondly, it
was also found that the transition layer of TiN between the die and dielectric layer has a pronounced
influence on decreasing the local stress in the passivation layer by comparison analysis. These
studies would be beneficial to improve the reliability of stacked IC micro-structure packages.
915
Abstract: Interfacial delamination is a recognized failure mode in Integrated circuits (ICs). A major
cause for this failure is the mismatch of Thermal Expansion Coefficients, Young’s modulus, and
Poisson’s ratios of the package materials. Here, the influence of delamination between epoxy and
dielectric layers on pattern shift and passivation cracking in IC package under aeronautical
conditions, mainly temperature and load cycles, is studied by maximum plastic strain and maximum
principal stresses theory using a certain 2D FEM model with different delamination length
“L_c.right”. Delaminations are easy to introduce more dangerous impact to the package, because
the IC microstructures endure serious thermo-mechanical loading under aeronautical working
conditions. The method can be used to find the dangerous designed structure schedules and will
provide a basis for selecting passivation materials of aeronautical IC packages.
919
Abstract: The Kurdjumow -Sachs mechanism of martensite transformation is investigated in detail
in this paper. The distortion matrixes of the first shear, the second shear and lineal adjustment
according to the K-S mechanism are calculated. From the lattice distortion matrix, we can obtain
invariant normal planes. According to the assumption that the habit plane is constructed with some
of the invariant normal planes, the macroscopic habit plane (225)A is also discussed. The results
show that the K-S mechanism can account for the relief effects, habit plane, orientation relationship
and the change of structure.
924
Abstract: Carbon black (CB) filled rubber is microscopically heterogeneous although homogeneous
on a macroscopic scale. CB particles are generally in the form of aggregates, which form the CB
network in the rubber matrix. In this work, the junction width between CB aggregates is modeled as a
contact resistor and the tunneling conduction mechanism is taken into account, and then an infinite
circuit consisting of numerous contact resistors, interconnected with each other, is proposed to
simulate the CB network in filled rubber. Prior to determination of the junction width distribution, CB
spheres equivalent to CB aggregates in volume is assumed in a specifically random arrangement.
Thus, the effect of CB aggregate distribution on the electrical resistivity is discussed. It is found that,
for CB (N330) filled natural rubber with volume fraction of 27.5%, the simulated electrical resistivity
at a standard deviation of 0.1 mean junction width is in good agreement with the experimental data
available in the literature.
930