Key Engineering Materials
Vols. 345-346
Vols. 345-346
Key Engineering Materials
Vol. 344
Vol. 344
Key Engineering Materials
Vols. 342-343
Vols. 342-343
Key Engineering Materials
Vols. 340-341
Vols. 340-341
Key Engineering Materials
Vol. 339
Vol. 339
Key Engineering Materials
Vols. 336-338
Vols. 336-338
Key Engineering Materials
Vols. 334-335
Vols. 334-335
Key Engineering Materials
Vol. 333
Vol. 333
Key Engineering Materials
Vols. 330-332
Vols. 330-332
Key Engineering Materials
Vol. 329
Vol. 329
Key Engineering Materials
Vols. 326-328
Vols. 326-328
Key Engineering Materials
Vols. 324-325
Vols. 324-325
Key Engineering Materials
Vols. 321-323
Vols. 321-323
Key Engineering Materials Vols. 334-335
Paper Title Page
Abstract: The main purpose of this study is to evaluate the interfacial reaction between titanium
matrix composites (TMCs) and A380 alloy in aluminum die-casting. In-situ synthesized titanium
matrix composites and H13 tool steel were immersed in molten A380 alloy in a mold at 993 K for
times varying from 0 to 1200 s. In-situ synthesis TMCs and interfacial reaction between TMCs and
A380 alloy were examined by X-ray diffraction, optical microscope, scanning electron microscope
and electron probe micro-analyzer. The reaction behavior shows that TMCs can a substitution for
H13 tool steel.
433
Abstract: Liquid molding processes are becoming more popular among the composite
manufacturing industries due to their versatility and economy among other merits. In analyzing the
flow during the process, permeability is the most important parameter. Permeability has been
regarded as a property of the porous medium. However, in many practical cases, the value may vary
depending on the flow conditions such as the flow rate. It is speculated that this deviation is caused by
inhomogeneous microstructure of the medium. In this study, numerical simulations as well as
experimental measurements have been done to investigate the cause of deviation. Microstructure of
porous medium was modeled as an array of porous cylinders. Resin flow through the array was
simulated numerically. Simulations were performed for two different flow conditions, namely
saturated flow and unsaturated flow. Based upon the results, permeabilities were estimated and
compared for the two flow conditions. In addition, a model was proposed to predict the permeability
for different flow conditions. Results showed that experimental data were in agreement with the
prediction by the model.
437
Abstract: To meet the demands of technology for the development of new materials with tailormade
properties, we propose the use of smart materials of nanostructure synthesized by solidifying
a poorly conducting alloy in a microgravity environment in the presence of an electric field and
surface tension. Energy method combined with a single term Galerkin expansion is used to find the
condition for the onset of Marangoni marginal electroconvection (MMEC) in a composite material
modeled as a porous layer. It is shown that a proper choice of electric parameter and the ratio of
Brinkman viscosity to viscosity of the fluid λ control Marangonielectroconvection (MEC).
441
Abstract: This paper is concerned with the fatigue life prediction of CFRP laminates under variable
cyclic loading using the linear cumulative damage (LCD) rule with statistical approach. Three-point
bending fatigue tests for plain-woven CFRP laminates were carried out undervarious cyclic loading
with constant and variable stress amplitude and frequency. As results, the applicability of LCD rule to
the flexural fatigue life was confirmed for this CFRP laminates.
445
Abstract: Interlaminar fracture behavior of carbon fabric/epoxy composite, which is one of the
candidate composites for the Korean tilting train carbody, was investigated. Specimens were made of
a CF3227 plain fabric with an epoxy resin. An initial starter crack was formed by inserting a 12.5
thick Teflon film at the one end of the specimen. Interlaminar fracture toughness was evaluated using
the mixed mode flexural fixture, which provides a wide range of mixed mode deformation by varying
the length of lever arm. According to the results, the crack growth was progressive and stable under
mode I dominantly mixed mode ratio and was relatively rapid and unstable under mode II dominantly
mixed mode ratio. The mixed mode interlaminar fracture behavior can be predicted by a mixed mode
fracture criterion depending on the point at which the crack growth was associated.
449
Abstract: In the traditional iterative design process for composite structures, it is difficult to achieve
an optimal solution even though a great effort is made. A genetic optimization system based on grid
technology offers an automatic and efficient approach for composite structure redesign and
optimization. A genetic algorithm system, which integrates Genetic Algorithm Optimization (GAO)
software and a Finite Element Analysis (FEA) based commercial package, has been developed as a
tool for composite structure design and analysis. The GAO is capable of tailoring large number of
composite design variables and taking the time-consuming FEA results to calculate objective function
value and conduct optimization in high accuracy. By operating the system employing the Grid
technology and Artificial Neural Network (ANN) method, significant time saving in numerical
analysis can be achieved. A user friendly interface has also been built in the system. In the paper,
aeroelastic tailoring of a composite wing has been taken as a numerical example to demonstrate the
optimization approach. The numerical results show that an optimal design has been achieved to meet
the design requirement.
453
Abstract: Satellite structural components must be able to withstand various loading and
environments that will experience during integration, tests, transportation, launch, and on-orbit
operation. A polymeric composite optical bench that fixes delicate optical payloads such as a camera
or a telescope was developed based on static strength, thermal deformation, and vibration. The optical
bench consists of composite sandwich panels with and without a hole and composite struts with end
fittings. In this paper, the optimum stacking sequence of the composite optical bench was calculated
to minimize severe thermal deformations during orbital operation using a genetic algorithm and the
finite element analysis. Then, the optimum design is evaluated whether it withstands launch loads
(high inertia, vibration, etc.), that are not usually significant compared to orbital thermal loadings, or
not. The thermal deformation of sandwich panels was minimized at the stacking sequence of [0/±45]s
and that of composite struts was lowest at the angle of [02/90]s. There was no buckling in the
compressive loading. By vibration analysis, the natural frequencies of the composite components
were much higher than aluminum structures (i.e., sandwich panel: 10.7%; strut: 27.79%) and the
stiffness condition expected was satisfied. Then, a composite optical bench was fabricated for tests
and all analyses results were verified by structural testing. There were good correlations between two
results. To increase the structural stiffness, several Nitinol shape memory alloy wires installed on it
and the natural frequencies were measured.
457
Abstract: Targeted at improving the overall integrity of functionalised composite structure, an
embedded sensor network technique was developed using circuited piezoelectric wafers. The
technical difficulties due to sensor embedment, such as electrical insulation, were addressed. With
Hilbert transform-based signal processing and a correlation-based identification algorithm, Lamb
wave signals, excited and captured by the integrated sensor network, were evaluated for damage
assessment. Effectiveness of the sensor network and proposed identification algorithm was
demonstrated by identifying delamination in orthotropic woven fabric CF/EP composite laminates.
Excellent identification capacity of the built-in sensor network indicates its considerable application
potential in providing high-fidelity data acquisition/condition monitoring for composite structures.
461
Abstract: This study provides a practical method regarding the development of a complete
self-diagnostic technique for monitoring the bearing damage of bolted composite or metallic joints.
The basic concept is based on making BG (Bolt Gauge) measurements that has been proposed in
earlier work [1,2]. That is, bonding a strain gauge onto the surface of bolt head to monitor the bolt
strain changes that would identify bearing damage. Extensive tests using double lap bolted joint
specimens are performed to verify the health monitoring technique, including the effects of the bolt
clamp-up, material response, joint geometry and loading history. The results have shown that the
bearing damage detected by BG measurements agreed well with acoustic emission (AE)
measurements. Finite element analysis is performed to discuss the monitoring mechanisms.
465
Abstract: This paper presents experimental results on the mechanical performance of advanced
carbon/epoxy composites with embedded polymeric films. The composite laminates with polymeric
films, which are potentially used as a sensor/actuator carrier for structural health monitoring
applications, were investigated under various mechanical loadings including low velocity impact,
single lap shear and short beam shear. The preliminary work showed that embedment of those
polymeric films does not degrade, but could significantly improve, the mechanical properties of the
composite laminates.
469