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
Vol. 320
Vol. 320
Key Engineering Materials
Vol. 319
Vol. 319
Key Engineering Materials
Vols. 317-318
Vols. 317-318
Key Engineering Materials
Vols. 315-316
Vols. 315-316
Key Engineering Materials
Vol. 314
Vol. 314
Key Engineering Materials Vols. 324-325
Paper Title Page
Abstract: Recently, people devote to the development of beta titanium alloys which have better
biocompatibility because of the addition of Mo, Nb, Ta, Zr, Sn, et al. In this paper, the effects of
heat treatment and cold roll deformation on the mechanical properties of the Ti-11.3Mo-6.6Zr-4.3Sn
alloy (TMZS) are investigated by tensile test. The results show that the excellent combination of
strength and ductility can be obtained by heat treatment or cold deformation. The TMZS alloy can
obtain intermediate modulus, stronger than nickel titanium, weaker than stainless steel. The
corrosion resistance of this alloy in the Hank's solution, 0.9% NaCl physiological solution and
artificial saliva with different pH values at 37 are investigated by means of open-circuit potential
(OCP), Tafel and potentiodynamic anodic polarization techniques. All the test results suggest that
the TMZS alloy has excellent corrosion resistance in the three simulated solutions especially in the
artificial saliva and has a large potential for biomedical application. In addition, the pH value and
simulated solutions have some influence on the corrosion resistance of the TMZS alloy.
695
Abstract: Based on full layerwise displacement shell theory, the vibration and damping
characteristics of cylindrical sandwiched panels with viscoelastic layers are investigated. The
transverse shear deformation and the normal strain of the cylindrical hybrid panels are fully taken into
account for the structural damping modeling. The layerwise finite element model is formulated by
using Hamilton’s virtual work principle and the cylindrical curvature of hybrid panels is exactly
modeled. Modal loss factor and frequency response functions are analyzed for various structural
parameters of cylindrical sandwich panels. Present results show that the full layerwise finite element
method can accurately predict the vibration and damping characteristics of the cylindrical hybrid
panels with surface damping treatments and constrained layer damping.
699
Abstract: To consider the corrosive effects on aircraft structural life under natural environments, we
have the calendric life to represent its impact. A new concept of Aircraft Structural Life Envelope
(ASLE) to consider the combined effects of fatigue loads and corrosive conditions is developed and
the sketch of ASLE is presented, then the basic determining methods of ASLE under different
corrosive conditions are obtained too. Finally the linear damage cumulative rules are employed to
analyze the usage of aircraft in different corrosive conditions, and the residual fatigue life and
calendric life of aircraft structures can be predicted and supervised.
703
Abstract: Biaxial compressive tests of plain concrete specimens under normal temperature and
suffering high temperature(200600 )were completed under four lateral constant stress rates.
The tests were completed by using the large static-dynamic triaxial test system for concrete in the
State Key Laboratory of Coastal and Offshore Engineering, Dalian University of Technology. The
biaxial compressive strength and deformation characteristics of concrete confined by lateral stress
after suffering different temperature were studied in a systematic way. On the basis of the tests, the
failure criterion of concrete subjected to constant lateral compressive stress after suffering different
temperature was established in the Octahedral stress space. The conclusions can provide the testing
and theoretical basis for deeper study of the concrete construction subjected to biaxial compressive
combined loads suffering different temperature such as chimney, building after fire and safety shell
for nuclear reactor.
707
Abstract: The paper deals with the problem of service life evaluation of counterweight bar bolted
connection by means of computational analysis and experimental testing. Computational analysis
has been performed using the local strain-life approach (ε-N), where appropriate material properties
for treated high strength steel S1100Q has been determined previously. Experimental fatigue tests
of bars were carried out in a specially constructed hydraulic pulsation machine. Comparison of
computational and experimental results shows a reasonable agreement.
711
Abstract: Five twisted steel fibers (steel cord, SC) are used to improve the post-cracking behavior
of cement composites. In addition to these steel cord macrofibers, microfibers are used to enhance
the pre- and post-cracking strength and behavior. The three specific hybrid fiber blends pursued in
this investigation are SC and polyethylene (PE), SC and polypropylene (PP) as well as SC and
polyvinyl alcohol (PVA) fibers. The research results show that SC macrofibers with high ultimate
strain, strength and bond stress can bridge the macrocracks in the matrix. Therefore, cement-based
composites reinforced with SC fibers exhibit a pseudo-strain hardening in tension as a result of the
formation of multiple cracks. The microfibers improved pre-peak mechanical performance, strength,
and fracture process by delaying the formation of a macrocrack. The tensile strength, energy
consumption capacity and ductility of SC macrofibers and high elastic modulus microfiber PE
reinforced cement-based composites are tremendously improved compared to SC macrofibers with
lower elastic modulus microfibers PVA and PP.
715
Abstract: Fatigue test on a full scale panel with complex loading and geometry has been carried out
by using a tri-axial test machine located in the laboratory of the University of Naples. The
aeronautical test panel was designed and manufactured by Alenia. The demonstrator is made up of
two parts which are linked by a transversal joint that is parallel to the stringer direction. A fatigue load
was applied in the normal direction to the longitudinal joint, while a constant load was applied in the
joint direction. The full scale panel was equipped with strain gauges for deformation state
measurements. Preliminary static load tests were performed in order to provide deformation
measurements for numerical correlation. The outcomes confirmed that the applied load level is
consistent with a linear elastic material behaviour. Three intermediate failures occurred before the
final one: the first two under a clip, while in the third case a panel frame failed. Finally after about
177,000 cycles the demonstrator broke down. A non linear finite element analysis was also carried out
in order to correlate failure events that occurred during the demonstrator testing.
719
Abstract: This paper investigates the effect of the ductile deformation behavior of high
performance hybrid fiber-reinforced cement-based composites (HPHFRCCs) on the shear behavior
and damage of diagonally reinforced coupling beams under reversed cyclic loading. The effects of
matrix ductility on deflections, crack widths, crack patterns, failure modes, and ultimate shear load
of the coupling beams have been examined. The combination of a ductile cement-based matrix and
steel reinforcement is found to result in improved energy dissipation capacity and damage-tolerant
inelastic deformation behavior. Test results showed that the coupling beam constructed with an
HPHFRCC material exhibited excellent strength, deformation capacity, and damage tolerance
capacity, in comparison with the regular reinforced concrete beam.
723
Abstract: In order to understand the effects of the metal components embedded in adhesive fillets
on the strength of adhesively bonded single lap joint, the failed surfaces were studied with diagrams
of scanning electron microscopy (SEM) and Fourier transform infrared (FT-IR) spectrometer. The
stress distribution along the length of the bondline of single lap steel joints was also studied with an
elasto-plastic finite element analysis (FEA) model to understand its effect in the view of mechanics.
The SEM images and the FT-IR spectra diagrams revealed that the failure in the interface was
primarily mixture mode with fillets and they also presented the interface strength being higher and
there were more polar links formed in the adhesive fillets with metal components. The result
obtained from the numerical modeling is in compliance with it from experiment that the stress
distributed in lap zone of the joint is gentler when a couple of steel wires embedded in fillet.
727
Abstract: The mechanical behaviors were investigated by nonlinear creep tests of poly(methyl
methacrylate) under different temperatures. The test duration was 4000 seconds. The corresponding
temperature shift factors, stress shift factors and temperature-stress shift factors were obtained
according to time-temperature superposition principle, the time-stress superposition principle and
the time-temperature-stress superposition principle (TTSSP). The master creep compliance curve up
to about 1-month at a reference temperature 22 degrees centigrade and a reference stress 14 MPa
was constructed, and the effect of stress-induced damage evolution on the long-term creep behavior
of polymeric material was accounted. It was shown that TTSSP provides an effective accelerated
test technique in the laboratory, the results obtained from a short-term creep test of poly(methyl
methacrylate) 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, and the master creep compliance curve with damage considered can be
applied to accurately characterize the long-term creep behavior of nonlinear viscoelastic polymer.
731