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
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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: In this paper the Fractional Spline Wavelet Transform (FrSWT) is introduced based on the
definitions and properties of the fractional B-spline and the symmetric fractional B-spline. Then the
computation process and approximation properties of the FrSWT are also discussed and especially,
the truncation error of computation is obtained analytically. At last, the FrSWT is applied to detect the
abrupt information in the simulated and measured signal of fault gear system.
371
Abstract: Three-dimensional finite element simulations were carried out to investigate the hydraulic
progressive damage and associated flow behavior in rock. In this study cohesive elements were used
to simulate the damage of rock. A three-dimensional coupled pore fluid flow and stress model was
proposed. The commercial engineering software ABAQUS is employed to simulate the damage
process in rock along several predefined paths. A user-subroutine named FLOW was developed to
enhance the capability of ABAQUS to deal the moving loadings. With the proposed coupling model,
we studied the stress distribution, the pore pressure, the fluid loss, the geometry of the progressive
damage. The results show that the length and the width of the path of the progressive damage are
strongly influenced by both the hydraulic pressure and the injection time. The results provide good
interpretation and understanding of the mechanism of hydraulic progressive damage in rock. This
study is very useful and important to the oil engineering and some other rock engineering fields.
375
Abstract: A fatigue crack growth model under constant amplitude loading based on the total plastic
energy dissipation per cycle ahead of the crack was proposed. With the energy balance concept, the
crack growth rate was correlated with the total plastic dissipation per cycle, and the total plastic
dissipation per cycle was obtained through 2-D elastic–plastic finite element analysis of a stationary
crack under constant amplitude. The predictions of the model were in good with the experimental
results.
379
Abstract: Numerical simulation of hydraulic fracturing propagations in the permeable reservoirs was
carried out with the finite element analysis software (ABAQUS). A model of coupling the stress
equilibrium and fluid continuity equations was proposed and implemented. The nonuniform of sink
pore pressure on the fracture surfaces which changes associated with the propagation of fracture was
described by a self-developed subroutine through the FLOW in ABAQUS. Samples under different
conditions were conducted for studying the rules of the propagation of hydraulic fracturing. The
results show that the permeability at the fracture tip is more serious than any other places of the
fracture face. The model also illustrates that the fracture geometry is mainly determined by the
minimal in-situ stress. The model can be used to simulate the effects of hydraulic fracturing pressures
and injection rates on fracture propagation. The results are of much significance for the design of
hydraulic fracturing treatments.
383
Abstract: Major nuclear components have been designed by conservative codes to prevent
unanticipated fatigue failure. However, more realistic and effective assessment is necessary in proof
of continued operation beyond the design life. In the present paper, three-dimensional stress and
fatigue evaluation is carried out for pressurizer employing complex full geometry itself instead of
conventional discrete subcomponents. For this purpose, temperature and mechanical stress transfer
Green’s functions are derived from finite element analyses and applied to critical locations of
pressurizer. In accordance with comparison of resulting stresses obtained from the Green’s function
and detailed finite element analysis, suitability of the specific Green’s function is investigated. Finally,
prototype of fatigue life assessment results is provided along with relevant ongoing activities.
387
Abstract: Based on ANSYS/LS-DYNA code, the finite-element models were created to simulate the
response of the aircraft panel structure impacted by high velocity projectile. The models proved to be
effective through the comparison between the results of simulation and relative experiments. Then the
impact process was simulated respectively considering the states of various types of stress in the
panel. Through analyzing the simulation results, the influence of various stress states in the panel on
impact response and damage mechanism was summed up. The conclusions indicated that the stress
and particularly compression stress in aircraft panel structure can facilitate much more deformation
and damage when the panel suffers high velocity impact.
391
Abstract: A 3D finite element model of bolt composite joint has been established to determine the
stress distribution on the contact surface. The effects of clamping torque and friction on the contact
stress and interlaminar normal stress are considered. From the analysis results, contact stress is bared
mainly by the 0° layer. The distribution and magnitude of contact stress are conducted by friction.
The effect of clamping torque on interlaminar normal stress is very strong. A 3D damage user
subroutine is added to the FEM to simulate the damage of joint. By the means of damage simulation,
the initiation and progression direction of three types damage are predicted. Matrix cracking and
fiber-matrix shear occur at first, and fiber buckling is founded subsequently. The matrix cracking and
fiber-matrix debonding initiate at circumferential angle 45°and 135°, and fiber buckling initiate at the
0° layer on the bearing plane. The friction and bolt clamping torque can restrain damage initiation
and development.
395
Abstract: Based on Reissner plate theory and using Hamilton variational principle, the nonlinear
equations of motion are derived for the moderate thickness rectangular plates with transverse
surface penetrating crack on an elastic foundation under the action of periodic load. The suitable
expressions of trial functions satisfied all boundary conditions and crack’s continuous conditions are
proposed. By using the Galerkin method and the Runge-Kutta integration method, the nonlinear
equations are solved. The possible bifurcation and chaos of the system are analyzed under the action
of external load. In numerical calculation, the influences of the different location and depth of crack
and external load on the bifurcation and chaos of the rectangular moderate thickness plates with
freely supported boundary are discussed.
399
Abstract: Based on the analytical solution for an elliptical cavity and the self-consistent method,
the exact solutions for a crack in a two-dimensional magnetoelectroelastic medium is derived. The
strain energy density factors are calculated for mixed mode cracks in a composite made of BaTiO3
as the inclusion and CoFe2O4 as the matrix.
403
Abstract: This paper is aimed at investigating the damage and remaining life of a whole HP-Nb
hydrogen reformer tube serviced for 12 years. The damage and remaining life evaluation of
different parts of the tube were made using metallographic examination, ambient and high
temperature uniaxial tensile tests, creep rupture tests and damage mechanics analysis. The results
showed that different parts of the tube have the different damage and remaining life due to different
service temperature, higher the service temperature, severer the damage and shorter the remaining
life. Based on these research results, a case of local maintenance of the reformer tube was
introduced.
407