Key Engineering Materials
Vols. 361-363
Vols. 361-363
Key Engineering Materials
Vols. 359-360
Vols. 359-360
Key Engineering Materials
Vols. 353-358
Vols. 353-358
Key Engineering Materials
Vol. 352
Vol. 352
Key Engineering Materials
Vol. 351
Vol. 351
Key Engineering Materials
Vol. 350
Vol. 350
Key Engineering Materials
Vols. 348-349
Vols. 348-349
Key Engineering Materials
Vol. 347
Vol. 347
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. 348-349
Paper Title Page
Abstract: A special specimen was created cutting a rectangular notched area from the surrounding
of the upper left corner of a wide body aircraft door. Then a fatigue traction load was applied in
order to induce an MSD crack initiation and propagation. An innovative DBEM (Dual Boundary
Element Method) modelling approach was devised, capable of explicitly modelling the different test
article layers with their rivet connections even in a 2d approach. The rivets that are close to the
propagating crack are coupled with the corresponding holes by non linear contact conditions, and
the accuracy improvements are assessed in comparison with a previous linear analysis, in which
traction and displacements continuity conditions on the hole-rivet interface had been imposed.
The importance of such influence on the simulation precision need to be assessed due to the strong
impact that a non linear analysis produces on computational times.
For such a complex problem (three different panels, made of different materials, each one with a
variable thickness and connected by numerous rivets), experimental crack propagation data were
available for the numerical-experimental comparison. With such non linear approach, a significant
improvement on the growth rate correlation is obtained, that justify the increased computational
effort.
593
Abstract: In order to overcome the weakness in traditional high arch dam safety evaluation without
considering the randomness, failure mode and risk analysis, it is proposed to apply three indexes
namely failure probability, economic loss and life loss to high arch dam safety evaluation. On the
basis of the analysis of accidents and on-site measured data, expert discussion as well as analytical
analogy and by means of Fault Tree Analysis, a probe is made into the four major failure modes and
the causes of high arch dam failure, namely destabilization collapse, shear-slipping collapse, excess
cracking and man-caused destruction. Based on the calculating of the probability of high arch dam
shearing-slipping failure, the computational method and procedures are established by means of
Second Moment Method for the calculation of the occurrence probability of the major failure modes
of high arch dam. A study is made of the degree of correlation between the major failure modes and
of the method for calculating the high arch dam failure probability under multi-failure-modes.
597
Abstract: It is proposed to make use of dam risk rate, economic loss risk value and life loss risk
value in evaluating the risk of high arch dam. The acceptable standards of risk for high arch dam in
the developing country should not be set too high,it should reflect the level of economic and
technology development, the policy for energy sources,the life value as well as the degree of the
importance attached. Based on study of the characteristics of high arch dam and by means of the
comparison of the levels of economic development, the life values and the degrees of the
importance attached between developing and developed countries, as well as the analogy analysis of
rare risk events occurring in developing countries, the reference value of the single high arch dam
acceptable risk rate, economic loss risk and life loss risk in developing countries are found to be
10 /(yr dam) 6 ⋅ − , 10000$/(yr ⋅ dam) and 0.001person/(yr ⋅ dam) respectively;a method is worked out for
determining the acceptable risk rate,the acceptable economic loss risk value and life loss risk value.
601
Abstract: Composite materials are used in aerospace structures due to their considerable bending
stiffness and strength-to-weight ratio. A composite sandwich is composed of a face-sheet and an
aluminum core. The face-sheet of the sandwich takes the bending stress and core of sandwich takes
the shear stress. A compression test and FEM analysis accomplished about composite sandwich
panels that have curvature. The FEM analysis was performed using a commercial code, ANSYS and
the compression test was performed until failure occurred in the sandwich panel. A strain gauge and a
displacement gauge were used to acquire the data. In this paper, the failure strength and failure mode
was checked. Additionally, the results of the test and analysis were compared.
605
609
Abstract: Forced vibration and liquid corrosion are important reasons for last stage blade failure in
steam turbine. In order to improve reliability of blades in wet steam stages, the dynamic stress and
the liquid-solid impact stress of blade were analyzed firstly, then Neuber’s rule, rainflow counting
method and improved cumulative damage rule were introduced to develop a new model to evaluate
service life of last stage blade. Many factors such as manufacturing quality, metal quality and
operation status were considered, so it is more reasonable for service life assessment of last stage
blade. At last, the service life of a last stage blade of 680mm was analyzed and the result
approximates the practical service life. It is shown the new fatigue model can give some significant
data and is usable for engineering application.
613
Abstract: The distribution of stress in a nonrectangular compressed area, such as a section under a
biaxial moment, is different than that of a rectangular compressed area. The properties of the
compressive stress distribution of concrete have only a minor effect on the pure bending moment
capacity of reinforced concrete beams, but they are important influencing factors for columns
subjected to a combined axial load and a biaxial bending moment. The variation of ultimate strain
of concrete according to the angle and depth of a neutral axis was investigated. Thus, the modified
rectangular stress block (MRSB) model for nonrectangular compressed areas is formulated and
compared to the experimental results and the existing RSB model. The MRSB method is able to
provide more accurate predictions of test results for the biaxial bending moment strength than the
RSB method.
617
Abstract: Spalling is defined as damages to concrete exposed to high temperature during fire,
causing cracks and localized bursting of small pieces of concrete. As the concrete strength
increases, the degree of damage caused by spalling becomes more serious due to impaired
permeability. It has been reported that polypropylene(PP) fiber has an important role in protecting
concrete from spalling, and the optimum dosage of PP fiber is 0.2%. However, this result was based
on the fire test of non-reinforced concrete specimens. The high-temperature behavior of highstrength
reinforced concrete columns with various concrete strength and various quantity of PP
fibers is investigated in this study. The results revealed that the ratio of unstressed residual strength
of columns increased as the concrete strength increased and as the quantity of PP fiber increased
from 0% to 0.2% the residual strength of columns increase. However, the effect of PP fiber quantity
on residual strength of column was barely above 0.2%.
621
Abstract: The present paper deals with the research on the crack growth in a bolt connection of a
lug for crane counter weight bars. Counter weight bars are structural elements that are subjected to
very heavy loads and therefore special attention must be paid. The main purpose of this research is
to determine the number of the load cycles required for a crack to propagate from initial to critical
crack length, when the final failure can be expected to occur. All required material parameters and
the experimental results were determined in our previous research.
The influence of the initial crack size upon the remaining life of the lug is researched
numerically by means of finite element analysis and analytically by use of the corrected analytical
model.
625
Abstract: A review is given about FEM-techniques to compute the coupled electromechanical
boundary value problem of cracks in piezoelectric structures under static and dynamic loads. To
calculate the relevant fracture parameters very precisely and efficient, the following numerical
techniques are presented: i) Special singular crack tip elements, ii) Modified crack closure integral,
iii) Computation of electromechanical J-integral and iv) Usage of interaction integrals. Special
emphasis is devoted to different electric crack face boundary conditions. The accuracy, efficiency
and applicability of these techniques are examined by various example problems and discussed with
respect to their advantages and drawbacks for practical applications.
629