Abstract: Due to the numerous advantages of steel corrugated
web girders, its application field is growing for bridges as well as for
buildings. The global stability behavior of such girders is
significantly larger than those of conventional I-girders with flat web,
thus the application of the structural steel material can be
significantly reduced. Design codes and specifications do not provide
clear and complete rules or recommendations for the determination of
the lateral torsional buckling (LTB) resistance of corrugated web
girders. Therefore, the authors made a thorough investigation
regarding the LTB resistance of the corrugated web girders. Finite
element (FE) simulations have been performed to develop new
design formulas for the determination of the LTB resistance of
trapezoidally corrugated web girders. FE model is developed
considering geometrical and material nonlinear analysis using
equivalent geometric imperfections (GMNI analysis). The equivalent
geometric imperfections involve the initial geometric imperfections
and residual stresses coming from rolling, welding and flame cutting.
Imperfection sensitivity analysis was performed to determine the
necessary magnitudes regarding only the first eigenmodes shape
imperfections. By the help of the validated FE model, an extended
parametric study is carried out to investigate the LTB resistance for
different trapezoidal corrugation profiles. First, the critical moment of
a specific girder was calculated by FE model. The critical moments
from the FE calculations are compared to the previous analytical
calculation proposals. Then, nonlinear analysis was carried out to
determine the ultimate resistance. Due to the numerical
investigations, new proposals are developed for the determination of
the LTB resistance of trapezoidally corrugated web girders through a
modification factor on the design method related to the conventional
flat web girders.
Abstract: Induction assisted single point incremental forming
(IASPIF) is a flexible method and can be simply utilized to
form a high strength alloys. Due to the interaction between the
mechanical and thermal properties during IASPIF an evaluation for
the process is necessary to be performed analytically. Therefore, a
numerical simulation was carried out in this paper. The numerical
analysis was operated at both room and elevated temperatures
then compared with experimental results. Fully coupled dynamic
temperature displacement explicit analysis was used to simulated the
hot single point incremental forming. The numerical analysis was
indicating that during hot single point incremental forming were a
combination between complicated compression, tension and shear
stresses. As a result, the equivalent plastic strain was increased
excessively by rising both the formed part depth and the heating
temperature during forming. Whereas, the forming forces were
decreased from 5 kN at room temperature to 0.95 kN at elevated
temperature. The simulation shows that the maximum true strain was
occurred in the stretching zone which was the same as in experiment.
Abstract: The objective of this article is to improve the passive vibration damping of solar array (SA) used in space structures, by the effective application of numerical optimization. A case study of a SA is used for demonstration. A finite element (FE) model was created and verified by experimental testing. Optimization was then conducted by implementing the FE model with the genetic algorithm, to find the optimal placement of aluminum circular patches, to suppress the first two bending mode shapes. The results were verified using experimental testing. Finally, a parametric study was conducted using the FE model where patch locations, material type, and shape were varied one at a time, and the results were compared with the optimal ones. The results clearly show that through the proper application of FE modeling and numerical optimization, passive vibration damping of space structures has been successfully achieved.
Abstract: This paper presents the results of a study aimed at establishing the temperature distribution during the welding of aluminum alloy plates by Pulsed Current Gas Tungsten Arc Welding (PCGTAW) and Constant Current Gas Tungsten Arc Welding (CCGTAW) processes. Pulsing of the GTA welding current influences the dimensions and solidification rate of the fused zone, it also reduces the weld pool volume hence a narrower bead. In this investigation, the base material considered was aluminum alloy AA 6351 T6, which is finding use in aircraft, automobile and high-speed train components. A finite element analysis was carried out using ANSYS, and the results of the FEA were compared with the experimental results. It is evident from the study that the finite element analysis using ANSYS can be effectively used to model PCGTAW process for finding temperature distribution.
Abstract: In this paper the effect of faults in the elements and
parts of discrete event systems is investigated. In the occurrence of
faults, some states of the system must be changed and some of them
must be forbidden. For this goal, different states of these elements are
examined and a model for fail-safe behavior of each state is
introduced. Replacing new models of the target elements in the
preliminary model by a systematic method, leads to a fail-safe
discrete event system.