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Issue 1, Volume 3,
January 2008 Title of the Paper: Consideration on
Stainless Steel Plate Plastic Deformed by Fluid Impact Substances and
Pressured Nitrogen Blasting Authors: Adrian Rosca,
Daniel Rosca, Vasile Nastasescu Keywords: Pressured
nitrogen blasting, Plastic deformation, Stainless steel thin plates Title of the Paper: Homogenisation Procedure to Evaluate the Effectiveness of Masonry Strengthening by CFRP Repointing Technique Authors: A. Cecchi, A. Barbieri Keywords: Masonry, CFRP repointing, Homogenisation, in
plane moduli. Title of the Paper: Calculation of
Dynamic Stresses using Finite Element Method and Prediction of Fatigue
Failure for Wind Turbine Rotor Authors: Z. I. Mahri, M. S. Rouabah Keywords: Wind Energy,
structural dynamics, Aerodynamics, fluid mechanics and Numerical Analysis. Issue 2, Volume 3,
February 2008 Title of the Paper: Optimum Determination of Partial Transmission Ratios of Three-Step Helical Gearboxes Authors: Vu Ngoc Pi Keywords: Gearbox design;
Optimum design; Helical gearbox; Transmission ratio. Title of the Paper: An Original
Approach of Tensile Behaviour and Elastic
Properties of Multiphase Pre-Impregnated Composite Materials Authors: Horatiu
Teodorescu, Sorin Vlase, Luminita Scutaru, Keywords: Prepregs, Sheet Molding Compounds, Substitute matrix,
Homogenization, Heterogeneity, Estimation method, Elliptic equations, Elastic
coefficients. Title of the Paper: Consideration Concerning the Static and Dynamic Stability of Metallic Bunker on Environmental Engineering Authors: Adrian Rosca, Daniela Rosca Keywords: metallic bunker,
static/dynamic stability, air shock waves, environment engineering Issue 3, Volume 3,
March 2008 Title of the Paper: Finite Element Analysis of Tunnel-Soil-Building Interaction using Displacement Controlled Model Authors: Ma Keshuan, Ding Lieyun Keywords: Finite Element;
Three-dimensional; Slurry shield tunneling; Structure; Excavation; Settlement Title of the Paper: Development of a
Spiral Trajectory for High Speed Roughing of Light Alloy Aerospace Components Authors: Jean-Francois Chatelain, Rejean Roy, Rene
Mayer Keywords: CAD, Title of the Paper: Die Attach Film Performance in 3D QFN Stacked Die Authors: A. Jalar,
M. F. Rosle, M. A. A. Hamid Keywords: Die attach
film, QFN, delamination Issue 4, Volume 3,
April 2008 Title of the Paper: Finite Element Analysis of Micro – Electro – Mechanical Systems: Towards the Integration of MEMS in Design and Robust Optimal Control Schemes of Smart Microstructures Authors: John K. Sakellaris Keywords: Finite Element
Analysis, Micro – Electro – Mechanical Systems, ANSYS software, Coupled
problems, Micro - actuator, Bi - stable electromagnetic actuation, UV-LIGA
technology, Simulation, Active structural control, Smart beam, Composite
structure, Piezoelectric layer. Title of the Paper: Spectral
Distribution of a Star-Shaped Coupled Network Authors: Xu
Gen Qi, Nikos E. Mastorakis Keywords: Star shape
network stabilization string beam Title of the Paper: Nonlinear Effects in Seismic Base Isolations Authors: Dinu
Bratosin Keywords: Earthquake
engineering, Nonlinear dynamics, Seismic base-isolation Title of the Paper: Dynamical Behavior
of Foundations in Linear and Nonlinear Elastic Characteristic Hypothesis Authors: Adrian Leopa, Silviu Nastac Keywords: vibration,
non-linear, linear, detect, damage, frequency Issue 5, Volume 3,
May 2008 Title of the Paper: New Structural
Configurations for Vibroisolation Devices with High
Isolation Performances Authors: Silviu
Nastac, Adrian Leopa Keywords: isolation
efficacy, passive elastic devices, rubber elements Title of the Paper: Enhancement of
Panel zone (PZ) Contribution to the Ductility of post-Northridge Welded
Connections Authors: Amir
A. Hedayat, Murude Celikag Keywords: Post-Northridge
connections; Panel zone; Ductility; Inelastic shear deformation Title of the Paper: The Influence of the Lubricant from a Rectilinear Pair above the Work Accuracy of the Elastic Elements from the High Precision Mechanisms Authors: Madalina
Calbureanu, Raluca Malciu, Mihai Lungu, Dan Calbureanu Keywords: Lubricated
rectilinear pair, elastic element, pressures field, film breaking phenomenon,
spectral analysis Title of the Paper: Advanced
Computational Concepts about Projecting a Multiple Designs of Self-Supporting
Metallic Structure using Finite Element Method in Determination the Buckling
Factor and Running the Stress Analysis Authors: Madalina
Calbureanu, Emil Albota, Raluca Malciu,
Keywords: Self-supporting
metallic structure, design, buckling factor, stress analysis Issue 6, Volume 3,
June 2008 Title of the Paper: A Strain-based
Non-linear Elastic Model for Geomaterials Authors: Andrew Heath Keywords: Elasticity, Geomaterials, Non-linear, Finite Element, Elastic strain Title of the Paper: On the Eigenvalues Optimization of Beams with Damping Patches Authors: Veturia
Chiroiu Keywords: eigenvalues, optimization, damping patches, Euler-Bernoulli beam, nonlocal theory, auxetic material Issue 7, Volume 3,
July 2008 Title of the Paper: Mechanical Behavior
Analysis with the Finite Elements Method of
Solar Collector’s Tracking Systems Authors: Mihai
Tiberiu Lates Keywords: Solar
collector, Tracking system, FEM, Stresses, Displacements, Vibrations. Title of the Paper: Bending Beams, a
Computer-Aided Approach Authors: Carmen E. Eisinger-Borcia Keywords: bending, lumped beam, influence coefficients,
computer-aided optimization, Mathematica®. Title of the Paper: The Effect of
Frequency and Amplitude of Vibration on the Coefficient of Friction for
Metals Authors: Jamil
Abdo, Mahmoud Tahat Keywords: Frequency and
amplitude of vibration, Coefficient of friction, Pin on disc. Title of the Paper: Creep Analysis of
Thin Rotating Disc under Plane Stress with no Edge load Authors: Sanjeev Sharma, Manoj Sahni
Key words: Creep, Transition, Stresses,
Strain Rates, Transversely Isotropic and Rotating Disc Title of the Paper: Intelligent Modular Design of Automatic Dimensional Inspection Systems Authors: Luciana Cristea, Mihai Manescu Abstract: The new production has
to undertake a continuous quality improvement due to its major economic
involvement; the consequence consists in high performances in the quality
assurance. Therefore the author of this work wants to present some concerns
in the automatic dimensional inspection systems field. The new production has
to undertake a continuous quality improvement due to its major economic
involvement; the consequence consists in high performances in the quality
assurance. Therefore the author of this work wants to present some concerns
in the automatic control system field. This paper presents aspects of the
design for an intelligent modular inspection system. The performed researches
aimed at an original method of grouping the parts based on the relation
between dimensional inspection process characteristics and modular design of
all inspection equipments with a high universality and flexibility degree. Keywords: Inspection, mechatronics, modular design, automation, dimension. Issue 8, Volume 3, August 2008 Title of the Paper: A Hierarchical Relevance Feedback Algorithm for Improving the Precision of Virtual Tutoring Assistant Systems Authors: Ji-Wei Wu, Judy C. R. Tseng Abstract: In recent years, several virtual tutoring assistant systems had been proposed based on question-answering systems. These virtual tutoring assistant systems are very helpful for the students to get instant helps when the teachers are not available. Pedagogic scholars think that when a student is stuck on a certain problem while learning, an instant tutoring assistant is very helpful to promote his/her study. Therefore, the qualities (precision) of the answers of virtual tutoring assistant systems are very important. It determines the effectiveness of these systems. In practices, some students are suffered from not being able to properly express their need; some may not even know exactly what information they need. As a result, some problems do not match any existing solutions, even if they do contain some clues for finding solutions. That makes the effectiveness of the virtual tutoring assistant systems not being acceptable. In the literatures, researchers found that relevance feedback information are quite useful for information retrieval systems to improve their effectiveness. Among them, the Rocchio’s Relevance Feedback (RRF) algorithm is the most well-known and have been employed in several information retrieval systems. In this paper, we proposed a novel pseudo relevance feedback algorithm, called Hierarchical Relevance Feedback (HRF) algorithm. The HRF algorithm is used for improving the precision of virtual tutoring assistant systems. After a query is submitted by some student, the new virtual tutoring assistant system will automatically modify the student’s query according to the HRF algorithm and re-submit it to the system. Experimental results showed that the effectiveness of the system is improved by automatically modifying user’s query using the HRF algorithm. Moreover, the HRF algorithm is also outperformed the famous RRF algorithm. Keywords: E-learning, Tutoring assistant, Information Retrieval, Question-answering, Relevance feedback Title of the Paper: Variational Formulations and Extended Thermodynamics for Resting Irreversible Fluids with Heat Flow Authors: Stanislaw Sieniutycz, Piotr Kuran Abstract: Nonequilibrium statistical mechanics helps to estimate corrections to the entropy and energy of the fluid with heat flux in terms of the nonequilibrium distribution function, f. This leads to the coefficients of wave model of heat: relaxation time, propagation speed and thermal inertia. With these data a quadratic Lagrangian and a variational principle of Hamilton’s type follows for the fluid in the field representation of fluid’s motion. We analyze canonical conservation laws and show the satisfaction of the second law under the constraint of these conservation laws. Keywords: Grad solution, variational calculus, wave equations, conservation laws, entropy Title of the Paper: Sub-Optimal Orbital Maneuvers for Artificial Satellites Authors: Bruno Nunes Vaz, Antonio Fernando Bertachini De Almeida Prado Abstract: The determination of a specific orbit and the procedure to calculate orbital maneuvers for artificial satellites are problems of extreme importance in the study of orbital mechanics. Therefore, the transferring problem of a spaceship from one orbit to another, and the attention to this subject has increased during the last years. Many applications can be found in several space activities, for example, to put a satellite in a geostationary orbit, to change the position of a spaceship, to maintain a specific satellite’s orbit, in the design of an interplanetary mission, and others. The orbit and the general data of the Brazilian Satellite SCD-1 (Data Collecting Satellite) will be used as example in this paper. It is the first satellite developed entirely in Brazil, and it remains in operation to this date. SCD-1 was designed, developed, built, and tested by Brazilian scientists, engineers, and technicians working at INPE (National Institute for Space Research) and in Brazilian Industries. During its lifetime we will study its orbital behavior and we will perform some orbital maneuvers that could be necessary, being this one either an orbital transferring, or just to make periodical corrections. The purpose of the transferring problem is to change the position, velocity and the satellite’s mass to a new pre-determined state. This transfer can be totally linked (in the case of “Rendezvous”) or partially free (free time, free final velocity, etc). In the global case, the direction, the orientation and the magnitude of the thrust to be applied must be chosen, respecting the equipment’s limit. In order to make this transferring, either sub-optimal or optimal maneuvers may be used. In the present study, only the sub-optimal will be shown, since we want to study an algorithm for this type of maneuver. Hence, this method will simplify the direction of thrust application, to allow a fast calculation that may be used in real time, with a very fast processing. The thrust application direction to be applied will be assumed small and constant, and the purpose of this paper is to find the time interval that the thrust is applied. This paper is basically divided into three parts: during the first one the sub-optimal maneuver is explained and detailed, the second presents the Satellite SCD-1, and finally the last part shows the results using the sub-optimal maneuver applied to the Brazilian Satellite. Keywords: Astrodynamics, Spatial Mechanics, Brazilian Satellites, Orbital Maneuvers, Space Trajectories Title of the Paper: Modeling the Nonlinear Vibration Response of a Cracked Rotor by Time Delay and Embedding Technique Authors: Alfayo A. Alugongo Abstract: In this paper, a non-linear model for a cracked rotor is established based on constitutive equations and local flexibility due to a transverse breathing crack on a rotor shaft. The crack is characterized by a switching function and change in shaft stiffness, whose variation and value defines the closing-opening or breathing condition of the crack during rotation of the shaft. The model accounts for the rotor shaft weakening parallel and perpendicular to the direction of the crack opening. The system equation bears discontinuity, and its numerical solution exhibits bifurcation and chaos. The model is used to investigate the dynamics of the vibrating rotor system, and the crack force reconstructed’ by Time delay and Embedding Technique. The crack force manifests the action of the crack on the rotor. It is observed that the largest computed Lyapunov exponent of the simulated time series is a good and sufficient indicator of the system’s chaotic state. Various scenarios of the system at sub-critical and super-critical speeds have been simulated and discussed. Keywords: Bifurcation, Chaos, Lyapunov exponent, Cracked rotor dynamics, Switching function Issue 9, Volume 3, September 2008 Title of the Paper: The Application of Computational Fluid Dynamic (CFD) on the Design of High Subsonic Wing Authors: Prasetyo Edi, Nukman Yusoff, Aznijar Ahmad Yazid Abstract: This paper intends to present the application of Computational Fluid Dynamic (CFD) on the design of high subsonic wing of transport aircraft. The computation was performed using RAMPANT, an unstructured, multigrid flow solver. A 2-D and 3-D model of the wing was created using CATIA (2D and 3D modeling). A corresponding grid was created using preBFC and TGrid. The paper describes the technique of creating the grid and using the CFD on the wing design process. It then discusses the benefits and penalties of using the above tools. Description is then given in using the aerodynamic analysis result to optimize the wing. It concludes with a discussion of the results and recommendations for future work. Keywords: Computational fluid dynamic (CFD), wing design, aircraft design, aerodynamic configuration Title of the Paper: New Design Approach of Compound Helicopter Authors: Prasetyo Edi, Nukman Yusoff, Aznijar Ahmad Yazid, Catur Setyawan K., Nurkas W., Suyono W. A. Abstract: Current trends in the design of helicopter have shown that in order to be economically viable and competitive it is necessary to investigate new design concept which may give an improvement in performance and operational flexibility goal and expanding the flight envelope of rotorcraft, but must be shown to be cost-effective. The helicopter has carved a niche for itself as an efficient vertical take-off and landing aircraft, but have limitation on its cruising speed due to restrictions of retreating blade stall and advancing blade compressibility on the rotor in edgewise flight. This is a challenging task, which might be solved by the use of new design approach. It is believed that the application of a compound helicopter design concept would assist in achieving such a task. This paper describes an investigation aimed to examine the suitability of a compound helicopter design concept, allowing for the use of a combined conventional fix-wing aircraft with single propeller in the nose and conventional helicopter to satisfy the above objectives. The paper describes the phenomenon of presents VTOL (vertical take-off and landing) aircraft. It then discusses the benefits and penalties of the presents concept. Description is then given of the concept proposed compound helicopter which incorporated combines main rotor-wing-auxiliary propeller. It concludes with a discussion of the results and recommendations for future work. Keywords: Compound helicopter, VTOL (vertical take-off and landing), high speed helicopter, aircraft design Title of the Paper: The Design Improvement of Airfoil for Flying Wing UAV Authors: Prasetyo Edi, Nukman Yusoff, Aznijar Ahmad Yazid Abstract: This paper intends to presents the design improvement of airfoil for flying wing UAV (Unmanned Aerial Vehicle) when the Author works with Universiti Putra Malaysia. The design was performed using XFOIL code (an interactive program for the design and analysis of subsonic isolated airfoils) and the wind tunnel test results for verification. Eppler E334 (thickness to chord ratio, t/c = 11.93%) is used as a based airfoil. The final design was using Eppler E334 with t/c = 13.5%. It was shown from this work that the result from XFOIL is fairly accurate. Keywords: Airfoil design, flying wing, UAV (Unmanned Aerial Vehicle), aerodynamic design Title of the Paper: Development of a Mathematical Model for Analysis on Ship Collision Dynamics Authors: M. Rafiqul Islam, Zobair Ibn Awal, Adi Maimun Abstract: This research work attempts to develop a model for ship to ship collision. The collision model is fundamentally divided into two segments namely, model for simulation before collision and model for simulation after collision. In the first part, mathematical formulations are derived for finding the possibility of a collision, determining the spatial location of collision and identification of the contact points on the ships. In the later part, a mathematical model is developed to study the kinetic energy losses, collision forces and dynamic responses with respect to different variables such as coefficient of restitution, ship speed, angle of attack, location of hitting, added mass for sway force and others. In the model, expressions for collision forces are derived based on changes in linear momentum. By incorporating the collision force into the equation of motion, which is a linear differential equation with constant coefficients, the dynamic responses are calculated for different collision scenarios. The study considered two different vessels of length 46 meter and 32 meter for conducting the simulations. Results obtained from the mathematical model suggest that collision forces can be reduced significantly by altering the considered variables; e.g. motion amplitudes can be reduced very significantly (as high as eighty five percent) by using materials with lower coefficient of restitution in the fenders and may save ships from capsizing in severe cases. Finally, a number of recommendations have been put forward and further investigations on such models are also proposed. Keywords: Collision Dynamics, Coefficient of Restitution, Collision Forces, Ship Capsizing, Mathematical Model Title of the Paper: Research Regarding the Establishment of Force and Energetic Characteristics of the Bucket Wheel Excavator in given Working Conditions Authors: Marin Silviu Nan, Iosif Kovacs, Iosif Andras, Dumitru Jula Abstract: This paper presents the power and energy characteristics whit the view to defining and analyzing the working mode of the rotor excavators in operation at Oltenia lignite open casts, for lignite mining and for mining of the predominantly overburden rock, i.e. the sandy clay. The forces which act on a bucket and wheel, the force needed for the excavation and for lifting the material, as well as the force necessary for turning around the superior platform of the excavator during operation will be calculated. The calculus method applies to bucket wheel excavators type EsRc 1400 and SRs 1300. A software for the study of force and energetic excavation parameters is presented. Keywords: Rotor excavator, Working mode, Forces, Power, Power consumption, Excavation capacity, Case study, Software Issue 10, Volume 3, October 2008 Title of the Paper: Physical Modelling of a Continuous Casting Tundish: a Parametric Study of Residence Time Distribution Curves Authors: Amel Ferial Boudjabi, Ahmed Bellaouar, Mohammed Lachi, Nadim Elwakil Abstract: More than 94% steelmaking and ironmaking are released in continuous casting process. Product quality is closely related to metal cleanness and non-metallic inclusions removal. So, lliquid metal flow in ladles, tundishes and moulds is recognised to be of great importance in the quality of these products. The metal jet from the ladle to tundish tends to induce turbulent motions which can play important roles in non-metallic inclusions removal at the slag surface, thereby helping in the production of cleaner steel. To improve particle decantation, flow control devices such as dams and weirs are used. The present work is an experimental study released using similarity criteria, through Reynolds and Froude numbers. A reduced scale (1/4) water model of an industrial tundish is used to visualise and measure different parameters of a tracer flow injected in water. The analysis of residence time distribution curves (RTD) by the combined model for different configurations is carried out to establish the interest of placing weirs in the amelioration of inclusions flotation and decantation. Keywords: Continuous casting, Non-metallic inclusions decantation, Similarity criteria, Water model, Residence time, Combined model Title of the Paper: Low Thrust Maneuvers for Artificial Satellites Authors: Vivian Martins Gomes, Antonio F. B. A. Prado, Helio Koiti Kuga Abstract: An orbital maneuver is an important phase of a space mission. The idea is to change the orbit of a spacecraft, in order to be able to complete the mission goals required. It can be done to insert a spacecraft in its nominal orbit or during the mission to compensate undesired effects of perturbations. To perform the orbital maneuvers, a software that calculates an optimal maneuver is developed. This method will be used as a reference for comparison and analises of the suboptimal methods to be used on board. This method id based on an analytical development that generate equations that can be computed in a shorter time, allowing real time applications. In all the simulations, low thrust is used to make the maneuvers. Keywords: Orbital maneuvers, low thrust, astrodynamics, artificial satellites, orbital dynamics Issue 11, Volume 3, November 2008 Title of the Paper: Swing-By Maneuvers for a Cloud of Particles with Planets of the Solar System Authors: Vivian Martins Gomes, Antonio F. B. A. Prado Abstract: The idea of the present paper is to study the swing-by maneuver between one of the planets of the Solar System and a cloud of particles. This is what happens when a fragmented comet crosses the orbit of a planet like Jupiter, Saturn, etc. We used the dynamical system that is formed by two main bodies (the Sun and one of the planets of the Solar System) and we assumed that they are in circular orbits around their center of mass and a cloud of particles is moving under the gravitational attraction of these two primaries. The motion is assumed to be planar for all the particles and the dynamics given by the “patched-conic” approximation is used, which means that a series of two-body problems are used to generate analytical equations that describe the problem. The main obejctive is to understand the change of the orbit of this cloud of particles after the close approach with the planet. It is assumed that all the particles that belong to the cloud have semi-major axis a ± da and eccentricity e ± de before the close approach with the planet. It is desired to known those values after the close approach. In particular, we will study the effects of the periapsis distance in this maneuver. Keywords: Astrodynamics, Orbital maneuvers, Swing-By, Gravity assisted maneuvers, Orbital motion Title of the Paper: On the Mechanics of the Particle on a Curve Authors: Nicolae–Doru Stanescu, Stefan Tabacu Abstract: In this paper we present a new method to study the mechanics of a particle on a curve without friction. Two aspects are discussed. First is the static developed in linear independent co-ordinates, not necessary orthogonal. The second aspect treats the dynamics in intrinsic co-ordinates, obtaining not only the speed but also the components of the acceleration and the time variation of the generalized co-ordinate on the curve. The theory is applied in practical situations. Keywords: Linear independent co-ordinates, static, dynamics Issue 12, Volume 3, December 2008 Title of the Paper: Analysis of a Drainage Efficiency in Stratified Porous Media Authors: Chakib Seladji Abstract: The oil recovery from reservoirs formed of more subsurface rock formations can be hindered by the variability of the rocks permeability. This element can strongly influence the oil recovery and the efficiency of the drainage process. In order to understand this phenomenon and to propose a technical solution thereafter, the simulation of an ascending air phase flow in a saturated vertical porous channel, composed of two layers with different permeabilities is done. The numerical study is performed in order to evaluate the effect of injected air mass flow rate, the effect of the porous column width and their permeability variations. The results show that some regions in the channel are not correctly drained due to high pressure losses in those regions. Keywords: Inertial two-phase flow, pressure drop, recovery process, stratified porous matrix, saturation behavior Title of the Paper: Design and Analysis of Modular Mobile Robot with Magnetic Wheels Authors: Fei Yanqiong, Song Libo Abstract: In the paper, a modular climbing-wall mobile robot with four magnetic wheels is presented. It can move on the vertical steel wall and inspect the weld seam. First, the structure of the mobile robot is analyzed. It is modular, which consists of a light manipulator module, an ultrasonic probes module and a weld testing sensors module. Then, the magnetic wheels are designed and analysed. One magnetic wheel consists of two pieces of magnet and three pieces of pure steel plates. Second, the motion of the robot on the vertical cylindrical vessel is analysed in detail. The position deviation and angle deviation are adjusted with the geometric method. At last, the experiments of the modular climbing-wall robot on real vertical steel vessel are shown to verify the above motion analysis and design requirements at Nanjing refinery factory in China. It is of high reliability and simple control. Keywords: Mobile robot, Magnetic wheel, Motion, Modular, Structure |
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